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**ON A/C ALL
5. Close-up
________ **ON A/C 001-049, 101-105, 151-199, 201-210,
Subtask 36-12-00-860-059-A
A. Put the aircraft back to the serviceable condition.
(1)
On the AIR COND panel 30VU, push the APU BLEED pushbutton switch (the OFF legend comes on).
(2)
Shut down the APU (Ref. TASK 49-00-00-860-009).
(3)
On the AIR COND panel 30VU, set the X-BLEED selector switch in the AUTO position.
(4)
Do the EIS stop procedure
(Ref. TASK 31-60-00-860-002).
(5)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
**ON A/C 051-099,
Subtask 36-12-00-860-059
A. Put the aircraft back to the serviceable condition.
(1)
On the AIR COND panel 30VU, push the APU BLEED pushbutton switch (the OFF legend comes on).
(2)
Shut down the APU (Ref. TASK 49-00-00-860-004).
(3)
On the AIR COND panel 30VU, set the X-BLEED selector switch in the AUTO position.
(4)
Do the EIS stop procedure
(Ref. TASK 31-60-00-860-002).
(5)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
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R **ON A/C 106-149, 211-299, 301-399, 401-499,
Subtask 36-12-00-860-059-B
A. Put the aircraft back to the serviceable condition.
(1)
On the AIR COND panel 30VU, push the APU BLEED pushbutton switch (the OFF legend comes on).
(2)
Shut down the APU (Ref. TASK 49-00-00-860-006).
(3)
On the AIR COND panel 30VU, set the X-BLEED selector switch in the AUTO position.
(4)
Do the EIS stop procedure
(Ref. TASK 31-60-00-860-002).
(5)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
**ON A/C 001-049, 051-099, 101-149, 201-299,
Subtask 36-12-00-410-052
B. Close Access
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
For the APU bleed-air ducts between FR35 and FR36:
(a)
Install the access panels 191BB and 191EB.
(b)
Remove the access platform from below the access panels 191BB and 191EB.
(3)
For the APU bleed-air ducts between FR36 and FR42:
(a)
Install the access panel 191JB.
(b)
Remove the access platform from below the access panel 191JB.
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(4)
For the APU bleed-air ducts between FR42 and FR50:
(a)
Install the access panels 147AB, 147EB, 147FB and 197BB.
(b)
Remove the access platform from below the access panels 147AB, 147EB, 147FB and 197BB.
(5)
For the APU bleed-air ducts between the FR46 and FR47:
(a) Install the partition panel 151BW (Ref. TASK 25-55-11-400-001).
(6)
For the APU bleed-air ducts between the FR47 and FR49:
-Install the access panel 151CW.
(7)
For the APU bleed-air ducts between the FR49 and FR52:
-Install the access panel 151DW.
(8)
For the APU bleed-air ducts between the FR52 and FR55:
-Install the access panel 151EW.
(9)
For the APU bleed-air ducts between the FR55 and FR58:
-Install the access panel 151HW.
(10)
For the APU bleed-air ducts between FR58 and FR59:
-Install the access panel 151JW.
(11)
For the APU bleed-air ducts between the FR59 and FR62:
-Install the access panel 161AW.
(12)
For the APU bleed-air ducts between the FR62 and FR63:
-Install the access panel 161BW.
(13)
For the APU bleed-air ducts between the FR63 and FR65:
-Install the access panel 161CW.
(14) 中國航空網(wǎng) m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM PNEUMATIC 氣源 2(65)
