SwiftBroadbandWi-FiAntennas ICASupplement
|
|
- Dorothy Neal
- 5 years ago
- Views:
Transcription
1 AIRCRAFTDIVISION WICHITA,KANSAS67277 SwiftBroadbandWi-FiAntennas ICASupplement MODELNO:750 SUPPLEMENTNO: SUPPLEMENTDATE:9/22/2014 CessnaAircraftCompany
2
3 AIRCRAFTDIVISION WICHITA,KANSAS67277 REVISIONS Rev: - Date: 09/22/2014 ICA Summary Pages 1-6 Manuals Affected Description Title Maintenance Manual pages COBHAMSATCOMTT-5040ASWIFTBROADBAND UNIT(SBU)- REMOVAL/INSTALLATION Updates the title and changes Thrane and Thrane to Cobham Satcom throughout the document. Maintenance Manual pages SWIFTBROADBAND WI-FI ANTENNA - REMOVAL/INSTALLATION Adds removal and installation instructions for the SwiftBroadband Wi-Fi antennas. Appendix A: Illustrated Parts Catalog Appendix B: Wiring Diagram Manual 1. ExportCompliance NOTUSED Figure 1 SWIFTWIFI A. ThispublicationcontainstechnicaldataandissubjecttoU.S.exportregulations.Thisinformationhas been exported from the United States in accordance with export administration regulations. Diversion contrary to U.S. law is prohibited. ECCN: 9E Revision Bars A. RevisionbarsinthisICAsupplementidentifynewICAsand/orchangestothecurrentICAsinthe released maintenance manual. NewICAsthatarenotinthecurrentmaintenancemanualwillhavearevisionbarfromtopto bottom along the left margin. ICAs that are in the current maintenance manual and have information added, deleted or revised will have a revision bar(s) in the left margin adjacent to the added, deleted or revised information. Neworchangedillustrationswillhaveachangebarfortheentirelengthofthepage. 3. Page Numbering A. The page number system for ICA included in this supplement have three-element numbers that are separated by dashes. The three-element number is found at the bottom right corner of the page, left ofthepagenumber. Thedateisfoundbelowthepagenumber. B. When the chapter/system element number is followed with zeros in the section/subsystem and subject/unit element number( ), the information is applicable to the entire system. CessnaAircraftCompany Page1of6 Sep 22/2014
4 AIRCRAFTDIVISION WICHITA,KANSAS67277 C. When the section/subsystem element number is followed with zeros in the subject/unit element number( ), the information is applicable to the subsystems in the system. D. The subject/unit element number is used to identify information applicable to units in the subsystems. The subject/unit element number continues in sequence from the number-01- with the number of subsystem units in which maintenance information is necessary. E. Allsystem/subsystem/unit (chapter/section/subject) maintenance data is separated into specified types of information: Description and Operation, Troubleshooting, Maintenance Practices, etc. Blocksofpagenumbersthatareinsequenceareusedtoidentifythetypeofinformation: (1) Description and Operation or Troubleshooting information may not be included if the procedure is easy. When subtopics are short, they may be put together into the Maintenance Practices section. Maintenance Practices can have a mix of subtopics that includes information to service, remove, install, adjust, test, clean, paint or do approved repairs. (2) Longerproceduresthatarenotaseasytodomaybeincludedinaspecifiedsection. Page 1 through 99- Description and Operation Page 101 through 199- Troubleshooting Page 201 through 299- Maintenance Practices Page301through399-Servicing Page 401 through 499- Removal/Installation Page 501 through 599- Adjustment/Test Page 601 through 699- Inspection/Check Page 701 through 799- Cleaning/Painting Page 801 through 899- Approved Repairs F. A typical page number: G. Illustrations use the same figure numbers as the page block in which they appear. For example, Figure 202 would be the second figure in a Maintenance Practices section. 4. Supplement Revisions A. Revisions to this supplement may be accomplished if changes to this supplement are required after release of the original issue and prior to incorporation into the manuals listed in the REVISIONS table. B. All revisions to this supplement will have changes identified in detail in the revision block(s) above. C. AllpagesinthisICAsupplementwillhavethesamedateandarevalidasofthedateshown. CessnaAircraftCompany Page2of6 Sep 22/2014
5 AIRCRAFTDIVISION WICHITA,KANSAS ICAIncorporationintoApplicableManuals NOTE: Most ICA supplements will be incorporated in the next available revision to the manuals listed above and should be used in conjunction with those manuals until the next available revision is released. A. The ICA Supplement List located in the Introduction section of each manual listed in the REVISIONS table will indicate the incorporation status as of the release date of the published revision. B. The manual revision level of the supplement incorporation will be listed in the"manual Incorporation Status" column in the ICA Supplement List, when those ICAs associated with that manual have been incorporated. After ICAs are incorporated, the manual that they are incorporated in must now be used for those ICAs instead of the supplement. Based on revision cycle times for the affected manuals, MM ICAs, WDM ICAs, etc. in this supplement may be incorporated in the manuals at different times. There will not be a revision to this supplement to indicate incorporation in the manuals. Users are required to check the ICA Supplement List for each manual affected to determine incorporation status. C. This supplement will be completely superseded by the manuals listed in the REVISIONS table when ithasbeenincorporatedinallofthemanuals. CessnaAircraftCompany Page3of6 Sep 22/2014
