B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific talcum powder Material No. 05-013A C Z-24.223 RELEASE AGENT (Ref. 20-31-00) Material No. 09-005 USA MIL-S-81733 CLASS C CORROSION INHIBITIVE INTERFAY SEALANT (Ref. 20-31-00) Material No. 11-026 GB DEF-STAN 68-148/1 SOLVENT GENERAL PURPOSE (Ref. 20-31-00) Material No. 19-003 USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
57-41-37-000-004 Removal of the Pressure-Relief Panels 521AB(621AB), 521CB(621CB), 521EB(621EB), 522AB(622AB), 522CB(622CB)
3. Job Set-up
__________
Subtask 57-41-37-941-063
A. Safety Precautions
(1)
Make sure that the safety barriers are in position.
(2)
Make sure that the TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER (98D27803500001) is installed on the flap/slat control lever.
(3)
Make sure that the warning notice is in position in the cockpit to tell persons not to operate the slats.
(4)
Make sure that the adjustable access platform is in position below the applicable pressure-relief panel to be installed.
1EFF : ALL 1 57-41-37Page 405 1 1 May 01/05R 1 1 1CES 1
Subtask 57-41-37-865-073
B. 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 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
4. Procedure
_________ R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-216,
Subtask 57-41-37-420-055
A. Installation of the Pressure-Relief Panels 521AB(621AB), 521CB(621CB), 521EB(621EB), 522AB(622AB), 522CB(622CB)
NOTE : On many of the pressure-relief panels, the screws that retain the
____ panel have different lengths. Make sure that the correct screws are installed in their correct positions.
(1)
For the panel 521AB(621AB):
(a)
Hold the panel (1) in position and install the screws (2).
(b)
TORQUE tighten the screws (2) to between 0.8 and 0.9 m.daN (70.79 and 79.64 lbf.in).
(2)
For the panel 521CB(621CB):
(a)
Hold the panel (3) in position and install the screws (4).
(b)
TORQUE tighten the screws (4) to between 0.8 and 0.9 m.daN (70.79 and 79.64 lbf.in).
(3)
For the panel 521EB(621EB):
(a)
Hold the panel (5) in position. Install the four screws (6) and the screws (7).
(b)
TORQUE tighten the screws (6) and (7) to between 0.8 and 0.9 m.daN (70.79 and 79.64 lbf.in).
(4)
For the panel 522AB(622AB):
(a)
Hold the panel (8) in position. Install the five screws (9) and the screws (10).
(b)
TORQUE tighten the screws (9) and (10) to between 0.8 and 0.9 m.daN (70.79 and 79.64 lbf.in).
(5)
For the panel 522CB(622CB):
(a)
Hold the panel (11) in position. Install the screw (12) and the screws (13).
(b)
TORQUE tighten the screws (12) and (13) to between 0.8 and 0.9 m.daN (70.79 and 79.64 lbf.in).
R **ON A/C 106-149, 217-299, 301-399, 401-499,
Subtask 57-41-37-420-055-A
A. Installation of the Pressure-Relief Panels 521AB(621AB), 521CB(621CB), 521EB(621EB), 522AB(622AB), 522CB(622CB)
NOTE : On many of the pressure-relief panels, the screws that retain the
____ panel have different lengths. Make sure that the correct screws are installed in their correct positions.
(1)
For the panel 521AB(621AB):
(a)
Hold the panel (1) in position and install the screws (2).
(b)
TORQUE tighten the screws (2) to between 0.45 and 0.5 m.daN
(39.82 and 44.24 lbf.in).
(2)
For the panel 521CB(621CB):
(a)
Hold the panel (3) in position and install the screws (4).
(b)
TORQUE tighten the screws (4) to between 0.45 and 0.5 m.daN
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM WINGS 機(jī)翼2(132)
