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2010 Warranties - West Construction
SEBASTIAN AIRPORT RUNWAY 4-22 IMPROVEMENTS OPERATION AND MAINTENANCE INSTRUCTIONS ■ ON Sebastian Airport Runway 4-22 OPERATION AND MAINTENANCE MANUAL TABLE OF CONTENTS VOL. SPEC. SPEC SUPPLIER/ CONTACT SEC. # TITLE SUBCONTRACTOR INFORMATION 1 West Warranty West Construction, Inc 318 South Dixie Hwy Lake Worth, FI 33460 561-588-2027 1 2 Survey Geodetic Survey Services 1418 Norman St. Palm Bay, FI 32907 772-724-66596 1 3 Striping Gene's Striping 3001 Industrial Ave Fort Pierce, FI 34946 772-464-9737 1 6 Electrical H.L. Pruitt Corporation 501 Wade St. Winter Springs, FI 32708 407-327-3848 Cil' CITY OF SEBASTIAN 1225 MAIN STREET SEBASTIAN, FL 32958 WEST CONSTRUCTION, INC. 318 S. Dixie Hwy. Suite 4 - 5 Lake Worth, FL 33460-4452 Phone (561)588-2027 Fax (561)582-9419 Re: SEBASTIAN AIRPORT—RUNWAY 4-22 IMPROVEMENTS West Warranty, General Construction Work All work not covered by specific warranty We hereby guarantee all labor and materials used on the referenced project to be free from defect in materials and/or labor for a period of one year. We will correct any defective materials or labor during the period commencing on the date of substantial completion, January 28, 2010 and ending January 28, 2011. We acknowledge and transfer all manufacturers' warrantees to the owner operator for the period specified by the manufacturers and the project specifications. WEST CONSTRUCTIONINC. el-) 2hpqz4, Martha Morgan, President The forgoing instrument was acknowledged before me this 09th day of February, by Martha A. Morgan, who is personally known to me. Sworn to and subscribed before me this 09th day of February 2010. State of Florida County of Palm Beach ,v`""'•"8� GENERAL CONTRACTORS CGC1516626 Notary Public: My Commission Expires: o'i\a�.1`1 CONSTRUCTION MANAGERS DESIGN/BUILD SERVICES CBC057038 AR93859 SUSAN RILEY MY COMMISSION I DO 930101 t EXPIRES: February 2, 2014 N��FOF itOQ'� Baled Tin Bodo Notary B&M:as GENERAL CONTRACTORS CGC1516626 Notary Public: My Commission Expires: o'i\a�.1`1 CONSTRUCTION MANAGERS DESIGN/BUILD SERVICES CBC057038 AR93859 wi SURVEY ►el Wl ■ ,0NSTRUCT;0N maw"" •.r r1� pi vQ ��°'a O O CV O w O ENNS IRt LO Fr-�IV- V- O Z N CD ,n M CN � N a O fes. Q� a l6Jn9 +� w o o. �� z5A 1N O M N O L, ®� ti + z�f,o Z}ao �aI Z Q �� �� n'C)0 C14 LL it U-� �d �I�) o�o� Z Deo w H Q U OJ O - co W �n co �' •�,�� i E.., Z V -W zo w w U" O X z x N a �u c+� �_ M--1 C\2 W co w � O w w millQ � w a ww w j Y a co o A" �� a 0930 0�=0.� °C WW :5 LLI I N Ov PCIc a co a z aa CD � �: �W Ir 0 as aW < co W CY) G. W CV i cn J Q Q LL J Z Q �- O aQ K W � N ° N � z am W NC N a ° S2 w E Z Z m S! 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T N 0o 9: .,Yr t Y 47 Q� �•M axI< IFIL I will e F tv diY � n I V m 1� Z w p 3 u m 3 w . m F r eR `n Y: ff € �o F r s 0 3 z � x > � zm �w R� �o �i r II m� 9+6 ----$+ Bn x= R $ 3 HMI'IHJ,LVNi E� o ii � 00 N•4b, U ■ � 0 < � 0 ¥ w � � Cl) IL :5 0 k � 0 $ 2 a 0 a 2 a z k � § a § q z § 2 z / El � \Z §� U§ LU j \/k ) C\~ c CL \ CN z_ f ] z § § ; LU z 00 j § , m G % > j CN m 00 m CD 04 // }} j IAP SURVEY DATA FORM AIRPORT AND RUNWAY DATA GENERAL INFORMATION Airport Name: Sebastian Municipal Airport FAA Site Number: N/A City/State: Sebastian, FL Airport LOCID X26 PROJECT INFORMATION AIP Project Number: 3-12-0145-009-2009 Project Summary: Runway 4-22 Improvements SURVEY INFORMATION: All required survey data that is provided shall meet the accuracy requirements of FAA No. 405, "Standards for Aeronautical Surveys and Related Products' including change 1, effective April 15, 1998, as referenced in AC 150/5300-13, Airport Design, change 6, Table A16-2. Survey Requirements for Instrument Approach Procedures. The survey data shall be tied to the NGS National Spatial Reference System using established PACS and SACS. Nearby NGS control stations may be used if a PACS and SACS has not been established at an airport. NGS Control Station Permanent Identifier (PID) AF7421 Date of Last Station Recovery 2-20-2008 Type of Control Station: ❑ Primary Airport Control Station (PACS) ❑ Secondary Airport Control Station (SACS) ® Nearest NGS Control Station Is horizontal control based on NAD83 DATUM? ® Yes ❑ No Is vertical control based on NAVD88 DATUM? ® Yes ❑ No AIRPORT INFORMATION Existing Airport Reference Point (ARP) Latitude: (Accuracy. One Decimal place of a second) Longitude: Revised Airport Reference Point (ARP) Latitude: (Accuracy: One Decimal place of a second) Longitude: Page 1 of 2 RUNWAY INFORMATION Runway Designation RWY 4 RWY 22 Ref., Para. 7 of AC 15015340-1h Runway Geodetic Azimuth Accuracy: One nearest whole second Runway End Coordinates Accuracy: Four decimal places of seconds Latitude: 27-48-31.1550 Longitude: 080-30-01.2472 • Displaced Threshold (If Applicable) Latitude: Longitude: Approach End Elevation Accuracy: One decimal place in feet (MSL) • Displaced Threshold (If Applicable) Highest Point in Touchdown Zone Accuracy: one decimal place in feet (MSL) 18.0 EM 27-48-59.39489 080-29-29.3847 21.0 20.5 Supplemental Runway Profile Points Accuracy: Distance one foot/Elevation one decimal place in feet. Ref. Glossary of FAA Standard 405 for locations. Distance from approach end/elevation: I I Distance from approach end/elevation: I / Distance from approach end/elevation: I / Distance from approach end/elevation: Runway Length 4039.55' 4039.55' Accuracy: Two decimal places of a foot. CERTIFICATION NOTE: The registered surveyor must certify that the information submitted herein meets or exceeds the informational accuracy requirements of FAA Standard 405. The Surveyor is not certifying that this information submittal constitutes a full FAA Standard 405 survey. The surveyor shall apply their official seal to the completed form. The form shall be signed and dated in blue ink across the applied seal. I hereby certify that the information provided herein above has been compiled from accurate field surveys conducted under my direct supervision and that said information meets or exceeds the minimum accuracy requirements of FAA Standard No. 405 "Standards for Aeronautical Surveys and Related Products" (including Change 1, effective April 15, 1998). Surveyor's Name: / c..y W <SellI > Surveyor's License Number: 5597 Page 2 of 03 STRIPING ■ ON J1%6. GENE'SSTRIPING Warranty Project: Sebastian Airport Runway 4-22 202 Airport Drive East Sebastian, FL 32958 Owner: City of Sebastian 1225 Main Street Sebastian, FL 32958 Contractor: West Construction, Inc. 318 South Dixie Hwy, Suite 4-5 Lake Worth, FL 33460 Substantial Completion Date: January 28, 2010 Whiteleaf, Inc. dba/Gene's Striping warrants its work against all deficiencies and defects in materials and/or workmanship and agrees to satisfy same without cost to Owner or Contractor for a period of one (1) year from the date of Substantial Completion of the Project shown above. David Warner, President Whiteleaf, Inc. dba/Gene's Striping State: F\I:pC aa, County: S�,�kkC.x_Q The above was sworn and subscribed before me this 9 day of -F-eb • 2010 by b0.6�6 W amk� - ices dace of Ge_,\1 s 5k; (ins who is Name Title Company personally known to me or_ has produced identification �]Y MY COMMISSION k DDB09153 y o .r EXPIRES: JuIY 27, 3012 1'?YV1YrrN�OP''TAHY Fl. NdYY Dimnl Attic. Co. Notary Signature Stamp D• ELECTRIC a'i'1=" ■ CON S T R 11 C T ION CONTRACTORS WARRANTY FORM Project Name: RUNWAY 4-221MPROVEMENTS Location: SEBASTIAN MUNICIPAL AIRPORT Owner: CITY OF SEBASTIAN We, HL PRUITT CORPORATION, Electrical Subcontractor for the above referenced project, do hereby warrant that all labor and materials furnished and work performed are in accordance with the Contract Documents and authorized modifications thereto, and will be free from defect due to defective materials or workmanship for a period of one year from Date of Substantial Completion. This warranty commences on: Sao1w q �-9, X010 (Date of Substantial Completion Affixed by Engineer and expires on: Sav, my V 2l 2 d (One year from Commencement Date) This warranty covers that portion of the project described below: • All installed electrical conductor system(s) — including installed airfield lighting equipment and material pertaining to this project. If items of equipment or materials carry a manufacturer's warranty for any period in excess of (12) twelve months, then the manufacturer's warranty shall apply for that particular piece of equipment or material. Should any defect develop during the warranty period due to improper materials and/or workmanship, the defect shall, upon written notice by the Owner, be made good by the undersigned at no expense to the Owner. Nothing in the above shall be deemed to apply to work which has been abused or neglected by the Owner. FEBRUARY 24. 2010 Date H.L. PRUITT CORPORATION Contractor (Name of sole ownership, corporation, or partnership) (Signature of Authorized Representative) PRESIDENT Title L-861, L -861E, L -861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Document No. 96AO097 Issued: June 12, 1987 Rev. J: July 7, 2009 ETL Certified to FAA Specification AC 150/5345-46B ADB Airfield Solutions P.O. Box 30829 Tel: (614) 861-1304 977 Gahanna Parkway Fax: (614) 864-2069 Columbus, OH 43230 Copyright © 2009 by ADB Airfield Solutions, LLC. All rights reserved. L-861, L -861E, L -861T QuarbJlncandescent Elevated Runway/Taxiway Edge Light Record of Changes s'►, Record of Changes Page Rev Description EC No. Checke d Approved Date B Revised Parts List Table 4-1. EP ED 4-2 C Added stake assembly parts to Table 4-1. EP WT All D Reformatted manual. 00026 is VP 9/26/03 5, 9, 10, 11,28-29, 31,34,36, 38 E Added red -blue light configuration for Declared Distance applications. Added quantities to parts lists and recommended spare parts. 00473 JS WT 6/19/00 28 F Changed Lens Color ordering code (Figure 8) from 10 to A. 00515 JY WT 7/19/00 All G Changed to new title page. Changed ADB to ADB Airfield Solutions. 00696 JY WT 5/16/01 8, 12, 14, 16-23,28, 38 H Updated Table 4. Updated weight of light fixture. Added note in Assembly Instructions about pre - assembly. Updated Figures 4 and 5. Revised Stake Mounting and Base Mounting procedures. Updated Figures 6 and 7. Updated ordering code in Figure 8. Updated L-867 Base Plate Parts List by deleting art 2935 16 -inch base plate). 00930 JY WT 9/3/02 9, 14, 28, 29, 38, 39 1 Designated 30 W/6.6 A Quartz lamp as not ETL certified; deleted the L861E only red -blue lens color from the ordering code and the parts list; deleted the name AMGLO EXM and AMGLO EXL from the parts list. 01087 JY WT 6/3/03 29 J Updated order codes and parts, ADB 2483 ER GM 7/7/09 O 2009 ADB Airfield Solutions, LLC. 96A00973 All rights reserved Issued 7/09 Page ii rao L-861, L -861E, L -861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Table of Contents Table of Contents Recordof Changes........................................................................................ii .. Tableof Contents.........................................................................................In Warranties..................................................................................................... v 1. Safety.......................................................................................................1 SafetySymbols.....................................................................................1 QualifiedPersonnel..............................................................................2 IntendedUse........................................................................................2 Installation............................................................................................3 Operation.............................................................................................. 3 Action in the Event of a System or Component Malfunction ..............4 Maintenanceand Repair.......................................................................4 2. Description...............................................................................................5 L-861 Elevated Light Fixture: Required Equipment ............................7 Specifications....................................................................................... 8 Lampsand Lens Colors....................................................................9 Input..................................................................................................9 RatedLamp Life...............................................................................9 Lamps.............................................................................................10 Lens................................................................................................10 PhotometricData............................................................................10 Weather...........................................................................................l l Environmental Operating Conditions.............................................12 Weight............................................................................................12 Dimensions.....................................................................................12 3. Installation..............................................................................................13 introduction........................................................................................13 Unpacking..........................................................................................13 Assembly Instructions........................................................................14 Installation..........................................................................................17 StakingMounting...........................................................................17 BaseMounting................................................................................21 4. Maintenance...........................................................................................25 5. Troubleshooting 6. Repair.....................................................................................................26 Introduction........................................................................................26 LampReplacement.............................................................................26 ® 2009 ADB Airfield solutions, LLC. 96AO097J All rights msorved Issued 7/09 Page iii L-861, L-861 E, L -861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Table of Contents Table of Contents (cont'd.) VIA Using the Illustrated Parts List...........................................................28 L-861 Light Fixture Ordering Code...................................................29 L-861 Light Fixture Parts List............................................................29 Required Equipment Supplied.....................................................7 L-861 Head Assembly Parts List.......................................................31 Table 4. L-861 Head Assembly (Phenolic and Porcelalin Sockets).............31 L-861 Head Assembly (Quartz Socket)..........................................34 Isolation Transformers.................................................................8 L-861 Stake Assembly Parts List.......................................................36 Table 6. L-867 Base Plate Parts List................................................................38 Recommended Spare Parts.................................................................38 Lamps.........................................................................................10 L-861 Light Fixture Spare Parts.....................................................38 Table 8. L-861 Head Assembly Spare Parts.................................................39 List of Figures Figure 1. L-861 Light Fixture ....................................................................6 Figure 2. L-861 Light Fixture Dimensions..............................................13 Figure 3. Head Assembly with Phenolic Socket......................................15 Required Equipment Supplied.....................................................7 Figure 4. L-861 Light Fixture Assembly.................................................16 Table 4. Figure 5. Stake Assembly........................................................................18 Figure 6. Stake Mounting.........................................................................19 Isolation Transformers.................................................................8 Figure 7. Base Mounting..........................................................................21 Table 6. Figure 8. L-861 Light Fixture Ordering Code.........................................28 Figure 9. L-861 Light Fixture ..................................................................30 Lamps.........................................................................................10 