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A 737-300/400/500MAINTENANCE MANUAL
 | | 48 | Quick Disconnect Coupling *[1] | | | 170 | | | 49 | Nut *[1] | | | 160 | | | 50 | Cap *[1] | | | 165 | 2......…........…...................................…..........….....….........1
 *[1] You will not have these parts when you remove the VSCF. Get new parts or
 parts from a storage area for this installation. *[2] One more clamp is necessary when you install the CSD. *[3] It is possible that these clamps are installed on the engine. *[5] This item is not installed on all airplanes. *[6] The one-piece and two-piece collector rings may be used in place of each
 other, however they are not directly interchangeable due to extra parts
 required.
 ~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 203 | 1 | VSCF Generator/Converter *[4] | 24-11-11 | 01 | 130 | | | 2 | Clamp, BACC-10GU107 | | | | | | 3 | Clamp, BACC-10GU116 | | | | | | 4 | Clamp, BACC-10GU110 | | | | | | 5 | QAD Ring | 24-11-11 | 01 | 85 | | | 6 | Mounting Pad Adapter Plate | | | 70 | | | 7 | O-Ring | | | 80 | | | 8 | QAD Adapter Gasket | | | 75 | | | 9 | O-Ring | 24-11-11 | 01A | 45 | | | 10 | O-Ring, M83248/2-908 | | | | | | 11 | Retainer, MS28773-08 *[4] | | | | | | 12 | Nut, AN6289-8 *[4] | | | | | | 13 | Elbow, MS21908-08 *[4] | | | | | | 14 | O-Ring, M83248/2-910 | | | | | | 15 | Retainer, MS28773-10 | | | | | | 16 | Nut, AN6289-10 | | | | | | 17 | Elbow, MS21908-10 | | | | | | 18 | Clamp | 24-10-00 | 34 | 80 | | | 19 | Screw | | | 125 | | | 20 | Washer | | | 135 | | | 21 | Blast Cover Adapter | | | 111 | 2......…........…...................................…..........….....….........1
 *[4] You will not use these parts when you install the CSD. Keep them in a storage area for a subsequent VSCF installation.
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 ~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 205 | 1 | Master Marker (CSD Installation) | 11-13-00 | 15A | 5 | | | 1 | Master Marker (VSCF Installation) | | | 30 | | | 2 | Oil Marker | | | 10 | | | 2 | Oil Marker (Alternative) | | | 15 | | | 3 | Oil Marker | | | 20 | | | 3 | Oil Marker (Alternative) | | | 25 | 2......…........…...................................…..........….....….........1
 D. References
 (1)  
AMM 24-11-11/401, Generator Constant Speed Drive

 (2)  
AMM 24-11-11/401, Variable Speed Constant Frequency Generator/Converter

 E.
Access

 (1)  
Location Zones 506 Engine 1 - Accessory Gearbox, 8 o'clock 606 Engine 2 - Accessory Gearbox, 8 o'clock

 (2)  
Access Panels
 5746L Left Fan Cowl - Engine 1
 5846L Left Fan Cowl - Engine 2

 F.
Procedure

 (1)  
Remove the VSCF (1, Fig. 203) (AMM 24-11-11/401).

 S 032-035

 (2)  
Remove the necessary parts from the VSCF (1):

 S 022-025
 (a)  Remove the blast cover adapter (21): 1) Remove the five screws (19) and washers (20).
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737-300/400/500MAINTENANCE MANUAL
 2) Remove the blast cover adapter (21).
 (b)  Remove the parts from the oil inlet port of the VSCF:
 NOTE: You will keep the parts installed in the oil outlet port
____ for the subsequent installation of the VSCF.
 1) Remove the elbow (17).
 2) Remove the nut (16).
 3) Remove the retainer (15).
 4) Remove the O-ring (14) and discard it.
　
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