6 AIRCRAFTDIVISION WICHITA,KANSAS Purpose INTRODUCTION A. The purpose of this Supplement is to provide the maintenance technician with the information necessary to ensure the correct functionality and performance of the SwiftBroadband Wi-Fi Antenna on the Cessna Model 750 until this information gets incorporated into the next revision to the manuals listed in the"revisions" section of this supplement. B. This ICA supplement is designed to satisfy the requirements of 14 CFR "Instructions for Continued Airworthiness" associated with this installation. This document is a supplement to the Model 750 Maintenance Manual and will be incorporated in the next revision to the manual. C. When this information is incorporated in the next revision to the manuals listed in the"revisions" section, those manuals shall take precedence over this supplemental document. Refer to the"ica Supplement List" in the"introduction" section of the respective manual for the status of all applicable ICA Supplements. D. RevisionstothissupplementmayoccurifthereisachangetoanyoftheICAsinthissupplement prior to incorporation into all of the affected manuals. 2. Effectivity NOTE: This document must be placed with the aircraft operator's Technical Library CD-ROM or Model 750 Maintenance Manual and incorporated into the operator's scheduled maintenance program. A. These Instructions for Continued Airworthiness(ICA) are effective for the following aircraft model and serialization. Model BeginningEffectivity EndingEffectivity and On 3. CompleteICADocuments A. The following document(s), in conjunction with this supplement, constitute the Instructions for Continued Airworthiness for the SwiftBroadband Wi-Fi Antenna on the Cessna Model 750.All items must be available to the operator at initial delivery. (1) Model 750(0501& On) Maintenance Manual (2) Model750(0501&On)WireDiagramManual 4. SystemComponents A. Refer to Appendix A: Illustrated Parts Catalog CessnaAircraftCompany Page4of6 Sep 22/2014
7 AIRCRAFTDIVISION WICHITA,KANSAS Model750MaintenanceManual LIST OF INSTRUCTIONS FOR CONTINUED AIRWORTHINESS A. Chapter 23 Communications (1) Refer to , Cobham Satcom TT-5040A SwiftBroadband Unit(SBU) (2) Refer to , SwiftBroadband Wi-Fi Antenna 2. Model750WiringDiagramManual A. Chapter 23 Communications (1) Refer to Appendix B, (Figure 1, Sheet 1) Swift WIFI wiring diagram. CessnaAircraftCompany Page5of6 Sep 22/2014
8 AIRCRAFTDIVISION WICHITA,KANSAS ContinuousInspectionProgram INSPECTION PROGRAM AND AIRWORTHINESS LIMITATIONS A. ThisICASupplementdoesnotaffectthecurrentinspectionprogram. 2. Airworthiness Limitations A. Cessna Aircraft Company Model 750(0501& On) Maintenance Manual, Chapter 4, Airworthiness Limitations, contains the system and airframe limitations for the Model 750. NOTE: The Airworthiness Limitations section is FAA-approved and specifies maintenance required under Section and of Title 14 Code of Federal Regulations, unless an alternative program has been FAA approved. (1) There are no new(or additional) airworthiness limitations associated with this equipment and/or installation. CessnaAircraftCompany Page6of6 Sep 22/2014
9 MODEL750(SERIAL-0501ANDON) MAINTENANCEMANUAL 1. General COBHAMSATCOMTT-5040ASWIFTBROADBANDUNIT(SBU)-REMOVAL/INSTALLATION A. This section gives the removal and installation procedures for the optional Cobham Satcom TT-5040A SwiftBroadband Unit(SBU)(UK503). For a general description of the Cobham Satcom TT-5040A SwiftBroadband Unit(SBU), refer to Satellite Communication System- Description and Operation. 2. ToolsandEquipment NOTE: For the tool, equipment, and special consumable part numbers and the manufacturer data, refer to Communications- General. For the supplier publication part number and manufacturer data, refer to the Introduction, Supplier Publication List. A. Tools and Equipment None. B. SpecialConsumables None. C. Reference Material Chapter 6, Airplane Dimensions and Areas- Description and Operation Chapter 6, Access Plates and Panels Identification- Description and Operation Chapter 20, Electrical Bonding- Maintenance Practices Chapter 23, Satellite Communications System- Adjustment/Test Chapter 24, External Electrical Power- Maintenance Practices. 3. Setup A. Prepare the Airplane for the Cobham Satcom TT-5040A SwiftBroadband Unit(SBU) Removal. (1) Remove the electrical power from the airplane. Refer to Chapter 24, External Electrical Power - Maintenance Practices. (2) Open the baggage door. Refer to Chapter 6, Airplane Dimensions and Areas- Description and Operation. (3) Removeaftbaggagecompartmentpanel312ATCtogetaccesstotheDCpowerjunctionbox(J- Box). Refer to Chapter 6, Access Plates and Panels Identification- Description and Operation. (4) Disengage the circuit breaker shown in Table 401. Table 401. Circuit Breakers Circuit Breaker Name BROADBAND 2(HZ255) Circuit Breaker Location RightDC Power J-Box 4. CobhamSatcomTT-5040ASwiftBroadbandUnit(SBU)Removal A. Remove the Cobham Satcom TT-5040A SwiftBroadband Unit(SBU)(Refer to Figure 401). (1) Loosen the knob that attaches the SwiftBroadband unit(sbu)(uk503) to the mounting tray. (2) Carefully pull the SBU out to disengage it from the electrical connectors(pk590a and PK590B) intherearofthemountingtray. NOTE: The electrical connectors for the SBU are attached to the rear of the mounting tray. (3) RemovetheSBUfromthemountingtray. (4) RemovetheSBUfromtheairplane. 5. CobhamSatcomTT-5040ASwiftBroadbandUnit(SBU)Installation A. Install the Cobham Satcom TT-5040A SwiftBroadband Unit(SBU)(Refer to Figure 401) Page 401 CessnaAircraftCompany Sep 22/2014
10 MODEL750(SERIAL-0501ANDON) MAINTENANCEMANUAL Cobham Satcom TT-5040A SwiftBroadband Unit(SBU) Installation Figure 401(Sheet 1) Page 402 CessnaAircraftCompany Sep 22/2014
11 MODEL750(SERIAL-0501ANDON) MAINTENANCEMANUAL CAUTION: Makesurethattheelectricalconnectors(PK590AandPK590B)in the rear ofthe mounting tray are aligned correctly. If the electrical connectors are not aligned correctly, damage to the pin contacts canoccur. (1) Put the SBU(UK503) in its position on the mounting tray. (2) CarefullypushtheSBUtotherearofthemountingtrayuntilitistight. (a) Make sure that the electrical connectors are engaged correctly. (3) TightentheknobthatattachestheSBUtothemountingtray. 6. CobhamSatcomTT-5040ASwiftBroadbandUnit(SBU)Post-MaintenanceChecks A. Do the Cobham Satcom TT-5040A SwiftBroadband Unit(SBU) Post-Maintenance Checks. (1) Do an electrical bonding check(type I) between the Cobham Satcom TT-5040A SwiftBroadband Unit(SBU)(UK503) and the structure. Refer to Chapter 20, Electrical Bonding- Maintenance Practices. (2) Engage the circuit breaker shown in Table 401. (3) Do the Cobham Satcom TT-5040A SwiftBroadband (SBU) System Configuration and Operational Check. Refer to Satellite Communication System- Adjustment/Test. 7. Closeout A. Put the Airplane Back to its Initial Condition. (1) Install aft baggage compartment panel 312ATC. Refer to Chapter 6, Access Plates and Panels Identification- Description and Operation. (2) Close the baggage door. Refer to Chapter 6, Airplane Dimensions and Areas- Description and Operation Page 403 CessnaAircraftCompany Sep 22/2014
