32-31-01
ALL ú ú 04 Page 404 ú Oct 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
SEE A
STRUCTURE
QUADRANT A CASE ATTACH MODULE
SCREW
FACE PLATE
SEE B
A
HANDLE
A
Landing Gear Control Module Installation
Figure 401 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-31-01
ALL ú ú 03 Page 405 ú Feb 10/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
STRUCTURE
MODULE
CONTROL
HANDLE
ALTERNATECONNECTOR FLAP EXTEND SWITCHES
ALIGNMENT PIN NUT HANDLE
LOCK OVERRIDECONTROL ROD
ALTERNATEQUADRANT
EXTEND
SWITCHES
A-A
LANDING GEAR CONTROL MODULE FACEPLATE B
Landing Gear Control Module Installation Figure 401 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-31-01
ALL ú ú 01 Page 406 ú Jun 10/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
(b)
Remove allen head screws that hold flap selector knob to the shaft.
(c)
Remove the screws and nylon washers that attach the faceplate to the control handle module.
(d)
Remove the faceplate.
(e)
Remove the screws that attach the control handle module to the structure.
(f)
While you hold the slot with a screwdriver, remove the nut which attaches the control rod to the handle trunnion.
(g)
Pull the module out of the instrument panel.
NOTE: If the module is not easy to pull out of the
____ instrument panel, examine the perimeter of the module. Paint or sealant along the perimeter of the module can hold the module in its position. If you find paint or sealant along the perimeter, carefully remove it before you pull on the module.
NOTE: This also disconnects the connectors D12461 and
____ D12462 of the control handle module.
(h) Install the safety pin to the control module quandrant.
NOTE: This will prevent inadvertent rotation of the quadrant
____ assembly after you remove the control module out of the instrument panel.
TASK 32-31-01-404-012
3. Landing Gear Control Handle Module Installation
_______________________________________________
A. Special Tools and Equipment
(1)
MIT65B81230 - Safety Pin, Landing Gear Control Lever Quadrant
(2)
G12001 Kit (Rigging Pins) ~................................................................. | Rigging Pin No. | Length (inch) | Diameter (inch) | ................................................................... | LG-1 | 4.0 | 0.309 to 0.311 | ................................................................... | LG-2 | 4.0 | 0.309 to 0.311 | 2....................…......................….....................1
B.
References
(1)
AMM 09-11-00/201, Towing
(2)
AMM 24-22-00/201, Manual Control
(3)
AMM 27-51-00/501, Trailing Edge Flap System
(4)
AMM 27-81-00/501, Leading Edge Flap System
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
32-31-01
ALL ú ú 04 Page 407 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
(5)
AMM 29-11-00/201, Hydraulic Supply System
(6)
AMM 32-00-30/201, Landing Gear Door Locks
(7)
AMM 32-09-02/201, Air/Ground Relays
(8)
AMM 32-35-00/501, Nose and Body Gear Alternate Extension System
(9) 中國(guó)航空網(wǎng) m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：747-400 AMM 飛機(jī)維護(hù)手冊(cè) 起落架 LANDING GEAR 4(28)
