Genx-1B P-N S-N Check List
|
|
- Ambrose Gardner
- 5 years ago
- Views:
Transcription
1 Engine P/N Genx-1B P-N S-N Check List CM Project (if relevant) 2305M70G07 ACCESSORY GEARBOX ASSY (MODULE 64X) core lwr l/h 1962M22P01 ACCLRM-TURBINE CENTER FRAME core upr l/h HPT ACTIVE CLEARANCE CONTROL VALVE core upr l/h LPT ACTIVE CLEARANCE CONTROL VALVE core upr l/h 2121M84P03 L/H ACTUATOR-VBV core upr l/h 2121M84P03 R/H ACTUATOR-VBV core upr r/h 2122M17P04 L/H ACTUATOR-VSV core upr l/h 2122M17P04 R/H ACTUATOR-VSV core upr r/h 1F8962 ASSEMBLY LUBRICLONE fan r/h BOOSTER ANTI ICE VALVE core upr r/h 721Z CENTREBODY - FORWARD CONTROL ALTERNATOR STATOR core lwr l/h CONTROLLER - VALVE - ENGINE ANTI-ICE core upr r/h COOLER-CONTROL,AIR,L-ENGINE ANTI-ICE core upr l/h 2122M33P01 CORE COMPARTMENT TEMP SENSOR core upr l/h Form No: ENG/ Issue 2 - Page 1 of 6
2 1G8842 DEBRIS MONITOR SENSOR fan r/h 1H8843 DMS AMPLIFIER fan r/h H02 ENG ANTI-ICE PRESS REG & SHUTOFF VLV 2121M82P06 ENGINE CONTROL-ELECTRONIC fan l/h ENGINE MONITORING UNIT fan l/h 2125M31P68 ENGINE RATING PLUG - GENE-1B64/P1 fan l/h 721Z EXHAUST AFT CENTER BODY 721Z EXHAUST NOZZLE ASSEMBLY (GE) FANCASE OVERHEAT DETECTOR -GE ENGINE core upr l/h Form No: ENG/ Issue 2 - Page 2 of 6
3 2300M94G02 FAN-SPINNER fan 2122M20P07 FMU-METERING UNIT. FUEL core lwr r/h 2122M21P04 FUEL FLOW METER core lwr r/h 2510M03P01 FUEL FLOW SPLIT VALVE core upr r/h FUEL PRESSURE SENSOR core lwr r/h FUEL PRESSURE SENSOR core lwr r/h FUEL PUMP core lwr r/h 2122M26P05 FUEL/OIL HEAT EXCHANGER core lwr r/h ER6083G01 LH VFSG SURFACE COOLER core lwr l/h LR47760E1 LUBE AND SCAVENGE PUMP core lwr l/h ER6230G01 MAIN ENGINE AIR OIL COOLER core upr r/h 2122M11P02 N1 SPEED SENSOR core lwr l/h 2122M25P01 OIL DELTA P SWITCH core lwr l/h 2121M86P01 OIL TEMPERATURE SENSOR (ENGINE) fan r/h 2121M86P01 OIL TEMPERATURE SENSOR (VFSG OIL IN) fan lwr r/h 2121M86P01 OIL TEMPERATURE SENSOR (VFSG OIL IN) fan lwr r/h 2121M86P01 OIL TEMPERATURE SENSOR (VFSG OIL OUT) core lwr l/h Form No: ENG/ Issue 2 - Page 3 of 6
4 2121M86P01 OIL TEMPERATURE SENSOR (VFSG OIL OUT) core lwr l/h 2376M20G09 PROPULSOR MODULE ASSEMBLY core upr l/h PUMP-ENGINE DRIVEN HYDRAULIC PUMP core lwr r/h ER6084G01 RH VFSG SURFACE COOLER core lwr r/h 2125M65P01 T25 SENSOR core lwr l/h 2122M10P01 T3 SENSOR core upr r/h 2121M96P01 T49 HARNESS BOTTOM core upr r/h 2121M95P01 T49 HARNESS TOP core upr r/h 2315M10G04 TANK-OIL (FULL ASSEMBLY) fan r/h 2315M11G04 TANK-OIL (TANK ONLY) fan r/h 2140M58P01 TRANSDUCER-MANIFOLD VALVE - ENGINE ANTI-ICE (EAI) 2121M88P02 VALVE-CCC core upr l/h 2121M87P02 VALVE-SUMP EDUCTOR core lwr l/h 2122M15P02 VALVE-TRANSIENT BLEED core upr r/h H02 VARIABLE FREQUENCY STARTER GENERATOR core lwr l/h H02 VARIABLE FREQUENCY STARTER GENERATOR core lwr l/h Form No: ENG/ Issue 2 - Page 4 of 6
5 2122M69P03 VFSG FUEL OIL HEAT EXCHANGER core lwr l/h VFSG POWER FEEDER CABLE # VFSG POWER FEEDER CABLE #2 2139M91P03 W05 WIRE HARNESS 2139M92P02 W06 WIRE HARNESS 2506M00P01 W07 WIRE HARNESS 2140M31P01 W071F HARNESS 2139M94P02 W08 WIRE HARNESS 2140M32P01 W081F HARNESS 2122M38P03 W1 HARNESS 2443M57P01 W10 WIRE HARNESS 2443M58P01 W12 WIRE HARNESS 2443M59P01 W13 WIRE HARNESS 2122M58P03 W131F HARNESS 2122M59P03 W14 HARNESS 2122M60P03 W15 HARNESS 2122M64P04 W17 WIRE HARNESS Form No: ENG/ Issue 2 - Page 5 of 6
6 2122M39P03 W2 HARNESS 2122M40P03 W3 HARNESS W30 HARNESS W31 HARNESS W32 HARNESS W33 HARNESS W34 HARNESS W35 HARNESS 2122M41P03 W4 HARNESS 2443M56P01 W9 HARNESS Date: Stamp: Notes Dispatch is only required to be completed if different from receipt Mark box as 'not fitted' if component is not installed Form No: ENG/ Issue 2 - Page 6 of 6
