DOC AIRBUS | AIPC A320F77-22-10-01A THERMOCOUPLE INSTL-T5,CFM56,400
77-22-10-01A THERMOCOUPLE INSTL-T5,CFM56,400
Zone(s): 400
| FIG-ITEM | PART NUMBER | NOMENCLATURE | FIN ACCESS/PANEL | UNIT PER ASSY |
|---|---|---|---|---|
| 01A-010 | J643P06A |
. BOLT
5A ENGINE
|
004 | |
| 01A-020 | MS9556-08 |
. BOLT
5B ENGINE
|
004 | |
| 01A-030 | J626P03 |
. NUT
POST SB 77-0001
|
002 | |
| 01A-040 | J626P03 |
. NUT
5B ENGINE
|
002 | |
| 01A-050 | 649-411-010-0 |
. CLAMP
PRE SB 72-0351
|
004 | |
| 01A-050A | 649-411-650-0 |
. CLAMP
POST SB 72-0351
|
004 | |
| 01A-060 | 649-411-650-0 |
. CLAMP
5B ENGINE
|
004 | |
| 01A-060A | 649-411-850-0 |
. CLAMP
ALT PN ABOVE
|
004 | |
| 01A-070 | J626P03 |
. NUT
|
002 | |
| 01A-080 | NAS1101E04H4 |
. SCREW
PRE SB 72-0019
|
008 | |
| 01A-080A | NAS1101E04H5 |
. SCREW
POST SB 72-0019
|
008 | |
| 01A-090 | NAS1101E04H5 |
. SCREW
5B ENGINE
|
008 | |
| 01A-100 | 620-857-346-0 |
. PLATE-HALF
5A ENGINE
|
004 | |
| 01A-105 | 620-857-346-0 |
. PLATE-HALF
5B ENGINE
|
004 | |
| 01A-105A | 305-870-801-0 |
. PLATE-HALF
ALT PN ABOVE
|
004 | |
| 01A-110 | TC199-00 |
. SENSOR TEMP
PRE SB 77-0023
|
002 | |
| 01A-110A | TC199-01 |
. SENSOR TEMP
POST SB 77-0023
|
002 | |
| 01A-120 | TC266-00 |
. SENSOR TEMP
PRE SB 77-0011
|
002 | |
| 01A-120A | TC266-01 |
. SENSOR TEMP
ALT PN ABOVE
|
002 | |
| 01A-130 | J644P09A |
. BOLT
|
004 | |
| 01A-140 | J626P04 |
. NUT
|
004 |