(69)
Push and hold the MEM READ button.
S 985-080
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S 985-081
(70)
Release the LOC TEST button. S 985-082
(71)
Release the MEM READ button. S 285-083
(72)
Make sure code 97 is shown. NOTE: Code 97 displays for 1 minute.
____
S 985-038
(73) Push and release the MEM CLR button while code 96 is shown. NOTE: If step 3.C.(71) is missed do the procedure again from
____
3.C.(63) to 3.C.(70).
S 285-039
(74)
Make sure code 25 or 75 is shown. S 985-040
(75)
Push and release the MEM CLR button. S 285-041
(76)
Make sure the display is blank. S 985-042
(77)
Push and release the MEM READ button. S 285-043
(78)
Make sure code 25 or 75 is shown. S 985-044
(79)
Push and release the MEM CLR button.
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S 285-045
(80)
Make sure the display is blank.
S 985-046
(81)
Push and release the MEM READ button.
S 285-047
(82)
Make sure code 97 is shown.
S 985-048
(83)
Push and release the MEM READ button.
S 285-049
(84)
Make sure the display is blank.
S 865-040
(85)
Remove the DO-NOT-CLOSE tags and close these circuit breakers on the P6 panel.
(a)
6C1 L FUEL COND CONT
(b)
6C2 R FUEL COND CONT
E. Put the airplane back to its initial condition.
S 865-050
(1)
Close the cover on the electrical system card file, P50.
(2)
Remove electrical power if it is not necessary (AMM 24-22-00/201).
S 865-015
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DUCT LEAK DETECTOR - REMOVAL/INSTALLATION
_________________________________________
1. General (Fig. 401)_______
A. Duct leak detectors are installed next to the pneumatic air ducts in the wings and in the fuselage.
B. The removal/installation procedure is the same for all units except for access to the units.
TASK 26-18-01-024-031
2. Remove Duct Leak Detector_________________________
A. Equipment
(1)
Main Gear Door Locks (AMM 32-00-15/201)
(2)
Caps to fit 35303-64 connectors
(3)
Bonding Meter, AVTRON T477W
B. References
(1)
AMM 06-41-00/201, Fuselage Access Doors and Panels
(2)
AMM 06-42-00/201, Empennage Access Doors and Panels
(3)
AMM 06-44-00/201, Wing Access Doors and Panels
(4)
AMM 25-50-02/401, Cargo Compartment Sidewall Panels
(5)
AMM 32-00-15/201, Landing Gear Door Locks
(6)
AMM 32-00-20/201, Landing Gear Downlocks
C. Access
(1) Location Zones
133/134 Wing Center Section (Left and Right)
310 Fuselage Body Section 48
500/600 Wing (Left and Right)
730/740 Main Landing Gear Wheel Well
D. Prepare for Removal of the Wing Detectors (Fig. 402) 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(3)
