28-CONTENTS
BEJ Page 9 Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
CHAPTER 28 - FUEL
TABLE OF CONTENTS
_________________
Chapter Section Subject_______ Subject ____ Effectivity
_______ Page ___________
FUEL QUANTITY INDICATING SYSTEM 28-41-02 Description and Operation 1 [*] General 1 Indicator - Fuel Quantity 7 Indicator - Refuel Quantity 7 Sticks - Fuel Measuring 8 Trimmers - Capacitance 8 Unit - Compensator 6 Unit - Fuel Summation 8 Unit - Tank 6 Operation 9 [*] AIRPLANES WITH SIMMONDS DIGITAL FUEL QUANTITY INDICATORS
Trouble Shooting 101 ALL General 101 Adjustment/Test 501 CONFIG 1 [*] General 501 Operational Test 502 System Test 512 System Trim 503 [*] AIRPLANES WITH SIMMONDS DIGITAL FUEL QUANTITY INDICATORS (GULL SYSTEM TESTER)
Adjustment/Test 501 CONFIG 2 [*] General 501 Operational Test 502 System Test 517 ú System Test 528 System Trim 503 [*] AIRPLANES WITH SIMMONDS DIGITAL FUEL QUANTITY INDICATORS (SIMMONDS SYSTEM TESTER)
Adjustment/Test 501 CONFIG 3 [*] General 501 Operational Test 502 System Test 514 System Trim 503 [*] AIRPLANES WITH SIMMONDS DIGITAL FUEL QUANTITY INDICATORS (BARFIELD SYSTEM TESTER)
Inspection/Check 601 [*] [*] AIRPLANES WITH SIMMONDS DIGITAL FUEL QUANTITY INDICATORS
28-CONTENTS
BEJ.1 Page 10 Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
CAL
CAL
CAL
CAL
A
737-300/400/500MAINTENANCE MANUAL
CHAPTER 28 - FUEL
TABLE OF CONTENTS
_________________
Chapter Section Subject_______ Subject ____ Effectivity
_______ Page ___________
HARNESS - WIRE, FUEL QUANTITY 28-41-31 INDICATING SYSTEM Approved Repairs 801 [*] [*] AIRPLANES WITH FQIS WIRE HARNESSES THAT ARE CRIMPED AND NOT SOLDERED
INDICATOR - FUEL QUANTITY 28-41-51 Removal/Installation 401 ALL INDICATOR - FUELING QUANTITY 28-41-61 Removal/Installation 401 ALL PLUG - TANK AND COMPENSATOR UNIT 28-41-41 BUSSING Removal/Installation 401 ALL RESISTANCE - SYSTEM TOTAL - FUEL 28-41-91 QUANTITY INDICATING Inspection/Check 601 CONFIG 1 [*] [*] AIRPLANES WITHOUT ISOLATED FUEL QUANTITY TRANSMITTER (IFQT)
Inspection/Check 601 CONFIG 2 [*] [*] AIRPLANES WITH ISOLATED FUEL QUANTITY TRANSMITTER (IFQT)
STICK - FUEL MEASURING 28-41-11 Removal/Installation 401 ALL Approved Repairs 801 CONFIG 1 [*]
Leak Around Bayonet Base 803
Leak Around Measuring Stick 803
Leak At Measuring Stick Head 801
[*] AIRPLANES WITH DRIPSTICK TYPE FUEL MEASURING STICKS
Approved Repairs 801 CONFIG 2 [*]
Replacement of O-Ring 801
Between the Housing and
Base
[*] AIRPLANES WITH THE MAGNETIC FLOAT TYPE OF FUEL MEASURING STICK
TRANSMITTER - ISOLATED FUEL 28-41-72 QUANTITY (IFQT) Removal/Installation 401 [*][*] AIRPLANES WITH GOODRICH ISOLATED FUEL QUANTITY TRANSMITTER (IFQT)
Adjustment/Test 501 [*][*] AIRPLANES WITH GOODRICH ISOLATED FUEL QUANTITY TRANSMITTER (IFQT)
28-CONTENTS
BEJ Page 11 Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
CHAPTER 28 - FUEL
TABLE OF CONTENTS
_________________
Chapter Section Subject_______ Subject ____ Effectivity
_______ Page ___________
UNIT - FUEL SUMMATION 28-41-81 Removal/Installation 401 ALL Adjustment/Test 501 ALL
UNIT - FUEL SUMMATION 28-41-82 Adjustment/Test 501 [*] [*] AIRPLANES WITH DIGITAL FUEL QUANTITY INDICATORS
UNIT - TRIM, CAPACITANCE 28-41-86 Removal/Installation 401 ALL
UNITS - TANK AND COMPENSATOR 28-41-21 Removal/Installation 401 ALL Adjustment/Test 501 ALL Cleaning/Painting 701 ALL
WIRE HARNESS - FUEL TANK 28-41-44
BULKHEAD (SPAR) RECEPTACLE Removal/Installation 401 ALL Inspection/Check 601 ALL
WIRE HARNESS - ISOLATED FUEL 28-41-45
QUANTITY TRANSMITTER (IFQT)
Removal/Installation 401 [*]
CAL [*] AIRPLANES WITH ISOLATED FUEL QUANTITY TRANSMITTER (IFQT)
CAL FUEL FEED LOW PRESSURE INDICATING 28-42-00 SYSTEM Description and Operation 1 ALL General 1 Switches - Fuel Feed Low 1 Pressure Operation 1 Trouble Shooting 101 ALL Adjustment/Test 501 ALL SWITCH - FUEL FEED LOW PRESSURE 28-42-11 Removal/Installation 401 ALL FUEL TEMPERATURE INDICATING SYSTEM 28-43-00 Description and Operation 1 ALL General 1 Bulb - Fuel Temperature 1 Indicator - Fuel Temperature 3 Trouble Shooting 101 ALL Adjustment/Test 501 ALL BULB - FUEL TEMPERATURE 28-43-11 Removal/Installation 401 ALL
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737-300 400 500 AMM 飞机维护手册 燃油 FUEL 1(4)