Technical Manual Index March 1, 2018
Technical Manual Index March 1, 2018 Following is the GEnx Component Maintenance Manual Section of the Technical Manual Index. AR in the Next Rev Column indicates As Required. An asterisk (*) behind the
More informationTHOMSON AIRWAYS LIMITED DISCREPANCY SHEET
IPC REF FIG ITEM DESCRIPTION FROM 72.35.01 01 085/220 ROTATING FAIRINGS 72.31.11 01 280 LP BLADES (22 OFF) 73.11.07 01 645/725 MAIN FUEL INLET TUBE 29.11.03 02 100 HYD. SUPPLY,RIGID TUBE 29.11.03 02 200
More informationTechnical Manual Index
(58828) Part [73] ENGINE FUEL AND CONTROL 73-11-05 CM.004-1A, -1C MAIN FUEL PUMP 2496M32P04 6970-115 Woodward (66503) May 11, 2016 01 March 23, 2017 AR 73-11-06 CM.004-1B MAIN FUEL PUMP 2566M05P04 6970-126
More informationCOMPONENT IDENTIFICATION
This CFMI publication is for Training Purpose Only. The information is accurate at the time of compilation; however, no update service will be furnished to maintain accuracy. For authorized maintenance
More informationCFM REGULATION THE POWER OF FLIGHT
CFM56-3 3 REGULATION 1 CFM56-3 2 Speed Governing System Fuel Limiting System VBV VSV N1 Vs P Idling System HPTCCV N1 Vs Z N1 Vs T Main Tasks Additional Tasks Corrections MEC PMC CFM 56-3 ENGINE OPERATIONAL
More informationTYPE CERTIFICATE DATA SHEET
TYPE CERTIFICATE DATA SHEET For Models: No. IM.E.102 for Engine GEnx Series Engines Type Certificate Holder GE Aviation One Neumann Way Cincinnati Ohio 45215 United States of America GEnx 1B GEnx 2B GEnx
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET For Models: No. IM.E.102 for Engine GEnx Series Engines Type Certificate Holder GE Aviation One Neumann Way Cincinnati - Ohio 45215 United States of America GEnx-1B GEnx-2B
More informationCF34-10 Technical Manual Index January 1, 2018
CF34-10 Technical Manual Index January 1, 2018 Following is the CF34-10 Component Maintenance Manual Section of the Technical Manual Index. All. An asterisk (*) behind the Rev No. indicates the manual
More informationTCDS NUMBER E00078NE U.S. DEPARTMENT OF TRANSPORTATION REVISION: 3 DATE: April 12, 2011
TCDS NUMBER E00078NE U.S. DEPARTMENT OF TRANSPORTATION REVISION: 3 DATE: April 12, 2011 FEDERAL AVIATION ADMINISTRATION GENERAL ELECTRIC COMPANY MODELS: TYPE CERTIFICATE DATA SHEET E00078NE GEnx-1B54 GEnx-1B58
More informationREPAIR STATION MANUAL
Propulsion Technologies International, LLC. 15301 S.W. 29th Street Miramar, Florida 33027 REPAIR STATION MANUAL APPENDIX A CAPABILITIES LIST Manual Control #: Electronic Assigned To: PTI LLC TABLE OF CONTENTS
More informationGENERAL The Honeywell model TFE731-40AR turbofan engine is a lightweight, two-spool, geared-stage, front-fan, jet engine.
ENGINE GENERAL The Honeywell model TFE731-40AR turbofan engine is a lightweight, two-spool, geared-stage, front-fan, jet engine. The cross section of the engine is shown in Figure 7-71-1, page VII-71-3.
More informationPneumatic Air Conditioning System Citation, Citation I
Pneumatic Air Conditioning System Citation, Citation I COCKPIT VENT FOOT WARMER OVERHEAD COCKPIT WINDSHIELD WEMAC OPTIMAL VENT OVERHEAD CONDITIONED AIR DUCTS BLOWER SIDE WINDOW UNDER FLOOR CONDITIONED
More informationCF34-8 Technical Manual Index July 1, 2018
CF34-8 Technical Manual Index July 1, 2018 Following is the CF34-8 Component Maintenance Manual Section of the Technical Manual Index. All. An asterisk (*) behind the Rev No. indicates the manual has been
More informationENGINE ACCESSORIES. D20DT Engine. PCV valve and oil separator. Turbo charger. EGR pipe (LH, Center, RH) Cooling fan clutch. Auto tensioner.
