S 434-011-C02
(12)
If you remove an inboard thrust reverser half, wrap a protective mat around the wing leading edge adjacent to the thrust reverser half.
S 434-012-C02
(13)
Attach the mat to the leading edge with tape.
S 014-012-C02
WARNING: OBEY THE INSTRUCTIONS IN THE PROCEDURE TO OPEN THE THRUST
_______ REVERSERS. IF YOU DO NOT OBEY THE INSTRUCTIONS, INJURIES TO PERSONS AND DAMAGE TO EQUIPMENT CAN OCCUR.
(14) Open the thrust reverser (AMM 78-31-00/201).
Thrust Reverser Hinge Fitting Seal Support Installation Figure 401
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
COWL/REVERSERS USED ON STRUTS WITH ú 78-31-01
VIBRATION ISOLATOR SUSPENSION AND ú CONFIG 2 WITH HINGE CROSS RODS ú C02 Page 403 (AIRPLANES PRE-BOEING-SB 737-54-1036) 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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.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 034-014-C02
(15) Remove these items at the aft hinge fitting (View E, Fig. 402) as follows:
NOTE:____ Keep the forward and aft halves of the slider together as a
set. The slider halves must be examined for wear before you
install them again. The minimum distance between the curved
surfaces of the hinge slider is 0.978 inch (24.84 mm).
NOTE:____ If you install the same thrust reverser again, measure
the distance between the inner curved surfaces of the hinge
track fitting. The maximum permitted distance between the
curved surfaces is 1.067 inches (27.10 mm), (Fig. 402, sheet
6). The maximum permitted gap between the hinge slider and
the hinge track is 0.067 inch (1.70 mm).
(a)
Remove the forward half of the slider.
(b)
Remove the aft half of the slider with the eccentric pins attached.
S 954-015-C02
(16) Apply masking tape along the seal segments on the primary sleeve assembly.
S 414-109-C02
CAUTION: MAKE SURE THERE IS PROPER CLEARANCE BETWEEN THE THRUST REVERSER
_______ AND THE SEAL SEGMENTS OF THE PRIMARY SLEEVE ASSEMBLY WHEN YOU CLOSE THE THRUST REVERSER HALF. DAMAGE TO EQUIPMENT CAN OCCUR.
(17)
Close but do not latch the thrust reverser half (AMM 78-31-00/201).
S 034-017-C02
(18)
Disconnect the opening actuator of the thrust reverser from the upper attach fitting on the reverser (View B, Fig. 402).
S 434-018-C02
(19)
Secure the upper end of the opening actuator to the engine with string to make sure it is clear of the thrust reverser.
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
COWL/REVERSERS USED ON STRUTS WITH ú 78-31-01
VIBRATION ISOLATOR SUSPENSION AND ú CONFIG 2 WITH HINGE CROSS RODS ú C01 Page 404 (AIRPLANES PRE-BOEING-SB 737-54-1036) ú Jul 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
SEE A
COMPRESSION PADS AFT UPPER
SEE D SEE C
SEE E
(INBOARD HALF ONLY) DOOR DEFLECTORS FLAP SEAL
UPPER BIFURCATION
FORWARD UPPER COMPRESSION PAD
SEE B
LOWER BIFURCATION
LOWER COMPRESSION PADS (LEFT HALF ONLY)
A
Thrust Reverser Installation
Figure 402 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù.
COWL/REVERSERS USED ON STRUTS WITH ú 78-31-01
VIBRATION ISOLATOR SUSPENSION AND ú CONFIG 2
WITH HINGE CROSS RODS ú C01 Page 405
(AIRPLANES PRE-BOEING-SB 737-54-1036) ú Jul 12/00
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