B.
Access
(1)
Location Zone
801 Nose Cargo Door
C.
Prepare For Removal
S 494-002
(1)
Install the safety barrier across the door opening.
S 484-003
(2)
Supply electrical power (Ref 24-22-00/201).
S 864-004
(3)
Open the nose cargo door to get access to the push-pull cam mechanism.
NOTE: The push-pull cam actuator must be in the fully extended
____ position during the removal and installation of the push-pull cam mechanism.
S 864-005
(4)
Open these circuit breakers and attach the DO-NOT-CLOSE tags:
(a)
On the Auxilary External 2 Power Center-Right panel P715: 1) NOSE CARGO DOOR
(b)
On the Power Distribution Center-Right panel P415: 1) 415F16, NOSE CARGO DOOR CONTROL
(c)
On the Nose Cargo Door Power panel H122: 1) DOOR LIFT 2) PULL UP CAM
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
52-31-09
ALL ú ú 02 Page 401 ú Feb 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
PUSH-PULL CAM
SEE A CAM ROLLERS A
ELECTRICAL
CABLE ACTUATOR
PUSH-PULL ROD END
CAM
ACTUATOR
CAM ROLLER
SUPPORT FITTING
BOLT
A CAM SUPPORT
FITTING
BOLT
NOTE: ACTUATOR IS SHOWN____
FWD FULLY CLOSED.
BOLT
A
Nose Cargo Door Push-Pull Cam Mechanism Installation
Figure 401 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
52-31-09
ALL ú ú 02 Page 402 ú Feb 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
B26923
A
747-400
MAINTENANCE MANUAL
SUPPORT FITTING
SERRATED PLATES
B-B Nose Cargo Door Push-Pull Cam Mechanism Installation Figure 401 (Sheet 2)
B26924
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
52-31-09
ALL ú ú 02 Page 403 ú Feb 10/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
D.
E.
F.
G.
A
747-400 MAINTENANCE MANUAL
3) LATCHES 1-4R
4) LATCHES 1-4L
5) LATCHES 5-8R
6) LATCHES 1-4L
S 024-038
(5) Disconnect the electrical connector from the push-pull cam actuator.Push-Pull Cam Actuator Removal
S 024-006
CAUTION: DO NOT CLOSE THE NOSE CARGO DOOR WITH THE PUSH-PULL CAM
_______ ACTUATOR REMOVED. THIS CAN CAUSE DAMAGE TO THE PUSH-PULL CAM AND CAM ROLLERS.
(1) Remove the atachment bolts, nut and washers on the support fitting
and cam and remove the actuator.Push-Pull Cam Removal
S 034-007
(1)
Make sure the actuator pushrod is disconnected from the cam.
S 024-008
(2)
Remove the attachment bolts, nuts, and washers and remove the cam.Cam Support Fitting Removal
S 214-009
(1)
Make sure the actuator pushrod is disconnected from the cam.
S 034-010
(2)
Remove bolt, nut, and washers that attach the push-pull cam to the cam support fitting and remove the cam, if it is necessary.
S 024-011
(3)
Remove the atachment bolts and remove the support fitting, shims and fillers.
NOTE: Make sure to keep shims and fillers for installation.
____
Cam Roller Support Fitting Removal
S 024-012
(1) Remove the attachment bolts and remove the support fitting, shims and serrated plates.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:747-400 AMM 飞机维护手册 舱门 DOORS 2(54)