01 41 ENGINE ACCESSORIES Engine GENERAL PCV valve and oil separator Turbo charger Power steering pump Fuel return hose Alternator EGR pipe (LH, Center, RH) Cooling fan clutch EGR valve Auto tensioner Cable
More informationCYLINDER HEAD (for Bank 2 4WD and Pre-Runner)
144 1GR-FE ENGINE MECHANICAL CYLINDER HEAD (for Bank 2 4WD and Pre-Runner) CYLINDER HEAD (for Bank 2 4WD and Pre-Runner) ENGINE 1GR-FE ENGINE MECHANICAL COMPONENTS 88 (897, 65) x4 88 (897, 65) x4 NO. 1
More informationTechnical Manual Index
The manuals are listed in number order. The column indicates the following planned revision frequency for each publication listed: AR As Required revision cycle SEI185 is included on GEK 109944, CT58 Manuals
More informationV2527E-A5 ENGINE MINI-PACK
V2527E-A5 ENGINE MINI-PACK Engine Serial Number: Total Time / Total Cycles: V10136 47,579:58 / 23,093 Time/Cycles Since Last 5,994 / 11,562 Shop Visit LHT 2012 Time/Cycles Since Last 5,994 / 11,562 Performance
More informationEuropean Aviation Safety Agency
European Aviation Safety Agency EASA TYPE CERTIFICATE DATA SHEET Number : IM.E.026 Issue : 03 Date : 04 January 2013 Type : Engine Alliance LLC GP7200 series engines Variants: GP7270 GP7277 List of Effective
More informationCFM56-3 (FINAL_) 856A1027G01 Fixture, Lift - Compressor Rotor Stage 3 Disk And Blades 1 856A1028 Fixture 1
8100 Sweeney S/N STM014 1 107029435 BRKTs -3 Tooling 2 527241105 Fixture(combustion Chamber Fixture) 1 537241146 Fixture (combustion Chamber Fixture) 1 278114-1 CFM56-3 Fuel Pump Backlash Tool 1 301-360-005-0
More informationTYPE CERTIFICATE DATA SHEET
TYPE CERTIFICATE DATA SHEET No. IM.E.096 for PW800 Series Engines Type Certificate Holder 1000 Marie Victorin Longueuil, Quebec J4G1A1 Canada For : TE.CERT.00052 001 European Aviation Safety Agency, 2016.
More informationParts Book. VGT series engine
Parts Book VGT series engine Rev 2.2 AUG 2017 1 Dear customer In this catalog you will find all the components that your Marinediesel VGT-engine is constructed of. We have listed a couple of tips that
More informationLEAP-X Program Update
LEAP-X Program Update 29 Oct 09 NYC CFM International Proprietary Information The information in this document is CFM Proprietary Information and is disclosed in confidence. It is the property of CFM International
More informationCFM56-7B POWER PLANT REMOVAL & INSTALLATION
Task No: 737-71-00-00 NG Maint Prog Ref: BAL/BOE/11 Station: A/C Reg: Issue: 5 Date: NOV 2017 A.M.M. Ref: 71-00-02 Check: Aircraft Type CAA App Ref. UK.145.00112 Scheduled / Unscheduled Delete as applicable
More informationMTU Maintenance Dallas, Inc. Integrated Management System. MM 03D-03 Capability List Manual
Chapter 0 Page 2 of 15 Revision: Initial Date: 01NOV2012 0.1 Table of Contents 0 Title Page... 1 0.1 Table of Contents... 2 0.2 List of Effective Pages... 3 0.3 Record of Revision... 4 0.4 Record of Temporary
More informationOIL PUMP (for 4WD and Pre-Runner)
1GR-FE BRICATION OIL PUMP (for 4WD and Pre-Runner) OIL PUMP (for 4WD and Pre-Runner) ENGINE 1GR-FE BRICATION COMPONENTS 23 88 (897, 65) 88 (897, 65) NO. 1 ENGINE UNDER COVER SUB-ASSEMBLY FRONT PROPELLER
More informationTSE (PPOH) AIRWORTHINESS MANAGEMENT DIVISION MINIPACK GE CF6-50C2 ESN P a g e
MINIPACK GE CF6-50C2 528-154 1 P a g e CUURENT DATA TYPE CF6-50C2 S/N 528-154 46563 19073 REASON OF REMOVAL T/X DATE OF REMOVAL 22-May-2007 2 P a g e LLP SHEET NOMENCLATURE P/N S/N LIMIT REMAINING FAN
More informationRolls-Royce Corporation 501-D22 COMMERCIAL ENGINE BULLETIN (CEB) Technical Publications Index
Corporation 501-D22 COMMERCIAL ENGINE BULLETIN (CEB) Technical Publications Index May 1. 2018 72-- ENGINE 72--1001 Engine -- Reduction Gear Prop Recommended No Later Than 11--01--66 No. 2, 11--15--68 Brake
