0.500
INCH
MIN.
TYING
MATERIAL
FLEXIBLE
SLEEVE
B
BOLT (NAS6703-3) (2 LOCATIONS) WASHER (AN960C10L) (2 LOCATIONS)
D26 CONNECTOR
DUST CAP
WIRE BUNDLE W1502
DPCT CONNECTOR
DPCT CONNECTOR ASSEMBLY
C
DPCT Wire Harness Installation
Figure 204 (Sheet 2)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
24-11-00
ALL ú ú 04 Page 217 ú Nov 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
S 432-033
(8) Install the blast cover adapter (21) on the VSCF (1):
(a) Put the blast cover adapter (21) on the VSCF (1). 1) Install the five screws (19) and washers (20).
S 432-034
(9)
Make sure that the correct markers are installed to show the oil for the VSCF (Fig. 205).
S 422-024
(10)
Install the VSCF (1, Fig. 203) and do the specified test (AMM 24-11-11/401).
TASK 24-11-00-902-019
4. VSCF to CSD Replacement (Fig. 202 and 203)
_______________________
A. General
(1)
This procedure refers to a constant speed drive as a CSD. This procedure refers to a variable speed constant frequency generator/converter as a VSCF.
(2)
This procedure gives instructions to install a CSD on an engine which has a VSCF installed.
B. Consumable Materials
(1)
D00193 Lubricating Oil, MIL-L-7808 or MIL-L-23699
(2)
G00000 Tubing, Non-Rigid ASTM D3295, Type I, Class C or MIL-I-23053
(3)
G00000 Tying Material, BMS 13-54
C. Parts
NOTE: These tables have parts that you remove and install in this
____
procedure and in the other specified procedures.
~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 202 | 1 | Constant Speed Drive (CSD) *[1] | 24-11-11 | 01A | 5 | | | 2 | Generator *[1] | 24-11-11 | 01 | 105 | | | 3 | Screw *[1] | 24-11-00 | 02 | 40 | | | 4 | Washer *[1] | | | 50 | | | 5 | Nut *[1] | | | 55 | | | 6 | Clamp *[1] | | | 30 | | | 7 | Half-Shell Clamp *[5] *[1] | | | 35 |
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
24-11-00
ALL ú ú 03 Page 218 ú Mar 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
1. MASTER MARKER
2. OIL MARKER
2. OIL MARKER
Oil Marker Installation
Figure 205 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
24-11-00
ALL ú
ú 05 Page 219
ú Nov 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
3. OIL MARKER 0.5 INCH (13 mm) 0.5 INCH (13 mm)
CSD OIL LEVEL SIGHT GLASSCSD INSTALLATION 2. OIL MARKER SEE C 0.6 INCH (15 mm)
CSD DRIVE PAD
CSD FWD CAVITY FILL PORT
CSD INSTALLATION
C
SEE D
2
1
1
0.30 2
INCH (8 mm)
3. OIL MARKER
2. OIL
0.20 INCH MARKER
(5 mm)
1
AIRPLANES WITH -14 VSCF GENERATOR/CONVERTER VSCF INSTALLATION
2
AIRPLANES WITH -15 AND -16 VSCF
D
GENERATOR/CONVERTER
Oil Marker Installation
Figure 205 (Sheet 2)
A98717
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：737-300 400 500 AMM 飞机维护手册 电源 ELECTRICAL POWER(25)
