(2)
Remove the cotter pin (149) and discard it.
(3)
Remove the nut (148), the washers (150), (151), the bolt (153) and disconnect the flexible control cable (152).
(4)
Remove the nuts (146), (162), the washers (147), (163), the tapper pins (144), (165) and the levers (145), (164).
(5)
Remove the nuts (157), (158) the washers (156), (161) and the tapper pins (154), (160).
(6)
Disengage and remove the shaft (167) and remove the bellcrank (155) and the spacer (159).
Subtask 52-13-22-020-050
F. Removal of the Escape Slide Control Mechanism
(Ref. Fig. 408/TASK 52-13-22-991-014)
(1)
Remove the cotter pin (193).
(2)
Remove the nut (194), the washer (192), the bolt (185), the washer
(186) and disengage the rod (180).
(3)
Remove and discard the cotter pin (190).
(4)
Remove the nut (191), the washer (189), the bolt (187), the washer
(188) and disengage the rod end (199).
(5)
Remove the rod end (199), the spring (200) and the bushing (201).
(6)
Remove the cotter pin (195).
(7)
Remove the nut (196), the washer (197), the bolt (181) and the washers (182), (183).
1EFF : ALL 1 52-13-22Page 416 1 1 Nov 01/99R 1 1 1CES 1
Telescopic Forks and Control Shaft Figure 407/TASK 52-13-22-991-006
1EFF : 1 1R 1CES ALL 1 11 1 52-13-22 Page 417 Nov 01/99
Escape Slide Control Mechanism Figure 408/TASK 52-13-22-991-014
1EFF : 1 1R 1CES ALL 1 11 1 52-13-22 Page 418 May 01/98
(8) Remove the hook (198) and the spacer (194).
1EFF : ALL 1 52-13-22Page 419 1 1 Nov 01/99R 1 1 1CES 1
TASK 52-13-22-400-001
Installation of the Release Mechanism of the Emergency Escape Slide of the Aft Passenger/Crew Door
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------
REFERENCE QTY DESIGNATION
-------------------------------------------------------------------------------
No specific grease gun
R No specific Torque Wrench : range 0.00 to 1.20 m.daN
R (0.00 to 9.00 lbf.ft) 98DNSA20206120 2 RIGGING PIN
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. 05-027 USA MIL-L-81309
RUST INHIBITOR(FOR CORROSION USE 15-004)
(Ref. 20-31-00)
Material No. 09-016 USA MIL-PRF-81733D TYPE II CLASS B
CORROSION INHIBITING FILLET CONSISTENCY
(Ref. 20-31-00)
Material No. 09-019 USA AMS 3267/3
LOW ADHESION CORROSION INHIBITING SEALANT
(Ref. 20-31-00)
Material No. 11-004 USA MIL-T-81533
1.1.1TRICHLOROETHANE (METHYL CHLOROFORM)
(Ref. 20-31-00)
1EFF : ALL 1 52-13-22Page 420 1 1 May 01/05 1 1 1CES 1
-------------------------------------------------------------------------------
REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 15-007
Material No. 16-001 Material No. 16-002 Material No. 19-003
C. Expendable Parts
AIB TN 10138 TYPE II GRADE 1
CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND
(Ref. 20-31-00)
ANTI-CORROSION PRIMER (POLYURETHANE ) (Ref. 20-31-00)
GB BAEP 3536
POLYURETHANE TOPCOAT GREY (FOR INTERNAL APPLIC.)
(Ref. 20-31-00)
USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
-------------------------------------------------------------------------------FIG.ITEM |DESIGNATION |IPC-CSN -------------------------------------------------------------------------------
R
R
R
R
R
R
3 cotter pin 7 cotter pin 7 cotter pin 15 cotter pin 16 cotter pin 16 cotter pin 25 cotter pin 28 cotter pin 43 cotter pin 49 cotter pin 85 cotter pin 85 cotter pin 85 cotter pin 85 cotter pin 85 cotter pin 95 cotter pin 95 cotter pin 95 cotter pin 95 cotter pin 95 cotter pin 149 cotter pin 149 cotter pin 149 cotter pin 149 cotter pin 149 cotter pin 166 cotter pin 52-13-22 02B-010 52-11-22 02A-01052-11-22 02B-01052-13-22 02B-010 52-11-22 02A-01052-11-22 02B-01052-13-22 02B-01052-13-22 02B-01052-13-22 03B-01052-13-22 03B-010 52-13-22 01G-01052-13-22 01J-01052-13-22 01K-01052-13-22 01P-01052-13-22 01Q-010 52-13-22 01G-01052-13-22 01J-01052-13-22 01K-01052-13-22 01P-01052-13-22 01Q-010 52-13-22 01G-01052-13-22 01J-01052-13-22 01K-01052-13-22 01P-01052-13-22 01Q-010 52-13-22 01G-010 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2(143)
