-
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.
Details of the Proximity-Sensors 37CV (38CV), 39CV (40CV)
Figure 403/TASK 27-51-44-991-003
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 27-51-44Page 426 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1R Details of the Proximity-Sensors 37CV (38CV), 39CV (40CV) R Figure 403A/TASK 27-51-44-991-003-A
1EFF : 301-399, 1 27-51-44Page 427 1 1 May 01/04 1 1 1CES 1R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 27-51-44-020-051
A. Removal of the Proximity Sensor
(1)
Disconnect the applicable electrical connector(s) (11) and/or (12).
(2)
Put blanking caps on the applicable electrical connector(s) (10) and/or (13).
(3)
Remove the applicable proximity sensor (1):
FOR 37CV, 38CV
(a)
Remove the nuts (2), the bolts (5) and the washers (4).
(b)
Remove the proximity sensor (1) from the bracket (3).
(4)
Remove the applicable proximity sensor (14):
FOR 39CV, 40CV
(a) Remove the nuts (9), the bolts (6) and the washers (7).
(b) Remove the proximity sensor (14) from the bracket (8).
**ON A/C 301-399,
Subtask 27-51-44-020-051-A
A. Removal of the Proximity Sensor
(1)
Disconnect the applicable electrical connector(s) (12) and/or (13).
(2)
Put blanking caps on the applicable electrical connector(s) (9) and/or (10).
(3)
Remove the applicable proximity sensor (1):
FOR 37CV, 38CV
(a)
Remove the nuts (2), the bolts (5) and the washers (4).
(b)
Remove the proximity sensor (1) from the bracket (3).
R (4) Remove the applicable proximity sensor (14):
R FOR 39CV, 40CV
R (a) Remove the nuts (11), the bolts (6) and the washers (7).
R (b) Remove the proximity sensor (14) from the bracket (8).
R **ON A/C ALL
TASK 27-51-44-400-002
Installation of the Proximity-Sensor 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 -------------------------------------------------------------------------------
No specific safety barriers
No specific warning notice
No specific access platform 3.5 m (11 ft. 6 in.)
98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
FOR FIN 39CV, 40CV
98D27504031000 1 PIN-SETTING
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-026 GB DEF-STAN 68-148/1
SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-00-00-480-002 Installation of the Flap/Slat Control-Lever Locking
Tool (98D27803000000) 27-50-00-866-009 Retraction of the Flaps on the Ground 27-51-00-710-002 Operational Test of the Flap Interconnecting Strut
and the Flap-Attachment Failure-Detection Sensors 27-54-61-000-002 Removal of the Flap Kink-Seals 27-54-61-400-006 Installation of the Flap Kink-Seals
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