More informationCanadair Regional Jet 100/200 - Auxiliary Power Unit
1. INTRODUCTION The auxiliary power unit (APU) is installed within a fireproof titanium enclosure in the aft equipment compartment. The APU is a fully automated gas turbine power plant which drives an
More informationTSE (PPOH) AIRWORTHINESS MANAGEMENT DIVISION MINIPACK GE CF6-50E2 ESN P a g e ESN
MINIPACK GE CF6-50E2 517-131 1 P a g e CUURENT DATA TYPE CF6-50E2 S/N 517-131 57367 23857 TSO 2541 CSO 1147 TSR 2206 CSR 971 REASON OF REMOVAL DATE OF REMOVAL LAST SHOP STATUS LAST TEST CELL EGT MARGIN
More informationTHOMSON AIRWAYS LIMITED RB E4 RECEIPT/DESPATCH SHEET
ENGEERG DEPARTMENT B757 RB211-535E4 RECEIPT/DESPATCH SHEET THE FOLLOWG DETAILS MUST BE COMPLETED AS APPLICABLE. A/C REG: POS'N: S/N. OFF: HRS RUN: DATE: S/N. ON: HRS RUN: BATCH NO: REASON FOR CHANGE: TECH
More informationLM2500 BORESCOPE INSPECTION REPORT
LM2500 BORESCOPE INSPECTION REPORT UC DAVIS CUSTOMER UNIT NAME/NUMBER: N/A ENGINE SERIAL NUMBER: 481-743 TCT SALES ORDER NUMBER: US9010290 DATE INSPECTED:11-29-2018 SERVICEABILITY AT DATE OF INSPECTION:
More informationEuropean Aviation Safety Agency
European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET Number : IM.E.016 Issue : 07 Date : 21 May 2014 Type : Williams International Co. FJ44 Series Engines s FJ44-1A FJ44-1AP FJ44-2A FJ44-2C
More informationTSE (PPOH) AIRWORTHINESS MANAGEMENT DIVISION MINIPACK GE CF6-50E2 ESN P a g e ESN
MINIPACK GE CF6-50E2 455-358 1 P a g e CUURENT DATA TYPE CF6-50E2 S/N 455-358 64659 25342 TSO 4061 CSO 1363 REASON OF REMOVAL CONVINIENT DATE OF REMOVAL LAST SHOP STATUS LAST TEST CELL EGT MARGIN 08-May-2013
More informationMedium Duty/School Bus Parts
Blue Bird # Description 00008588 ALTERNATOR, L/N, 12V/270 AMP 00016333 ASSY - MODE SWITCH 00019435 ALTERNATOR, 12V 00031531 KNOB 1-1/8 00033722 BLOWER WHEEL 00035868 RESISTOR, 12V, 3-SP, 3-TERM 00035883
More informationTechnical Manual Index
The manuals are listed in number order. The column indicates the following planned revision frequency for each publication listed: 90 - - - - - 90 day revision cycle (Quarterly updates) 180 - - - - - 180
More informationLMS100 Gas Turbine System
GE Energy LMS100 Gas Turbine System A flexible growth platform to meet changing energy needs. The LMS100 game changing technology from frame and aero gas turbines LMS100 CFM TECH56 CAPPs Combustor LM6000
More informationRolls-Royce Corporation T56-A-14LFE COMMERCIAL ENGINE BULLETIN (CEB) Technical Publications Index
Corporation T56-A-14LFE COMMERCIAL ENGINE BULLETIN (CEB) Technical Publications Index November 1, 2017 72-- ENGINE 72--4001 Cancelled Prior to Publication A--72--4002 Engine -- Reduction Gear, Propeller
More informationDASSAULT AVIATION Proprietary Data
FALCON 7X 02-70-05 CODDE 1 PAGE 1 / 6 GENERAL ACRONYMS LIST ACOC AGB APU A/T ATSV BOV CAS CB CL CMC CR DC DCU ECS EEC FADEC FBW FCU FF FOHE FSOV HP HPC HPT IGV ITT LP LPC LPT LRU MV N1 N2 PDU PLA PMA PMU
More informationBALLAST UNIT Ea 5 New REPAIRABLE INDICATOR FLAP POSITION Ea 1 Overhauled ROTABLE
Part Number Description UoM Qty Condition Aircraft type Aircraft type Part Class 05939-108 BALLAST UNIT Ea 5 New REPAIRABLE 07311P000-02 BALLSCREW Ea 1 Overhauled B737-; B737-800 10-60791-13 INDICATOR
More informationFAA-Approved Parts Price List
FAA-Approved Parts Price List Downloaded From Website: Sun, Feb 4, 2018 MDHI P/N Name Aerometals P/N Price 369A1003-501 Scissors Link 369X1003-501 $550.00 369A1004-5 Folding Pin 369X1004-5 $445.00 369A1005-3
More informationCFM Technology. realizing the promise 50% LOWER NOX EMISSIONS. ANOTHER LEAP FORWARD FOR LEAP TECHNOLOGY.
