DOC AIRBUS | AIPC A320F52-22-21-21A TUBE-TORSION AND SPRING-TORSION
52-22-21-21A TUBE-TORSION AND SPRING-TORSION
| FIG-ITEM | PART NUMBER | NOMENCLATURE | FIN ACCESS/PANEL | UNIT PER ASSY |
|---|---|---|---|---|
| 21A-001B | D5227936000074 |
TUBE-TORSION AND SPRING-TORSION
|
REF | |
| 21A-040 | MS16625-4075 |
. RING-RETAINING
|
002 | |
| 21A-050 | ASNA0033-028 |
. CLAMP
|
001 | |
| 21A-060 | A5217225420000 |
. BUSHING HALF
|
002 | |
| 21A-070 | D5227946220000 |
. LEVER-TORSION
|
001 | |
| 21A-080 | A5227148120000 |
. SCREW
|
001 | |
| 21A-090 | NSA5355-4CA |
. WASHER-LOCK
|
001 | |
| 21A-100A | D5227945120200 |
. SPRING-TORSION
|
001 | |
| 21A-130 | D5227945220400 |
. TUBE-TORSION
|
001 | |
| 21A-150 | A5217240232200 |
. WASHER
USAGE RANGE FROM 0 TO 1
|
AR | |
| 21A-160 | A5217240235000 |
. WASHER
USAGE RANGE FROM 0 TO 1
|
AR | |
| 21A-170 | A5217240235200 |
. WASHER
USAGE RANGE FROM 0 TO 1
|
AR |