12
13 MODEL750(SERIAL-0501ANDON) MAINTENANCEMANUAL 1. General SWIFTBROADBANDWI-FIANTENNA-REMOVAL/INSTALLATION A. The SwiftBroadband system has optional antennas installed to provide direct Wi-Fi connectivity. Maintenance of these Wi-Fi antennas includes removal and installation. 2. ToolsandEquipment NOTE: For the tool, equipment, and special consumable part numbers and the manufacturer data, refer to Communications- General. For the supplier publication part number and manufacturer data, refer to the Introduction, Supplier Publication List. A. Tools and Equipment None. B. Special Consumables None. C. Reference Material Chapter 6, Airplane Dimensions and Areas- Description and Operation Chapter 6, Access Plates and Panels Identification- Description and Operation Chapter 20, Electrical Bonding- Maintenance Practices Chapter 23, Satellite Communications System- Adjustment/Test Chapter 24, External Electrical Power- Maintenance Practices. 3. Setup A. Prepare the Airplane for the SwiftBroadband Antenna(YC581 and YC583) Removal. (1) Remove the electrical power from the airplane. Refer to Chapter 24, External Electrical Power - Maintenance Practices. (2) Open the baggage door. Refer to Chapter 6, Airplane Dimensions and Areas- Description and Operation. (3) Removeaftbaggagecompartmentpanel312ATCtogetaccesstotheDCpowerjunctionbox(J- Box). Refer to Chapter 6, Access Plates and Panels Identification- Description and Operation. (4) Disengage the circuit breaker shown in Table 401. Table 401. Circuit Breakers Circuit Breaker Name BROADBAND 2(HZ255) Circuit Breaker Location Right DC Power J-Box (5) Openthecabinetdoorontheleftsideoftheaftclosettogetaccesstotheequipmentrack.Refer to the Model 750 Interior Maintenance Manual and Illustrated Parts Catalog. 4. SwiftBroadband Antenna(YC581 and YC583) Removal A. Disconnect the coaxial cable connector(jc581 and JC583). B. Remove the screws that attach the antenna to the equipment rack. 5. SwiftBroadbandAntenna(YC581andYC583)Installation A. Install the two screws that attach the SwiftBroadband antennas(yc581 and YC583) to the equipment rack. B. Connect the coaxial cable connector(jc581 and JC583) Page 401 CessnaAircraftCompany Sep 22/2014
14 MODEL750(SERIAL-0501ANDON) MAINTENANCEMANUAL 6. CobhamSatcomTT-5040ASwiftBroadbandUnit(SBU)Post-MaintenanceChecks A. Do the Cobham Satcom TT-5040A SwiftBroadband Unit(SBU) Post-Maintenance Checks. (1) Do an electrical bonding check(type I) between the Cobham Satcom TT-5040A SwiftBroadband Unit(SBU)(UK503) and the structure. Refer to Chapter 20, Electrical Bonding- Maintenance Practices. (2) Engage the circuit breaker shown in Table 401. (3) Do the Cobham Satcom TT-5040A SwiftBroadband (SBU) System Configuration and Operational Check. Refer to Satellite Communication System- Adjustment/Test. 7. Closeout A. PuttheAirplaneBacktoitsInitialCondition. (1) Install aft baggage compartment panel 312ATC. Refer to Chapter 6, Access Plates and Panels Identification-DescriptionandOperation. (2) Close the baggage door. Refer to Chapter 6, Airplane Dimensions and Areas- Description and Operation Page 402 CessnaAircraftCompany Sep 22/2014
15 AIRCRAFTDIVISION WICHITA,KANSAS67277 SUPPLEMENTNO: APPENDIXA:ILLUSTRATEDPARTSCATALOG NOTAPPLICABLE CessnaAircraftCompany
16
17 AIRCRAFTDIVISION WICHITA,KANSAS67277 SUPPLEMENTNO: APPENDIXB:WIRINGDIAGRAMMANUAL CessnaAircraftCompany
18
19 CESSNA AIRCRAFT COMPANY MODEL750 WIRING DIAGRAM MANUAL SWIFT WIFI Figure01(Sheet1) Figure01 Page0 Sep/22/2014 CESSNA AIRCRAFT COMPANY Mmm D/YYYY
20 CESSNA AIRCRAFT COMPANY MODEL750 WIRING DIAGRAM MANUAL FIG UNITS REF PART NUMBER NOMENCLATURE EFFECTIVITY PER DES FROM TO ASSY 01 SWIFT WIFI AVAILABLEWHENINSTALLEDASOPTIONALEQUIPMENT &ON JC ADAPTER(ZONE283)....V R JC ADAPTER(ZONE283)....V R JQ580 REF. ADAPTER(ZONE283) R JQ582 REF. ADAPTER(ZONE283) R PC581A CTS722. COAX CONNECTOR PART OF CABLE ASSEMBLY R (ZONE283)... PC583A CTS722. COAX CONNECTOR PART OF CABLE ASSEMBLY (ZONE283)... 01R PK590A DPX2NA ARINC404CONNECTOR(ZONE315/316)...V R PQ580A CTS722. COAX CONNECTOR PART OF CABLE ASSEMBLY R (ZONE283)... PQ580B CTS722. COAX CONNECTOR PART OF CABLE ASSEMBLY R (ZONE283)... PQ582A CTS722. COAX CONNECTOR PART OF CABLE ASSEMBLY R (ZONE283)... PQ582B CTS722. COAX CONNECTOR PART OF CABLE ASSEMBLY R (ZONE283)... UK A. SWIFTSBU(ZONE315/316)...V0U8J3 01R YC SWIFTBBWIFIANTENNA(ZONE283)....V1TLP3 01R -ITEMNOTILLUSTRATED Figure01 Page1 Sep/22/2014 CESSNA AIRCRAFT COMPANY Mmm D/YYYY
Instructions for Continued Airworthiness Supplement
CESSNA AIRCRAFT COMPANY AIRCRAFT DIVISION WICHITA, KANSAS 67277 Instructions for Continued Airworthiness Supplement MODEL NO: 510 REPORT NO: ICA-510-34-00001 REPORT: GA36 & GA37 GPS ANTENNAS REPORT DATE:
More informationSERVICE BULLETIN TITLE FLIGHT CONTROLS - RUDDER AND ELEVATOR AUTOPILOT SERVO CABLE REPLACEMENT
TITLE FLIGHT CONTROLS - RUDDER AND ELEVATOR AUTOPILOT SERVO CABLE REPLACEMENT EFFECTIVITY REASON MODEL SERIAL NUMBERS 525 (M2) -0685, -0800 thru -0870 The equivalent of this service bulletin has been incorporated
More informationGTS 825 TAS/ADS-B OUT AND PHASE 14 SOFTWARE UPDATE ICA Supplement
AIRCRAFT DIVISION WICHITA, KANSAS 67277 GTS 825 TAS/ADS-B OUT AND PHASE 14 SOFTWARE UPDATE ICA Supplement MODEL NO: 208 SUPPLEMENT NO: ICA-208-34-00001 SUPPLEMENT DATE: 2/18/2016 Cessna Aircraft Company
More informationGTS 8XX Traffic System Instructions for Continued Airworthiness as installed in
GTS 8XX Traffic System Instructions for Continued Airworthiness as installed in (Make and Model Airplane) Reg. No. S/N Dwg. Number: 190-00993-01 Rev. 1 Garmin Ltd. Or its subsidiaries c/o Garmin International,
More informationSERVICE BULLETIN REVISION TRANSMITTAL
