R R Slat-Track Pinion Assembly - Location and Detail Figure 401/TASK 27-84-68-991-001- 34 (SHEET 3)
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R R Slat-Track Pinion Assembly - Location and Detail Figure 401/TASK 27-84-68-991-001- 44 (SHEET 4)
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- for track 10 pinion, remove 6039CM (6089CM) - for track 11 pinion, remove 6041CM (6091CM) - for track 12 pinion, remove 6045CM (6095CM).
R (2) For slat tracks 2, 3, 5, 6, 7, 8, 9 and 12:
R (a) For slat track 5, 6 and 8 only:
1_ Remove and discard the lockwire from the bolts (3).
2_ Remove the bolts (3) and the bracket (4).
(b) Remove the bolts (1) and the actuator housing (2).
(c) Remove the bolts (7) and the end cover (8).
(d) Remove together, the bearing (5) and the pinion assembly (6).
R (e) Remove the bearing (5) from the pinion assembly (6).
R R R R R NOTE : The pinion assembly (6) and bearing (5) can be installed____ with the bearing on the inboard or outboard side. Record the initial position of the pinion assembly (6) before removal.
R (3) For slat tracks 10 and 11:
(a) Remove the bolts (19), the washers (20) and the actuator housing (21).
(b) Remove the bolts (24), the washers (25) and the end cover (26).
(c) Remove together, the bearing (22) and the pinion assembly (23).
R (d) Remove the bearing (22) from the pinion assembly (23).
R R R R NOTE : The pinion assembly (23) and bearing (22) can be installed____ with the bearing on the inboard or outboard side. Record the initial position of the pinion assembly (23) before removal.
TASK 27-84-68-400-001
Installation of the Slat-Track Pinion Assembly
WARNING : MAKE SURE THAT THE FLIGHT CONTROL SAFETY-LOCKS AND THE WARNING
_______ NOTICES ARE IN POSITION.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific safety barriers No specific safety line No specific warning notice No specific access platform 4.0 m (13 ft. 1 in.) 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER 98D27804006000 1 TOOL-ALIGNMENT AND LOCKING (SLAT TRACKS 2 AND 3) 98D27804007000 1 TOOL-ALIGNMENT AND LOCKING (SLAT TRACKS 5 TO 12) 98D27804019000 1 BEAM SUPPORT-SLATS 3, 4 AND 5
B. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 04-022 USA MIL-PRF-81322 GRADE 2 SYNTHE.HYDROCARBON GREASE HIGH PRESSURE (Ref. 20-31-00)
Material No. 04-024 AIB AIMS 09-06-001 SYNTHETIC GREASE FOR FLAP & SLAT MECHANISM (Ref. 20-31-00)
Material No. 05-063 USA MIL-A-907E NEVERSEEZ NICKEL SPECIAL GRADE (Ref. 20-31-00)
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-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 09-018 USA AMS 3267/3
CORROSION INHIBITING LOW ADHESION SEALANT
(Ref. 20-31-00)
Material No. 09-019 USA AMS 3267/3
LOW ADHESION CORROSION INHIBITING SEALANT
(Ref. 20-31-00)
Material No. 11-026 GB DEF-STAN 68-148/1
SOLVENT GENERAL PURPOSE (Ref. 20-31-00)
Material No. 15-007 AIB TN 10138 TYPE II GRADE 1 CORROSION PREVENTIVE TEMPORARY PROTECTIVE COMPOUND (Ref. 20-31-00)
Material No. 19-003 USA AMS 3819
LINT-FREE COTTON CLOTH (Ref. 20-31-00)
Material No. 19-010 USA AMS 5687
LOCKWIRE STAINLESS STEEL ANNEALED 0.8MM DIA
(Ref. 20-31-00)
C. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-80-00-866-005 Retracting the Slats on the Ground
27-84-00-710-001 Operational Test of the Slat System
27-84-48-400-001 Installation of the Type A Actuators
6013CM(6063CM)/6015CM(6065CM) 27-84-49-400-002 Installation of the Type B Actuators 6033CM(6083CM)/6037CM(6087CM)/ 6041CM(6091CM) R 27-84-68-991-001 Fig. 401 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱8(153)
