D.
Parts
(1)
Refer to the AIPC for the part numbers and effectivities of the items in the table that follow:
~..............................................................................
| AMM | | AIPC |
................. ............................
| FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM |
................................................................................ ú| 411 | 1 | Bolt | 54-32-01 | 01 | 25 |
2......…........…...................................…..........….....….........1
~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 412 | 1 | Bolt | 54-30-00 | 47 |255, 260 | 2......…........…...................................…..........….....….........1
~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 417 | 1 | Bolt | 71-21-02 | 01 | 10 | | | 2 | Washer | | | 15 | | | 3 | Washer | | | 20 | | | 4 | Nut | | | 25 | | | 5 | Bolt | 71-21-01 | 02 | 70 | | | 6 | Washer | | | 75 | 2......…........…...................................…..........….....….........1
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
71-00-02
ALL ú ú C07B.1 Page 475 ú Jul 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / /
CFM56 ENGINES
737-300/400/500/ /MAINTENANCE MANUAL ////////////////////////
Power Plant Installation - Bootstrap Method
___________________________________________
~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 418 | 1 | Bolt | 71-21-01 | 02 | 59 | | | 2 | Washer | | | 60 | | | 3 | Nut Retainer | | | 55 | | | 4 | Nut | | | 45 | | | 5 | Washer | | | 40 | | | 6 | Nut Retainer | | | 50 | | | 7 | Retainer | | | 35 | | | 8 | Nut | | | 68 | | | 9 | Washer | | | 62 | | | 10 | Nut Retainer | | | 52 | | | 11 | Retainer | | | 48 | | | 12 | Bolt | | | 57 | | | 13 | Nut | | | 69 | 2......…........…...................................…..........….....….........1
~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 419 | 1 | Washer | 71-21-01 | 02 | 10 | | | 2 | Nut | | | 15 | | | 3 | Nut Retainer | | | 20 | | | 4 | Washer | | | 25 | | | 5 | Bolt | | | 30 | 2......…........…...................................…..........….....….........1
E. References
(1)
AMM 08-11-00/201, Level Airplane
(2)
AMM 54-32-01/401, Forward Fairing
(3)
AMM 71-11-02/401, Fan Cowl Panels
F.
Access
(1)
Location Zone
506 Engine No. 1
606 Engine No. 2
(2)
Access Panels
5739L/5738L Thrust Reverser - Engine No. 1
5839R/5838R Thrust Reverser - Engine No. 2
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
71-00-02
ALL ú ú C07B Page 476 ú Mar 12/02
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
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