REVISION TRANSMITTAL TO: Cessna Distributors, Multi-Engine Authorized Service Facilities, and CPC's SUBJECT: Multi-Engine Service Bulletin Revision 1: Control Column Internal Glide Attach Screw Installation
More informationSERVICE BULLETIN TITLE NAVIGATION - CI COMM/GPS/XM ANTENNA REPLACEMENT (NON-WAAS ONLY)
TITLE NAVIGATION - CI2480-400 COMM/GPS/XM ANTENNA REPLACEMENT (NON-WAAS ONLY) EFFECTIVITY REASON The airplanes that follow equipped with the Garmin G1000 Nav III System: MODEL SERIAL NUMBERS 172R 17281241
More informationSTC GROUP LLC 480 RUDDIMAN DRIVE MUSKEGON, MICHIGAN REPORT NO: REV - TRIO AUTO PILOT INSTALLATION INSTRUCTIONS CESSNA MODEL 182
STC GROUP LLC 480 RUDDIMAN DRIVE MUSKEGON, MICHIGAN 49445 REPORT NO: 1006003 REV - TRIO AUTO PILOT INSTALLATION INSTRUCTIONS CESSNA MODEL 182 DATE: Original Issue 10 July, 2017 WRITTEN BY: Paul Odum APPROVED
More informationSTC GROUP LLC 480 RUDDIMAN DRIVE MUSKEGON, MICHIGAN REPORT NO: G REV E TRIO AUTO PILOT INSTALLATION INSTRUCTIONS
STC GROUP LLC 480 RUDDIMAN DRIVE MUSKEGON, MICHIGAN 49445 REPORT NO: G-1006-51 REV E TRIO AUTO PILOT INSTALLATION INSTRUCTIONS CESSNA MODEL 182 WITH PREVIOUS CESSNA EQUIPPED AUTO PILOT DATE: Original Issue
More informationSERVICE BULLETIN TITLE EQUIPMENT/FURNISHINGS - SEAT CONTROL CABLE ROUTING IMPROVEMENT
TITLE EQUIPMENT/FURNISHINGS - SEAT CONTROL CABLE ROUTING IMPROVEMENT EFFECTIVITY REASON MODEL SERIAL NUMBERS 525B (CJ3) -0451 thru -0504 The equivalent of this service bulletin has been incorporated on
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
UNIVERSAL ACCESS TRANSCEIVER. GENERAL This section covers the GDL UAT/ADS-B Transceiver. A. GDL UAT/ADS-B Transceiver - Serials w/ GDL The optionally installed GDL UAT/ADS-B Transceiver system consists
More informationSERVICE BULLETIN TITLE ELECTRICAL POWER - RIGHT HAND ENGINE WIRE BUNDLE ROUTING IMPROVEMENT
TITLE ELECTRICAL POWER - RIGHT HAND ENGINE WIRE BUNDLE ROUTING IMPROVEMENT EFFECTIVITY REASON MODEL SERIAL NUMBERS 560XL (Citation XLS+) -6001 thru -6232 The equivalent of this service bulletin has been
More informationInstructions for Continued
+ LORD BULLETIN NO. SM-6553 BELL 206 Instructions for Continued Airworthiness INSTRUCTIONS FOR CONTINUED AIRWORTHINESS FOR LORD P/N LORD206-310-004101 AND P/N LORD206-310-004103 INSTALLED ON BELL 206A,
More informationC I R R U S EMERGENCY DESCRIPTION A. Emergency Locator Transmitter (ELT)
EMERGENCY 1. DESCRIPTION A. Emergency Locator Transmitter (ELT) This airplane is equipped with a self-contained ELT. The ELT transmitter is installed immediately behind the aft cabin bulkhead. The ELT
More informationSERVICE BULLETIN. SERIAL NUMBERS thru
TITLE WINGS - ACCESS PANEL INSTALLATION FOR FORWARD SPAR EFFECTIVITY REASON MODEL SERIAL NUMBERS 425 425-0001 thru 425-0236 Customers have requested an access panel to gain easy access to the forward spar
More informationTo give parts and instructions to replace the wing root canted rib upper cap with a new strengthened replacement cap.
Conquest SERVICE KIT TITLE CANTED RIB CAP MODIFICATION EFFECTIVITY MODEL SERIAL NUMBERS 441 441-0001 thru 441-0362 441 698 DESCRIPTION To give parts and instructions to replace the wing root canted rib
More informationSERVICE BULLETIN. SERIAL NUMBERS thru A0001 thru 402A B0001 thru 401B thru
TITLE WINGS - ACCESS PANEL INSTALLATION FOR FORWARD SPAR EFFECTIVITY REASON MODEL SERIAL NUMBERS 401 401-0001 thru 401-0322 401A 401B 401A0001 thru 401A0132 401B0001 thru 401B0221 402 402-0001 thru 402-0322
More informationINSTRUCTIONS FOR CONTINUED AIRWORTHINESS
823 McTavish Road NE Calgary, Alberta, Canada T2E 7G9 PH: (800) 564-6469 www.eaglecopters.com INSTRUCTIONS FOR CONTINUED AIRWORTHINESS FOR P139-HD DIGITAL AUDIO SYSTEM MDL GA212 FOR EUROCOPTER BK117 (EC145)
More informationRADAR ALTIMETER CABLES, REPLACEMENT OF. HELICOPTERS AFFECTED: Serial numbers through
TECHNICAL BULLETIN 42-7-24 23 October 207 MODEL AFFECTED: SUBJECT: 42EP RADAR ALTIMETER CABLES, REPLACEMENT OF. HELICOPTERS AFFECTED: Serial numbers 37002 through 3703. [Serial number 3704 and subsequent
More informationSERVICE BULLETIN SB
TITLE NAVIGATION - RADIO ALTIMETER CONVERTER UPGRADE EFFECTIVITY MODEL SERIAL NUMBERS 525-0360 thru -0515 The equivalent of this service bulletin has been incorporated on production airplanes -0516 and
More informationFAA APPROVED AIRPLANE MAINTENANCE MANUAL SUPPLEMENT. Eyebrow Window Replacement
FAA APPROVED AIRPLANE MAINTENANCE MANUAL SUPPLEMENT AIRPLANE MAKE: Boeing AIRPLANE MODEL: 737-100, -200, -200C, -300, -400, -500, -600, -700, -700C, -800, -900 TO BE ADDED TO AMM CHAPTER 56-11-XX This
More informationRadio Control Installation and Operating Instructions System 4
Radio Control Installation and Operating Instructions System 4 P.O. Box 403, One Cedar Parkway, Jackson, WI 53037 Phone: 800-628-1909 Fax: 262-677-2058 Revision: April 19, 2012 Contents Introduction 3
More informationINTRO, CONTENTS INTRODUCTION TABLE OF CONTENTS. Chapter Section Subject Subject Page
SD3-60 AIRCRAFT MAINTENANCE MANUAL z TABLE OF CONTENTS Chapter Section Subject Subject Page General 1 Companion Manuals 1 Content 1 Method of using the manual 1 List of Effective Pages 3 Revisions 3 Conventions
More informationWILLIAM P WITZIG Date: :55:37-04'00'
FAA Approved Airplane Flight Manual Supplement For Airplanes listed in AML with Avidyne AXP340 Transponder p/n 200-00247-XXX or Avidyne AXP322 Transponder p/n 200-00269-XXX in Make and Model Airplane Registration
More informationSERVICE LETTER SERIAL NUMBERS thru with Hydraulic Pump
TITLE HYDRAULIC POWER - ENGINE DRIVEN HYDRAULIC PUMP VERIFICATION EFFECTIVITY REASON MODEL 525B (CJ3) 525B (CJ3+) SERIAL NUMBERS -0001 thru -0415 with 9912062-8 Hydraulic Pump Installed -0451 thru -0485
More informationCAS-67A TRAFFIC ALERT AND COLLISION AVOIDANCESYSTEM(TCASII) ICASupplement
AIRCRAFTDIVISION WICHITA,KANSAS67277 CAS-67A TRAFFIC ALERT AND COLLISION AVOIDANCESYSTEM(TCASII) ICASupplement MODELNO:S550 SUPPLEMENTNO: SUPPLEMENTDATE:6/15/2015 CessnaAircraftCompany AIRCRAFTDIVISION
More informationSERVICE BULLETIN REVISION
Revision 3 REVISION TRANSMITTAL SHEET This sheet transmits Revision 3 to, which: A. Removes the 453-5000-999 ELT from the kits and makes it a stand alone part. B. Changes part numbers within the kits.