50% LOWER NOX EMISSIONS. CFM Technology realizing the promise ANOTHER LEAP FORWARD FOR LEAP TECHNOLOGY. Bill Brown General Manger CFM Marketing June 2010 CFM International Proprietary Information The information
More informationCHAPTER ICE AND RAIN PROTECTION SYSTEM
15--00--1 ICE AND RAIN PROTECTION SYSTEM Table of Contents REV 3, May 03/05 CHAPTER 15 --- ICE AND RAIN PROTECTION SYSTEM Page TABLE OF CONTENTS 15-00 Table of Contents 15--00--1 INTRODUCTION 15-10 Introduction
More informationFull Authority Digital Electronic Control (FADEC)
Eng.10 Engines-Description and Operation General The aircraft is equipped with three GE CF6-80C2 engines or three P&W PW4460 or PW4462 engines. Each engine has dual rotors, a Low Pressure Compressor (LPC)
More informationENGINE ASSEMBLY COMPONENTS EM 170 1GR-FE ENGINE MECHANICAL ENGINE ASSEMBLY V-BANK COVER VACUUM HOSE AIR CLEANER ASSEMBLY NO. 2 VENTILATION HOSE
170 ENGINE 1GR-FE MECHANICAL COMPONENTS 1GR-FE ENGINE MECHANICAL ENGINE 7.5 (76, 66 in.*lbf) V-BANK COVER 8.0 (82, 71 in.*lbf) 8.0 (82, 71 in.*lbf) VACUUM HOSE AIR CLEANER NO. 2 VENTILATION HOSE MASS AIR
More informationTYPE-CERTIFICATE DATA SHEET
Issue: 02 & LEAP-1C series engines Date: 11 March 2016 TYPE-CERTIFICATE DATA SHEET No. E.110 for Engine & LEAP-1C series engines Type Certificate Holder SA SA 2, boulevard du Général Martial Valin 75015
More informationEASA and FAA Released Doc. Version 8/21/15
Part Number Description 0101KIP05-015 0101KPR2 0101KPU2 FUEL QTY PRESELECTOR 0102KFP01 0102KIP01-017 0102KIP01-021 0103KFP03 0105KIP06-016 0106KIP02-022 0107KPU1 FUEL QTY PRESELECTOR 0108KTU04 0116KTU01
More informationWind Turbine Machine Head Evaluation Page 1 of 32 Appendix I. Sketch of 1.5XLE (from GE literature).
Wind Turbine Machine Head Evaluation Page 1 of 32 Figure 1 Sketch of 1.5XLE (from GE literature). Figure 2 Sketch of 1.5XLE (from GE literature). Wind Turbine Machine Head Evaluation Page 2 of 32 Figure
More informationRolls-Royce Corporation T56 SERVICE INFORMATION LETTER (SIL) Technical Publications Index
Corporation T56 SERVICE INFORMATION LETTER (SIL) Technical Publications Index November 1, 2017 91--00 Use of the Service Information Letter 08--05--91 91--01 Compressor Inlet Sensing Probe Torque 06--28--91
More informationAircraft Status Report - Engine One
Aircraft Status Report - Engine One Current Aircraft Hours: 9060 : 25 Total Engine Hours: 9905 : 55 Engine Serial No. CAE-840294 Engine Hours Since 9905 : 55 Total Engine Cycles: 17486 Insp Comp Comp Eng
More informationTECHNICAL MANUAL AVIATION UNIT AND AVIATION INTERMEDIATE MAINTENANCE MANUAL ENGINE, GAS TURBINE MODEL T55-L-714 NSN
TECHNICAL MANUAL AVIATION UNIT AND AVIATION INTERMEDIATE MAINTENANCE MANUAL ENGINE, GAS TURBINE MODEL T55-L-714 NSN 2840-01-353-7635 DISTRIBUTION STATEMENT A: Approved for public release; distribution
More informationREPLACEMENT. 9. REMOVE TRANSMISSION CONTROL CABLE BRACKET NO.1 (a) Remove the 2 bolts and control cable bracket No.1.
AUTOMATIC TRANSMISSION / TRANS REPLACEMENT 1. REMOVE HOOD SUBASSY 2. REMOVE BATTERY 3. REMOVE WINDSHIELD WIPER LINK ASSY (See page 666) 4. REMOVE FRONT PANEL ASSY (See page 2610) 5. REMOVE CYLINDER HEAD
More informationAIR FORCE LIFE CYCLE MANAGEMENT CENTER
AIR FORCE LIFE CYCLE MANAGEMENT CENTER PROPULSION DIRECTORATE F108-100 Industry Day 9 January 2017 I n t e g r i t y - S e r v i c e - E x c e l l e n c e For Official Use Only 1 Disclaimer The information
More informationONTIC MAINTENANCE, REPAIR & OVERHAUL CAPABILITY CHATSWORTH, CA
ONTIC MAINTENANCE, REPAIR & OVERHAUL CAPABILITY CHATSWORTH, CA EASA and FAA Released Part Number Description 0101KIP05-015 COMBINED PROCESSOR 0101KPR2 REFUEL PANEL 0101KPU2 FUEL QTY PRESELECTOR 0102KFP01
More informationTECHNICAL MANUAL AVIATION UNIT AND AVIATION INTERMEDIATE MAINTENANCE MANUAL ENGINE, GAS TURBINE MODEL T55-L-714 NSN
TM 1-2840-252-23--2 TECHNICAL MANUAL AVIATION UNIT AND AVIATION INTERMEDIATE MAINTENANCE MANUAL ENGINE, GAS TURBINE MODEL T55-L-714 NSN 2840-01-353-7635 DISTRIBUTION STATEMENT A: Approved for public release,
More informationEuropean Aviation Safety Agency
