S 415-029
(19)
Put the cap on the fitting.
F. Put the Airplane Back In Its Usual Condition.
S 445-005
(1)
Put the safety-sensitive systems back to their initial conditions (AMM 32-09-02/201).
S 095-030
(2)
Remove the pneumatic power source and the opposite pneumatic service outlet blocking device, if it is not necessary (AMM 36-00-00/201).
S 415-031
(3)
Install the fixed upper wing panel 522BL (AMM 06-44-00/201).
S 415-032
(4)
Install the fixed lower wing panel 521AB (AMM 06-44-00/201).
S 445-034
(5)
Do the activation procedure for the thrust reverser
(AMM 78-31-00/201).
NOTE: If you plan to do the next task in this procedure (the test
____ for the right wing TAI system), do not do this step.
S 865-033
(6) Remove electrical power if it is not necessary (AMM 24-22-00/201).
TASK 30-11-00-735-035
3. Test - Right Wing TAI System
____________________________
A. Equipment
(1)
Timing Device - 15 seconds minimum
(2)
Ground Air Supply (80 lbs/min at 13 to 20 psig)
(3)
Pressure Gage - 0-50 psig |1% accuracy with hose and fittings
B. References
(1)
AMM 06-44-00/201, Wings (Major Zones 500 and 600) Access Doors and Panels
(2)
AMM 24-22-00/201, Electrical Power - Control
(3)
AMM 31-41-00/201, Engine Indication and Crew Alerting System (EICAS)
(4)
AMM 32-09-02/201, Air/Ground Relays
(5)
AMM 36-00-00/201, Pneumatic - General
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
30-11-00
ALL ú ú 02 Page 507 ú Dec 20/94
A
757
MAINTENANCE MANUAL
(6) AMM 78-31-00/201, Thrust Reverser System
C. Access
(1)
Location Zones
621 Leading edge to Front Spar (Right)
622 Slat No. 7 (Right)
(2)
Access Panels
621AB Fixed lower wing panel
622BR Fixed upper wing panel
D. Prepare for the Test (Fig. 501)
S 865-036
WARNING: DO THE THRUST REVERSER DEACTIVATION PROCEDURE TO PREVENT THE
_______ OPERATION OF THE THRUST REVERSER. ACCIDENTAL OPERATION OF THE THRUST REVERSER CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
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