-
FOR 24HF, 51HF
panel 522AB
-
FOR 40HF, 67HF
panel 622AB.
Subtask 36-22-16-865-062
C. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/SLT/CTL AND MONG/SYS1 5CV B06 49VU AIR BLEED/ENG 1/CTL 3HA1 D12 49VU AIR BLEED/ENG 1/MONG 2HA1 D11 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21 122VU AIR BLEED/ENG 2/CTL 3HA2 Z23 122VU AIR BLEED/ENG 2/MONG 2HA2 Z22
4. Procedure
_________
(Ref. Fig. 404/TASK 36-22-16-991-004, 405/TASK 36-22-16-991-005)
Subtask 36-22-16-420-059
A. Preparation for Installation
(1)
Clean the component interface and/or the adjacent area with a MISCELLANEOUS (Material No. 19-003) made moist with CLEANING AGENTS (Material No. 11-026).
(2)
Do an inspection of the component interface and/or the adjacent area.
(3)
Make sure that the parts retained from the removed component are clean and in the correct condition.
(4)
Examine the cable (13) and/or (18) for the correct condition.
(5)
Remove the blanking caps from the cable (13) or (18) connectors and examine the connectors for the correct condition. Put the blanking caps on the connectors again.
Subtask 36-22-16-420-052
R B. Installation of the Cables
CAUTION : REFER TO THE MATCH MARKS MADE DURING THE REMOVAL WHEN YOU
_______ CONNECT THE ELECTRICAL WIRES. INCORRECT CONNECTION OF THE WIRES WILL CAUSE DAMAGE TO EQUIPMENT.
(1)
Install the cable (13) or (18).
(2)
Remove the blanking caps from the connectors (19) and (23).
(3)
For the cable 24HF(40HF):
(a)
Install the connector (23) in the flanged attachment (21)
(b)
Install the nut (20) on the connector (23).
(c)
TORQUE the nut (20) to between 0.56 and 0.68 m.daN (49.55 and
60.17 lbf.in)
(d)
Install the connector (19) on the connector (23). (e) TORQUE the connector (19) to between 0.56 and 0.68 m.daN (49.55 and 60.17 lbf.in).
(4)
For the cable 51HF(67HF):
(a)
Install the connector (24) in the connector (22).
(b)
TORQUE the connector (24) to between 0.56 and 0.68 m.daN (49.55 and 60.17 lbf.in).
(5)
Safety the connectors (19), (23) and (24) and the nut (20) with MISCELLANEOUS (Material No. 19-010).
(6)
Cut the cable (13) or (18) to the correct length and connect it to
the electrical cable with the in-line splice NSA936809RG0001 (Ref. R ESPM 204312).
(7)
Install the cable (13) or (18) in the applicable electrical raceway:
-
FOR 24HF, 51HF
in route 1S
-
FOR 40HF, 67HF
in route 2S.
(8)
Install the clamps (33) on the cable (13) or (18) and install the bolts (35).
Subtask 36-22-16-865-063
C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 3HA1, 2HA1, 3HA2, 2HA2.
Subtask 36-22-16-710-052
D. Test
(1) Do an operational test of the overheat detection system (Ref. TASK 36-22-00-710-001).
5. Close-up
________ Subtask 36-22-16-410-052
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 24HF, 51HF
install 522AB
-
FOR 40HF, 67HF
install 622AB.
Subtask 36-22-16-865-064
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 5CV, 7CV.
Subtask 36-22-16-860-068
C. Aircraft Configuration
(1) Retract the slats fully (Ref. TASK 27-80-00-866-005). Subtask 36-22-16-942-052
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 439 1 1 May 01/05R 1 1 1CES 1
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