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S 214-015
(5) Inspect the supply duct assembly and the shroud assembly (AMM 30-21-04/601).
TASK 30-21-04-024-033
3. Remove The Engine TAI Pressure Indicator________________________________________
A. Access
(1) Location Zones
413 No. 1 Power Plant
423 No. 2 Power Plant
B. Prepare to Remove the Engine TAI Pressure Indicator (Fig. 405)
S 034-034
(1)
Remove the screws that attach the access panel to the inlet cowl.
S 014-035
(2)
Remove the access panel.
C. Remove the Engine TAI Pressure Indicator (Fig. 405)
S 034-036
(1)
Disconnect the pipe from the pressure indicator.
S 034-037
(2)
Cut and discard the lockwire between the pressure indicator and the lock tab.
S 034-038
(3)
Release the nut and remove the pressure indicator.
S 024-039
(4)
ENGINES WITH SB 71-9850; Remove and keep the shim washer for use during the installation.
S 424-040
(5)
Install approved caps on all openings.
TASK 30-21-04-424-016
4. Install the Engine to TAI Ring Duct___________________________________
A. Reference
(1)
70-12-02/201, Fitting Vee-Bank Coupling Clamps
(2)
70-51-00/201, Torque Tightening Technique
(3)
71-11-04/201, Fan Cowl Panels
(4)
78-31-00/201, Thrust Reverser System
B. Access
(1) Location Zones
413 No. 1 Power Plant
423 No. 2 Power Plant
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. RB211-535E4 ENGINES WITH TAI DUCT BURST ú
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(2) Access Panels
413AL Engine Fan Cowl
423AL Engine Fan Cowl
C. Procedure
S 034-017
(1) Remove the caps from the openings.
S 424-018
CAUTION: YOU MUST BE CAREFUL TO NOT DAMAGE THE PISTON SEALS DURING
_______ INSTALLATION. THE SEALS ARE EASILY DAMAGED IF NOT HANDLED CAREFULLY.
(2)
Carefully install the supply duct assembly (2) (Fig. 404).
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本文链接地址：757 AMM 飞机维护手册 防冰和排雨 CHAPTER 30 - ICE AND RAIN PROTECTION(72)
