Interconnecting Strut - Location and Detail
Figure 401/TASK 27-51-44-991-001
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-51-44Page 403 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1R Interconnecting Strut - Location and Detail R Figure 401A/TASK 27-51-44-991-001-A
R 1EFF : 301-399, 1 27-51-44Page 404 1 1 May 01/04 1 1 1CES 1 Subtask 27-51-44-860-052
B. Aircraft Maintenance Configuration
(1)
Extend the flaps to position 1 (Ref. TASK 27-50-00-866-008).
(2)
Install the LOCKING TOOL - FLAP/SLAT CONTROL LEVER (98D27803000000) on the flap/slat control lever (Ref. TASK 27-00-00-480-002).
Subtask 27-51-44-865-059
C. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/FLP/CTL AND MONG/SYS1 6CV B07 121VU FLIGHT CONTROLS/FLP/CTL AND/MONG/SYS2 8CV Q21
Subtask 27-51-44-010-056
D. Get Access
(1)
Put the access platform in position:
-
for the left wing, below zone 580
-
for the right wing, below zone 680.
(2)
Remove the lower kink seal, the cushion seals and the upper kink seals from the flaps (Ref. TASK 27-54-61-000-002).
4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
(Ref. Fig. 401/TASK 27-51-44-991-001)
**ON A/C 301-399,
(Ref. Fig. 401A/TASK 27-51-44-991-001-A) **ON A/C ALL
CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING
_______
EDGE:
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
-MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-51-44-020-050
A. Removal of the Interconnecting Strut
(1)
Remove the electrical connectors (10) and (11) from the connectors
(9) and (8) on the inboard flap.
(2)
Put blanking caps on the disconnected electrical connectors.
(3)
Remove and discard the cotter pins (7) and (12).
(4)
Hold the interconnecting strut (1).
(5)
Remove the nuts (6) and (13) and the washers (5) and (14).
(6)
Remove the bolts (2) and (15) and remove the interconnecting strut (1).
(7) Remove the washer (3) and the bush (4).
**ON A/C 301-399,
Subtask 27-51-44-020-050-A
A. Removal of the Interconnecting Strut
(1)
Remove the electrical connectors (14) and (15) from the connectors
(12) and (13) on the inboard flap.
(2)
Put blanking caps on the disconnected electrical connectors.
(3)
Remove the nuts (10), the bolts (5) with the washers (6) and remove the failsafe bracket (9).
R (4) Remove and discard the cotter pins (2) and (17).
R (5) Hold the interconnecting strut (1).
R (6) Remove the nuts (3) and (16) and the washers (4) and (18).
R (7) Remove the bolts (11) and (19) and remove the interconnecting strut
R (1).
R (8) Remove the guide washer (7) and the bush (8).
R 1EFF : 301-399, 1 27-51-44Page 407 1 1 May 01/04 1 1 1CES 1R **ON A/C ALL
TASK 27-51-44-400-001
Installation of the Interconnecting Strut
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______
NOTICES ARE IN POSITION.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
_______
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.
-
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.
-MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
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