ENGINE FIRE CONTROL PANEL, M10443 TEST SWITCH, S1 A SQUIB TEST CONTROL PANEL, M10401 PRESSURE SWITCH
B
SAFETY RELIEF AND FILLER PORT
DISCHARGE CARTRIDGE (SQUIB) ELECTRICAL CONNECTOR ENGINE FIRE EXTINGUISHER BOTTLE, B17 OR B18 C
Engine Fire Extinguishing System - Component Location Figure 102
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
26-21-00
ALL ú ú 01 Page 102 ú Mar 20/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757 MAINTENANCE MANUAL
ENGINE FIRE EXTINGUISHING SYSTEM - ADJUSTMENT TEST
__________________________________________________
1. General_______
A. This section contains procedures to perform the tests that follow:
(1)
The operational test makes sure the system operates correctly. It can be done in a minimum of time and uses only the equipment installed in the airplane.
(2)
The system test has different tests for each part of the system. When all the tests are done, the engine fire extinguishing system is ready to operate correctly.
(3)
The discharge line test makes sure the connections are correct from the fire extinguisher bottles to the discharge nozzles.
TASK 26-21-00-715-199
2. Operational Test________________
A. General
(1) The engine fire extinguishing system has two identical fire bottles located in the forward of the aft cargo compartment, an engine fire control panel, and a squib test panel. The extinguishing plumbing is connected to the left and right engine, which lets each engine receive extinguishing agent from either bottle. Each engine has an independently operated fire extinguishing system.
WARNING: DO NOT TOUCH THE SQUIB BEFORE YOU DO THE PROCEDURES FOR DEVICES
_______ THAT ARE SENSITIVE TO ELECTROSTATIC DISCHARGE. ELECTROSTATIC DISCHARGE CAN CAUSE THE FIRE BOTTLE TO RELEASE ITS CONTENTS SUDDENLY AND CAUSE INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(2) Before you touch the squib, do the procedure for devices that are sensitive to electrostatic discharge (AMM 20-41-01/201).
B. References
(1)
AMM 20-41-01/201, Electrostatic Discharge Sensitive Devices
(2)
AMM 24-22-00/201, Electrical Power Control
C. Access
(1)
Location Zones
153 Aft Cargo Compartment (Left)
154 Aft Cargo Compartment (Right)
(2)
Access Panels
822 Aft Cargo Compartment Door
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
26-21-00
ALL ú ú 01 Page 501 ú Sep 28/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
757
MAINTENANCE MANUAL
ENGINE FIRE
EXTINGUISHING ENGINE FIRE
BOTTLES EXTINGUISHING ENGINE FIRE
SEE A AFT CARGO BOTTLE NO. 1 BOTTLE NO. 2 EXTINGUISHING
DOOR SEE B
SEE B
TO RIGHT
ENGINE
HARD POINT
CONNECTOR
TO LEFT
ENGINE
HARD POINT
CONNECTOR
A
RUPTURE
PRESSURE SWITCH DISK
SAFETY RELIEF
AND FILLER PORT
GROUND TEST
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:757 AMM 飞机维护手册 防火 FIRE PROTECTION 2(10)