ENGINE 2 THR REV CONT SYS
3) ENGINE 1 THR REV IND SYS
ENGINE 2 THR REV IND SYS 4) LANDING GEAR AIR/GND RELAY & LIGHTS 5) ENGINES MASTER CAUTION 6) MASTER CAUTION ANNUNCIATOR NO. 1 7) MASTER CAUTION ANNUNCIATOR BAT 8) DIM & TEST 9) SECT 1, SECT 2, SECT 3, SECT 4, SECT 5, SECT 6 10) INDICATOR MASTER DIM BUS BAT, NO. 1 DC and NO. 2 DC
(b)
On circuit breaker panel P18:
1) RADIO ALTM-1
(c)
For engine No. 1, make sure these circuit breakers are closed: 1) ENG 1 SYNC LOCK
(d)
For engine No. 2, make sure these circuit breakers are closed: 1) ENG 2 SYNC LOCK 2) ENG 2 SYNC LOCK - ALTN 3) ENG 2 THR REV CONT SYS - ALTN
S 845-010-C00
WARNING: KEEP PERSONS AND EQUIPMENT CLEAR OF THE FLIGHT CONTROL
_______ SURFACES, THE THRUST REVERSERS, AND THE LANDING GEAR. THESE COMPONENTS CAN MOVE SUDDENLY WHEN YOU SUPPLY HYDRAULIC POWER. THIS CAN CAUSE INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT.
CAUTION: DO NOT OPERATE HYDRAULIC SYSTEM "A" OR "B" ON AIRCRAFT ELECTRIC
_______ PUMPS MORE THAN 2 MINUTES UNLESS THE NO. 1(2) FUEL TANK CONTAINS MORE THAN 250 GALLONS OF FUEL. DAMAGE TO EQUIPMENT CAN OCCUR. IF PUMPS ARE OPERATED 2 MINUTES WITHOUT FUEL IN THE TANKS, ALLOW THE RESERVOIR TO COOL TO AMBIENT TEMPERATURE BEFORE RESUMING TEST.
(9) If it is necessary, supply the hydraulic power using either a test bench or aircraft electric pumps (AMM 29-15-00/201).
(a) Set bench flow rate to 7.0 (+/- 0.5) gallons (26-27 liter) per minute and 2800 (+/- 50) psig.
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78-31-00
ALL ú ú C01A Page 502 ú Mar 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
(b)
For engine No. 1:
1) Pressurize system A.
(c)
For engine No. 2:
1) Pressurize system B.
TASK 78-31-00-735-011-C00
3. Fire Shut-Off Test__________________
A. Access
(1)
Location Zones
504/604 Thrust Reverser - Left
505/605 Thrust Reverser - Right
101 Control Cabin - Left
102 Control Cabin - Right
B.
Procedure
S 845-211-C00
(1) If not already done, do the paragraph: Prepare for the System Tests.
S 865-212-C00
CAUTION:_______DO NOT TURN THE HANDLE. THE FIRE EXTINGUISHING AGENT WILL BE DISCHARGED.
(2)
Pull the engine No. 1 fire switch handle on the engine and APU fire control module with the lock override under the handle.
S 865-213-C00
(3)
Slowly move the engine No. 1 reverse thrust lever up and aft to the extended position.
(a) Make sure that the reverser sleeves do not extend.
S 865-214-C00
(4) Move the engine No. 1 reverse thrust lever forward and down to the stowed position.
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78-31-00
ALL ú ú C01A Page 503 ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
S 865-215-C00
(5) Reset the fire switch handle of engine No. 1.
S 865-207-C00
CAUTION:_______DO NOT TURN THE HANDLE. THE FIRE EXTINGUISHING AGENT WILL BE DISCHARGED.
(6)
Pull the engine No. 2 fire switch handle on the engine and APU fire control module with the lock override under the handle.
S 865-206-C00
(7)
Slowly move the engine No. 2 reverse thrust lever up and aft to the extended position.
(a) Make sure that the reverser sleeves do not extend.
S 865-208-C00
(8)
Move the engine No. 2 reverse thrust lever forward and down to the retracted position.
S 865-209-C00
(9)
Reset the fire switch handle of engine No. 2.
S 845-210-C00 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 EXHAUST(33)