European Aviation Safety Agency EASA TYPE CERTIFICATE DATA SHEET Number: IM.E.021 Issue: 05 Date: 03 January 2013 Type: General Electric Company CF34-10E Series Engines Variants CF34-10E2A1 CF34-10E5 CF34-10E5A1
More informationATA 49 AUXILIARY POWER UNIT
F900EX EASY 02-49-00 CODDE 1 PAGE 1 / 2 TABLE OF CONTENTS 02-49 02-49-00 TABLE OF CONTENTS 02-49-05 GENERAL Introduction Sources APU location 02-49-10 DESCRIPTION Introduction Description Operating principle
More informationCHAPTER 4 ---AUXILIARY POWER UNIT
Table of Contents Vol. 1 04--00--1 CHAPTER 4 ---AUXILIARY POWER UNIT Page TABLE OF CONTENT 04-00 Table of Contents 04--00--1 INTRODUCTION 04-10 Introduction 04--10--1 POWER PLANT 04-20 APU Power Plant
More informationEMBRAER 190. Powerplant DO NOT USE FOR FLIGHT
EMBRAER 190 Powerplant DO NOT USE FOR FLIGHT Embraer 190 - Systems Summary [Powerplant] Two wing-mounted General Electric CF34-10E engines produce power to the EMBRAER 190. The General Electric CF34-10E
More information2007 A119 Koala Price: Make an Offer
2007 A119 Koala Price: Make an Offer Aircraft Details Manufacture Date: 2007 Hours: 87hrs Airframe: Aluminium alloy & bonded panel fuselage Semimonocoque aluminium alloy tail boom Skid type landing gear
More informationPOWERPLANT. Table of Contents. May 06/2005 Flight Crew Operating Manual Volume 2 REV 2 CSP REV 2
Table of Contents Introduction... 18-01-01 Honeywell AS907 Engine Sections... 18-01-01 Engine Construction... 18-01-02 Description... 18-01-02 Airflow Paths... 18-01-02 Major Powerplant Components... 18-01-03
More informationSTARTER COMPONENTS FOR REMOVAL AND INSTALLATION
Removal STARTER COMPONENTS FOR REMOVAL AND INSTALLATION Starter Components For Removal And Installation REMOVAL OF STARTER 1. DISCONNECT CABLE FROM NEGATIVE TERMINAL OF BATTERY CAUTION: Work must be started
More informationG ELECTRICAL WIRING ROUTING [2ZZ GE] Position of Parts in Engine Compartment
G ELECTRICAL WIRING ROUTING [2ZZ GE] Position of Parts in Engine Compartment A 1 A/C Magnetic Clutch A 2 ABS Speed Sensor Front LH A 3 ABS Speed Sensor Front RH A 4 Airbag Sensor Front LH A 5 Airbag Sensor
More informationELECTRICAL COMPONENT LOCATOR
ELECTRICAL COMPONENT LOCATOR 1988 Toyota Celica 1988 TOYOTA Celica Electrical Components ---------------------------------------------------------------------- BUZZERS, RELAYS & TIMERS ----------------------------------------------------------------------
More informationPOWER SOURCE (Current Flow Chart)
POWER SOURCE (Current Flow Chart) The chart below shows the route by which current flows from the battery to each electrical source (Fusible Link, Circuit Breaker, Fuse, etc.) and other parts. The next
More informationPARTIAL ENGINE ASSY COMPONENTS. Clip. Radiator Grille. Clip. Front Bumper Cover. Engine Under Cover LH. N m (kgf cm, ft lbf) : Specified torque
ENGINE MECHANICAL 1417 COMPONENTS 141FP01 Radiator Grille Front Bumper Cover Engine Under Cover RH Engine Under Cover LH A79361 962 1418 ENGINE MECHANICAL Heater Outlet Water Hose 7.0 (71, 62 in. lbf)
More informationPosition of Parts in Engine Compartment
ELECTRICAL WIRING ROUTING [5S FE] Position of Parts in Engine Compartment A 1 A/C Condenser Fan Motor E 4 Engine Coolant Temp. Sensor (EFI Water Temp. A 2 A/C Magnetic Clutch and Lock Sensor Sensor) A
More informationDiscount Tractor Parts Ph FORD 4000 Parts Catalogue Published July 2012
Discount Tractor Parts Ph 0800 872272 www.discounttractorparts.co.nz FORD 4000 Parts Catalogue Published July 2012 Discount Tractor Parts 7 Airdrie Rd., Box 70059, Ranui, Auckland Ph 0800 872 272 09 8337483
More informationCOMPONENT LOCATOR > DISASSEMBLED VIEWS
Page 1 of 45 2006 Pontiac Grand Prix 3.8L Eng Base Service Manual: ENGINE MECHANICAL - 3.8L COMPONENT LOCATOR > DISASSEMBLED VIEWS Fig 1: Engine Block Component Views Callout Component Name 100 Engine
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET No. IM.E.016 issue 10 for FJ44/FJ33 Series Engines Certificate Holder Williams International Co. Walled Lake Michigan 48390-0200 USA For Models: FJ44-1A FJ44-1AP FJ44-2A FJ44-2C