Figure 10. Lr861 Head Assembly with Phenolic Socket ...........................32 Table 8. Figure 11. L-861 Head Assembly with Porcelain Socket ..........................33 Figure 12. L-861 Head Assembly with Quartz Socket..............................35 Photometric Data for L-861 T Light Fixture...............................11 Figure 13. Stake Assembly........................................................................37 Table 10. List of Tables Table 1. L-861 Elevated Light Fixtures.....................................................5 Table2. Mounting Columns......................................................................7 Table 3. Required Equipment Supplied.....................................................7 Table 4. Required Equipment Not Supplied..............................................8 Table 5. Isolation Transformers.................................................................8 Table 6. Lamps and Lens Colors................................................................9 Table7. Lamps.........................................................................................10 Table 8. Photometric Data for L-861 Light Fixture.................................10 Table 9. Photometric Data for L-861 T Light Fixture...............................11 Table 10. Photometric Data for L-861 E Light Fixture ............................... l l Table 11. L-861 Light Fixture Maintenance ..............................................24 ® 2009 ADH Airfield Solutions, LLC. All rights reserved 96A0097J Issued 7/09 Page iv /"1 /ftt% L-861, L-861 E, L -861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Warranties Products of ADB Airfield Solutions manufacture are guaranteed against Warranties mechanical, electrical, and physical defects (excluding lamps) fora period of one year from the date of installation or a maximum of two years from the date of shipment and are guaranteed to be merchantable and fit for the ordinary purposes for which such products are made. ADB Airfield Solutions will correct by repair or replacement, at its option, equipment or parts which fail because of mechanical, electrical or physical defects, provided that the goods have been properly handled and stored prior to installation, properly installed and properly operated after installation, and provided further that Buyer gives ADB Airfield Solutions written notice of such defects after delivery of the goods to Buyer. ADB Airfield Solutions reserves the right to examine goods upon which a claim is made. Said goods must be presented in the same condition as when the defect therein was discovered. ADB Airfield Solutions furthers reserves the right to require the return of such goods to establish any claim. ADB Airfield Solutions' obligation under this guarantee is limited to making repair or replacement within a reasonable time after receipt of such written notice and does not include any other costs such as the cost of removal of defective part, installation of repaired product, labor or consequential damages of any kind, the exclusive remedy being to require such new parts to be furnished. ADB Airfield Solutions' liability under no circumstances will exceed the contract price of goods claimed to be defective. Any returns under this guarantee are to be on a transportation charges prepaid basis. For products not manufactured by, but sold by ADB Airfield Solutions, warranty is limited to that extended by the original manufacturer. This is ADB Airfield Solutions' sole guarantee and warranty with respect to the goods; there are no express warranties or warranties of fitness for any particular purpose or any implied warranties of fitness for any particular purpose or any implied warranties other than those made expressly herein. All such warranties are expressly disclaimed. Disclaimers This manual could contain technical inaccuracies or typographical errors. ADB Airfield Solutions reserves the right to revise this manual from time to time in the contents thereof without obligation of ADB Airfield Solutions to notify any person of such revision or change. ® 2009 ADB Airfield solutions, LLC. All rights reserved Details and values given in this manual are average values and have been compiled with care. They are not binding, however, and ADB Airfield Solutions disclaims any liability for damages or detriments suffered as a result of reliance on the information given herein or the use of products, processes or equipment to which this manual refers. No warranty is made that the use of the information or of the products, processes or equipment to which this manual refers will not infringe any third party's patents or rights. The information given does not release the buyer from making their own experiments and tests. 96AO097J Issued 7/09 Page v L-861, L -861E, L-861 T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Safety L-8619 L -861T, L -861E Quartz/Incandescent Elevated Runway/Taxiway 1. Safety This section contains general safety instructions for using your ADB Airfield Solutions equipment. Some safety instructions may not apply to the equipment in this manual. Task- and equipment -specific warnings are included in other sections of this manual where appropriate. Note all warnings and follow all instructions carefully. Failure to do so may result in personal injury, death, or property damage. To use this equipment safely, • Refer to the FAA Advisory Circular AC 150/5340-26, Maintenance of Airport Visual Aids Facilities, for instructions on safety precautions. • Observe all safety regulations. To avoid injuries, always remove power prior to making any wire connections and touching any parts. Refer to FAA Advisory Circular AC 150/5340-26. • Read and become familiar with the general safety instructions provided in this section of the manual before installing, operating, maintaining, or repairing this equipment. • Read and carefully follow the instructions given throughout this manual for performing specific tasks and working with specific equipment. • Store this manual within easy reach of personnel installing, operating, maintaining, or repairing this equipment. • Follow all applicable safety procedures required by your company, industry standards, and government or other regulatory agencies. • Obtain and read Material Safety Data Sheets (MSDS) for all materials used. Safety Symbols Become familiar with the safety symbols presented in this section. These symbols will alert you to safety hazards and conditions that may result in personal injury, death, or property and equipment damage. AWARNING: Failure to observe this warning may result in personal injury, death, or equipment damage. ® 2009 ADB Airfield Solutions, LLC. All rights reserved WARNING: Risk of electrical shock. Failure to observe this / warning may result in personal injury, death, or equipment rdamage. 96A0097J Issued 7/09 Page I L-861, L -861E, L -861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Safety Safety Symbols (cont'd) WARNING: Disconnect equipment from line voltage. Failure to observe this warning may result in personal injury, death, or equipment damage. WARNING: Wear safety goggles. Failure to observe may result in serious injury. CAUTION: Failure to observe may result in equipment ' damage. Qualified Personnel The term quaked personnel is defined here as individuals who thoroughly understand the equipment and its safe operation, maintenance, and repair. Qualified personnel are physically capable of performing the required tasks, familiar with all relevant safety rules and regulations and have been trained to safely install, operate, maintain, and repair the equipment It is the responsibility of the company operating this equipment to see that its personnel meet these requirements. Intended Use WARNING: Use of this equipment in ways other than described in this manual may result in personal injury, death., or A property and equipment damage. Use this equipment only as described in this manual. 82009 ADB Airfield Solutions, LLC. All rights reserved ADB Airfield Solutions cannot be responsible for injuries or damages resulting from nonstandard, unintended applications of its equipment. This equipment is designed and intended only for the purpose described in this manual. Uses not described in this manual are considered unintended uses and may result in serious personal injury, death, or property damage. Unintended uses may result from taking the following actions: • making changes to equipment that have not been recommended or described in this manual or using parts that are not genuine ADB Airfield Solutions replacement parts • failing to make sure that auxiliary equipment complies with approval agency requirements, local codes, and all applicable safety standards • using materials or auxiliary equipment that are inappropriate or incompatible with your ADB Airfield Solutions equipment • allowing unqualified personnel to perforin any task 96A0097J Page 2 Issued 7109 L-861, L-861 E, L-861 T QuaruAncandescent Elevated Runway/Taxiway Edge Light Safety /'-k Installation Read the installation section of all system component manuals before installing your equipment. A thorough understanding of system components and their requirements will help you install the system safely and efficiently. WARNING: Failure to follow these safety procedures can ' result in personal injury or death. • Allow only qualified personnel to install ADB Airfield Solutions and auxiliary equipment. Use only approved equipment Using unapproved equipment in an approved system may void agency approvals. • Make sure all equipment is rated and approved for the environment in which you are using it. • Follow all instructions for installing components and accessories. • Install all electrical connections to local code. • Use only electrical wire of sufficient gauge and insulation to handle the AWN rated current demand. All wiring must meet local codes. • Route electrical wiring along a protected path. Make sure they will not be damaged by moving equipment. • Protect components from damage, wear, and harsh environment conditions. • Allow ample room for maintenance, panel accessibility, and cover removal. • Protect equipment with safety devices as specified by applicable safety regulations. • If safety devices must be removed for installation, install them immediately after the work is completed and check them for proper functioning. Operation Only qualified personnel, physically capable of operating the equipment and with no impairments in their judgment or reaction times, should operate this equipment. Read all system component manuals before operating this equipment. A thorough understanding of system components and their operation will help you operate the system safely and efficiently. ® 2009 ADB Airfield Solutions, LLC. 96AO097J Page 3 All rights reserved Issued 7/09 L-861, L-861 E, L -861T Quartz/Incandescent ^ Elevated Runway/Taxiway Edge Light Safety Operation (cont'd) Before starting this equipment, check all safety interlocks, fire - detection systems, and protective devices such as panels and covers. Make sure all devices are fully functional. Do not operate the system if these devices are not working properly. Do not deactivate or bypass automatic safety interlocks or locked -out electrical disconnects or pneumatic valves. • Never operate equipment with a known malfunction. • Do not attempt to operate or service electrical equipment if standing water is present. • Use this equipment only in the environments for which it is rated. Do not operate this equipment in humid, flammable, or explosive environments unless it has been rated for safe operation in these environments. • Never touch exposed electrical connections on equipment while the power is ON. Action in the Event of a Do not operate a system that contains malfunctioning components. If a System or Component component malfunctions, turn the system OFF immediately. i•y Malfunction • Disconnect and lock out electrical power. • Allow only qualified personnel to make repairs. Repair or replace the malfunctioning component according to instructions provided in its manual. Maintenance and Repair Allow only qualified personnel to perform maintenance, troubleshooting, and repair tasks. Only persons who are properly trained and familiar with ADB Airfield Solutions equipment are permitted to service this equipment • Always use safety devices when working on this equipment. • Follow the recommended maintenance procedures in your equipment manuals. • Do not service or adjust any equipment unless another person trained in first aid and CPR is present • Connect all disconnected equipment ground cables and wires after servicing equipment Ground all conductive equipment. • Use only approved ADB Airfield Solutions replacement parts. Using unapproved parts or making unapproved modifications to equipment may void agency approvals and create safety hazards. ® 2009 ADB Airfield Solutions, LLC. 96AO097J Page 4 All rights reserved Issued 7/09 ,/0hk r L-861, L-861 E, L -861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Description Maintenance and Repair • Check interlock systems periodically to ensure their effectiveness. (cont'd) • Do not attempt to service electrical equipment if standing water is present. Use caution when servicing electrical equipment in a high - humidity environment. • Use tools with insulated handles when working with electrical equipment. 2. Description See Figure 1. This section describes the medium intensity elevated light fixtures (quartz/incandescent) referred to in Table 1. These fixtures are designed to provide definition to the edges and the end of nonprecision IFR airport runways and taxiways. The light fixtures are available with a mounting column and are protected with aviation yellow gloss alkyd enamel paint. ® 2009 ADB Airfield Solutions, LLC. All rights reserved Table 1. L-861 Elevated Licht Fixtures Light Fixture Function L-'6LRunway Edge Light -861T E-86 IT Taxiway Ede Light L -861E I Runway Threshold/End Li ht/Declared Distance 96AO097J Issued 7/09 Page 5 L-861, L -861E, L -861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Description 2. Description (conr'd) Figure 1. L-861 Light Fixture I. Lamp 2. Clamp Band 3. Column 4. Coupling 5. L-823 Cordset 6. Head Assembly 7. Lens ® 2009 ADB Airfield Solutiow, LLC. 96AO097J Page 6 All rights reserved Issued 7/09 /"\ L-861, L -861E, L -861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Description 2. Description (cont'd) L-861 Elevated Light Fixture: Required Equipment The light fixtures are available in a number of color or color combination lenses and lamp wattages. All L•861 light fixtures have the following physical configuration: • a cast aluminum head assembly (6) • a stainless single -latch encircling clamp band (2) to hold the lens cap (7) • a standard mounting column (3) • a single gasket between the lens and the head assembly • four screws in the head assembly to allow a four -degree fixture leveling adjustment after installation The fixtures can be stake mounted on a 30 -inch (762 mm) galvanized steel stake or mounted on a base plate for a 12- or 16 -inch- (304.8 or 406.4 min-) diameter L-867 base. Base mounting is recommended because maintenance is easier to perform and the equipment has added protection. Stake - mounted lights require transformers, cables, and connectors that are designed for direct earth burial. Refer to Table 2 for mounting heights. NOTE: The measurements in Table 2 are taken from the grade to the top of the light fixture. T91.1e 9 Mnmfino Heivhtc Type Hei ht in. Heigh mm Standard FAA minimum 14 355.6 Standard 24 610 Standard fPAA maximum 30 762 Refer to Table 3 for required equipment that is supplied. Refer to Table 4 for required equipment that is not supplied. Refer to the Pans section for part numbers. Ta1de 4 RelnllreA F.nninment Sunolied -Descrition Quantity Light fixture (with steel column, frangible fitting, lamp and L-823 cordset 1 Instruction manual 1 ner order O 2009 ADB Airfield Solutions, LLC. 96AO097J Page 7 All rights reserved Issued 7/09 r L-861, L-861 E, L -861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Description L-861 Elevated Light Fixture: Required Equipment (cont'd) Table 4. Required Eouioment Not Suoolied Description Quantity Torque wrench 0 to 200 in -Ib with 9/16 socket 1 Screw driver medium blade 1 Loctite Grade "or equivalent As required Wrench for 1/4 in. hex head cap screw 1 L-867 base plate assembly (for 12- or 16 -inch diameter L-867 base) when fixture is base mounted I Wrench for 1 13/16 hex screw on frangible coupling I L-867 base, 12 -or 16 -inch- 304.8 or 406.4 mm- diameter 1 Stake assembly (30 -inch galvanized steel) when fixture is stake mounted. 1 Isolation transformer for series circuit Refer to Table 5 for the correct transformer to use. 1 L-823 sin le -conductor rim connector kit 1 Table 5. Isolation Transformers If you have this circuit.., And this lamp wattage... Use this isolation transformer... 