(1)
Install the cable (15) or (16).
(2)
Remove the blanking caps from the connectors (23) and (24).
(3)
Install the connector (23) in the flanged attachment (21).
(4)
Install the nut (20) on the connector (23).
(5)
TORQUE the nut (20) to between 0.56 and 0.68 m.daN (49.55 and 60.17 lbf.in).
(6)
For the cable 25HF(41HF):
-connect the connector (24) to the connector (22).
(7)
For the cable 52HF(68HF):
-connect the connector (19) to the connector (23).
(8)
TORQUE the connectors (19) and (23) to between 0.56 and 0.68 m.daN
(49.55 and 60.17 lbf.in).
(9)
Safety the connectors (19), (22), (23) and (24) and the nuts (20) with MISCELLANEOUS (Material No. 19-010).
(10) Cut the cable (15) or (16) to the correct length and connect it to
the electrical cable (15) or (16) with the in-line splice R NSA936809RG0001 (Ref. ESPM 204312).
(11)
Install the cable (15) or (16) in the applicable electrical raceway:
-
FOR 25HF, 41HF
in route 1S
-
FOR 52HF, 68HF
in route 2S.
(12)
Install the clamps (33) on the cable (15) or (16) and install the bolts (35).
Subtask 36-22-16-865-076
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 3HA1, 2HA1, 3HA2, 2HA2.
Subtask 36-22-16-710-056
D. Test
(1) Do an operational test of the overheat detection system (Ref. TASK 36-22-00-710-001).
5. Close-up
________ Subtask 36-22-16-410-056
A. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Install the applicable access panels:
-
FOR 25HF, 52HF
install 522EB, 522FB
-
FOR 41HF, 68HF
install 622EB, 622FB.
Subtask 36-22-16-865-077
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
Subtask 36-22-16-860-076
C. Aircraft Configuration
(1) Fully retract the slats (Ref. TASK 27-80-00-866-005). Subtask 36-22-16-942-056
D. Removal of Equipment
(1)
Remove the safety barriers.
(2)
Remove the warning notice(s).
(3)
Remove the access platform(s).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
1EFF : ALL 1 36-22-16Page 448 1 1 May 01/05R 1 1 1CES 1
TASK 36-22-16-000-004
Removal of the Overheat Sensing Elements 26HF(42HF),53HF(69HF)
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______
START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______
GEAR.
1. Reason for the Job
__________________
R R Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s)
No specific safety barriers
No specific warning notice
No specific access platform 3.6 m (11 ft. 10 in.)
98D27803000000 1 LOCKING TOOL - FLAP/SLAT CONTROL LEVER
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-80-00-866-004
57-41-37-000-003 R 57-41-37-000-004 R R R 57-41-37-000-006 R R R
36-22-16-991-001
36-22-16-991-002 R 36-22-16-991-003 R 36-22-16-991-004 R 36-22-16-991-005
3. Job Set-up
__________
Extending the Slats on the Ground
Removal of the Access Panel 522AT(622AT)
Removal of the Pressure-Relief Panels 521AB(621AB),
521CB(621CB), 521EB(621EB), 522AB(622AB),
522CB(622CB)
Removal of the Access Panels 522FB(622FB),
522JB(622JB), 522KB(622KB), 522LB(622LB),
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM PNEUMATIC 气源 2(128)