More informationHoneywell ADS-B Out ICA Supplement
AIRCRAFT DIVISION WICHITA, KANSAS 67277 Honeywell ADS-B Out ICA Supplement MODEL NO: 560 SUPPLEMENT NO: ICA-560-34-00005 SUPPLEMENT DATE: 4/26/2016 Cessna Aircraft Company Form 2261 Rev 1 AIRCRAFT DIVISION
More informationST02893CH FAA Supplemental Type Certificate
ST02893CH FAA Supplemental Type Certificate Installation of a SATCOM System on Boeing 767 Series Aircraft (FAA STC ST02893CH) OVERVIEW FAA STC ST02893CH. Argentina Civil Aviation Administration STC 1205.18.
More informationSERVICE LETTER. EFFECTIVITY Model 206H airplanes that have replaced the 10880A Oil Cooler after May SERIAL NUMBERS 206H thru
MANDATORY SERVICE LETTER TITLE OIL - OIL COOLER REPLACEMENT EFFECTIVITY Model 206H airplanes that have replaced the 10880A Oil Cooler after May 2014 MODEL SERIAL NUMBERS 206H 20608001 thru 20608353 REASON
More informationSERVICE LETTER. EFFECTIVITY The Model T206H airplanes were delivered from Textron Aviation with a suspect 10865B Oil Cooler.
MANDATORY SERVICE LETTER TITLE OIL - OIL COOLER REPLACEMENT EFFECTIVITY The Model T206H airplanes were delivered from Textron Aviation with a suspect 10865B Oil Cooler. MODEL SERIAL NUMBERS T206H T20609001
More informationMandatory: shall be accomplished at the next scheduled 100 hour or annual/12 month type inspection, not to exceed 12 months, whichever occurs first.
Single Engine Service Bulletin February 26, 2007 TITLE WING STRUT TO FUSELAGE CUFF MODIFICATION EFFECTIVITY Model Serial Numbers 206H 20608001 thru 20608289 T206H T20608001 thru T20608734 REASON It has
More informationCH-SE-UN-FIG PAGE DATE
List of Effective Pages CH-SE-UN-FIG PAGE DATE Introduction-LOEP Feb 0/8 Introduction thru Feb 0/8 -LOEP Page FEB 0/8 Beechcraft Corporation SUPER KING AIR B00GT SERIES ILLUSTRATED PARTS CATALOG PAGE INTENTIONALLY
More informationSTC GROUP LLC 480 RUDDIMAN DRIVE NORTH MUSKEGON, MICHIGAN REPORT NO: REVISION H
STC GROUP LLC 480 RUDDIMAN DRIVE NORTH MUSKEGON, MICHIGAN 49445-2783 REPORT NO: 1006004 REVISION H TRIO AUTO PILOT PROVISIONS INSTALLATION INSTRUCTIONS 1953 CESSNA 180 THROUGH 1962 180E 1956 CESSNA 182
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
DEPENDENT POSITION DETERMINING 1. GENERAL This section covers that portion of the system which provides information to determine position from sources which are mainly dependent on ground installations.
More informationHP LaserJet Pro M401/M425MFP Printer Series Continuous Paper Jams, Possible Noises and/or Broken Parts in Toner Cartridge Area
HP LaserJet Pro M401/M425MFP Printer Series Continuous Paper Jams, Possible Noises and/or Broken Parts in Toner Cartridge Area Users may report that new-out-of-box or lightly used devices continuously
More informationMighty Mo GX Series Cabinet Installation Guide. OR Rev /11
Mighty Mo GX Series Cabinet Installation Guide OR-71601787 Safety and Warning ATTENTION The exclamation point within an equilateral triangle is intended to alert the user to the presence of important operating
More informationKGX 150/130 ADS -B Certified Transceivers & Receivers
BendixKing By Honeywell 9201 -B San Mateo Blvd. NE Albuquerque, NM 87113 U.S.A. CAGE: 6PC31 Telephone: 1-505 -903-6148 Telephone: 1-855 -250-7027 (Toll Free in U.S.A.) Web site: http://www.bendixking.com
More informationDEPARTMENT OF DEFENSE
NOTE: DoD-STD-863B has been designated as a handboook, and is to be used for guidance purposes only. This document is no longer to be cited as a requirement. For administrative expediency, the only physical
More informationAPS M1P Single-phase Micro-inverter Installation and User Manual
APS M1P Single-phase Micro-inverter Installation and User Manual Version: 2.0 ALTENERGY POWER SYSTEM, INC. All rights reserved 1 Contact Information ALTENERGY POWER SYSTEM Inc. 1 Yatai Road, Jiaxing, PR
More informationSECTION OPERATION AND MAINTENANCE DATA
SECTION 01787 OPERATION AND MAINTENANCE DATA PART 1 GENERAL 1.01 SUMMARY A. Compile product data and related information appropriate for OWNER's maintenance and operation of products furnished under Contract.
