(b)
 If the distance 'D' is not in tolerance then you must replace the ram-air outlet (Ref. TASK 21-61-52-000-003) and (Ref. TASK 21-61-52-400-003) before you do the next work steps.

 (c)
 If the distance 'D' is in tolerance continue with the next work steps.

 (8)
 TORQUE the nut (6) to between 0.63 and 0.77 m.daN (55.75 and 68.14
 lbf.in).

 (9)
 Remove the blanking caps from the disconnected electrical connectors.

 (10) Make sure that the electrical connectors are clean and in the correct condition.
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 (11)
 Connect the electrical connector (3).

 (12)
 Make sure that the work area is clean and clear of tool(s) and other items.

 Subtask 21-61-52-865-059
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
 FOR 9HH
 1HH, 2HH, 3HH, 4HH.

 FOR 29HH
 21HH, 22HH, 23HH, 24HH.

 Subtask 21-61-52-710-052
 C. Positioning of the Ram-Air Outlet Flap
 (1) For this test we recommend two persons with interphone communication. One person in the cockpit to monitor the test and one person at the related air outlet to measure the outlet flap gap.
 WARNING : KEEP AWAY FROM THE PARTS OF THE RAM AIR OUTLET FLAPS THAT
_______ MOVE. THESE CAN CAUSE INJURY TO PERSONS, AND/OR DAMAGE TO EQUIPMENT.
 (2) In the cockpit do the operational test of the pack
 temperature-control system (Ref. TASK 21-61-00-710-001).

 NOTE : The purpose of this test is to get movement of the ram-air
____ outlet flap. During the test the ram-air outlet flap positions are as follows:
 -
movement to the fully retracted position,

 -
movement to the fully open position,

 -
movement to the fully retracted position (the flap is stopped in this position for apprx. 30 seconds).

 -
movement to the flight open position,

 -
movement to the pack off position.

 (3) The person at the ram-air outlet flap must tell the person in the cockpit when the ram-air outlet flap is stopped in the fully retracted position.
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 (4) The person in the cockpit must then do the work step which follows.
 NOTE : The test is stopped when you do this.
____ You can ignore this for this part of the procedure.
 Subtask 21-61-52-865-065
 D. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 9HH
 122VU AIR COND/PACK TEMP/CTL SYS1/1/115VAC 1HH X22 122VU AIR COND/PACK TEMP CTL SYS2/1/115VAC 2HH Y18
 FOR 29HH 122VU AIR COND/PACK TEMP/CTL SYS1/2/115VAC 21HH W22 122VU AIR COND/PACK TEMP CTL SYS2/2/115VAC 22HH Y20
 Subtask 21-61-52-220-051
 E. Flap Measurement
 (1)
 At the ram-air outlet flap make sure that the flap is flush with the aircraft surface to 3.0 mm (0.1181 in.) at dimension 'B'.

 (2)
 In the cockpit do the work step which follows.

 Subtask 21-61-52-865-066
 F. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 9HH
 122VU AIR COND/PACK TEMP/CTL SYS1/1/115VAC 1HH X22 122VU AIR COND/PACK TEMP CTL SYS2/1/115VAC 2HH Y18
 FOR 29HH 122VU AIR COND/PACK TEMP/CTL SYS1/2/115VAC 21HH W22 122VU AIR COND/PACK TEMP CTL SYS2/2/115VAC 22HH Y20
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 G. Test
 (1) Do the operational test of the pack temperature-control system (Ref. TASK 21-61-00-710-001).
 5. Close-up
________ Subtask 21-61-52-410-055
 A. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Install the access panel (Ref. TASK 53-35-13-400-002).

 FOR 9HH
 Close 191KB
 FOR 29HH

 Close 192KB Subtask 21-61-52-862-054
 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
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