More informationPosition of Parts in Engine Compartment
[1UZ FE] Position of Parts in Engine Compartment A 1 A/C Ambient Temp. Sensor E 4 Engine Coolant Temp. Sensor (Water Temp. Sensor A 2 A/C Dual Pressure SW and A/C High Pressure SW (for Cooling Fan)) A
More informationProduction began January 8, 2001
Replacement Parts Single Deck Open Well Merchandiser Production began January 8, 2001 9000620 NF8 Low-Temp 8 Open Well FF Merchandiser 9000621 NF12 Low-Temp 12 Open Well FF Merchandiser 9000622 NFS8 Low-Temp
More informationRolls -Royce M250--C47M OPERATION AND MAINTENANCE
TABLE 603 Inspection Checksheet Owner Date A/C Make/Model S/N Reg No. TSN Engine S/N TSN TSO This inspection checksheet is to be used when performing scheduled inspections. This form may be locally reproduced
More informationFOLDING TOP HYDRAULIC CYLINDER HOSE IDENTIFICATION
Page 1 of 50 Service Manual: POWER ROOF SYSTEM AND Print Date: CONVERTIBLE TOP FOLDING TOP HYDRAULIC CYLINDER HOSE IDENTIFICATION Fig 1: View Of Folding Top Hydraulic Cylinder 2006 Pontiac G6 3.9L Eng
More informationCustomer Focused, Customer Driven
Customer Focused, Customer Driven FAA approved repair station specializing in the repair and overhaul of engine components and accessories for commercial, military, industrial and airframe applications
More informationREPLACEMENT. 4. REMOVE ENGINE UNDER COVER RH 5. REMOVE FAN AND GENERATOR V BELT (See page 14 4)
5540 550JH01 REPLACEMENT HINT: COMPONENTS: See page 5539 1. DISCHARGE REFRIGERANT FROM REFRIGERATION SYSTEM (See page 5511) SST 0711058060 (0711758080, 0711758090, 0711778050, 0711788060, 0711788070, 0711788080)
More informationPage 1 of 14 Oil Pan Removal & Installation 4.2L Engine 4WD Vehicles To Remove: 1. Before servicing the vehicle refer to the precautions at the beginning of this section. 2. Raise and support the vehicle.
More informationPosition of Parts in Engine Compartment
ELECTRICAL WIRING ROUTING [3S GTE] Position of Parts in Engine Compartment A 1 A/C Ambient Temp. Sensor D 1 Date Link Connector 1 (Check Connector) A 2 A/C Condenser Fan Motor D 2 Distributor A 4 A/C Magnetic
More informationPosition of Parts in Engine Compartment
ELECTRICAL WIRING ROUTING [5S FE] Position of Parts in Engine Compartment A 1 A/C Ambient Temp. Sensor D 1 Distributor A 2 A/C Condenser Fan Motor A 3 A/C Idle Up VSV E 1 ECT Solenoid A 4 A/C Magnet Clutch
More informationG ELECTRICAL WIRING ROUTING
G ELECTRICAL WIRING ROUTING Position of Parts in Engine Compartment A 1 A/C Condenser Fan Motor A 2 A/C Magnetic Clutch and Lock Sensor A 3 A/C Triple Pressure SW (A/C Dual and Signal Pressure SW) A 4
More informationItem MF CMF EMF LP Code Part Description Part # GRP
MF SERIES FLAKERS MF2006-CMF2306-EMF2306 AIR, WATER & REMOTE Item MF CMF EMF LP Code Part Description Part # GRP 2006 2306 2306 2306 AIR COOLED 5 Air Condenser 9141056-01 AC X X X 10 Fan Blade 9131053-01
More informationBREAKER TRAY BACK/BOTTOM
1 0F7135 1 BREAKER TRAY BACK/BOTTOM 2 0F7022 1 SUPPORT CONTROL PANEL SIDE RH 3 0F7021 1 SUPPORT CONTROL PANEL SIDE LH 4 0F7260 1 COVER CIRCUIT BREAKER 2P 0F7136 1 COVER CIRCUIT BREAKER 3P 5 0F6156 1 PLATE
More informationG ELECTRICAL WIRING ROUTING
2 6 G ELECTRICAL WIRING ROUTING [2JZ-GTE] Position of Parts in Engine Compartment A 1 A/C Ambient Temp Sensor A 2 A/C Condensor Fan Motor A 3 A/C Triple Pressure SW (A/C Dual and Single Pressure SW) A
More informationEuropean Aviation Safety Agency
European Aviation Safety Agency EASA TYPE-CERTIFICATE DATA SHEET Number : E.036 Issue : 04 Date : 10 September 2013 Type : Rolls-Royce plc Trent 1000 series engines Models Trent 1000-A Trent 1000-A2 Trent
More informationRolls -Royce M250--C40B OPERATION AND MAINTENANCE. Table 603. Inspection Checksheet
Table 603 Inspection Checksheet Owner Date A/C Make/Model S/N Reg. No. TSN Engine S/N TSN TSO This inspection checksheet is to be used when performing scheduled inspections. This form can be locally reproduced
More informationInventory Majestic Jet
Inventory Majestic Jet TO BE SOLD IN BULK Description Transceiver-VHF Comm P/N:822-1114-001 Transceiver-VHF Comm P/N:822-1114-001 Coupler-Mode P/N:792-6255-001 Coupler-Mode P/N:792-6255-001 Computer-Flight