6.6 A 30 or 45 W L-830-1 6.6 A/6.6 A 20 A 30 or 45 W L-830-2 20 A/6.6 A Specifications This subsection provides specifications for the L-861 elevated light fixtures. ® 2009 ADB Airfield Solutions, LLC. 96AO097J page 8 All rights reserved Issued 7/09 L-861, L-861 E, L -861T Quartz/Incandescent 100% Elevated Runway/Taxiway Edge Light Description 00", Lamps and Lens Colors Refer to Table 6. Table 6_ 11-861 Lamns and Lens Colors Type se Available Lams Light Direction Lens Color Note L-861 30 W/6.6 A Incandescent Omnidirectional Clear (Runway Edge 45 W/6.6 A Incandescent Yellow A Nonprecision IFR 40 W/120 Vac Incandescent Runways) 30 W/6.6 A Quartz 45 W/6.6 A Quartz Bidirectional Clear -Yellow A Clear -Green A Clear -Red L -861T 45 W/6.6 A Quartz Omnidirectional Blue B (Taxiway Edge) 45 W/6.6 A Incandescent 40 W/120 Vac Incandescent 30 W/6.6 A Quartz 30 W/6.6 A Incandescent L -861E 45 W/6.6 A Incandescent Omnidirectional/ Red/Red-Blue (Runway Threshold/End, 45 W/6.6 A Quartz Bidirectional Nonprecision IFR Runways and Declared Distance) 30 W/6.6 A/Quartz Bidirectional Red -Green Omnidirectional Green NOTE A: Not FAA approved color. B: The L -861T 40 W/120 Vac incandescent lam is nota refocus lamp. Itis also not ETL certified. Input 6.6Aor120Vac Rated Lamp Life 1000 hours (minimum) 0 2009 ADB Airfield Solutions, LLC. 96A0097J All rights reserved Issued 7/09 Page 9 owl L-861, L -861E, L -861T QuaruAncandeseent Elevated Runway/Taxiway Edge Light Description Lamps Refer to Table 7. Table 7. Lamps Lamp Type Lamp Wattage Manufacturer Prefocus incandescent (phenolic socket) 30 W/6.6 A OSRAM/SYLVANIA 55041 125 45 W/6.6 A OSRAM/SYLVANIA 55048 142.4 40 W/120 Vac GE 15421 Nonprefocus (porcelain socket) 40 W/120 Vac GE 40 A/fS Prefocus quartz (bi-pin socket) 30 W/6.6 A OSRAM/SYLVANIA 55041 67 45 W/6.6 A GE EXM Lens Heat- and shatter -resistant glass lens Photometric Data This subsection provides photometric data for the L-861, L-86 IT, and L -861E light fixtures. L-861 Light Fixture Refer to Table 8. Tahle R. Photometric Data for L-861 LiPht Fixture Color Lam Average Peak Intensity Candelas (cd) 2-10 Degrees Vertical FAA Minimum Clear 30 W/6.6 A, quartz 144.2 125 Clear 40 W/120 Vac, incandescent 142.4 125 Yellow 30 W/6.6 A, quartz 95.4 67 Yellow 40 W/120 Vac, incandescent 97.4 67 Clear 45 W, incandescent 273.2 125 Yellow 45 W, incandescent 172 167 Clear 45 W, quartz 289.8 125 Yellow 45 W, quartz 171.4 67 0 2009 ADB Airfield Solutions, LLC. 96AO097J All rights reserved Issued 7/09 Page 10 L-861, L -861E, L -861T QuartzAncandescent Elevated Runway/Taxiway Edge Light Description L -861T Light Fixture Refer to Table 9. Tnhle 9. Photometric Data for L -861T Lieht Fixture Color Lamp Measured Peak Intensity Candelas (cd) 5 De reel Vertical FAA Minimum Note Blue 40 W/120 Vac, incandescent 3.4 2 Blue 30 W, incandescent 3.34 2 Blue 45 W, incandescent 4.1 2 Blue 30 W, quartz 3.72 2 Blue 45 W, quartz 6.84 2 L -861E Light Fixture Refer to Table 10. T.,lao t o Phnfomrrrin nntn for t -R61 F, Light Fixture Color Lam Measured Peak Intensity Candelas (ed) (FAA minimum is in parentheses) t 5 Degrees t 3 Degrees 11.5 Degrees Note Green 45 W/6.6 Aquartz 373.2 90 415 180 423.2 300 Red 45 W/6.6 A, quartz 697.8 10 none none A Green 45 W/6.6 A, incandescent 328 90 364.3 180 374 300 Red 45 W/6.6 A, incandescent 663 10 none none A Blue 45 W/6.6 A, incandescent 8.8(2) Not applicable Nota licable Red 30 W, quartz 33 (10 Nota licable Nota licable Blue 30 W, quartz 5 2 Not applicable Not applicable NOTE A: FAA minimum average intensity not specified. Weather Designed for exposure to rain, snow, ice, and standing water © 2009 ADB Airfield Solutions, LLC. 96A0097J All rights reserved Issued 7/09 Page 11 n L-861, L-86 IE, L -861T QuartMileandescent Elevated Runway/Taxiway Edge Light Description O 2009 ADB Airfield Solutions, LLC. All rights reserved Environmental Operating Conditions The medium intensity elevated light fixture is designed to operate under the conditions presented below for temperature, wind, altitude, and relative humidity. Temperature -55 to +55 °C (-67 to +131 °F) Wind Velocities up to 350 mph (560 kph) Altitude Sea level to 10,000 feet (3000 m) Relative Humidity Up to 100 % Weight Refer below for weight of assembled light fixtures. 14 -inch overall height: 5 Ib (2.27 kg) 24 -inch overall height: 6.25 Ib (2.84 kg) 30 -inch overall height: 7 Ib (3.18 kg) 96A0097J Issued 7109 Page 12 L-861, L -861E, L -861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Description Dimensions See Figure 2. 5-7/64 in. (129.77 mm) j9! I i 4-3/8 in. (111.12 mm) Figure 2. L-861 Light Fixture Lens Dimensions 6 2009 ADB Airfield Solutions, LLC. 96AO097J Page 13 All rights reserved Issued 7/09 .0^. L-861, L-861 E, L-86IT QuartztIncandescent Elevated Runway/Taxiway Edge Light Installation 3. Installation WARNING: Allow only qualified personnel to perform the ' following tasks. Observe and follow the safety instructions in this document and all other related documentation. Introduction This section provides instructions for installing the L-861 medium intensity elevated light fixture. Refer to the airport project plans and specifications for the specific installation instructions. Unpacking The equipment is shipped ready for installation. Handle equipment very carefully to prevent component damage. Unpack the carton upon receipt and check the contents and their condition. Note any exterior damage to the carton that might lead to detection of equipment damage. If you note any damage to any equipment, file a claim with the carver immediately. The carrier may need to inspect the equipment. Assembly Instructions NOTE: Check the packing list with the parts list to verify that all parts are present before proceeding. See the Parts section. NOTE: The elevated light fixtures are completely assembled at the factory. Use the assembly instructions below if assembly for repair or maintenance is necessary. 8 2009 ADB Airfield Solutions, LLC. All rights reserved 96AO097J Issued 7/09 Page 14 L-861, L -861E, L -861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Installation Assembly Instructions (cont'd) To assemble parts, perform the following procedure: 1. Place the L-823 cordset (Item 4, Figure 3) into the column (Item 4, Figure 4). NOTE: Figure 3 shows a head assembly with a phenolic socket The L-861 light fixtures with porcelain and quartz sockets are similar. 1. Lens Clamp 2. Lamp Base 3. Self -Taping Set Screw 4. L-823 Cordset 5. Level Screws ® 2009 ADB Airfield Solutions, LLC. All rights reserved 96A0097J Issued 7/09 Page 15 L-861, L-861E,L-861T QuartzlIncandescent Elevated Runway/Taxiway Edge Light Installation 2. See Figure 4. Insert the column into the base of the head assembly (3). I 2 3 7 4 6 5 10 8 — — — r_ 9 I 11 I 12 LlI I L Figure 4. L-861 Light Fixture Assembly 1. Lens 5. Self -Taping Set Screw 9. Gasket 2. Clamp Band 6. Frangible Coupling 10. Stake Hub 3. Head Assembly 7. Leveling Screws 11, L-867 Light Base Transformer Housing 4. Column 8. L-867 Base Plate 12. Optical Stake Assembly © 2009 ADB Airfield Solutions, LLC. 96A0097J Page 16 All rights reserved Issued 7/09 I- I� L -861, L-861 E, L -861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Installation Assembly Instructions (cont'd) 3. See Figure 3. Secure the column to the base by tightening the self -taping set screw (3) located on the side of the base. 4. Insert the lamp into the socket. Refer to the Repair section. CAUTION: Touching quartz lamps with bare fingers may ' seriously shorten lamp life. If the quartz lamp has been touched, clean the lamp with tissue moistened with isopropyl alcohol. 5. See Figure 4. Place the lens (1) on the upper base of the head assembly. Attach with clamp band (2). 6. Secure the lens to the head assembly (3) by tightening the clamp band. 7. Insert the end of the column into the frangible coupling (6) and secure by tightening the self -taping set screw (5). Installation This subsection provides installation instructions for "61 medium intensity elevated light fixtures. Light fixtures can be mounted on a stake or a base. 02009 ADB Airfield Solutions, LLC. All rights reserved Stake Mounting When you use 120 Vac parallel -powered lighting systems, mount the column light fixtures on 30 -inch (762 -mm) galvanized steel stakes with a fitting attached to the top of each stake to receive the male thread of the fangible coupling. Stake mounting requires cables and connections that are designed for direct earth burial. Install according to appropriate FAA and local contractor specifications. 96AO097J Issued 7/09 Page 17 #OWN L-861, L-861E,L-861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Installation Stake Mounting (cont 1d) To install the light fixture on the stake, perform the following procedure: 1. See Figure 5. Attach the stake hub (2) to the metal stake (5) using two 3/8-16 x 3/4 -in. hex head screws (3) and 3/8 -in. lockwashers (4). Figure 5. Stake Assembly 1. L-823 Male Plug 2. Stake Hub 3. Hex Head Screw 4. Lockwasher 5. Metal Stake 6. Transformer Secondary Female Plug 7. Cable Connector Support 8. Hex Head Screw 9. Lockwasher 10. Grounding Screw Hole 11. Transformer Secondary Lead ® 2009 ADB Airfield Solutions, LLC. %A00971 Page 18 All rights reserved Issued 7/09 /"Al /amk� L-861, L -861E, L -861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Installation Stake Mounting (coned) 2. See Figure 6. Install the stake (4) in 6 -inch- (152.4 -mm-) diameter holes in the ground at a depth of 30 inches (762 mm) so that the mounting hub (8) of the stake is level. NOTE: The top of the stake should be even with the ground within one degree of the vertical. In areas where frost may cause heaving, anchor the stake with concrete and use a permeable backfill material such as sand around the buried electrical components. Cover the top surface with an impervious material to reduce moisture penetration. ACAUTION: Do not drive stakes. Driving stakes may damage the stake and cause light fixture misalignment. Refer to FAA specification AC 150/5340-24. 1 b!Y i0. II 1 E3 � _ iii i 7 12 6 \ 1830 3 i 54 Figure 6. Stake Mounting 1. Frangible Coupling and Disconnect Plug 7. L-830 Transformer 2. Connectors S. Stake Hub 3. 5 KV, L-824 Cable 9. Transformer Secondary Plug 4. Metal stake (30 in.) 10. Hex Head Screw 5. Concrete Anchor (Recommended 6 x 6 x 12 -in.) 11. Lockwasher 6. Optional Bare Copper Counterpoise Wire 12. Cable Connector Support © 2009 ADB Airfield Solutions, LLC. 96AO097J Page 19 All rights mserved Issued 7/09 /\ L-861, L -861E, L -861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Installation Stake Mounting (cont'd) 3. Backfill around the stake with compacted earth passing a 1 -inch (25.4 mm) sieve. © 2009 ADB Airfield Solutions, LLC. All rights reserved NOTE: Use a bubble level or carpenter's level to ensure the stake is vertical before backfilling around stake. Backfill with concrete (5) in case of unstable soil conditions. 4. Make electrical connections by installing the transformer primary cables (3) to the field circuit. Then insert the transformer secondary plug (9) in the cable connector support's forked tine and attach the cable connector support (12) to the stake hub (8) using 1/4-20 x 3/4 -in. hex head screw (10) and 1/4 -in. split lockwasher (11). NOTE: The small hole at the lower end of the stake is provided for counterpoise wire connection (6). 5. Install the light fixture on the stake. 96A0097J Issued 7/09 Page 20 /'\ L-861, L-861 E, L -861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Installation Base Mounting See Figure 7. The 1,861 light fixtures can be mounted on an L-867 base (2) mated with a base plate (1) with a diameter and bolt -hole corresponding to either a 12 -inch- or 16 -inch- (304.8 or 406.4 mm-) diameter L-867 base. The base plate is designed to receive a frangible coupling (8) using a female thread. Figure 7. Base Mounting 1. Base Plate 2. L-867 Base 3. L-823 Primary Connector 4. Two -foot Slack for Connections (Minimum) 5. 5 KV, L-824 Cable 6. optional Bare Copper Counterpoise Wire 7. Four -Inch Concrete Backfill Recommended S. Frangible Coupling and Disconnect Plug 9. L-823 Secondary Connector 10. L-830 Isolation Transformer ® 2009 ADB Airfield Solutions, LLC. All rignts reserved 96AO097J Issued 7/09 Page 21 /%, /'! n L-861, L -861E, L -861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Installation Base Mounting (contd.) NOTE: See Figure 4. A gasket (9) is used with the base plate to form a watertight seal between the base plate and the L-867 base. NOTE: Install the light fixture on the base according to appropriate FAA and local contactor specifications. To install the light fixture on the base, perform the following procedure: 1. See Figure 7. Install the L-867 base on undisturbed soil. If the soil is unsuitable, remove soil to an adequate depth and replace with compacted acceptable material. NOTE: In closed duct systems, install in soil conditions with good drainage. Use light bases having a drain hole to prevent water accumulation. 2. Orient the cable entrance hubs of the base in the proper directions. 3. Level the light base so that the mounting flange surface is level with finished grade. 4. With the base at the proper orientation and held at proper elevation, place approximately 4 inches (101.6 mm) of concrete backfill (7) around the outside base. NOTE: If the concrete backfill is omitted, the earth backfill must be compacted to maintain proper elevation and orientation of the base. 5. Slope the top of the concrete away from the flange portion of the base so the sloped outer edges of the concrete are at surface grade. 6. To install the light fixture on the base, connect the 6.6/20 A series circuit to the primary of the appropriate isolation transformer. Use an L-830-1 transformer for 6.6 A series circuits and L-830-2 for 20 A series circuits. NOTE: Use a brick or other device to raise the transformer about 3 inches (76.2 mm) above the bottom surface of the L-867 base (2) to avoid the possibility of the transformer being partially immersed in water in case water accumulates under the level of the ducts or pipes. ® 2009 ADB Airfield Solutions, LLC. 96AO097J All rights reserved Issued 7/09 Page 22 /"k L-861, L-861 E, L -861T QuarftAncandescent Elevated Runway/Taxiway Edge Light Installation Base Mounting (cont'd) 7. After you have connected the transformer, check the continuity of the series loop. 8. Wrap the connector joints in the primary circuit with at least one layer of rubber or synthetic rubber tape and one layer of plastic tape one-half lapped, extending at least one and a half inches on each side of the joint. 9. Clamp the female secondary plug from the L-830 transformer to the L-867 base plate fitting. 10. Bolt the base plate (1) with the base plate gasket to the L-867 base using six 3/8-16 stainless steel bolts. Apply a drop of Loctite Grade AV to each bolt thread, and use a torque wrench to torque bolts down to 100 in -Ib. 11. Connect a male L-823 plug (3) from the light fixture to the female plug on the secondary lead of the L-830 transformer. 