More informationSERVICE BULLETIN. No. SB-AG-45 Rev. B JUNE 1, 2007 FIN SPAR & ATTACH FITTINGS INSPECTION AND UPGRADE IMPORTANT:
THRUSH AIRCRAFT, INC. P.O. Box 3149 300 Old Pretoria Rd. Albany, GA 31706-3149 Product Support 229-883-1440 ext. 341 FAX 229-436-4856 jbays@thrushaircraft.com SERVICE BULLETIN No. SB-AG-45 Rev. B JUNE
More informationAVIATOR 300. Single Channel SwiftBroadband with Intermediate Gain Antenna Data Sheet. The most important thing we build is trust
AVIATOR 300 Single Channel SwiftBroadband with Intermediate Gain Antenna 2013 Data Sheet The most important thing we build is trust Satcom for aircraft of any size and application Connect your tablet or
More informationSoundPals. DAC-24 User Guide. Stereo D-to-A converter
SoundPals DAC-24 User Guide Stereo D-to-A converter Printing History SoundPals DAC-24 D-to-A converter Rev. N/C SEPTEMBER 2016 Printed in U.S.A. Part Number 08-2044-00 The information contained in this
More informationSUPPLEMENT REVISION CESSNA MODEL 182T
SUPPLEMENT REVISION CESSNA MODEL 182T NAV III AVIONICS OPTION - Serials 18281228 and 18281318 thru 18281868 and 18281870 thru 18281875 PILOTS OPERATING HANDBOOK AND AIRPLANE FLIGHT MANUAL REVISION 1 1
More informationSERVICE BULLETIN SB-GL12-01R GREAT LAKES AIRCRAFT HORIZONTAL STABILIZER SPAR INSPECTION COMPLIANCE TIME: APPROVAL: PURPOSE: BACKGROUND:
SUBJECT: AFFECTED MODELS: 2T-1A 0501 and 0502 2T-1A-1 0503 through 0699 2T-1A-2 0701 through 1012 COMPLIANCE TIME: APPROVAL: PURPOSE: BACKGROUND: Released: 01/25/2012 Page 1 of 5 HORIZONTAL STABILIZER
More informationSTC GROUP LLC 480 RUDDIMAN DRIVE MUSKEGON, MICHIGAN REPORT NO REVISION D TRIO AUTO PILOT INSTALLATION INSTRUCTIONS
STC GROUP LLC 480 RUDDIMAN DRIVE MUSKEGON, MICHIGAN 49445 REPORT NO. 1006003 REVISION D TRIO AUTO PILOT INSTALLATION INSTRUCTIONS CESSNA MODEL 182 WITH CESSNA NAVOMATIC EQUIPPED AUTO PILOT DATE: Original
More informationTactical repeater for Ground and Airborne use
Tactical repeater for Ground and Airborne use Ground 1. Replace fixed repeater. 2. Use at a Mission or Activity Base. 3. Deployable for forward Ground Team support. Air 1. Highbird operations. 2. Wide
More informationAPS M1P Single-phase Micro-inverter Installation and User Manual
APS M1P Single-phase Micro-inverter Installation and User Manual Version: 1.0 ALTENERGY POWER SYSTEM, INC. All rights reserved 1 Contact Information ALTENERGY POWER SYSTEM Inc. 1 Yatai Road, Jiaxing, PR
More informationSECTION CLOSEOUT SUBMITTALS SECTION CLOSEOUT SUBMITTALS
PART 1 GENERAL 1.01 SECTION INCLUDES A. Project Record Documents. B. Operation and Maintenance Manuals. C. Warranties and bonds. 1.02 RELATED REQUIREMENTS SECTION 01 78 00 A. Section 01 30 00 - Administrative
More informationSI-125 Power Amplifier Manual 6205 Kestrel Road; Mississauga, Ontario; Canada; L5T 2A1 November 2016, Rev 0.5
SI-125 Power Amplifier Manual 6205 Kestrel Road; Mississauga, Ontario; Canada; L5T 2A1 November 2016, Rev 0.5 Phone: (905) 564-0801 Fax: (905) 564-0806 www.telecor.com E:\T2-108\T2-M108-ABC\T2-M108-B.doc/AD
More informationTechnical Standard Order
Department of Transportation Federal Aviation Administration Aircraft Certification Service Washington, D.C. TSO-C23f Effective Date: 09/21/2012 Technical Standard Order Subject: Personnel Parachute Assemblies
More informationEQUIPMENT INSTALLATION MANUAL. for the GDC62 RADIO ALTIMETER INTERFACE UNIT P/N
EQUIPMENT INSTALLATION MANUAL for the GDC62 RADIO ALTIMETER INTERFACE UNIT P/N 1102-4000-01 DAC International 6702 McNeil Drive Austin, TX 78729 Copyright 2013, DAC International. All rights reserved.
More informationSECTION WIRELESS CLOCK/TONE GENERATOR SYSTEM
SECTION 13805 WIRELESS CLOCK/TONE GENERATOR SYSTEM PART 1 GENERAL 1.01 SUMMARY A. Section Includes: Satellite based, synchronized wireless clock/tone generator system, including clocks, tone generator,
More informationINSTALLATION INSTRUCTIONS FOR EXHAUST CUFF MODIFICATION
INSTALLATION INSTRUCTIONS FOR EXHAUST CUFF MODIFICATION Document # PCA1001-21 Revision LTR: NC Date: 09/15/08 1 Notes: 1. The Exhaust Cuff comes assembled with the three attachment brackets secured. We
More informationP/N ( )
GDC Data Converter EQUIPMENT INSTALLATION MANUAL For the GDC DATA CONVERTER P/N ---( ) ARINC TO ARINC DAC International McNeil Drive Austin, TX Copyright, DAC International. All rights reserved. -- IR.doc
More informationBANTAM INSTRUMENTS SOFTWARE USER S MANUAL MIL-STD-461E PRE-COMPLIANCE MEASUREMENT SYSTEM MODEL EMC-461. Model EMC-461 Software User s Manual
BANTAM INSTRUMENTS MIL-STD-461E PRE-COMPLIANCE MEASUREMENT SYSTEM MODEL EMC-461 SOFTWARE USER S MANUAL MIL-STD-461E PRE-COMPLIANCE MEASUREMENT SYSTEM MODEL EMC-461 Software User s Manual BANTAM INSTRUMENTS
More informationSERVICE LETTER. FAA-Approved Propeller Repair Stations, Aircraft Manufacturers, Owners and Operators.