More informationL PART NUMBER OF CONNECTORS
L PART NUMBER OF CONNECTORS Code Part Name Part Number Code Part Name Part Number A 1 A/C Ambient Temp. Sensor 90980-11070 B15 Blower Motor Controller (Rear) 90980-11136 A 2 A/C Magnetic Clutch 90980-11271
More informationEngine Diagrams
100-002 Engine Diagrams Engine Views The illustrations that follow show the locations of the major external engine components, the filters, and other service and maintenance points. Some external components
More informationGeneral. Airfoil Anti-Ice System
General Ice.10 Ice and Rain Protection-Description and Operation Ice and rain protection consists of: Airfoil (wing and tail) anti-ice systems. Engine cowl anti-ice system. Air data heater system (pitot,
More informationFFTR1814QB5A FFTR1814QS5A FFTR1814QW5A
Product No. B5A S5A W5A Series R134a R134a R134a Color black stainless white Volts 115 115 115 Wiring Diagram 241582401 241582401 241582401 Owner's Guide Eng Spn A04555602 A04555602 A04555602 Owner's Guide
More informationEngine Front Cover. Special Tool(s) Lifting Bracket, Engine (2 required) 303-D087 (D93P-6001-A1) or equivalent. Support Bar, Engine 303-F070
SECTION 303-01C: Engine 5.4L (4V) 2009 Mustang Workshop Manual IN-VEHICLE REPAIR Procedure revision date: 07/25/2008 Engine Front Cover Special Tool(s) Lifting Bracket, Engine (2 required) 303-D087 (D93P-6001-A1)
More informationSECTION Automatic Transaxle/Transmission 4R70E/4R75E
307-01-i Automatic Transaxle/Transmission 4R70E/4R75E 307-01-i SECTION 307-01 Automatic Transaxle/Transmission 4R70E/4R75E CONTENTS PAGE Transmission Four Wheel Drive (4WD)... 307-01-2 307-01-2 Automatic
More informationTYPE-CERTIFICATE DATA SHEET
TYPE-CERTIFICATE DATA SHEET No. IM.E.093 for PW1100G-JM Series Engines Type Certificate Holder 400 Main Street East Hartford, CT 06118 United States of America For Models: PW1133G-JM PW1133GA-JM PW1130G-JM
More informationTRANSFER ASSY (VF4AM)
ASSY (VF4AM) 313 ASSY (VF4AM) COMPONENTS 3103202 ATF Level Gauge Transmission Oil Filler Tube Subassy Propeller Shaft Assy 12 (122, 9) ORing Oil Cooler Inlet Tube No.1 and Oil Cooler Outlet Tube No.1 34
More informationG ELECTRICAL WIRING ROUTING
G ELECTRICAL WIRING ROUTING Position of Parts in Engine Compartment A 1 A/C Condenser Fan Motor A 2 A/C Magnetic Clutch and Lock Sensor A 3 A/C Triple Pressure SW (A/C Dual and Single Pressure SW) A 4
More informationTABLE OF CONTENTS POWER PLANT. Page. 17-i
Chapter 17: Power Plant TABLE OF CONTENTS Page Introduction...17-1 Description...17-2 Engine Assembly and Airflow...17-2 Engine Modules...17-3 Full Authority Digital Electronic Control (FADEC)...17-4 Electronic
More informationBombardier Challenger Auxiliary Power Unit
GENERAL A Honeywell 36 150(CL) constant-speed gas turbine auxiliary power unit (APU) is installed within a fire-resistant compartment in the aft equipment bay. The APU drives a generator, providing AC
More informationSection - III SYSTEMS DESCRIPTION
Section - III SYSTEMS DESCRIPTION Pro Line 21 Table of Contents Page GENERAL...2-5 DESCRIPTION...2-6 Figure 1 - Engine Cutaway View...2-6 FAN...2-6 COMPRESSOR SECTION...2-6 Low Pressure Spool N 1...2-7
More informationISUZU DIESEL ENGINE 4LE1 DA07 PARTS CATALOG
ISUZU DIESEL ENGINE 4LE1 DA07 PARTS CATALOG How to refer to the Parts Catalog 1 2 4 3 5 1 FIG NO. A 3-digit (X-XX) Figure Number has been assigned to every section/illustration of the catalog. The first
More informationCAPABILITY MANUAL 3, HAWTIN PARK, BLACKWOOD, GWENT, SOUTH WALES, UK. NP12 2EU CAPABILITY MANUAL CONTROLLED COPY 1
Page 1 3, HAWTIN PARK, BLACKWOOD, GWENT, SOUTH WALES, UK. NP12 2EU CAPABILITY MANUAL EASA Part 21 Subpart J Approval No. EASA.21J.024 EASA Part 21 Subpart G Approval No. UK.21G.2575 EASA Part 145 Approval
More information2013 Mustang Workshop Manual
32. Attach the wiring harness retainers to the LH side of the oil pan and the front oil pan stud bolts and install the 2 nuts. Tighten to 8 Nm (71 lb-in). 33. Position the underbody shield and install
More information