12. Loosen the frangible coupling screw holding the coupling (8) to the light fixture column. Screw the coupling into the female thread on the base plate. NOTE: Apply anti -seize compound to the coupling threads to improve coupling removal and prevent thread corrosion. O 2009 ADB Airfield solutions, LLC. 96AO097J All rights reserved Issued 7/09 Page 23 ^► lo► L-861, L -861E, L -861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Maintenance 4. Maintenance To keep the L-861 light fixtures operating efficiently, follow a preventive maintenance schedule. Refer to Table 11. Refer to FAA AC 150/5340-26 for more detailed information. Tshle 11. L-861 Light Fixture Maintenance Interval Maintenance Task Action Daily Check for burned out lamp. After turning off power, replace burned -out lamps. Refer to the Repair section. Check for dim lamp. After turning off power, replace burned -out lamps. Refer to the Repair section. After turning off power, check isolation transformer on series circuit. Check for broken lens. Replace lens. Weekly Check for vegetation. Remove vegetation. Use weed killer. Check for dirty lens. Clean with glass cleaner. Monthly Check for misaligned fixture. Straighten, level, and align light fixture. Check for dirty lamp socket. After turning off power, clean the lamp socket. Check for dirty frangible coupling weep Clean weep holes. holes (for stake -mounted fixtures only). Check for dirt on fixture drain holes. Clean drain holes. Semi -Annually Check for improper ground elevation. Grade so frangible point is level with ground elevation. Check for improper light elevation. Maintain same elevation for all light fixtures. Check for moisture present in light Check drain holes and clamps. Check lens for housing or base. cracks. If damaged, replace. Use water pump to remove water from base. Check for corrosion present or paint loose Scrape and repaint light fixture. or chipped. Annually Check for cracks, corrosion, and shorts. Repair or replace light fixture. Check for dirty contacts. Clean contacts after turning off power. Check for loose wire connections. Tighten wire connections. Unscheduled Make prediction of heavy snowfall, if Use red flags or sticks to mark the location of necessary. fixtures to facilitate snow removal and lessen the chance of damage to fixtures by snow removal equipment 2009 ADB Airfield Solutions, LLC. 96AO097J All rights reserved Issued 7/09 Page 24 /0%, L-861, L-861 E, L -861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Troubleshooting 5. Troubleshooting WARNING: Allow only qualified personnel to perform the A! following tasks. Observe and follow the safety instructions in this document and all other related documentation. WARNING: De -energize the circuit and lock out the circuit or ' regulator so that the circuit cannot be energized by remote means before attempting to service the fixture. This section contains troubleshooting information. This information covers only the most common problems that you may encounter. If you cannot solve the problem with the information given here, contact your local ADB Airfield Solutions representative for help. Problem Possible Cause Corrective Action Lamps will not turn on. Defective lamp Replace lamp. Refer to the Repair section. Loose connection(s) Tighten wires. Transformer on series circuit bad Replace transformer. Moisture present in fixture Open up and dry light fixture. Inspect lens for cracks. Replace lamp and any damaged arts. Refer to the Repair section. © 2009 ADB Afield Solutions, LLC. All rights reserved 96AG097J Issued 7/09 Page 25 L-861, L-861 E, L -861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Repair 6. Repair Introduction Lamp Replacement © 2009 ADH Airfield Solutions, LLC. All rights reserved WARNING: Allow only qualified personnel to perform the ' following tasks. Observe and follow the safety instructions in this document and all other related documentation. This section provides instructions for replacing lamps for the L-861 medium intensity elevated light fixture. To replace a lamp, perform the following procedure: 1. De -energize the circuit and lock out the circuit. WARNING: Disconnect equipment from line voltage. Failure " to observe this warning may result in personal injury, death, or equipment damage. 2. Remove the lens from the fixture by loosening the lens clamp band on the lamp base. 3. Remove the lamp from the socket by performing one of the following: a) For quartz socket lamps, remove the lamp by pulling the lamp out of the socket. CAUTION: Touching quartz lamps with bare fingers may ' seriously shorten lamp life. If the quartz lamp has been touched clean the lamp with tissue moistened with isopropyl alcohol. b) For porcelain socket lamps, remove the lamp by unscrewing the lamp from the socket. c) For phenolic socket lamps, remove the lamp from the socket by pressing the lamp down and turning the lamp counterclockwise a quarter of a tum. 4. Install the new lamp by reversing the removal procedure. 96AO097J Issued 7/09 Page 26 L-861, L -861E, L -861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Parts ry 7. Parts Using the Illustrated Parts List To order parts, call ADB Airfield Solutions Customer Service or your local representative. Use this five -column parts list, and the accompanying illustration, to describe and locate parts correctly. This subsection describes how to use the illustrated parts list covered later in this section. It does not provide the actual parts list. The Item column numbers correspond to the numbers that identify parts in illustrations following each parts list. NS (not shown) indicates that a listed part is not illustrated. The Description column gives the part name, as well as its dimensions and other characteristics when appropriate. Indentions show the relationships between assemblies, subassemblies, and parts. The Part Number column gives the ADB Airfield Solutions part number. Item Description Part Number Quantity Note Sl Assembly xxxxxxxx I A NS Part xxxxx)= I HI Part or Assembly part/Assembly for option 1 xxxxxxxx 2 Part/Assembly for option 2 xxxxxxxx 2 TI Assembly xxxxxxxx I I • Part xxxxxxxx 2 • Part xxxxxxxx NOTE A © 2009 ADB Airfield Solutions, LLC. All rights reserved The Quantity column contains the quantity required per unit, assembly, or subassembly. The code AR (As Required) is used if the part number is a bulk item ordered in quantities or if the quantity per assembly depends on the product version or model. The Note column contains letters that refer to notes at the end of each parts list. Notes contain special ordering or product/part version information. 96A0097J Issued 7/09 Page 27 n L-861, L-861 E, L -861T Quattz(Incandescent Elevated Runway/Taxiway Edge Light Parts L-861 Light Fixture Ordering Code 44C1081 Figure 8 shows how to determine the ordering code for a particular L-861 light fixture. NOTE: If the head assembly for nonprefocus, screw -based lamps is required, contact the ADB Airfield Solutions sales department. X X X X Figure 8. L-861 Light Fixture Ordering Code © 2009 ADB Airfield solutions, LLC. All rights reserved Fixture Height 11 =14 inches (35.6 cm) 22 = 24 inches (61.0 cm) 33 = 30 inches (76.2 cm) 44 = 20 inches (50.8 cm) lens Color 0 =Nonstandard Lens (Special Order Only)** I = Omnidirectional Clear (L-861) 2 = Bidirectional Clear -Yellow (L-861) 3 = Bidirectional Clear -Red (L-861) 4 = Bidirectional Clear -Green (L-861)** 5 = Omnidirectional Blue (L-8617) 6 = Bidirectional Red -Green (L-861 E) 7 = Omnidirectional Red (L-861 E) 8 = Omnidirectional Green (L -861E)** 9 = Omnidirectional Yellow B = Unidirectional Green -Obscure Lamp 1= 30 W/6.6 A Incandescent* 2 = 45 W/6.6 A Incandescent* 5 = 30 W/6.6 A Quartz* 6 = 45 W/6.6 A Quartz* 7 =No Lamp, Incandescent Socket 8 = No Lamp, Quartz Socket 9 = 45 W/6.6 A, Quartz PKX30d*** *ETL certified **Not FAA recognized color ***Not ETI. certified 96A0097J Issued 7/09 Page 28 l� *ON 000"Ok L-861, L -861E, L -861T Quartz/lncandescent Elevated Runway/Taxiway Edge Light Parts L-861 Light Fixture Parts See Figure 9. Refer below for the L-861 light fixture parts list. List Item Description Part Number Quantity Note Al Head assembly I A Head assembly with phenolic socket for 14 -in. OAH 44B1079-11 Head assembly with phenolic socket for 24 -in. OAH 44BI079-12 Head assembly with phenolic socket for 30 -in. OAH 44B1079-13 Head assembly with porcelain socket for 14 -in. OAH 44B1080 -I 1 Head assembly with porcelain socket for 24 -in. OAH 44B1080-12 Head assembly with porcelain socket for 30 -in. OAH 44B1080-13 Head assembly with quartz socket for 14 -in. OAH 44B 148411 Head assembly with quartz socket for 24 -in. OAH 44B1484-12 Head assembly with quartz socket for 30 -in. OAH 44B1484-13 M1 Lens 1 Lens, clear 63A0141 Lens, clear -yellow 63A0142 Lens, clear -red 63A0144 Lens, clear -green 63A0146 Lens, blue 63A0151 Lens, red -green 63A0148 Lens, red 63A0149 Lens, green 63A0150 Lens, yellow 63A0143 Lens, yellow -red 63A0156 Lens, red -blue 63A0157 Ll Lamp 1 Prefocus lamp, 30 W/6.6 A (OSRAM/SYLVANIA 48A0006 55041 or GE 23294) Prefocus lamp, 45 W/6.6 A (GE 23295 or Phillips 48A0007 23419-6) Lamp, 40 W/120 Vac (GE 15421) 48A0002 Prefocus lamp, 40 W/120 Vac (GE 40T10P) 48A0012 B Lamp, 30 W/6.6 A (quartz) (OSRAM/SYLVANIA 48A0085 55041) (AMGLO EXL) Lamp, 45 W/6.6 A (quartz) (GE EXM) 48A0083 M3 Column I Column, 6 -inch 62A0007-6 Column, 12 -inch 62A0007-12 Column, 16 -inch 62A0007-16 Column, 22 -inch 62A0007-22 M2 Frangible coupling 62B0073 I NOTE A: Refer to L-861 Head Assembly Parts List in this section. NOTE B: Not ETL certified. © 2009 ADB Airfield Solutions, LLC. All rights reserved 96A0097J Issued 7/09 Page 29 001►, L-861, L -861E, L -861T Quartzgncandescent Elevated Runway/Taxiway Edge Light Parts L461 Light Fixture Parts List (cont'd) Figure 9. L-861 Light Fixture ® 2009 ADB Airfield Solutions, LLC. 96A0097J Page 30 All rights reserved Issued 7/09 L1 MI Al M3 M2 O Figure 9. L-861 Light Fixture ® 2009 ADB Airfield Solutions, LLC. 96A0097J Page 30 All rights reserved Issued 7/09 /NW -1 L-861, L-861 E, L -861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Parts L-861 Head Assembly Parts This subsection provides the parts list for the head assembly with phenolic, List porcelain, and quartz sockets. L-861 Head Assembly (Phenolic and Porcelain Sockets) See Figures 10 and 11. Refer below for the L-861 head assembly (phenolic and porcelain sockets) parts list. Item Description Part Number Quantity Note M3 Gasket 63B0015 1 Ll Lamp socket 1 Porcelain 49A0014 Phenolic 49A0002 Al Lens clamp assembly 44B0023 1 M2 Lamp base 62C0005 1 MI Leveling hub 6280006 1 CAI L-823 cordset 73A0009 -XX 1 A L 823 cordset terminal for incandescent fixture 7OA0208 NOTE A., when ordering this cordset, sed the overall height of the light fixture. ® 2009 ADB Airfield solutions, LLC. All rights reserved 96A0097J Issued 7/09 Page 31 /%41 L-861, L -861E, L -861T Quart7JIncandescent Elevated Runwayll'axiway Edge Light Parts L-861 Head Assembly (Phenolic and Porcelain Sockets) (cont'd) Figure 10. L-861 Head Assembly with Phenolic Socket ® 2009 ADB Afield Solutions, LLC. 96AO097J Page 32 All rights reserved Issued 7/09 r.. L-861, L-861 E, L -861T QuartzlIncandescent Elevated Runway/Taxiway Edge Light Parts 1-861 Head Assembly (Phenolic and Porcelain Sockets) (cont'd) LI Figure 11. L-861 Head Assembly with Porcelain Socket © 2009 ADB Airfield Solutions, LLC. 96AO097J All rights reserved Issued 7/09 Page Js /ft� L-861, L -861E, L -861T QuartzlIncandescent Elevated Runway/Taxiway Edge Light Parts 1-861 Head Assembly (Quartz Socket) See Figure 12. Refer below for the L-861 head assembly (quartz socket) parts list. Item Description Part Number Quantity Note M4 Gasket 63B0015 1 Al Lens clamp assembly 44B0023 1 M3 Lamp base 62C0005 1 M2 Leveling hub 62B0006 1 CAI L-823 cordset (includes terminal) 44A2387 1 A Ll Lamp socket, quartz 49AO032 1 Ml Lamp bracket for quartz lamp socket 60CI I69 1 NOTE A: When ordering this cordset, specify the overall height of the light fixture. © 2009 ADB Airfietd Solutions, LLC. 96AO097J All rights reserved Issued 7/09 Page 34 0104k L-861, L -861E, L -861T QuartzlIncandescent Elevated Runway/Taxiway Edge Light Parts 1-861 Head Assembly (Quartz Socket) (cont'd) Ll Figure 12. L-861 Head Assembly with Quartz Socket O 2009 ADB Airfield Solutions, LLC. 96A0097J All rights reserved Issued 7/09 Page 35 PN /"1 L-861, L-861 E,L-861T Quartz(Incandescent Elevated Runway/Taxiway Edge Light Parts L-861 Stake Assembly Parts See Figure 13. The stake assembly part number is 44B0348. List Item Description Part Number Quantity Note 1 Stake hub 62BO268-1 1 2 Hex head screw, 3/8-16 x 3/4 in. 64AO176-12 1 3 Split lockwasher, 3/8 in. 66AO026-29 1 4 Stake 62BO284 1 5 Cable connector support 62BO269 1 6 Hex head screw, 1/4-20 x 3/4 in. 64AO173-12 1 7 Split lockwasher,1/4 in. 66AO026-24 I a 2009 ADB Airfield Solutions, LLC. All rights reserved 96AO097J Issued 7/09 Page 36 AON L-861, L -861E, L -861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Parts L-861 Stake Assembly Parts List (contd.) Figure 13. Stake Assembly © 2009 ADB Airfield Solutions, LLC. 96AO097J Page 37 All rights reserved Issued 7/09 r1 L-861, L -861E, L -861T Quart7Ancandescent Elevated Runway/Taxiway Edge Light Pis L-867 Base Plate Parts List Refer below for the L-867 base plate parts list. Description Part Number Quantitv Note 12 -inch -diameter base plate, 1.5-12 UNF tap 1935 1 A NOTE A: Supplied without gasket. Recommended Spare Parts This subsection provides recommended spare parts for the L-861 light fixture and head assembly. 1-861 Light Fixture Spare Parts See Figure 9. Refer below for the L-861 light fixture spare parts. Item Description Part Number Note Al Head assembly Head assembly with phenolic socket for 14 -in. OAH 44B1079-11 Head assembly with phenolic socket for 24 -in. OAR 44B 1079-12 Head assembly with phenolic socket for 30 -in. OAH 44131079-13 Head assembly with porcelain socket for 14 -in. OAH 44B1080-11 Head assembly with porcelain socket for 24 -in. OAH 44BI080-12 Head assembly with porcelain socket for 30 -in. OAH 44B1080-13 Head assembly with quartz socket for 14 -in. OAH 44B1484-11 Head assembly with quartz socket for 24 -in. OAH 44B1484-12 Head assembly with quartz socket for 30 -in. OAH 44B1484-13 Ml Lens Lens, clear, L-861 63AO141 Lens, clear -yellow, L861 63AO142 Lens, clear -red, L-861 63AO144 Lens, clear -green, L-861 63AO146 Lens, blue, L -861T 63AO151 Lens, red -green, L-861 E 63A0148 Lens, red, L -861E 63AO149 Lens, green, Lr861E 63A0150 Lens, yellow 63A0143 Lens,yellow-red 63A0156 Continued on next e ® 2009 ADB Airfield Solutions, LLC. All rights reserved 96AO097J Issued 7/09 Page 38 L-861, L -861E, L -861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Parts L-861 Light Fixture Spare Parts (coned) Item Description Part Number Note L1 Lamp 63B0015 L] Prefocus lamp, 30 W/6.6 A (OSRAM/SYLVANIA 48A0006 55041 or GE 23294) 49AO014 Prefocus lamp, 45 W/6.6 A (GE 23295 or Phillips 48A0007 23419-6) 49AO032 Al Lamp, 40 W/120 Vac (GE 15421) 48A0002 M2 Prefocus lamp, 40 W/120 Vac (GE 40T10P) 48A0012 A MI Lamp, 30 W/6.6 A (quartz) (OSRAM/SYLVANIA 48AO085 CA] 55041 44A1707 A NOTE A: When ordering the L-823 cordset, specify the overall length of the light fixture. Lamp, 45 W/6.6 A (quartz) (GE EXM) 48AO083 M3 Column Column, 6 -inch 62A0007-6 Column, 12 -inch 62A0007-12 Column, 16 -inch 62A0007-16 Column, 22 -inch 62A0007-22 M2 Frangible coupling 62B0073 NOTE A: Not ETL certified. L-861 Head Assembly Spare Parts This subsection provides recommended spare parts for L-861 light fixtures with phenolic, porcelain and quartz sockets. L-861 Head Assembly (Phenolic and Porcelain Sockets) Spare Parts See Figures 10 and 11. Refer below for the L-861 head assembly (phenolic and porcelain sockets) spare parts. Item Description Part Number Note M3 Gasket 63B0015 L] Lamp socket Porcelain 49AO014 Phenolic 49A0002 Quartz 49AO032 Al Lens clamp assembly 44B0023 M2 Lamp base 62C0005 MI Leveling hub 62B0006 CA] L-823cordset includes terminal 44A1707 A NOTE A: When ordering the L-823 cordset, specify the overall length of the light fixture. ® 2009 ADB Airrield Solutions, LLC. 96AO097J All rights reserved Issued 7/09 Page 39 rMO L-861, L-861 E, L -861T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Parts L-861 Head Assembly (Quartz Socket) Spare Parts See Figure 12. Refer below for the L-861 head assembly (quartz socket) spare parts. Item Description Part Number Note M4 Gasket 63B0015 Al Lens clamp assembly 44B0023 M3 Lamp base 62C0005 M2 Leveling hub 62B0006 CAI L-823 cordset, 30 -inch (includes terminal) 44A1701 Ll Lamp socket, quartz 49AO032 Ml Lamp bracket for quartzlam socket 60CII69 ® 2009 ADB Airfield solutions, LLC. 96AO097J All rights reserved Issued 7/09 Page 40 r, 000% Sebastian Municipal Airport Runway 4-22 Improvements L-125 Base Cans SUBMITTAL REVIEW December 15, 2009 X 1. NO EXCEPTIONS TAKEN ❑ 4. REJECTED X 2. MAKE CORRECTIONS NOTED. NO RESUBMITTAL ❑ 5. NOT REQUIRED FOR REVIEW ❑ 3. MAKE CORRECTION NOTED, RESUBMIT REVIEW OF THIS SHOP DRAWING IS LIMITED TO GENERAL DESIGN CONCEPTS AND GENERAL COMPLIANCE WITH THE INFORMATION M THE PROJECT PLANS AND SPECIFICATIONS ONLY, AND IS NOT INTENDED TO BE A VERIFICATION OF TOTAL MATERIAL REQUIRED OR THAT ALL ITEMS REQUIRED ARE SHOWN. REVIEW SHALL NOT RELIEVE THE CONTRACTOR FROM THE RESPONSIBILITY OF DETAILS OF DESIGN, DIMENSIONS, JOB CONDITIONS, CONSTRUCTION MEANS AND METHODS, COORDINATION WITH OTHER TRADES, OR ANY OTHER REQUIREMENTS OF THE PLANS, SPECIFICATIONS OR CONTRACT. ANY NOTATIONS ON THIS SHOP DRAWING MADE SHALL NOT BE CONSTRUED TO AUTHORIZE ADDITONAL. WORK OR COST REVIEW OF DESIGN CALCULATIONS AND DRAWINGS PREPARED BY SPECIALTY ENGINEERS IS LIMITED TO DESIGN INTENT AND DOES NOT CONSTITUTE A DETAILED CHECK OF CALCULATIONS, NOR DOES IT RELIEVE THE SPECIALTY ENGINEERS FROM THE RESPONSIBILITY OF THE DETAILING OF THE SPECIALTY COMPONENT OR SYSTEM./ / BY: _ (N ` _ DATE: 1.2 1, rte% REVIEWING FIRM: Hillen Electrical Engineering I;)F Comments DATE: 1. L-867 Base Can — Make corrections noted, no resubmittal. Contractor shall provide openings for all conduit entries as shown on drawings. 2. L-868 Top Section — No exceptions taken. 3. L-868 Bottom Section — Make corrections noted, no resubmittal. Contractor shall provide openings for all conduits as shown on drawings. 4. Mud Plate — No exceptions taken. 5. Spacer Rings — Make corrections noted, no resubmittal. Contractor shall provide correctly sized spacer rings as required to meet the latest FAA Advisories, tolerances, requirements, and light fixture manufacturer's requirements. 6. Flange Rings — Make corrections noted, no resubmittal. Contractor shall provide correctly sized flange rings as required to meet the latest FAA Advisories, tolerances, and requirements. 