(c)
Remove the cotter pins (406) and (457) and discard them.
(d)
Remove the nuts (405) and (456), the washers (418) and (455) the bolts (403) and (451) the washers (404) and (452) and the set of washers (409) and (459).
(e)
Disconnect the support arm (410) from the upper and lower
connection links (461) and (423).
(6)
Disconnect the upper connection link (461).
(a)
Remove the cotter pin (450) and discard it.
(b)
Remove the nut (467), the washer (466) the bushing (465).
(c)
Remove the bolt (459) and remove the upper connection link (461).
(d)
Remove the washer (462) from the bolt (459).
(e)
Remove the bush (463) and the washer (464) and the bush (460) from the door structure.
(7)
Disconnect the rod (435).
(a)
Remove the cotter pin (420) and discard it.
(b)
Remove the nut (422), the washer (421).
(c)
Remove the bolt (431) and the washer (432) and the bushes (433) and (434).
(d)
Disconnect the rod (431).
1EFF : ALL 1 52-11-21Page 434 1 1 Feb 01/02R 1 1 1CES 1
(8)
Disconnect the rod (417).
(a)
Remove the cotter pin (416) and discard it.
(b)
Remove the nut (415) and the washer (437).
(c)
Remove the bolt (411), the washer (412) and the bushes (413) and (414).
(d)
Disconnect the rod (417).
(9)
Disconnect the lower connection link (423).
(a)
Remove the cotter pin (401) and discard it.
(b)
Remove the nut (402), the washer (430) and the bushing (429).
(c)
Remove the bolt (419) and the lower connection link (423).
(d)
Remove the washer (426) from the bolt (419).
(e)
Remove the bush (427) and the washer (429) and the bush (436) from the door structure.
1EFF : ALL 1 52-11-21Page 435 1 1 Feb 01/02R 1 1 1CES 1
TASK 52-11-21-400-001
Installation of the Door Locking Mechanism
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific two shims 0.2 mm (0.0078 in.)
No specific dynamometer 20 daN (44.9617 lbf) R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft) R
No specific Torque Wrench : range 0.20 to 3.60 m.daN
(2.00 to 26.00 lbf.ft) 98DNSA20206120 1 RIGGING PIN 98D52103006000 1 PIN - RIGGING
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-004 USA MIL-PRF-23827 TYPE I
SYNTH.ESTER BASED GREASE HIGH PRESSURE
(Ref. 20-31-00)
Material No. 04-017 USA A-A-59173 SILICONE GREASE (Ref. 20-31-00) Material No. 05-002 USA MIL-P-8116 PUTTY, ZINC CHROMATE GENERAL PURPOSE (Ref. 20-31-00) Material No. 06-005 USA MIL-L-87132 TYPE III LUBRICANT FOR FASTENERS (Ref. 20-31-00) Material No. 08-007A SEALANT, HIGH TEMP. (Ref. 20-31-00)
Material No. 09-016 USA MIL-PRF-81733D TYPE II CLASS B
CORROSION INHIBITING FILLET CONSISTENCY
(Ref. 20-31-00)
1EFF : ALL 1 52-11-21Page 436 1 1 May 01/05 1 1 1CES 1 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 09-018 Material No. 09-019 Material No. 11-004 Material No. 15-004
Material No. 15-007
Material No. 16-001 Material No. 16-002 Material No. 19-003
Material No. 19-010
C. Expendable Parts
USA AMS 3267/3
CORROSION INHIBITING LOW ADHESION SEALANT
(Ref. 20-31-00)
USA AMS 3267/3
LOW ADHESION CORROSION INHIBITING SEALANT
(Ref. 20-31-00)
USA MIL-T-81533
1.1.1TRICHLOROETHANE (METHYL CHLOROFORM)
(Ref. 20-31-00)
USA MIL-C-16173 GRADE 3
CORROSION PREVENTIVE COMPOUND (Ref. 20-31-00)
AIB TN 10138 TYPE II GRADE 1
CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND
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 DOORS 舱门1(172)