December 15, 2008 TITLE MODEL D3A34C447 PROPELLER SERVICE INFORMATION UPDATE TO: FAA-Approved Propeller Repair Stations, Aircraft Manufacturers, Owners and Operators. EFFECTIVITY Model D3A34C447 Propeller,
More informationDEPARTMENT OF TRANSPORTATION
DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [61 FR 625 No. 6; 01/09/96][SN] [Docket No. 94-ANE-63; Amendment 39-9458; AD 95-03-10] Textron Lycoming AD 95-03-10 Amendment
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
PROPELLER ASSEMBLY 1. DESCRIPTION The propeller assembly consists of a hollow aluminum hub which supports the propeller blades and also houses the pitch changing mechanism. Movement of propeller blades
More informationShuttle Frame Assembly (Figure 5 31 )
Shuttle Frame Assembly (Figure 5 31 ) Removal 1. Prepare the printer for maintenance (page 5 3). 2. Remove the shuttle cover assembly (page 5 24). 3. Disconnect the MPU cable connector (1). 4. Disconnect
More informationPARAVION TECHNOLOGY, INC AIRWAY AVENUE FT. COLLINS, COLORADO
PARAVION TECHNOLOGY, INC. 2001 AIRWAY AVENUE FT. COLLINS, COLORADO 80524 PR C208WS 900M For Workstation/Equipment Cabinet Cessna Model 208, 208B Airplanes Page ii of v REVISION HISTORY Revision Date Detail
More informationINSTRUCTIONS FOR CONTINUED AIRWORTHINESS
823 McTavish Road NE Calgary, Alberta, Canada.T2E 7G9 PH: (800) 564-6469 Website: www.eaglecopters.com INSTRUCTIONS FOR CONTINUED AIRWORTHINESS FOR P139-HD DIGITAL AUDIO SYSTEM MDL GA182 FOR MODEL EUROCOPTER
More informationSTC GROUP LLC 480 RUDDIMAN DRIVE NORTH MUSKEGON, MICHIGAN REPORT NO: REVISION A
480 RUDDIMAN DRIVE NORTH MUSKEGON, MICHIGAN 49445-2783 REPORT NO: 1006007 REVISION A TRIO AUTO PILOT INSTALLATION INSTRUCTIONS CESSNA MODEL 180F & LATER, CESSNA 185 ALL MODELS NO PREVIOUSLY INSTALLED FACTORY
More informationTECHNICAL MANUAL DIRECT SUPPORT, GENERAL SUPPORT, AND DEPOT MAINTENANCE MANUAL INCLUDING REPAIR PARTS AND SPECIAL TOOLS LISTS RADIO SET AN/PRC-47
TECHNICAL MANUAL DIRECT SUPPORT, GENERAL SUPPORT, AND DEPOT MAINTENANCE MANUAL INCLUDING REPAIR PARTS AND SPECIAL TOOLS LISTS RADIO SET AN/PRC-47 This copy is a reprint which includes current pages from
More informationAIRPLANE FLIGHT MANUAL AQUILA AT01. Date of Issue A.01 Initial Issue (minor change MB-AT ) all March
0.1 LIST OF REVISIONS AND AMENDMENTS Revision Reason for Amendment/Revision Affected Pages Date of Issue A.01 Initial Issue (minor change MB-AT01-00297) all 2009 19. March 0.2 LIST OF EFFECTIVE PAGES Page
More informationPilot s Operating Handbook Supplement AS-21
SECTION 9 Pilot s Operating Handbook Supplement Mode S Transponder GARMIN GTX 335 / GTX 345 This supplement is applicable and must be inserted into Section 9 of the POH when a GARMIN GTX 335 or GTX 345
More informationSERVICE BULLETIN TRANSMITTAL SHEET HC-SB De-ice - Wire Harness Replacement
TRANSMITTAL SHEET April 27, 2017 This page transmits a revision to Service Bulletin. Original Issue, dated Revision 1, dated Apr 27/17 Propeller assemblies that have previously complied with the terminating
More informationAS-3226C/URC VHF ANTENNA
TECHNICAL MANUAL OPERATION AND INSTALLATION INSTRUCTIONS AS-3226C/URC VHF ANTENNA REVISION SHEET Revision Description Date - - Original Issue - November 13, 2007 Errors in this publication can be reported
More informationCOMPONENT LOCATION INDEX
COMPONENT LOCATION INDEX 2004 ACCESSORIES & EQUIPMENT Audio System - TSX Fig. 1: Locating Audio System Components (1 Of 2) Tuesday, March 11, 2008 3:35:47 3:35:51 PM Page 1 Fig. 2: Locating Audio System
More information2 Parts and diagrams. Order parts by authorized service providers. Related documentation and software. Fasteners used in this product
2 Parts and diagrams Order parts by authorized service providers Related documentation and software Fasteners used in this product How to use the parts lists and diagrams Assembly locations Covers Document
More informationInstruction Sheet 2 mm Common Termination (CT) Head Assembly
Instruction Sheet 2 mm Common Termination (CT) 408-9426 Head Assembly 58372-1 05 MAY 14 Wire Inserter (Shown In Up Position) Carriage Drag Wire Guide Feed Pawl (Portion of Head Assembly Shown Cut Away
More informationSPECIAL NOTICE. All references to NAT product part numbers (and associated images) are equivalent to AEM product part numbers.
SPECIAL NOTICE This product is now licensed to Anodyne Electronics Manufacturing (AEM) from Northern Airborne Technology (NAT). AEM is responsible for all matters related to this product, including sales,
More information*MANDATORY SERVICE BULLETIN*
NUMBER: SB-004 DATE: 1/26/2009 SUBJECT: ELECTRICAL; Potentiometer Replacement KODIAK MANDATORY SERVICE BULLETIN SUMMARY RECURRENT REQUIREMENTS No recurrent requirements associated with this Mandatory Service
More information9800 Martel Road Lenoir City, TN
9800 Martel Road Lenoir City, TN 37772 www.ps-engineering.com MB10 Document P/N 200-023-0001 Rev. 7, April 2009 Marker Beacon Receiver/Indicator System Installation and Operation Manual FAA-Approved TSO,
More informationSECTION OPERATIONS AND MAINTENANCE MANUALS TRACTION POWER EQUIPMENT
SECTION 01832 OPERATIONS AND MAINTENANCE MANUALS TRACTION POWER EQUIPMENT PART 1 - GENERAL 1.01 DESCRIPTION OF WORK A. Furnish SEPTA with comprehensive Operations and Maintenance Manuals of all equipment
More informationBX1956 Installation Instructions Chrysler PT Cruiser (Include Turbo)
BX1956 Installation Instructions 2001-04 Chrysler PT Cruiser (Include Turbo) Serial No. The front fascia and metal bumper are removed for baseplate installation. Factory metal bumper will not be reinstalled.
More informationSigma 5 - Axis Servo Motor and Cables - Troubleshooting Guide
LAST UPDATED: 09/24/2018 Electrical Safety Caution: When you do maintenance or repair on CNC machines and their components, you must always follow basic safety precaut and mechanical damage. Set the main
More informationP/N X-00X( ) and P/N ( )
EQUIPMENT INSTALLATION MANUAL for the GAC27 BARO CONVERTER SYSTEM P/N 1043-4000-0X-00X( ) and P/N 1043-4001 -02-020( ) DAC International 6702 McNeil Drive Austin, TX 78729 Copyright 2007, DAC International.
More informationGWX 68 Weather Radar Installed in Beech 90 Series Installation Data
GWX 68 Weather Radar Installed in Beech 90 Series Installation Data FAA STC Project No. ST9355SE-A P/N Garmin Ltd. Or its subsidiaries c/o Garmin International, Inc. 1200 E. 151st Street Olathe, Kansas
More informationOrtel (Lucent) Fiber Optic Interface
Ortel (Lucent) Fiber Optic Interface 144-701-1 Serial Number May 5, 2009 Revision B ORTEL (LUCENT) FIBER OPTIC INTERFACE 1. GENERAL INFORMATION... 1 1.1. SCOPE OF OPTION... 1 1.2. PURPOSE OF EQUIPMENT...