7. Base Plate — No exceptions taken /'► REVIEWED DEC 212009 LPA 8. Stainless Steel Bolts — Make corrections noted, no resubmittal. Contractor shall provide all bolts such that they extend W beyond base can machine thread system as indicated on sheet E402. 9. Nord -Lock — No exceptions taken. Jim Kappes Hillers Electrical Engineering 561-451-9165 ext. 230 rMI'A ,/• PROJECT: SEBASTIAN MUNICIPAL AIRPORT ELECTRICAL CONTRACTOR: H. L PRUITT CORPORATION RUNWAY 4-22 IMPROVEMENTS ELECTRICAL CONTRACTOR FRANK PRUITT, PRESIDENT SUBMITTAL ITEM TO BE REVIEWED SECTION L-125 o L-867 / L-868 BASE CANS o ACCESSORIES GENERAL CONTRACTOR APPROVAL ENGINEER / ARCHITECT APPROVAL Z. b 0 0 52 4 N t.J �n Nit r ti 11 ou� wuwo� � W q �yya77� 2p �w a �w a¢ dWWkk Iv �z 0 3z> i WS?wA tU ¢O¢U S Q 0 J- LY O O U9 N m r Q u. -,. ') af'i i �.. Lro 3; t > Q {E^ LL O W i Li ~ O N (7 Jn ¢ H CC) N W�v IA Q� U Q w 8Lu �O ¢2 0 0l z a a ❑L7 VawU ��3J �{�� 'o � 0Z3 QSrm/� V cid ¢WO z i Y N a W 1 L¢ ¢ rc m pN0 ti w W N ~ r3w p W Q � r ¢ 2 W i W 21 -LL 4 a ¢ Z aNQ$N ¢¢U Q� Z uwz�3 r YNx aTU a1z L a W LO W ¢ cr O 2¢pO HN2 W�H� 8 r tI W � OWW LL W Y Y OW�aW Z$� 02� �QW2 Zz 22 ;:Xuwr¢1Ny 3Zjp �{ C4,:w >=¢r zp Op Ef�i/ , reY WtWOOWQ W ❑�¢S>ZU¢� ¢p¢U m ¢ m D O O O "! 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If the order received does not meet these requirements, it may result in a Supplier corrective action request, which couldjeopardize your status as an approved vendor. Unless otherwise specified, an refaenced consensus standards must be adhered to in their entirety. 30' �I d � �F E (r i Y(NOM)Lr (NONt) o• I -1S L [:11. NO EXCEM P2. MAKE CORF O 3. MAKE CORF REVIEW OF THIS WITH THE NNFORN VERIFICATION OF NOT RELIEVE THI NORESUBMITfAL Btq'5.NOT R ODUIREDFCW':': ':'.J f,Stis IT rtn t A Grou t Condition CW of ASTM F593 IMCiE ,p,ESi,Jf$,{) NERM. .•^a1M.- CMII S AN cAl''',�`Yl�iiSobNti", AND' %T INTEN ... SM THE MND ME MADE SHALL NOT 86COI�3py1' H���AiL�Et�O TO��AUT HORIZE.4BBCh�MI,�{l77C REVIEW OF DESIGN CALCUC7fr1O74NND�A/tWINGSE"[aA"� DESIGN INTENT AND DOES NOT CONSTITUTE A DETAI Mel RELIEVE THE SPECIALTY ENGINEERS FROM THE RESPONSII COMPONENT OR SYSTEM. BY: - %L✓/G REVIEWING FIRM: HILLERS ELECTRICAL ENGINE''R1Nu,, hNC. By: DATE: Page 1 of 1 "-_'_.--llisich-I8, 2006 This document was printed on 5/32007 and was current at that time. Please check current revision data to avoid using obsolete copies. THE DETAILING OF T11E SPE' -i,1 Y DATE: / -2;� gp% ing full above. All ii suC-X 74744-1 74AP ex*,7o(- -f/y ` 6cyo�.0 �a�.c ca.1 /Yl4C.%7 i7t firrl.Pd J'UJ 14^'+ q✓ /s'A%�a. %cls Oh J`iee Yf 151/07. Thread Length E F G H For Screw Nmina size Full Sae Body Wdlh Across Flats Width Head Height Shortteer tTIn. ((ce) as Mac Min. Basic I Max. Min. Max Min. Basle Max. I Mkt. Nom. Nem. 1/4 0.2500 0.2450 7/16 0.438 0.428 0.505 0.468 5132 0.163 0.150 0.750 1.000 5116 0.3125 0.3065 12 0.500 0.489 0.577 0.557 13164 0.211 0.195 0.875 1.125 ilk 3/8 0.3750 0.3690 9116 0.563 0551 0.850 0.628 15164 0.243 0.226 1.000 1250 7116 0.4375 0.4305 518 0.025 0.612 0.722 0.898 9/32 0.291 0.272 1.125 1.375 12 0.5000 0.4930 314 0.750 0.73s 0.868 0.840 5116 0.323 022 1.250 1.500 9116 0.6826 0.5545 13116 0.813 0.798 0.938 0.910 23164 0.371 0.348 1.375 1.625 5/8 0.6250 0.6170 15116 0.938 0.922 1.083 1.051 25164 0.403 0.378 1.500 1.750 3/4 0.7500 0.7410 1 118 1.125 1.100 1.299 1.254 15132 0.483 0.455 1.750 2.000 718 0.8750 0.8680 1 5/16 1.313 1.285 1.516 1.465 35164 0.583 0.531 2.000 2250 1 1.0000 0.9900 1 12 1.500 1.469 1.732 1.675 39164 0.527 0.591 2.250 2.500 1 118 1.1250 1.1140 111/15 1.688 1.631 1.949 1.859 11/16 0.718 0.858 2.500 2.750 1 114 1.2500 1.2390 1 718 1.875 1.812 2.165 2.066 25132 0.813 0.749 2.750 3.000 1 318 1.3750 1.3630 2 1/16 2.063 1.994 2.382 2.273 27132 0.878 0.810 3,000 3.250 1 12 1.5000 1.4880 1 2 1/4 2.250 1 2.175 1 2598 2.480 15116 0.974 0.902 3.250 3.500 [:11. NO EXCEM P2. MAKE CORF O 3. MAKE CORF REVIEW OF THIS WITH THE NNFORN VERIFICATION OF NOT RELIEVE THI NORESUBMITfAL Btq'5.NOT R ODUIREDFCW':': ':'.J f,Stis IT rtn t A Grou t Condition CW of ASTM F593 IMCiE ,p,ESi,Jf$,{) NERM. .•^a1M.- CMII S AN cAl''',�`Yl�iiSobNti", AND' %T INTEN ... SM THE MND ME MADE SHALL NOT 86COI�3py1' H���AiL�Et�O TO��AUT HORIZE.4BBCh�MI,�{l77C REVIEW OF DESIGN CALCUC7fr1O74NND�A/tWINGSE"[aA"� DESIGN INTENT AND DOES NOT CONSTITUTE A DETAI Mel RELIEVE THE SPECIALTY ENGINEERS FROM THE RESPONSII COMPONENT OR SYSTEM. BY: - %L✓/G REVIEWING FIRM: HILLERS ELECTRICAL ENGINE''R1Nu,, hNC. By: DATE: Page 1 of 1 "-_'_.--llisich-I8, 2006 This document was printed on 5/32007 and was current at that time. Please check current revision data to avoid using obsolete copies. THE DETAILING OF T11E SPE' -i,1 Y DATE: / -2;� gp% ing full above. All ii suC-X 74744-1 74AP ex*,7o(- -f/y ` 6cyo�.0 �a�.c ca.1 /Yl4C.%7 i7t firrl.Pd J'UJ 14^'+ q✓ /s'A%�a. %cls Oh J`iee Yf 151/07. Bolt securing system Stainless steel A4 pre -assembled pairs yNo Product Metric UNC d (mm) D (mm) Thickness T (mm) Weight, kg/100 pairs T NL3/8"ss Washer 318" 10,3 16,6 2,2 0,17 �. NO EXCEPTIONS TAKEN 04. REJECTED [(]] 2. MAKE CORRECTIONS NOTED. NO RESUBMITTAL ❑ S. NOT REOUIRED FCR nry,gyv 0S. MAKE COR?ECTION NOTED, RES(IL=MT REVIEW OF THIS SHOP DRAWING IS LIMITED TO GENERAL DESIGN CONCEPTS AND[?ENEPAL WITH THE INFORMATION IN THE PROJECT PLANS AND SPECIFICATIONS ONLY, AND IS *0T INTEN. � VERIFICATION OF TOTAL MATERIAL REQUIREDOR THAT ALL ITEMS REOUIRED ARE3HOWN.Iv�, •. ,n.._L NOT RELIEVE THE CONTRACTOR FROM THE RESPONSIBILITY OF DETAILS OF OESICN, NS. • CONDITK)NS, CONSTRUCTION MEANS AND METHOD6, COORDINATION WiTH OTHER •TRADES, fi'. REQUIREMENTS OF THE PLANS, SPECIFICATIONS OR CONTRACT. ANY NOTATIONS ON THIS SHOP us.ev:. MADE SHALL NOT BE CONSTRUED TO AUTHORIZE ADDITIONAL WORK OR COST. REVIEW OF DESIGN CALCULATIONS AND DRAWINGS PREPARED BY SPECIX.TY ENGINEERS IS LIMITED J DESIGN INTENT AND DOES NOT CONSTITUTE A DETAILED CHECK OF CALC':_-"I •� •":':, NOH DOES; RELIEVE THE SPECIALTY ENGINEERS FROM THE HESFONSIDiLrrY OF THE 6E)we.6`ii OF THE SPEciw- � COMPONENT OR SYSTEM. BY: .2zi DATE: ^ -- REVIEWING FIRM: di.LERS ELECTRIC& ENGINEERIWI. INC. i Ao1BY. nn•' aweximsnrulsl¢a :. 1 I a NL3/8"ss Washer 318" 10,3 16,6 2,2 0,17 �. NO EXCEPTIONS TAKEN 04. REJECTED [(]] 2. MAKE CORRECTIONS NOTED. NO RESUBMITTAL ❑ S. NOT REOUIRED FCR nry,gyv 0S. MAKE COR?ECTION NOTED, RES(IL=MT REVIEW OF THIS SHOP DRAWING IS LIMITED TO GENERAL DESIGN CONCEPTS AND[?ENEPAL WITH THE INFORMATION IN THE PROJECT PLANS AND SPECIFICATIONS ONLY, AND IS *0T INTEN. � VERIFICATION OF TOTAL MATERIAL REQUIREDOR THAT ALL ITEMS REOUIRED ARE3HOWN.Iv�, •. ,n.._L NOT RELIEVE THE CONTRACTOR FROM THE RESPONSIBILITY OF DETAILS OF OESICN, NS. • CONDITK)NS, CONSTRUCTION MEANS AND METHOD6, COORDINATION WiTH OTHER •TRADES, fi'. REQUIREMENTS OF THE PLANS, SPECIFICATIONS OR CONTRACT. ANY NOTATIONS ON THIS SHOP us.ev:. MADE SHALL NOT BE CONSTRUED TO AUTHORIZE ADDITIONAL WORK OR COST. REVIEW OF DESIGN CALCULATIONS AND DRAWINGS PREPARED BY SPECIX.TY ENGINEERS IS LIMITED J DESIGN INTENT AND DOES NOT CONSTITUTE A DETAILED CHECK OF CALC':_-"I •� •":':, NOH DOES; RELIEVE THE SPECIALTY ENGINEERS FROM THE HESFONSIDiLrrY OF THE 6E)we.6`ii OF THE SPEciw- � COMPONENT OR SYSTEM. BY: .2zi DATE: ^ -- REVIEWING FIRM: di.LERS ELECTRIC& ENGINEERIWI. INC. i Ao1BY. nn•' aweximsnrulsl¢a ^., Sebastian Municipal Airport Runway 4-22 Improvements L-125 Anti -Seize Compound SUBMITTAL REVIEW December 15, 2009 X L NO EXCEPTIONS TAKEN 0 4. REJECTED 0 2. MAKE CORRECTIONS NOTED. NO RESUBMITTAL 0 5. NOT REQUIRED FOR REVIEW 0 3. MAKE CORRECTION NOTED, RESUBMIT REVIEW OF THIS SHOP DRAWING IS LIMITED TO GENERAL DESIGN CONCEPTS AND GENERAL COMPLIANCE WITH THE INFORMATION M THE PROJECT PLANS AND SPECIFICATIONS ONLY, AND IS NOT INTENDED TO BE A VERIFICATION OF TOTAL MATERIAL REQUIRED OR THAT ALL ITEMS REQUIRED ARE SHOWN, REVIEW SHALL NOT RELIEVE THE CONTRACTOR FROM THE RESPONSIBILITY OF DETAILS OF DESIGN, DIMENSIONS, JOB CONDITIONS, CONSTRUCTION MEANS AND METHODS, COORDINATION WITH OTHER TRADES, OR ANY OTHER REQUIREMENTS OF THE PLANS, SPECIFICATIONS OR CONTRACT. ANY NOTATIONS ON THIS SHOP DRAWING MADE SHALL NOT BE CONSTRUED TO AUTHORIZE ADDITONAL WORK OR COST. REVIEW OF DESIGN CALCULATIONS AND DRAWINGS PREPARED BY SPECIALTY ENGINEERS IS LIMITED TO DESIGN INTENT AND DOES NOT CONSTITUTE A DETAILED CHECK OF CALCULATIONS, NOR DOES IT RELIEVE THE SPECIALTY ENGINEERS FROM THE RESPONSIBILITY OF THE DETAILING OF THE SPECIALTY COMPONENT OR SYSTEM. A BY: V✓/ -1, _ DATE: /(9� REVIEWI G FIRM: Millers Electrical Engineering BY: Comments DATE: 1. Anti -Seize Compound — No exceptions taken. Jim Kappes Hillers Electrical Engineering 561-451-9165 ext. 230 REVIEWED DEC 2 12009 PA" /m% PROJECT: SEBASTIAN MUNICIPAL AIRPORT ELECTRICALCONTRACTOR: H. L PRUITT CORPORATION RUNWAY 4-22 IMPROVEMENTS ELECTRICAL CONTRACTOR FRANK PRUITT, PRESIDENT SUBMITTAL ITEM TO BE REVIEWED • SECTION L-125 o ANTI -SEIZE COMPOUND GENERAL CONTRACTOR APPROVAL ENGINEER / ARCHITECT APPROVAL �W. NO EXCEPTIONS TAKEN ❑ 4. REJECTED ❑ 2. MAKE CORRECTIONS NOTED. NO RESUBMITTAL ❑ 5. NOT REQUIRED FOR REVIEW ❑ 3 MAKE CORPFCTION NOTED RFSUBM: T REVIEW OF THIS $HOP DRAWING 15 UMITED TO GENERAL DESIGN CONCEPTS AND GENERAL COMPLIAN^F WITH THE INFORMATION IN THE PROJECT PL6:NS AND SPECIFICATIONS ONLY, AND IS NOT INTENDED "+0 F;,. , i VERIFICATION OF TOTAL- MATERIAL REQUIRED OR THAT ALL ITEMS REQUIRED ARE SHOWN. REVIEW SHALL NOT RELIEVE THE CONTRACTOR FROM THE RESPONSIBILITY OF DETAILS OF DESIGN, DIMENSIONS, 306 CONDITIONS, CONSTRUCTION MEANS AND METHODS. COORDINATION WITH OTHER TRADES, OR ANY OTP REQUIREMENTS OFTHE PLANS, SPECIVICATIONS OR Conn RACT. ANY NOTATIONS ON THIS SHOP DRAWI' '-a MADE SHALL NOT BE CONSTRUED TO AUTHORIZE ADDRIONAL WORK OR COST. 1 REVIEW OF DESIGN CALCULATIONS AND DRAWINGS PREPARED BY SPECIALTY ENGINEERS IS LIMITED TO DESIGN INTENT AND DOES NOT CONSTITUTE A DETAILED CHECK OF CALCULATIONS, NOR DOES IT RELIEVE THE SPECIALTY ENGINEERS FROM THE RESPONSIBILITY OF THE DETAILING OF THE SPECIALTY COMPONENT OR SYSTEM. ` BY: ,TG✓L DATE: REVIEWING FIRM: HILLERS ELECTRICAL ENGINEERING, INC. BY: DATE' KOPHAOTI HIGH-TEMPERATUREANTI-SEIZE DESCRIPTION KOPR-KOTE® is a low -friction, anti -seize lubricant manufactured from a combination of micro -size copper Sakes and graphite dispersed in a water-resistant grease and fortified with antioxidants, plus rust and corrosion in- hibitors. KOPR-KOTE contains CZ-EXO: JET- LUIBE's EP additive, providing protection unequalled by competitive brands. KOPR-KOTE provides a shield against metal -to -metal contact, preventing seizure and corrosion. It fills irregulari- ties and imperfections and resists welding, hardening, or setting. KOPR-KOTE provides low friction and cush- ions impact and shock loads. Low shear between par- ticles reduces stick -slip, allowing quick disassembly with minimum wrench torque. It will not squeeze out of the threads, gum up, or wash off. • Not classified as marine pollutant - DOT Approval CA2004080025 • NSF Registered No. 120923 • Conforms to MIL -PRF -907E • Service rating: -65°F (-54°C) to 1800°F (9820C). • Contains no lead or zinc. • Lowers friction; reduces wrench torque. • Permits reuse of fittings; saves stud, bolt, and nut replacement. • Aluminum complex base for brushability and stability over a wide temperature range. • Not affected by contraction, expansion, or vibration. • Will not run, drip, or settle out. • Available in convenient aerosol form. APPLICATIONS KOPR-KOTE is ideal for use on threaded connections, pump housings, flanges, studs, exhaust manifold bolts, compressor heads, autoclaves, lathe centers, etc. Maidenhead, England PRODUCT CHARACTERISTICS Thickener Aluminum Complex Fluid Type Petroleum Dropping Point (ASTM 0-566) 450-F(232°C) Specific Gravity 1.15 Density(Ib/gal) 9.6 Oil Separation (ASTM D-6184) <3.0 WT. %Loss @ 212•17 (100°C) 1 Ib. Flash Point (ASTM D-92) >450°F (232°C) K -Factor .15 High Chrome Alloys @ 60,000 PSI Contact Stress Penetration @ 77°F (ASTM D-217) 310 - 330 Copper Strip Corrosion 1A (ASTM D-4048) 4 -Ball (ASTM D-2596) Weld Point, kgf 800 LoadWearindex 125 PACKAGING Code No. Container Size Container 10055 '/. Ib. Brush Top can 10002 '/x Ib. Brush Top can 10004 1 Ib. Brush Top can 10007 2lb. Plug Top can 10041 12 oz. Aerosol 10050 14 oz. Cartridge 10091 1 gal. Pail 10092 2'/1 gal. Pail 10093 5 gal. Pail LIMITED WARRANTY Jet -Lube, Inc. makes the Limited Express Warranty that at the date of calvary. this product shall be free from defects in Jet -lube. Inc. materials a ndworiunanship. This Limited Express Warrant, is expressly in lieu of any other express or implied warranties, including any implied warranty of merchantability or fitness far a particular purpose, and of any other obligation on the part of Jet -Lube. Inc. The sole remedy for breach of the Limited Express warranty shall be the refund of the purchase once. All other liability is negated and disclaimed. and Jet -Lube, Inc shall not be liable for incidental or consequential dam- ages. CORPORATEIOCATIOHS Houston, Texas—World Headquarters JET -LUBE, INC. 4849 HOMESTEAD RD., P.O. BOX 21258 (77226-1258) HOUSTON, TX 77028 Edmonton, Canada WATS: 800-538-$823V' E W E PHONE: 713.6747617 FAX: 713.678-4604DEC 15''10 E-MAIL: sales@jetlube.com www.jetlube.com H E E JET -LUBE, INC. MATERIAL SAFETY DATA SHEET Product Name: KOPR-KOTE• Manufacturer/Suoolier. JET -LUBE, INC. cbarnlg l Famuv: Petroleum basad lubricating grease Address, 4849 Homestead Rd., Ste, ffZOO Usa1 Anti -seize (MIL -PRF -907E) Houston, TR, 77028 USA Phone: 713.674.7617 Emergency Phone: 713-674.7617 Em 713578-4604 Chemtrec 24 hours (USA): 800.424.9300 TWA5mg1Me Nonhazardous Blend 82980549/471341 30-60 LN LN STEL: UN 778243511317335 12001262/14807966 Metallic Copper 7440508 10 WA 1mg/Me STEL 2mg1M' Petroleum Solvent (aerosol) 64742898 0-10 TWA-300ppm 300ppm LN Hydrocarbon Propellant (aerosol) 68476857 15-25 1000pom 100000m NIA Main Hazards -Health Effects Eves: May rause initiation. Inhalation: Viscous nature may block breathing passages If inhaled. Ingestion, May cause diarrhea. Skin: For hypersensitive persons• may irritate the skin after prolonged periods of contact. Eves: Flush with water until all residual material is gone. If irritation persists, seek medical help. Inhalation: Clear air passage. If respiratory dif lcudty continues, seek medical help.Ingestion: Wash out mouth immediately. Consult physician. Skin: Wash thoroughly with hand cleanser• followed by soap & water. Contaminated clothing should be dry cleaned before reuse. Extinguishing Media: Foam, dry powder, Halone, carbon dioxide, sand, earth & water mist. Unsuitable Extinguishing Media: Water jet. Protective Eauipment for Fire fighting: Self-contained breathing apparatus. ®Personal Precautions: Wear gloves & protective overalls. Environmental PrecaurtlgDX Do not allow it to enter drains. Spillage: Scrape up bulk, then wipe up remainder with doM. To prevent walking hazard, Dick up remaining residue with diatomaceous earth. ® Handling, No special handling precaudons necessary. Storage: Do not store at elevated temperatures. ®Respiratory Protection: None needed. Hand Protection: Protective gloves for hypersensitive persons. Eye Protection: Glasses, if applied to parts in motion. Body Protection: Overalls. Physical State: Semisolid paste Color. Copper/8ronze Odor: Petroleum &I Neutral Boiling Range/Point RF (RC1: <600 (316) Malting Point RF Mie 500 (260) Flash Point (COC) RF (aC): 430 (221) Auto gnition Temperature °F IgG1: >501) (260) Propellant Flash Point (COCKRF (RC): -76 (50) Explosive Propsrtles: LEL: 0.9% UEL: 7% Evaporation Rata (Butyl AcetateC <0.01 Partition Coefficient (Lou Powh N/A Vapor Pressure (kPa): <0.01 r-ngUV (glmm4_ 1.10 OAR Value: WA Flammability, Not flammable at ambient temp. Oxidizing Prop rte les: None Water Solubility: NII Vapor Density: >5 % Volatiles: NII ®Stability: Chemically stable under normal conditions. No photoreactive agents. Conditions to Avoid: Powerful sources of ignition & extreme temps. Materials to Avoid, Strong inorganic & organic adds, oxidizing & copper reactive agents. Hazardous Oecomoosition Products: Bumino generates smoke, airborne scot, hvdrocarbons & oxides of carbon, sulfur & nitrogen. Residue mainly comprised of scot & mineral oxides. ®Acute Toxicity: Not known. Ird nuv Skin: Very mild. Skin Sensitization: Not known. Subacute/Subchronic Toxicity: Not known. Genotoxicity: None known. Chronic Toxicity: None known. California Prop 65: WA Carcinogen: NTP: No IARC: No OSHA: No EC Classification (67/5481EEC): No Allergens: None known. LC -M >7.98mg/I (actual test data-mysidopsi bahia). LO -@Q; WA Possible Effects: Highly unlikely to may gemerate oil fractions that could act as a marine pollutant. Be avh .ior 81°accumulation potential nil. Environmental Fate: Highly unlikely to cause widespread contamination. Nontoxic to marine w land organisms. ®Product Disposal: Do not incinerate. Contact waste disposal company or local authority for advice. Container Disposal: Pails vAMlaut liner -see Product Disposal section above. Pails with plastic liner -pail may only be disposed of via standard waste disposal services, recycled or reused. JIM -see Product Disposal section above. O.Q,L; SJddk Nonhazardous D.O.T. exception CA2004080025 Agm Consumer Commodity ORM-D UN No: S18k Nonhazardous AM 1950, pass 2.1 Alr Transport (ICAO & IATA), $Olt Nonhazardous Awn Hazardous-pressudzed Container Sea Transport (IMO & IMDGI: 6Lit Nonhazard- ous A= 1950, Class 2 Road & Rall Transport (ADWRID): SOIL Nonhazardous Am Class 2, Aerosols Labeling Information: None needed EC Annex 1 Classillcatlon: Not Applicable. R Phrases: R22—harmful if swallowed. S Phrases: N/A as known. Ozone Depleting Chemdeals: N/A TSCA: Al components are listed. SARA 3.111312: None WHMIS (Canada): Bulk Not controlled Aero Class A, B-5 Canadian DSL: Al components listed. TSCA 12B Components: None 40 CFR Part 372 (SARA Section 3131: This product contains copper. CERCLA: Nonhazardous RCRA Hazard Class: Nonhazardous ® SDS flint Issued. SDS data revised. Now Jersey Right To Know: See Section II Signature: Prepared by: Donald A.Oldiges Date Issued: October 31,2006 Aad Isaeea4, IMilIhT181i0„QlllenlUN«enaaCQRelaand FNEN«eb ulstlM«JET1UBe'9MOMaaae. JETIUEIV op FnlwartenE«quere«aa ibxalrery«rMm0i0ry«ga001-dw Oademraay bsa«aama0a anlvg0ulg1a9ueeal«act. eisae uada reopen Uty b m1sty KW Mat Vu tlbmg eemil r« ib MYaMa4M 4 AYIa«e (OFIn P«hIINrIp1. L IOF.VnFlGMNI W INE 91HsiA' UPNEPyurl II. CWIgLipN INFORWFIOH OH INORIOIdif III. HPW0910ENIINGTOX V FNsr !lo EIFA9yNE9 y F. AGHnM MWIIRF9 1Il AFLWExr4 Rause ECAsyRSII VR Humuxc oxo srwu9f NLL E,mowae mxFNa/PFrtwrw morsnox X FxaGi uu a..c.A g,msnnu X1 ry .um NFAcm XI Tomc rovc«aaG. x,Fw,wnax A EmEuarx l«oNUNnox x10. XIV. lrs wINFm Nn XV. REUTORxFONYAiO VV O>xm ixroeu.nox + cow HMIS SYMBOL - BULK HMIS SYMBOL -AEROSOL F t HEALTH I 811J1Y 1ITY a REACTIVITY I a PR g NFPA SYMBOL NFPA S*ls L I a w.camr t NlFinar Sebastian Municipal Airport Runway 4-22 Improvements L-108 Electrical Tape SUBMITTAL REVIEW December 15, 2009 X 1. NO EXCEPTIONS TAKEN 0 4. REJECTED 0 2. MAKE CORRECTIONS NOTED. NO RESUBMITTAL 0 5. NOT REQUIRED FOR REVIEW 0 3. MAKE CORRECTION NOTED, RESUBMIT REVIEW OF THIS SHOP DRAWING IS LIMITED TO GENERAL DESIGN CONCEPTS AND GENERAL COMPLIANCE WITH THE INFORMATION M THE PROJECT PLANS AND SPECIFICATIONS ONLY, AND IS NOT INTENDED TO BE A VERIFICATION OF TOTAL MATERIAL REQUIRED OR THAT ALL ITEMS REQUIRED ARE SHOWN. REVIEW SHALL NOT RELIEVE THE CONTRACTOR FROM THE RESPONSIBILITY OF DETAILS OF DESIGN, DIMENSIONS, JOB CONDITIONS, CONSTRUCTION MEANS AND METHODS, COORDINATION WITH OTHER TRADES, OR ANY OTHER REQUIREMENTS OF THE PLANS, SPECIFICATIONS OR CONTRACT. ANY NOTATIONS ON THIS SHOP DRAWING MADE SHALL NOT BE CONSTRUED TO AUTHORIZE ADDITONAL WORK OR COST. REVIEW OF DESIGN CALCULATIONS AND DRAWINGS PREPARED BY SPECIALTY ENGINEERS IS LIMITED To DESIGN INTENT AND DOES NOT CONSTITUTE A DETAILED CHECK OF CALCULATIONS, NOR DOES IT RELIEVE THE SPECIALTY ENGINEERS FROM THE RESPONSIBILITY OF THE DETAILING OF THE SPECIALTY COMPONENT OR SYSTEM. BY: /L„//�� DATE: REVIEWI� Hillers Electrical Engineering BY: Comments DATE: 1. Electrical Tape and Scotchkote - No Exceptions Taken Jim Kappes Hillers Electrical Engineering 561-451-9165 ext. 230 REVIEWED DEC 212009 WA PROJECT: SEBASTIAN MUNICIPAL AIRPORT /M% RUNWAY 4-22 IMPROVEMENTS ELECTRICAL CONTRACTOR: H. L PRUITT CORPORATION SUBMITTAL ITEM TO BE REVIEWED • SECTION L-108 o ELECTRICAL TAPE o SCOTCHKOTE ELECTRICAL CONTRACTOR FRANK PRUITT, PRESIDENT GENERAL CONTRACTOR APPROVAL I I CERTIFY THAT I HAVE (,I i� This submittal for accuracy, completeness compliance with contract requirements, and it has been coordinated will all other submittals and Contract DOcl.m�'r'''s WEST CONSTR'J' e b.0,6) ENGINEER / ARCHITECT APPROVAL I %J�r1. NO EXCEPTIONS TAKEN ❑ 4. REJECTED [12. MAKE CORRECTIONS NOTED, NO RESUBMITTAL ❑ 5. NOT REQUIRED FOR REVIEW ❑ 3. MAKE CORRECTION NOTED. RESUBMIT _ REVIEW OF THIS SHOP DRAWING IS LIMITED TO GENERAL DESIGN CONCEPTS AND GENERAL C04"°I'.^'"' WITH THE INFORMATION IN THE PROJECT PLANS AND SPECIFICATIONS ONLY, AND IS NOT INTEN L'kc'- J VERIFICATION OF TOTAL MATERIAL REQUIRED OR THAT ALL ITEMS REQUIRED ARE SHOWN. REVIEW SHAD NOT RELIEVE THE CONTRACTOR FROM THE RESPONSIBILITY OF DETAILS OF DESIGN, DIMENSIONS, CONDITIONS, CONSTRUCTION MEANS AND METHODS, COORDINATION WITH OTHER. TRADES, OR' A'' � � OT ` REQUIREMENTS OF THE PLANS, SPECIFICATIONS OR COMPACT. ANY NOl"ATIONS ON THIS SHOP OPOYY 16", MADE SHALL NOT BE CONSTRUED TO AUTHORIZE ADDITIONAL WORK OR COST. REVIEW OF DESIGN CALCULATIONS AND DRAWINGS PREPARED BY SPECIALTY ENGINEERS IS LIMITED TO DESIGN INTENT AND DOES NOT CONSTITUTE A DETAIL£U CHECK OF CALCULAY4,'NS, NOR OUES RELIEVE THE SPECIALTY ENGINEERS FROM THE RESPONSIBILITY OF THE UETI.ILING OF THE SPEl'-ALTY COMPONENT OR SYSTEM. BY: R£ViiWiNG FLPMt HILLEkF: ELECTRICAL £NGikE::i,: •. BY: DATE: I /ftk 3M Electrical Tape Chart PRODUCT NAME PRODUCT TAPE SIZES TELpERATURE TYPICAL Vinyl Electrical Tapes OESCHUrM TIMMESS AVAILABLE RAT@G APPLICATIORS Scolchg Super 33. .._ Highly mdorrnable, super str" W 7 m8 314"x 20' 314"x fib' 220'F Primary insulation ProfessiorelUse all weaduer appfica0ms; resists UV 314'x M' 1'x 36 yd. 105'C for splices W to 60OV. Premium Vnyl rays, atxasim, MOS10n, 314' x 36 ye. 1 12' x 36 yd Proteclivejardreting. Electrical Tape alkalies and acids. Flame retardant. Scotch 35 Professiatal Lisa Nine fade resistant colors, wpm stretchy 7 mil 1/2' x 20' 220'F Phase Identification Vinyl Electrical Tape and conformable, excellent insulating 314% fib' 1051C and marking. for Coir Coring properties. Resist W rays, abrasion. Harnessing. corrosion, alkalies and acid. Scotch Super 88 :. All weather: heavy duty, professional 8.500 314"x 44' 1 12'x44' 2201F Primary insulatim Professional Use Premium use abrasion resistant fast build up. 314"x 66' 1 12" x 36 yd. 1051C for spices up to 60OV. Vnyl Electrical TapeIN 3/4"x 36 yd. 2"x 36 yd. Pmtectivajacketing. 1"x 35 yd. Scotch 22 Thicker far increased medianical 10 mil 112' x 36 yd, 11/2* x 36 yea. 176'F Bus bar in adatim. Heavy Duty strength and abrasion resistance. 314' x 36 yd. 2" x 36 yd 80'C Caeejacket Vinyl Electrical Tape Electrical ilsulatk4 1"x 36 yd. repair. Salm 66R Vinyl Excellent mechanical strength, 10 mil Common sizes; 314"x 36 yd. 220'F Primary inwla0on Electrical Tape It abrasion resistance and electrical 1"x 36 yd. 105'C for 600V bus bar. insulating properties. Other was available rpm r¢gtest Protectivejackeing. Haj*d-Commerce Flevlxe, strAft conform" mfmtaael 7ma 314'x66' 176'F ProWlivepcluxig. Grade Fleruial Tape gradevirtyl. Flame re I&L 80'C Hamessing. TemflexTM 1700 Economical, flexible, 7 con 314' x 36 yd. 176'F Prolective Generalpurpose ��\■ general Wpm tape 3/4'x60' 80'C jacketing. Vkjyl Pe �3�1/ 314" x 66' Harnessing Corrosion Protection Tapes Scotdrmp— 50 and 51 All-weamer 50 is 10 mu 1"x 100' 4'x 100' 176'F Corrosion All-weather Cmosim perfmnance and corrosion 51 is 20 m8 2'x 100' 6"1100, 801C protection on Praection Tapes 2 resistance. Resistant to 3'x 100' pipes, conduits .f. impact and abrasions. and 0fing , ec. ws, 4,PpH Temflex^ General purpose cel osim 10 ma 2'x 100' 17VF Cormsion protection 710OTape msWm tape. Good alvason 80'C on eafbuils, linings 2 resistance. andjoints, etc. rmaun rsmn.yvp nvn. Scotchmpy—dry.—�1 Pipe Primer Quick -dry non -sag mbber 1 Damon n a 176°F For use with base primer that prepares metal 80'C Scotchrap 50 and 51 surfaces for tape application tapes and Temllex 1100 Tape. Special Use Tapes Snitch 48 Thread Pipe Uuad sealml 3 mil 1/4"x260" 5007 Leakproof seal Sealant and Lubricant that provides a 12" x 260' 260'C helps prevent cross a leakproof seal. 12" x520" threading on pipe ! f 1/2'x 1296" threads. Temflex 1755 Cotton,�^�. High grade hiction tape. 15 mil 314" x 60' 176'F Abrasion protection Friction Tape Good abrasion resistance. 3/4" x 82.5' 80'C for splices and 112"x82.5' conxrecdma. Highland High pMmnmc2 duct tape, 10.8 mil 2" x 60 yd 200'F MGM" pnxlrng 6969 Duct Tape ='' excellent adhesion. 3'x GOyd. 93'C plumllkg, duct 9.- tears easily. Saver. Weyep,and Tenon'"" General purpose duct rape; 9.8 nal 1"x 60 ye. 150'F Sealing, 39391kKl Tape `k-�- 'y good adresion, suing backing. Saw. 2' x fi0 yea 3" x 60 65'C venuladen and au mnca"irg �,.. yd 4" x 60 yd j ducts. Scan 2000 Electrician's p General pupose 6 ma 1.9" x 50 yd. General holding f Duct Tapefar easy tear vinyl duct tape and bundling. 'IEWED -C 15 2009 HEE SccotchTM 130C Linerless Rubber Splicing Tape Data Sheet ` 1 ScotchTN I30C Electrical Tape is a highly conformable Physical Properties linerless Ethylene Propylene Rubber (EPR), high voltage Test Method Typical Value* insulating tape formulated to provide excellent thermal Colour Black dissipation of splice heat. The tape is designed for use in Thickness ASTM D-4325 0.762 mm splicing and terminating wires and cables. Rated up to Tensile Strength ASTM D-4325 1.72 Mpa 90-C continuous operating temperatures and short term Ultimate Elongation ASTM D-4325 1000% 1300C overload service. The tape will meet industry Operating Temperature ASTM D-4388 900C specifications for flame remrdance and has excellent Emergency Overload ASTM D4388 130DC physical and electrical properties which provide Thermal Resistivity 3000C immediate moisture seals and void -free buildups. This 3M Transient em/watt product can be used for low — and high— voltage (up to Ozone Resistance ASTM D4388 Passes 69 kV) applications. Heat Resistance ASTM D4388 Passes Tape Features IJV Resistance ASTM D-4388 Passes Linerless, self -bonding primary insulating tape rated Flame Resistance Passes up to 69 kV. IEEE Std 27-1974 ANSI High thermal conductivity. C37.20C 74 Ethylene propylene base. Flame retardant. Electrical Properties Excellent physical and electrical properties. Test Method Typical Value* Designed to insulate splices and terminate cables Dielectric Strength ASTM D4325 whose overload temperatures can reach 1300C. Original 29.5 MV/m .• Physical and electrical properties unaffected by 24 hrs in H2O 29.5 MV/m degree of stretch. 96 hrs @ 230C 28.7 MV/m 0 Physical and electrical properties unaffected by 960/6 RI -1 solvents normally used when splicing high-voltage Volume Resistivity ASTM D-4325 cables. Original >10" ohm -cm r Compatible with common solid dielectric cable Aged 96 hrs @ 230C 960/9 RH >I014 ohm-om insulation. .• Uniform tape unwind from roll. Insulation Resistance >l0e M ohms Small roll size (OD) Dielectric Constant ASTM D-4325 Five year shelf life. 1200 volts @ 60 IJz 4 Stable over wide applications temperature range. 230C 3.5 Weather resistant 900C 3.6 Dissipation Factor ASTM D-4325 1200 volts @ 60 Hz J Primary insulation for splicing all types of solid 230C 0.70% dielectric insulated cables up to 69 kV. 900C 3.00% • Primary insulation for building stress cones on all types of solid dielectric insulated cables up to 35 kV. *This data is not to be used for specification. Values • Jacketing (secondary insulation) on high-voltage listed are for typical properties and should not be splices and terminations. considered minimum or maximum. • Moisture sealing electrical connections. 4- Bus bar insulations. 4 -End sealing high-voltage cables. REVIEWED •: Motor leads. :• Jacket repairs. DEC 15 2009 HEE .. 3M UK PLC 3M Ireland 3M UK PLC Electrical Produeu Sala office Sales Otrue 3M Houx, PO Box 1 3M House, Adelphi Cenue PO Box 393 Backnell, BerkWtire lt= IJU Dun Iaoithalre, Co Dublin, ireland Bedford MK410vE Telephone: 01344 858616 Telephone: 353 1 280 3555 Telephone: 01234 229462 Fax 01344 959758 Fax: 353 1 280 3509 Fox: 01234 229433 00% 3M ScotchTM 130C r1 Linerless Rubber Splicing Tape Data Sheet Product The high-voltage corona -resistant tape must be supplied without a liner and based on ethylene propylene rubber and be capable of emergency operating cable temperature of 1300C (2660F). The tape must be capable of being applied in either stretched or unstretched conditions without any resulting loss in either physical or electrical properties. The tape must not split, crack, slip or flag when exposed to various environments (indoor and outdoor). The tape must be compatible with all synthetic cable insulations and have a shelf life of 5 years. The tape must be flame retardant. ScomhT 130C Electrical Tape should be applied in successive half -lapped, level -wound layers until desired build-up is reached. This tape should be applied like any rubber tape: that is, the side of the tape wrapped inside the roll should be applied outside on the splice. This will help prevent the roll from getting progressively further away from the work area To eliminate voids in critical areas, highly elongate 130C Tape. Stretch tape in these critical areas just short of the breaking point; doing so will not atter its physical or electrical properties. In less critical areas, less elongation may be used. Normally 130C Tape is stretched 3/4 of its original width in these critical areas. Always attempt to balf-lap to produce a uniform buildup. When using 130C Tape for splicing cables above 15 W, always highly elongate the tape throughout the entire splice. Under normal storage conditions, ScotchTat 130C Electrical Tape has a 5 -year shelf life. The tape is not impaired by freezing nor by overheated storage up to the point of flow which prevents removal from the package. Page 2 of 2 ImPoruat N.U. Toohoi W iuf'orm.tiopovidd by 3M 4 bud m axpaimce aodlou tcu heBevd to be rtliebl., bra tbe-arcw.oy 4 not gummed and 0a results m.y nm be relevam In every users applio For this ream, 3M does not ..pt mpwubddy or liability, d.t" coa..q.." juom fromrtlarce ,,on any 'udonatim provided ad flw ma should detamltn the suiubitity oftho prodwc for the - i I-ded uu. Nothing in this vmrmntwifl be dit dto excltde or rtstria lM's liability fpdeaW mpmmal-tlmY eriaiog fmmits oegligerce. All queslom ofliebility rtl.tmg to 3M p�o.d.m'�uzve gose trod by the seW'. tams of idlesub3eawhmaB H=blombcpreva. glaw. lfury godsapplldw Po.xd by a m behelfof3M pove on vup d.mbe&foo. moat or wdomehip. 3M will (a as pum) replace the smo m r.&A u the B,� the pine paid for the gods or sevi¢s. Pxepr u ser our above. as wuninu s and codistn, whether apes. m ®pled. sumo, or otos . w vcIuded to dK fWlma petmis Tloazlew. 3Mmd SeotcAerouademuksofdx3MCat.p.oy. Ptaudmbe UK 03M Unitd K'irgdom PLC. 2001. REVIEWED DEC 15 7009 HEE 3M OIC PLC 3M Ireland 3M UK PLC Electrical Product sal, Oma Sales Office 3M House, PO Box 1 3M House, Adelpld Centre PO Box 393 BraNmell, Berkshire RG1213U Dun IaoghMre, Co Dublin, hrdand Bedford MK41 OYE Telephone: 01344 858616 Telephone: 353 1 280 3555 Telephone: 01234 229462 Fax: 01344 859758 Fax: 353 1280 3509 Fax: 01234 229433 am Page I of l ScotchkoteTM Electrical Coating Data Sheet plastic electrical tape. The product is supplied in a 425g brush top can. • Compatible with SootchTM brand plastic electrical tapes 4 Fast drying Flexible when dry • Contains own applicator ae No waste, provided can is resealed after use ScotchkotelM electrical coating is intended for use as an outer seal on plastic tape applications which are subjected to excessive amounts of oil. It also improves the weather resistance and moisture resistance of the taped joint or splice. It is suitable for direct burial, direct water immersion or above ground applications Precautionary and fust aid information for this product may be found in it's Material Safety Data Sheet on the product container. Property Result r,k Oil -Proof Test (ASTM) Passed Adhesion to: Wood Good - Metal Good Rubber Good - Plastic Good Dielectric strength - Dry 450 volts/mil 24hrs. in HIO 200 volts/mil rroperry Typical Value Solvent Methyl ethyl ketone, toluene Solids (25%) Synthetic rubber & resin Flash Point +30nF/-1 ¢C After taping splices with Seel brand vinyl plastic electrical tape, apply ScotchkoteTM electrical coating evenly over splice, extending a short distance onto the cable insulation. Be sure the surface is clean, dry and free from oil or grease before electrical coating is applied. rm,amrons Nolan Taah" infumatim provided by 3M is baud to opoim¢e anirur leas bdimed m be ndigle, but rbeir ac" i¢art Frourr rd and the reatlas may no an, Wram mcvmy doraapplianW F«Nisram3Mdwu«reeptrepmvbairy«li¢biliry, dirtn«m¢vqumdY, erunaamrrdi¢oceupm anY iofumaYm Wavided and Jac use shoulJ davmi¢¢tbe aetabairy d'Ne pmduvaf« Neri«mded urn NONingia Nis sWama rill behmW b aa¢hge«reaim3M11'ubiary f« deN «pewW iryvry anSuy Rom IO ta6ligan Nl9uedamafaWairy rdating b IM pmNmas an D veved M N¢ Wlm'a term, o! Weaubject whw eppl«bl<m the pmeil'mg4w. V any yenta euppl1 W w pmoeaM by«mbbdfof3Mpawminprdm to be ddsdvemmamAnaa lanataddP 314 will(ativapdm)eO. tlwvme«rdbod lathe Buyer Neprig pad for Ne goods«xrvice. Pxaptout aur Wpve, YI wstmde aad wpddma, wheNe.,arss«implied, stamtay« otWA" so sadudW m No Mot armor pe ssible v law. lM 9cdrL oa Su¢tltt«e ve vademaha aNa )M CmpanY. NaW in We UK. O uhf Unitat