| MRC |
Requirement Statement |
Characteristics |
| SR-5 |
DESIGN CONTROL REFERENCE |
17P2A6519-3 |
| CZDJ |
AIRCRAFT LOCATION |
WG TO FUS PANEL, FILLET-OUTBD, UPR, AFT |
| SR-5 |
THE MANUFACTURERS DATA |
|
| MATT |
MATERIAL |
PLASTIC EPOXY AND PLASTIC POLYIMIDE |
| FEAT |
SPECIAL FEATURES |
CONSISTS OF 1(-5) PANEL, 1(-7) CORE, 1(-9) CORE, 2 RETAINERS, 2 SEALS AND 44 RIVETS. PANEL MATERIAL GLASS FIBER WOVEN FABRIC AND CARBON FIBER WOVEN FABRIC; CORE MATERIAL HONECOMB POLYMIDE PAPER, OVEREXPANDED |
| SR-5 |
MANUFACTURERS CODE |
88277 |
| CZEK |
AIRCRAFT MISSION DESIGN SERIES |
C-17 |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
DMS 2288,TYPE 2,CLASS 2,GRADE D MFR REF 1ST MATERIAL RESPONSE AND DMS 1974,TYPE 2,CLASS 2,GRADE B,DENSITY-3 PCF MFR REF 2ND MATERIAL RESPONSE |