More informationBroadband Step-Up Transformer. User Manual
Broadband Step-Up Transformer User Manual 990-1930 09/2004 Introduction Introduction About this unit The APC Step-Up Transformer provides 220 V power from 60 VAC Broadband cable systems. Safety Electrical
More informationService Bulletin No: Ref No: 136 Modification No: INSPECTION ATA Chapter: 57
PILATUS AIRCRAFT LTD. STANS, SWITZERLAND Service Bulletin No: 57-015 Ref No: 136 Modification No: INSPECTION ATA Chapter: 57 WING - AILERON INSTALLATION INSPECTION OF THE AILERON OUTBOARD-BEARING SUPPORT
More informationS6 User s Manual USER S MANUAL ver. 1.0
S6 User s Manual SKEETER - 1U LOW PROFILE SOLUTION Table of Contents Tabletop Configuration 2 Tabletop Configuration Accessories 4 Slide Configuration 5 slide configuration accessories 7 rack Mount configuration
More informationSERVICE INFORMATION LETTER
CUSTOMER SERVICES DIRECTORATE 1 ROND POINT MAURICE BELLONTE 31707 BLAGNAC CEDEX FRANCE TELEPHONE + 33 (0)5 61 93 33 33 TELEX AIRBU 530526F AIRBUS SUBJECT: Radio-Altimeter antennas, protection against water
More informationTechnical Manual Index July 1, 2018
Technical Manual Index July 1, 2018 The GE90 Technical Manual Index has been reformatted as follows: Manuals and Supporting Manuals - Section 1 EM DVDs ( Manuals) Section 2 Supplementary Support Manuals
More informationELECTRIC GROUNDING AND WIRING REQUIREMENTS BOOTHS-METAL
BELL SYSTEM PRACTICES Plant Series SECTION 508-100-100 Issue 3, October 1970 AT&TCo Standard ELECTRIC GROUNDING AND WIRING REQUIREMENTS BOOTHS-METAL I. GENERAL 1.01 This section is reissued to: Revise
More informationAT 3000 OPERATION/INSTALLATION MANUAL ALTITUDE ENCODER. Trimble 2105 Donley Austin, Texas (512) PUBLICATION NUMBER
AT 3000 ALTITUDE ENCODER OPERATION/INSTALLATION MANUAL Trimble 2105 Donley Austin, Texas 78758 (512) 432-0400 PRINTED IN U.S.A. PUBLICATION NUMBER 1900-4099-00 AT 3000 ALTITUDE ENCODER OPERATION/INSTALLATION
More informationOrtel (Lucent) Fiber Optic Interface
Ortel (Lucent) Fiber Optic Interface 144-701-1 Serial Number January 31, 2013 Part number 098-00120-000 Revision C ORTEL (LUCENT) FIBER OPTIC INTERFACE 1. GENERAL INFORMATION...1 1.1. SCOPE OF OPTION...1
More informationInstallation Manual REbus Beacon. Part of the Pika Energy Island M
Installation Manual REbus Beacon Part of the Pika Energy Island M00020-01 REbus Beacon Serial Number: RCP Number: We are committed to quality and constant improvement. All specifications and descriptions
More informationDEPARTMENT OF TRANSPORTATION
DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 Textron Lycoming AD 92-12-05 Amendment 39-8265 Effective July 10, 1992 Recurring: No [Docket No. 91-ANE-48; Amendment 39-8265;
More informationBO 76 SAFETY PAD. Ex. Coupe COMPONENTS
BO76 SAFETY PAD Ex. Coupe COMPONENTS BO77 COMPONENTS (Cont d) BO78 REMOVAL OF SAFETY PAD (See page BO76, 77) 1. DISCONNECT BATTERY CABLE FROM NEGATIVE TERMINAL 2. REMOVE STEERING WHEEL (See page SR3) 3.
More informationSERVICE BULLETIN REVISION
Revision 1 REVISION TRANSMITTAL SHEET This sheet transmits Revision 1 to. A. Removed the 4890307-2 Carpet from the -2 Kit and added the requirement to order it separately based on airplane color scheme.
More informationTechnical Newsletter #tnl e # 1 / 23
# 1 / 23 Change of the carbon brush replacement procedure in DAD3350 Maintenance Manual Purpose of this document There were cases where the replacement operation of the carbon brush was not correctly performed,
More informationCessna HID Light Assembly Kit INSTALLATION MANUAL No. HID-C-002
Cessna HID Light Assembly Kit INSTALLATION MANUAL No. HID-C-002 Model Applicability: Cessna Models - 180J, 180K, 182P, 182Q, 182R, T182, R182, TR182, A185F, U206F, TU206F, U206G, TU206G, 210L, T210L, 210M,
More informationGear Assembly Removal
Gear Assembly Removal 1 Remove the Top Cover, the Right Side Cover, the Fuser Assembly, and the Formatter Assembly. 2 Remove the Main Motor Assembly (see Figure 6-30). 3 Remove the (2) screws that hold
More informationAMERITRON RCS-12 AUTOMATIC ANTENNA SWITCH
AMERITRON RCS-12 AUTOMATIC ANTENNA SWITCH INSTRUCTION MANUAL PLEASE READ THIS MANUAL BEFORE OPERATING THIS EQUIPMENT! 116 Willow Road Starkville, MS 39759 USA 662-323-8211 Version 3B Printed in U.S.A.
More informationVENDOR SERVICE BULLETIN
HOLMBERG GMBH & CO. KG Ohlauer Strasse 5-11 D-10999 Berlin Telephone: +49-30-617 80-0 Telefax: +49-30-618 80-200 e-mail: info@holmco.de VENDOR SERVICE BULLETIN CAGE CODE: D 9240 VSB No.: 89-23-15 ATA SYSTEM:
More informationTOYOTA TUNDRA CARGO DIVIDER Preparation. Part Number: PT
Preparation Part Number: PT767-34070 Kit Contents 1 1 Divider Screen 2 1 LH Bracket with Warning Label 3 1 RH Bracket without Warning Label NOTE: Part number of this accessory may not be the same as the
More informationCOMPLIANCE RECORD. Document Reference: S21.COMP-0811 Issue 2. Introduction. Description
Introduction This design change will install and activate the Spectralux Dlink + ACARS Display Unit (DU) into the wiring provisions installed under STC Twenty One Change S21.23-13-1072, at the Operators
More informationOrtel (Lucent) Fiber Optic Interface AC
Ortel (Lucent) Fiber Optic Interface 144-701-1AC Serial Number March 11, 2010 CD P/N 098-00126-000 Revision B ORTEL (LUCENT) FIBER OPTIC INTERFACE 1. GENERAL INFORMATION... 1 1.1. SCOPE OF OPTION... 1
More information