Kiagsdam P3.C, M. 3M UK.PJL' L L AM% 3M [JK PLC 3M Ireland Electrical Products Sales Office Sates Office 3M House, PO Box I 3M House, Adelphi Centre PO Box 393 Braclmell, Berkshire R012 IJU Deus Laogbaire, Co Dublin, Ireland Bedford MK41 OYE Telephone: 01344858616 Telephone: 353 1 280 3555 Telephone: 01234229462 Fez: 01344 959758 Fac 353 1 280 3509 Fax 01234 229433 END L-108 Sebastian Municipal Airport Runway 4-22 Improvements L-125 Runway Edge Light SUBMITTAL REVIEW December 15, 2009 X 1. NO EXCEPTIONS TAKEN 0 4. REJECTED 0 2. MAKE CORRECTIONS NOTED. NO RESUBMITTAL 0 S. NOT REQUIRED FOR REVIEW 0 3. MAKE CORRECTION NOTED, RESUBMIT REVIEW OF THIS SHOP DRAWING IS LIMITED TO GENERAL DESIGN CONCEPTS AND GENERAL COMPLIANCE WITH THE INFORMATION IN THE PROJECT PLANS AND SPECIFICATIONS ONLY, AND IS NOT INTENDED TO BE A VERIFICATION OF TOTAL MATERIAL REQUIRED OR THAT ALL ITEMS REQUIRED ARE SHOWN. REVIEW SHALL NOT RELIEVE THE CONTRACTOR FROM THE RESPONSIBILITY OF DETAILS OF DESIGN, DIMENSIONS, JOB CONDITIONS, CONSTRUCTION MEANS AND METHODS, COORDINATION WITH OTHER TRADES, OR ANY OTHER REQUIREMENTS OF THE PLANS, SPECIFICATIONS OR CONTRACT. ANY NOTATIONS ON THIS SHOP DRAWING MADE SHALL NOT BE CONSTRUED TO AUTHORIZE ADDITONAL WORK OR COST REVIEW OF DESIGN CALCULATIONS AND DRAWINGS PREPARED BY SPECIALTY ENGINEERS IS LIMITED TO DESIGN INTENT AND DOES NOT CONSTITUTE A DETAILED CHECK OF CALCULATIONS, NOR DOES IT RELIEVE THE SPECIALTY ENGINEERS FROM THE RESPONSIBILITY OF THE DETAILING OF THE SPECIALTY COMPONENT OR SYSTEM. BY: REVIEWING IRM: Hillers Electrical Engineering BY: Comments DATE: !D/ I fl V' c/ DATE: 1. L-861 Runway Edge Light and Transformer — No exceptions taken. Jim Kappes Hillers Electrical Engineering 561-451-9165 ext. 230 REVIEWED DEC 212009 LPA A^ PROJECT: SEBASTIAN MUNICIPAL AIRPORT ELECTRICAL CONTRACTOR: H. L PRUITT CORPORATION RUNWAY 4-22 IMPROVEMENTS ELECTRICAL CONTRACTOR FRANK PRUITT, PRESIDENT SUBMITTAL ITEM TO BE REVIEWED • SECTION L-125 O L-861 RUNWAY EDGE LIGHTS o L-830 ISOLATION TRANSFORMER GENERAL CONTRACTOR APPROVAL Ago% 1 CERTIFY THAT I HAVE CHECKED This submittal for accuracy, completeness and COnPk'nce with contract requirements, and ii has been coordinated will all other submittals and Contract Documents WEST CONSTRUCTION, INC. sv: 7 ENGINEER / ARCHITECT APPROVAL Z. NO EXCEPTIONS TAKEN ❑ 4. REJECTED ❑ 2. MAKE CORRECTIONS NOTED. NO RESUBMITTAL EIS. NOT REQUIRED FOR RE`il �W 03 MAKE CORRECTION NOTED, RESUaMIT REVIEW OF THIS S40P DRAWING IS LIMITED TO GENERAL OF -910N CONCEPTS AND GENERAL r,"k' WITHTHE INFORMATIONINTHE PROJECT PU%NS AND S rECIFICATIONS ONLY. AND IS NOT INTEN VPS VERIFICATION OF TOTAL MATERIAL R EOUIRED OR THAT ALL ITEMS REQUIRED ARE SHOWN. REV IEvY Ste• _ NOT RELIEVE THE CONTRACTOR FROM THE RESPONSIBILITY OF DETAILS OF DESIGN, DIMENSIONS, CONDITIONS, CONSTRUCTION MEANS AND METHODS, COORDINATION WITH OTHER TRADES, UR k?� v ^T- REOUIREMENTS OF THE PLANS, SPECIFICATIONS OR CONTRACT. ANY NOTATIONS ON THIS SHOP Dnr+iv MADE SHALL NOT BE CONSTRUED TO AUTHORIZE ADDITIONAL WORK OR COST. REVIEW OF DESIGN CALCULATIONS AND DRAWINGS PREPARED BY SPECIALTY L=NGINFERS IS LIMITED TO DESIGN INTENT AND DOES NOT CONSTITUTE A DETAILED CHECK OF CALCULATIONS, NOR DOES Ff RELIEVE THE SPECIALTY ENGINEERS FROM THE RESPONSIBILITY OF THE DETAILING OF THE SPEC, .L;' Y COMPONENT OR SYSTEM. BY: 7 -Alf- DATE REVIEWING FIRM: MILLERS ELECTRICAL ENGINEERING, IIJC. BY: DATE: P► SIEMENS L-861, L-861 E, & L-861 T Quartz/Incandescent Elevated Runway/Taxiway Edge Light Compliance with Standards FAA: L-861, L-861 E, & L -861T AC 15015345-46 (Current Edition) ETL Certified ICAO: Annex 14, Vol. 1, para. 5.3.16 Uses L-861 • Runway edge • Non -precision IFR runways L-861 E • Runway thresholdlend • Non -precision IFR runways • Declared distance L -861T • Taxiway edge L-861 quartzfincandescent medium -intensity elevated light fixtures are used to delineate the edges of airport runways (L-861), taxiways (L -861T), and the threshold end (L-861 Q. Li Ordering Code 44C1081-XXXX Lamp 1 - 30W16.6A Incandescent (ETL Certified) 2 — 4SW16.6A Incandescent' �5 = 30W16.6A Quartz (ETL Certified) 6 = 45W16.6A Quartz (ETL Certified) 7 = No Lamp, Incandescent Socket 8 — No Lamp, Quartz Socket Lens Color 0 = Non-standard Lens (must specify when ordering)' �1 =Omnidirectional White (ErL Certified)'' 2 = Bidirectional W hite/Yellow (ETL Cenified)3.4 3 = Bidirectional WhitelRed (ETL Certified)" 4 = Bidirectional White/Green' 5 = Omnidirectional Blue (ETL Certified)1-4 6 — Bidirectional Red/Green (ETL Certified)14 Features 7 =Omnidirectional Red (ETL Certified)14 • Multiple lamp wattages and types (6.6A quartz or 6.6A 8 = Omnidirectional Green 1.3,4 incandescent) available 9 =Omnidirectional Yellow B — Unidirectional Green/Obscure • Single -latch, stainless steel clamping band allows easy removal of lens for lamp changes • Lamp Life: Rated at 1,000 hours at 6.6A • A gasket is used between the lens and the head assembly to form a tight seal • Three screws allow a 40 leveling adjustment of the fixture after installation Fixture Height y 1 =14 in (35.6 cm) 2 = 24 in (61.0 cm) 3 - 30 in (76.2 cm) 4 = 20 in (50.8 cm) • Fixture uses aluminum head assembly, stainless steel hardware, and is protected with aviation yellow enamel paint Operating Conditions Temperature:-67•Fto+131°F (-55°Cto+550C) Wind: Withstands wind velocities up to 350 mph (560 kph) Notes Contact the Siemens Airfield Solutions Sales Department for optional color configurations or for non-prefocus, screw -base lamp style fixtures, 44C1082-XXXX.I,z ' Color and/or color configuration not recognized by the FAA 2 Wattage not submitted for certification for all fixtures 3 30W Incandescent 4 30W and 45W Quartz M i pool CL REVIEWED DEC 15 M9 HEE 1030 Ray.K Manual No. 96A0097 E-7 i Packaging Assembled Dimensions of Cartons Indiv. Fixtures Individual 9Per Box Welghl 14 -Inch OAH 6.5x 6.5 x20.5 in 19.5 x 19.5 x 20.5 in 5 l 44A1707 17xl7x52cm 50x5Dx52cm 2.3 kg 24 -inch OAH 6.5x6.5 x31 in 19.5x 19.5 x31 in 6.25 lb 63BOO15 17x17x79cm 50x50x79 cm 2.8 kg 30 -inch OAH 6.5 x6.5 x 37 in 19.5x 19.5 x 37 in 71b 48A0007 17xl7x94cm 50 x50 x94 cm 3.2 kq Inside View Socket Steel Column L-823 Cord Set / \ 1-% !\ Single -Latch Clamp Band Head Lamp Assembly (incandescent Shown) Snare Comoonents Description Part No. Column, (steel) 6" (15.24 cm) for 14' OAH 62A0007-6 Column, (steel) 16"(40.64 cm) for 24" OAH 6ZA0007-16 Column, (steel) 22"(55.98 cm) for 30" CAH 6ZA0007-22 Cord set, quartz 44A1701 Cord set. incandescent 44A1707 Frangible coupling, 1.5 inch 6280073 Frangible coupling, 1.5 inch, with slot' 6280461 Frangible reducer coupling, 2.1 inch 61AO281 Gasket 63BOO15 Head assembly with phenolic socket 4487079-1X Head assembly with quartz socket 4487484-1X Lamp, prefocus, 30W16.6A (ETL Certified) 48A0006 Lamp, prefocus, 45W/6.6A (ETL Certified) 48A0007 Lamp, quartz, 30W16.6A(ErL Certified) 48AO085 Lamp, quartz, 45WI6.6A(ETL Certified) 4BA0083 Lamp socket, phenolic for incandescent 49A0002 Lamp socket, quartz 49AO032 Lamp base 62A2150 Lamp bracket (quartz lamp socket) 6001169 Lens, white (FAA L-861) 63AO141 Lens, whitelyellow (FAA L-861) 63AO142 Lens, whitelred (FAA L-861) 63AO144 Lens, whitelgreen (FAA L-861)1 63AO146 Lens, blue (FAA L-8617) 63AO151 Lens, redlgreen (FAA L-861 E) 63AO148 Lens, red (FAA L-861 E) 63AO149 Lens, green (FAA L-861 E) 63AO150 Lens, yellow 63AO143 Lens damn assembly, 4480023 Color andfor color configuration not recognized by the FAA Slot across threaded end allows easy replacement of broken frangible coupling REVIEWED DEC 15 100g HEE The informationcontuined in this dommentis subject change Wdhout norke. 5iernwsreserwstherightto m ikechongesondimprmorentsto its pmduUsand assumesno responsibitityformaking these modification; on any epuipmentpreviowly"Id 103OfWK Siemens Airfield solutions, Inc Telephone: 614861-1304 E-8 Manual No. 96Ap097 977 Gahanna Parkxay Fax: 674-864-2069 Columbus, OH 43230 w .um.4emens.snmfairneld-solutions ^, SIEMENS L-830 & L-831 Isolation Transformer Compliance with Standards Ordering Code 150 60 6.6 6.6 FAA: L-830 and L-831 AC 1501534547 (Current Edition) Style Rated Hz Prim. Sec Eff. Min. Part No. ICAO: Aerodrome Design Manual, Part 5 para. 3.2.1.7a L-830.7 Watts 60 60; Amps Amps at20-C 35CO082 35CO083 MIL: MILT -27535A L-830-16 10115 60 6.6 6.6 -70% 35A0578 CSA: C 22.2 No. 180-M1983 L-830-17 20125 60 6.6 6.6- 70% 35AO617 300- 60 . L-830-1 30145 60 6.6 6.6 80% 35CO077 Uses 20 L-830-2 30145 60 20 6.6 80% 3500078 " Designed for use in airfield lighting systems to isolate low- L-830-3 65 60 6.6 6.6 80% 35CO079 - voltage lamps from the high operating voltages present L-830.4 100 60 6.6 6.6 85% 35CO080. on airfield series lighting circuits. 4830-5 100 60 20 6.6 85% 3500081 Complete water tightness -Cables are an integral part of the transformer and their sheath is molded in the transformer body May be buried directly in the ground, exposed to the sun, immersed in water, and exposed to other weather elements The outer molded jacket is acid-, alkali-, and oil -resistant and also resists deicing fluids, ozone, and UV radiation Electrical Supply • Operates at 60Hz (L-830) or 50Hz (L-831) on series circuits rated up to 5,000V AC The primary windings of the transformer are connected in a 6.6A or 20A series circuit supplied by a constant cur- rent regulator. The continuity of the series lighting loop is maintained even if one or more lamps supplied by indi- vidual isolation transformer secondaries are open -circuit- ed due to lamp failures. In addition, there is a complete separation of the high-voltage primary and low -voltage secondary windings. Additional Isolation Transformers Siemens Airfield Solutions is an approved OEM supplier of Amerace and Integro isolation Transformers. if you would like information on transformers not described in this catalog sheet, please contact the Siemens Airfield Solu- tions Sales Department. L-830-14 500 60. 6.6 6.6 90% 35AO224 L-830-15 500 60 20 6.6 90% 35AO228 L-831-16 10115 50 6.6 6.6 70% 35A0667 L-831-17 L-830-18 150 60 6.6 6.6 85% 35AO650 FeaturesL-830-19 �L--830-6 50 150 60 20 6.6 85% 35AO651 • Quick and easy connection by means of factory -molded L-830.7 200 200 60 60; 6.6 20 6.6 6.6 90% 90%- 35CO082 35CO083 L-823 plugs and receptacles L-830-8 300 60 6.6 20 90% 35CO084 • Two single -conductor primary cables (8 AWG, S,000V) L-830-9 300 60 20 20 90%.- 35CO085 with a molded Style 2 plug on one lead and a molded L-830-10 300- 60 . 6.6 - 6.6 - 90% 3500086 Style 9 receptacle on the other lead; one two -conductor Ls30-11 300 60 20 6.6 90% 35CO087 secondary cable (12 AWG 600V) with Style 8 two -pin L830 -T2 500 60 6.6 20 90% 35CO088 receptacle G830-13 500. 60 20 20 90% 35CO089 Complete water tightness -Cables are an integral part of the transformer and their sheath is molded in the transformer body May be buried directly in the ground, exposed to the sun, immersed in water, and exposed to other weather elements The outer molded jacket is acid-, alkali-, and oil -resistant and also resists deicing fluids, ozone, and UV radiation Electrical Supply • Operates at 60Hz (L-830) or 50Hz (L-831) on series circuits rated up to 5,000V AC The primary windings of the transformer are connected in a 6.6A or 20A series circuit supplied by a constant cur- rent regulator. The continuity of the series lighting loop is maintained even if one or more lamps supplied by indi- vidual isolation transformer secondaries are open -circuit- ed due to lamp failures. In addition, there is a complete separation of the high-voltage primary and low -voltage secondary windings. Additional Isolation Transformers Siemens Airfield Solutions is an approved OEM supplier of Amerace and Integro isolation Transformers. if you would like information on transformers not described in this catalog sheet, please contact the Siemens Airfield Solu- tions Sales Department. L-830-14 500 60. 6.6 6.6 90% 35AO224 L-830-15 500 60 20 6.6 90% 35AO228 L-831-16 10115 50 6.6 6.6 70% 35A0667 L-831-17 20125 50 6.6 6.6 70% 35AO668 L-831-1 30145 50 6.6 6.6 -80% 35C0077,1 - L -831-2 30145 50 20 6.6 80% 35CO078-1 L-831-3 65 50 6.6 66 80% 35C0079 -1d. L-831.4. 100 501 6.6 6.6 85% - 35CO080-1 L-831-5 100 50 20 6.6 85% 35CO081-1' L-831-18 150 50 6.6 6.6 85% 35AC652 L-831-19 150 50 20 6.6 85% 35AC653 L-831-6 200 -50 6.6 6.6 90% 35CO082-1' L-831-7 200 50 20 6.6 90% 35CO083-1' L-831.8-- 300 50 6.6 - 20 90% 35C0084-1, L-831-9 300 50 20 20 90% 35CO085-1. L-831-10 300 50 6.6 6.6 90% 35CO086-1 L-831-11 300 50 20 6.6 90% 35CO087-1 L-831-12 500 50 6.6 20 g0% 3500088-1. Notes • All FAA -recognized L-830 and L-831 isolation transformers listed are ETL Certified. -- • Amerace products are manufactured in Toronto, Canada. • Integra products aremanufactured in Meriden. LL USA C DEC 15 2009 HEE 1215 Rev. J No Manual Packaging Style Part No. Avg. Weight Package Size Ib (kg) In (cm) 0830-16 35AO578 4.8 12 x 10 x 10 L-831-16 35AO667 (2.2) (30.5 x 25.4 x 25.4) L-830-17 35A0617 4.8 12 x 10 x 10 L-831-17 35AO668 (2.2) (30.5 x 25.4 x 25.4) L-830-1 35CO077 7.0 12 x 10 x 10 L-831-1 3500077-1 (3.2) (30.5 x 25.4 x 25.4) L-830-2 35CO078 7.0 12 X 10 x 10 L-831-2 35CO078-1 (3.2) (30.5 x 25.4 x 25.4) L-830-3 35CO079 10.0 12 x 10 x 10 L-831-3 35CO079.1 (4.6) (30.5 X 25.4 x 25.4) L-8304 35C0080 11.5 12 x 10 x 10 L-831-4 3500080.1 (5.2) (30.5 x 25.4 X 25.4) L-830.5 35CO081 11.5 12 x 10 x 10 L-831-5 35C0081.1 (5.2) (30.5 x 25.4 x 25.4) L-830-18 35A0650 13.5 12 x 10 x 10 L-831-18 35AD652 (5.2) (30.5 x 25.4 x 25.4) L-830-19 35A0651 13.5 12 x 10 x 10 L-831.19 35AO653 (5.2) (30.5 x 25.4 x 25.4) L-830-6 3500082 13.5 12 x 10 x 10 L-831-6 35CO082-1 (6.1) (30.5 x 25.4 x 25.4) L-830-7 3500083 13.5 12 x 10 x 10 L-831-7 3500083-1 (6.1) (30.5 x 25.4 x 25.4) L-830-8 35CO084 23.5 12 x 10 x 10 L-831-8 35CO084-1 (10.7) (30.5 x 25.4 x 25.4) L-830-9 35CO085 23.5 12 x 10 x 10 L-831-9 3500085.1 (10.7) (30.5 x 25.4 x 25.4) L-830-10 3500086 23.5 12 x 10 X 10 4831-10 3500086.1 (10.7) (30.5 x 25.4 x 25.4) L-830-11 35CO087 23.5 12 x 10 x 10 L-831-11 35CO087-1 (10.7) (30.5 x 25.4 x 25.4) L-830-12 3500088 28.0 12 x 10 x 10 L-831-12 35CO088-1 (12.7) (30.5 x 25.4 x 25.4) L-830-13 35CO089 28.0 12 x 10 x 10 (12.7) (30.5 x 25.4 x 25.4) L-830.14 35A0224 18.0 12 x 10 x 10 (8.2) (30.5 x 25.4 x 25.4) L-830-15 35AO228 18.0 12 x 10 x 10 (8.4) (30.5 if 25.4 x 25.4) Note: Actual shipping weight may vary by specific manufac- turer's transformer. Some orders are bulk shipped in a single container. 1215 Rev.1 No Manual 1 2 9 3 2. Fiange Ring 3. FAA 4368 3ase 4. dubber Granuvei 5. Conduit 9 6. tsolmmo Transformer 7. Earth Terminal (if any) 8. Primary Connectors 79.5ttondary Connectors A5 6 Deep Base Application - , I � IIII - !I n L-330 a Secondary 1 Stake Mount Application or:[ 1 'flog The information contained in this document is subject to change without notice. Siemens reserves the dght to make changes and improvements to its products and assumes no responsibility for making these modifications on any equipment previously said. Siemens Airfield Solutions Telephone: 614-861-1304 977 Gahanna Parkway Fax: 6148642069 Columbus. OH 43230 www.sas.siemensxom PROJECT: SEBASTIAN MUNICIPAL AIRPORT RUN WAY 4-22 IMPROVEMENTS ELECTRICAL CONTRACTOR: H. L. PRUITT CORPORATION ELECTRICAL CONTRACTOR FRANK PRUITT, PRESIDENT SUBMITTAL ITEM TO BE REVIEWED • SECTION L-125 o P-605 JOINT SEALING FILLER o P-606 ADHESIVE COMPOUND GENERAL CONTRACTOR APPROVAL RECEIVED OEC - g 2009 THE LPA GROUP INC Orlando Office I ENGINEER / ARCHITECT APPROVAL / \ F-405 EXCEEDING F_XPECTATIONS DESCRIPTION # 3405 Regular Hot Applied Sealant is formulated with selected asphaltic resins, synthetic polymeric rubber, plasticizers, stabilizers, and a blend of organic reinforcing fillers. This economical material is a hot applied, one part sealant that provides excellent results under extremely varying conditions. # 3405 Regular is the perfect joint and crack sealant for many applications. • Superior bonding characteristics • High resiliency and weather resistance • Excellent results throughout freeze and thaw cycles • ASTM D-6890, Type I, II & III • ASTM D-3405 • AASHTO M-301 ♦ • FAA P-605 • FED SPEC Specification Specification P-610 specifically calls for 39o -F Dow Corning890- aHoum 60%min. SL as previously approved on 90 max. 3 mm max. 178°F min. Submittal # 3. The Pam, 3 Compatblecles P-610 specification takes precedence ded for sealing of over the L-125 spec and asphaltic t is designed for use in this instance. lItractionlointsaswell rport Runways FEATURES AND BENEFITS • Premium quality joint and crack sealing compound for concrete and asphaltic pavements. • Actually prolongs the pavement service life. • Seats cracks and joints from water penetration. Product Data Sheet # 3405 REGULAR No. JTS-003 Revision: 001 EQUIPMENT Use an agitated oil -jacketed unit that has separate temperature gauges for both the sealant and the heat transfer fluid. Take the 30 Ib. plastic bag of sealant and load into the kettle one at a time. Melt only enough material for the day's activities. Once melted, additional material can be added as needed. Material can be safely reheated within the sealants service life. NOTE: Prolonged heating of the sealant above the maximum safe heating temperature may cause It to gel in the kettle. JOINT PREPARATIONS To facilitate proper adhesion, the joint or crack should be dry and clear of any dirt, dust or other contaminates. Substrate and ambient temperatures must be 40°F or above. Proper sizing of the joint will cause the maximum extension/compression to not exceed 50% of the width. Joints or random cracks of %• or less are difficult to property clean prior to applying the sealant. SERVICE IJFE - The service life ('pot -life•) at application temperatures is approximately 12 hours. Adding fresh material to the molter as sealant is being used will extend the service life. Material that has been overheated can thicken and gel in the melter. Any material that has exceeded the service life should be removed from the molter an(kdiscarded. COVERAGE Width Depth Pounds/1100fl feet 3/6• 318• 6.9 3/8• '�' 'h• 9.3 %* 12.3 J�'� & 3/.