-
between the FR65 and FR70 remove partition panel 161DW (Ref. TASK 25-55-12-000-001).
R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 36-12-00Page 514 1 1 May 01/05 1 1 1CES 1
(5) Get access to the APU bleed-air duct aft of FR70.
(a)
Put the access platform below the rear fuselage.
(b)
Open the applicable access door for the APU bleed-air ducts:
-between the FR70 and FR77
open the access door 312AR,
-aft of FR77
open the access door 314AR.
R **ON A/C 151-199, 401-499,
Subtask 36-12-00-010-052-A
A. Get Access R **ON A/C 151-199,
(Ref. Fig. 501A/TASK 36-12-00-991-001-A) R **ON A/C 151-199, 401-499,
NOTE : Remove only the related access panels in the area where you will
____
do the leak test.
(1)
Get access to the APU bleed-air ducts between FR35 and FR36.
(a)
Put the access platform in position below the access panels 191BB and 191EB.
(b)
Remove the access panels 191BB and 191EB.
(2)
Get access to the APU bleed-air ducts between FR36 and FR42.
(a)
Put the access platform in position below the access panel 191JB.
(b)
Remove the access panel 191JB.
(3)
Get access to the APU bleed-air ducts between FR42 and FR50.
(a)
Put the access platform in position below the access panels 147AB, 147EB, 147FB and 197BB.
(b)
Remove the access panels 147AB, 147EB, 147FB and 197BB.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 36-12-00Page 515 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1
APU Bleed Air Ducts - Access
Figure 501A/TASK 36-12-00-991-001-A
R 1EFF : 151-199, 1 36-12-00 Page 516
1 1 May 01/05
1 1
1CES 1
(4)
Get access to the APU bleed-air ducts between FR46 and FR70 from the AFT cargo compartment.
(a)
Open the AFT cargo compartment door (Ref. TASK 52-30-00-860-001).
(b)
Remove the applicable access panels for the APU bleed-air ducts:
-
between the FR46 and FR53 remove the partition panel 151BW (Ref. TASK 25-55-11-000-001) and remove the access panel 151SW
-
between the FR53 and FR56
remove the access panel 151TW
-
between the FR56 and FR58
remove the access panel 151UW
-
between the FR58 and FR59
remove the access panel 151VW
-
between the FR59 and FR62
remove the access panel 161AW
-
between the FR62 and FR63
remove the access panel 161BW
-
between the FR63 and FR65
remove the access panel 161CW
-
between the FR65 and FR70 remove the partition panel 161DW (Ref. TASK 25-55-12-000-001).
(5)
Get access to the APU bleed-air duct aft of FR70.
(a)
Put the access platform below the rear fuselage.
(b)
Open the applicable access door for the APU bleed-air ducts:
-between the FR70 and FR77
open the access door 312AR,
-aft of FR77
open the access door 314AR.
R 1EFF : 151-199, 401-499, 1 36-12-00Page 517 1 1 Aug 01/05 1 1 1CES 1 **ON A/C 301-399,
Subtask 36-12-00-010-052-B
A. Get Access NOTE : Remove only the related access panels in the area where you will
____
do the leak test.
(1)
Get access to the APU bleed-air ducts between FR35 and FR36.
(a)
Put the access platform in position below the access panels 191BB and 191EB.
(b)
Remove the access panels 191BB and 191EB.
(2)
Get access to the APU bleed-air ducts between FR36 and FR42.
(a)
Put the access platform in position below the access panel 191JB.
(b)
Remove the access panel 191JB.
(3)
Get access to the APU bleed-air ducts between FR42 and FR50.
(a)
Put the access platform in position below the access panels 147AB, 147EB, 147FB and 197BB.
(b)
Remove the access panels 147AB, 147EB, 147FB and 197BB.
(4)
Get access to the APU bleed-air ducts between FR46 and FR70 from the AFT cargo compartment.
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(63)