• 24. Q� 7/" '/.' 1 . ,say e 60#CA N(2SPUT�i 38 CAR 5 PER c`• Right/ Pointe Company • 234 Harvestore Dr. • Dekalb, It. 60115 •8811.755.700 wwwAghtpointe.com Burton='"_"'" \ o=° Vm Bondo P 606/ P -6065(P-9606 Flewble Traffic DetectorWira Loop Sealant ■ Da W4p.rinrrrt/.Wllc b.W wW .rdbiwtl xuti x!. bmmdd IM.Jprab, MbI mIN. treRe oi.den, ela ■ HepdcuinllomFinh.l.rpNd Ym. a W.mutl GdaM • an.dw,v:.px...Nbp mn;,nm pwletl'vndbppwm. ■ Exn.Sxd.d�Nbnroumw xM waedmplW mncnl. ■ vnnslend.wm�n.rr..nemd �mU,eu. ndh.�tl NHeM {smBi4 d<UnNeuedbp Inees Yuxryrb ■ slxnMar.11w'einp, avuukW ellcaplBhScrlddelMxroup uYN ■ svana n„mu.�wsbn°n ebNkalmdm ■ Aqunbhbcl.sdmedep.� p on.rnwudpl®byal wed ■ Bhd Hid l2moM. MYnnlwd N msrmnrded lerlptlenan BOHOOlWB�E CORP mmm Fgw.vigpN. WPMM.F TnftO btxryWO mTNn �xu n.w NFIlew.. a MAA C COM OI. PHooUCT4 dTOCN.loNp!lgcoV IPdbWbNL TI.. 1..bel°r Mm lrc°y°p lW.Na n pdduvicevpd+M Sd-d .,i d Lha m° xa MVP Me* •PYA WW.NP.,m .) 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W v�.w.N..r.N.� u w -Y .YpNiwY..aYnuw�4wNn...W NapNmY.n..�u. xarmmew..w. aamN..Nrry�xY....u.Ne.exrs.K9�/'a.+aw�nAxw. ruPMY.w ode END L-125 END OF SUBMI 40 YANMAR LIMITED WARRANTY FOR YANMAR INDUSTRIAL ENGINES and GENERATORS What is Covered by this Warranty? Yanmar warrants to the original retail purchaser that a new Yanmar Diesel Industrial Engine and / or Yanmar Diesel Generator will be free from defects in material and / or workmanship for the duration of the warranty period. Note: Yanmar engines may be equipped with external components including, but not limited to; wiring harnesses, electrical devices, control panels, radiators, air filters, fuel filters, and/or exhaust systems that are supplied and/or installed by manufacturers other than Yanmar. For warranty information on such external components, please contact the machine or component manufacturer directly or see your authorized Yanmar dealer or distributor. THIS WARRANTY IS PROVIDED IN LIEU OF ALL OTHER WARRANTIES, EXPRESS OR IMPLIED. YANMAR SPECIFICALLY DISCLAIMS ANY IMPLIED WARRANTIES OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE, except where such disclaimer is prohibited by law. IF SUCH DISCLAIMER IS PROHIBITED BY LAW, THEN IMPLIED WARRANTIES SHALL BE LIMITED IN DURATION TO THE LIFE OF THE EXPRESS WARRANTY. How Long is the Warranty Period? The Yanmar standard limited warranty period runs for a period of twenty-four (24) months or two -thousand (2000) engine operation hours, whichever occurs first. For TNV Series Industrial Engines only, an extended limited warranty of thirty-six (36) months or three thousand (3000) engine operating hours, whichever occurs first, is provided for these specific parts only: the cylinder block, cylinder head, crankshaft forging, connecting rods, Flywheel, flywheel housing, camshaft, timing gear, and gear case. The Warranty Period for both the standard limited warranty and the extended limited warranty (by duration or operation hours) begins on the date of delivery to the original retail purchaser and is valid only until the applicable warranted duration has passed or the operation hours are exceeded, whichever occurs first. What the Yanmar Owner Must Do: If you believe your Yanmar Industrial Engine or Generator has experienced a failure due to a defect in material and / or workmanship, you must contact an authorized Yanmar industrial engine dealer or distributor within thirty (30) days of discovering the failure. You must provide proof of ownership of the Yanmar product, proof of the date of the Yanmar product purchase and delivery, and documentation of the operation hours. Acceptable forms of proof of delivery date include, but are not limited to: the original warranty registration or sales receipts or other documents maintained in the ordinary course of business by Yanmar dealers and / or distributors, indicating the date of delivery of the Yanmar product to the original retail purchaser. This information is necessary to establish whether the Yanmar product is still within the warranty period. Thus, Yanmar strongly recommends you register your new Yanmar product as soon as possible after purchase in order to facilitate any future warranty matters. You are responsible for the transportation of the Yanmar product to and from the repair location as designated by Yanmar. What Yanmar Will Do: Yanmar warrants to the original retail purchaser of a new Yanmar Industrial Engine and / or Generator that Yanmar will make such repairs and / or replacements at Yanmaes option, of any part(s) of the Yanmar product covered by this Warranty found to be defective in material and / or workmanship. Such repairs and / or replacements will be made at a location designated by Yanmar at no cost to the purchaser for parts or labor. What is Not Covered by this Warranty? This Warranty does not cover parts affected by or damaged by any reason other than defective materials or workmanship including, but not limited to, accident, misuse, abuse, "Acts of God," neglect, improper installation, improper maintenance, improper storage, the use of unsuitable attachments or parts, the use of contaminated fuels, the use of fuels, oils, lubricants, or fluids other than those recommended in your Yanmar Operation Manual, unauthorized alterations or modifications, ordinary wear and tear, and rust or corrosion. This Warranty does not cover the cost of parts and / or labor required to perform normal / scheduled maintenance on your Yanmar engine. This Warranty does not cover consumable parts such as, but not limited to, filters, belts, hoses, fuel injector nozzles, lubricants and cleaning fluids. This Warranty does not cover the cost of shipping the product to or from the Warranty repair facility. Warranty Limitations: The foregoing is Yanmar's only obligation to you and your exclusive remedy for breach of warranty. Failure to follow the requirements for submitting a claim under this Warranty may result in a waiver of all claims for damages and other relief. In no event shall Yanmar or any authorized industrial engine dealer or distributor be liable for incidental, special or consequential damages. Such consequential damages may include, but not be limited to, loss of revenue, loss of perishable items, loan payments, cost of rental of substitute equipment, insurance coverage, storage, lodging, transportation, fuel, mileage, and telephone costs. The limitations in this Warranty apply regardless of whether your claims are based on breach of contract, tort (including negligence and strict liability) or any other theory. Any action arising hereunder must be brought within one (1) year after the cause of action accrues or it shall be barred. Some states and countries do not allow certain limitations on warranties or for breach of warranties. This Warranty gives you specific legal rights, and you may also have other rights which vary from state to state and country to country. Limitations set forth in this paragraph shall not apply to the extent that they are prohibited by law. Warranty Modifications: Except as modified in writing and signed by the parties, this Warranty is and shall remain the complete and exclusive agreement between the parties with respect to warranties, superseding all prior agreements, written and oral, and all other communications between the parties relating to warranties. No person or entity is authorized to give any other warranty or to assume any other obligation on behalf of Yanmar, either orally or in writing. Questions: If you have any questions or concerns regarding this Warranty, please call or write to the nearest authorized Yanmar industrial engine dealer or distributor or other authorized facility. It is very important for the original retail purchaser to register the Yanmar product. Registration enables Yanmar to provide the best support for your Yanmar product. At the time of purchase, Yanmar highly recommends registering the retail purchaser's information through the website http://www.yanmar.co.jp as soon as possible. If it is not possible to access the website, please contact the nearest authorized Yanmar industrial engine dealer or distributor. 9 YAG series OPERATION MANUAL Diesel Powered Generators YDG2700EV-6EH YDG3700EV-6E1 YDG5500EV 6EI P/N: OAYDG-000101 INDUSTRIAL ENGINES a� s YANMAR or WARRANTIES wt YANMAR LIMITED WARRANTY What is Covered by this Warranty? Yanmar warrants to the original retail purchaser that a new Yanmar YDG Diesel Generator will be free from defects in material and / or workmanship for the duration of the warranty period. THIS WARRANTY IS PROVIDED IN LIEU OF ALL OTHER WARRANTIES, EXPRESS OR IMPLIED. YANMAR SPECIFICALLY DISCLAIMS ANY IMPLIED WARRANTIES OF MERCHANTABILITY OR FITNESS RA PARTICULAR PURPOSE, except where such disclaimer is prohibited DISCLAIMER IS PROHIBITED BY LAW, IMPLIED WARRANTIES SHALL BE LIMITED IN SUCH DURATION TO THE LIFE OF THE EXPRESS WARRANTY. How Long is the Warranty Period? The Yanmar standard limited warranty period begins on the date of the delivery of the new Yanmar YDG Diesel Generator to the first retail purchaser and extends for a period of twenty-four (24) months or two -thousand (2000) engine operation hours, whichever occurs first. 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N U N U) p Q o a) cz o Q U .ttili I— .� _o o v) m 0 0 N 7 C W e 0 as A O N a) `m E c m } A>1 O) C N O N co CES 2 N L cz 3: "_ N p N E CL N +• N tip N U N VA. > O O •N �? O NC m N cin " m N f: cri (n N N N U O >+ N� C as U UU O) O C:N N =3 w�, co Q) + Q p N U Q w O C 0).N N O i a U OQ N — N llS Q O cn O ,F •U � C E +J C2 Co "O C N >i L I— N N N CO(� CL)Q E .'= •.n.s 0 C cd N U cii O L) .� Y c) Q U Q $1` O CL N to C N E N O cl C O A C QO N Q 0) UC)_ N N t "' N N O N cCf U N '- O C CS >, O 'N N � U L = N p -O N O O C N NO G •� i cn ' co a ami cn o W M :t=:N 0 0 U)+, `KN0 C C N N N N > N L Q Q O N =C U >% C) N N C - 0) ci ~i < 4 L N N N C O ' N N J C x Y N C1 = U J (TjG C O O N U -0 N 07 • w • • - U ?� N E c CO } r- 0 N v— O C i N C O CU :;= > Cf U Fz O LL (z Q -L 2 0 ? N C U Q U 3 0 -0-0 .�0 O N al O N N p U' �x "_ N LL• cc N Q CD so,� N 0 o O) O C: N E N C C (� O cn CS C N O U cz C)O 0) ,, co U cn U) co U . co p N N N d) L co N E } O `� Q � E >,N C O CRS M (� o a) .Q- C COcz _ C C N c N .r� 0) Q) cN N L N C N CS O a - ,x ? C1 0) O co N N N .0 Qi Q C_ 70 c -C N CCf > Ci -� C C E C ca c N O C Co C CS N a O O N O N N p N '' N U N CSi N N p N O (Lf C C 0 i� N co N U) cu co u, E E -a } cJn N = uCi C >' _0 .Q co N Ci N N p > N CZ L U 1 N N HW 0) ( OO 0 Z_0 0 U COm- in R as U `m E c m } A>1 O) N O N o 2 N L cz 3: "_ N p N E C.) ca i o 0 CS _ "' U VA. C .E NC CL � Q ( N m CS O N O N c U Q "i CO U UU O) O w�, co Q) + Q p N U O N V Ocn C U O ..0 N N — N llS Q O ,F •U � C E +J O a) O �— Q i -O N N L U Cf) O •cZ CS Q U Q N U N (D ; U N C C N co N Q 0) UC)_ N N tLLJ 1'- w CL V 0 W 0 L,L '+ �e• im W F– X W a- 0 0 0 ujW- 0 in M N O CZ) N i k --y L4 - .I �: ,� (ll @ �) •y w + O O O > U) Y U I = 0 to CTS O C C a E W (I) L .�+ C to O C1) � C to a •� 4 � V U o U _� L •U� C t1) to O O (ll LL OC --0 Cr, U CD O w �t� O U C O C13 (1) O C = E s - c E -Gay U� C E „r y) to O C O �UZ0 C O0- to V C. a C1) LS) w O .•-• 0 CO U) w :+.0 i O -O = O N CU 0 LL a cz I I �J = tU OUCC (RR V (3)to j. L C: rW o >y a (.jCLU�a), U V Li (� r •F- -g M N O CZ) N i k --y L4 - .I �: ,� (ll v i (D -0 5 u) "' C o > „�,, r .k p;ai („ ak�1..M• kr,,i�� s r � — O U O Y U I CD • '4- -6 CTS O C C N O `0,, C 41 W ti .0 CU tti O CCS liS 't•'. Cq..�•+ Q O ..ti=- . -0 to � T^' .� = U CCS CD U o cu _� L 0)0 _ O O7 2 O O (ll LL OC --0 Cr, U CD O -� 0-0 O U C O C13 (1) O C = Q O - c E 2: E U� C : O U) .0 ,� O E cT5 O C O �UZ0 C O0- to V C. O V LS) w O .•-• 0 CO U) w :+.0 i O -O = O N CU 0 LL a cz I I Cis C .0 0) y= "� Q OUCC o Oi 0 0 0 >T 0 US C: rW o >y a (.jCLU�a), U .0 Q � � 0-0.5 w �`-tom,-�c>-O�L�C�. )Q > -0 . 0 c U_�C�, I I �O E O U U) C1) (L) Q i L��(Do a)a)C�(DrLU) co co 0 CO U) 4/V 0) r- coW W 0) .- O i - L U U O m> CD E CM cu C � � (1) 4 -> (a CD C a) r [ CCS O .O ++ 5 a-+ C V W-0 yr r r r- CD N CV N O CD U) 0 O� O ) (1), QY C � _0 i r N Q)— O -0 Q) O O) U U C1) •U C O" O N u) U y+- l i- w O O" •E .0 01 ". V s� ca c O r- N `- O Sc Q L (U Cti to �' C CD O w U Co C Tom- N 0) (Z c 0'" m -O C u) O 0) O) O O Q O � W u) 0 X 0 0 0 O O W f1) v- C .. ' O -O C LL ` Y C > 'r •C .O = O r ''r0 4- to Cn O = O J N w 0 C N O I ... 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C C O Ir U U U= U r+ \ V U -0 O CD ' 0) O () = _ Cd > U Q— W to U) a) U L O (ll = C15 SZ v O L �S' CU _ r CQ L O m -0 (t3 s- �' C U V tt) co ) � W O � O (1) O O i Q) c U O-0 � O (1)U N (u (CS CCS -0 4-- = � � � .r• C 4- U •tom I z U -0 m w U v= O 4", 0 -S •- C < () _ n -Q -Q (TS � — •�. ..� — Eel 0 4- - (D N) C (D L C O) U O CO o A- 0 0 (6E i -0 O O C (D CC 3f (D -0 5T O O O N�^l` U ((V (D > k- U Or•-=_ E (D -0 O ' ,� 0 C LL ^' W 0 co 0) !? 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W w> p>' a)� p U ` ) p O� =u) I— O CO U) -0 o 0)cU� - 0O O ou)LLa `Zi •a .� >+ 0 U J p) U QL Q C o -ll N to O] 'j L 0) (U O •� co 0)LL 0)� �0 U- C O U) o 0�� c ai � � �'' � Q � � '4=; O ,0 cTS �- C i2 c a) W n) L)' a) .Q a) - co)� o) a) U) a) w c a) Q N NO j\ M m U . U) w (u C c o lz n a— _ o o } 7p o ��v) U w p X" U) (D cCd 0) p ,- O O U a) criZ Q 4-1� U) in -o O U Q U1 m Om 0) O a) U) O a) OCC o L O NS w w U a) -o .❑ C C r a) 4- �7� p co C o - () a) C O �5 p"� O C O )n)( t nn♦♦ '^^ � C) m a) a) r C p C Q (ll C = N V Q N co C co .0 N Cz u) E ("D a) ��+ oO � a W 0- w tlVi N Z •❑ C C UO -C a) a) C u) " 0 C O O _j 11! O- o a) _0 (n z° ¢ w -� w ' _r U) � •5 E E ca w a) � o : o L o U 0 d Y o v C a) � a) C E w- U) co CZ} CO ~ O O C o� o U) 4C- X U) O "_ �+ C > E CO C I.l... CU _ 4- w "= O m co O O U u o) a) o U J 0p �- C '_ p w= C o W C C4 (a) 20 ❑ 0r co N cy ❑ a) U) E a) ' ,� c O > C CV cz co U) w ❑ ) °D 0 Y CA N w _ vp- w (u C a) Q) O) u) (� o 0 O -o w 'a U) -o O O U) - >, G U) m -> cn Y Cs 't3 .� O p Lli O w ?� (u a) O C a CO C IL (o U T) a _m a w > L7] fl Z O U U) U) O . y • • • r • • r m Tov o o C td N Q LL, } O .. � � n r •::x 1 7 YA < ysl e� ..y x � 1 � Iry I , ED.. .. ED .0 N U) U) U wn CCV ED o m O j w C w L U O w w 0) o n •❑ y U- 7 W W CD a) N O) C a) � g (V) ON 4.O O= u) .11w �V w o U) �- f�. 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()> > := LiJ 'C (li J J J cu J _I I >Cu � V tJJ 0 OC (D C Cli O O C E (D e 0 O O C u) C N C C > Q O (D CCS L L > CD `i' 0) C > CTS :;� .0 > � •RS C U) co p 2r i3 O U O C U r CQ w c 0) o a) U o o (u a v c u) +- c o W Lr � a) •v > "' pN N C C O C co o N [t) C O 4 r U O -� O Co(JU � p) C � (D - � � .0 L U w -y E 0 -� 0 C � (1) �' 0-'O > upj C cCD '` (u O O C = Ir O OC Co :3O Qi o '� coD �) _ a CL E > CU ca i"' aoi c o `M„ Q °) o cn >' a CD c j O Y C C U CO �$ O Z U) co -0 N O CO U i a �) E L >, w U) C7 -C > 1l± 1Z. U Q w to WWl C O> U L y- •> > > 0 U .� ';:. o c •'' r,� C3 > >... 'o) •- c L U >, U) O L (li > f]_ (1) p ,w > O •U W w N c U U E > >. > p > (� u) CL_ "�- '� A C,u y- L Co '� > > > co O > p Q' (� (C U (n � •ci! U CO �) Er N c c E a Zu (i) �� > y— LL L G!. coo(�-0L QU •: Leo �;LLJ s,. 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C o > w t7) 0 s= W •y '- �- � � U a {� O � c a CD E oo (D u) •+-� iD E w w �' "w > a _0 - 0 � Q D-� z `L >= CL 0 � � P��°-a •34 CCL'c-,ao;�cu•- E w CL U=U0(10 � s=ao��ao0 a= N `a (� -0 a UJ :5 >' U w CL > 0 i �" a-• %�. i (TS Cy Cn (u y C O p C �- w C 'Ci V "CS > a �- 5 U O V Q) ,r 4�. a U sZ U V '� tiS O :~+ N iZ U QO t w_ w ,(,, i�>oaca OvwcD ws=(u'=gCy n �— cy- Via• "(-)oSwu) j a) a-0 u7 h co w •� y ?' y L o c o E C11 ° >, U) ^ ai U =- [ „a c oc c u•ca o u y.j E d o Kaci o ice- oa-`05� �a cs . - W ,� (CS -0 C CO ,C iV E E N D m 00 > } N CC) ❑ J 6 U E c N } 0 0 0 N O ,. .; ., . ,�,. ...,, d ., ,. ., r .. i�,. pr ., u i iry n., ,.AW.+wnan• rM..rd•.•3�'+ !M .. it .. rp .. 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