NIIN Output Data
NIIN:
NSN:
Item Name:
STRINGER , AIRCRAFT
Definition:
AN AUXILIARY LONGITUDINAL MEMBER OF THE STRUCTURAL FRAMEWORK OF A FUSELAGE, NACELLE, EMPENNAGE, WING, AND THE LIKE. IT IS DESIGNED TO STIFFEN AND/OR SUPPORT THE SKIN BY ATTACHMENT OF BULKHEADS, FORMERS, FRAMES, RIBS, AND THE LIKE.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| 74A180642-2022 | 76301 | A | 3 | 2 | A | ZZ |
CAGE Information
| Code | Company |
|---|---|
| 76301 | BOEING COMPANY THE DBA BOEING |
Federal Supply Class
Title
AIRFRAME STRUCTURAL COMPONENTS
Inclusions:
INCLUDES FLIGHT CONTROL SURFACES; INTERNAL AND EXTERNAL AUXILIARY FUEL TANKS; EXHAUST SYSTEMS; PYLONS, TRIM TABS; AIRCRAFT.
Exclusions:
EXCLUDES FITTED COVERS; HELICOPTER ROTOR BRAKE SYSTEM COMPONENTS; AIRCRAFT LOOSE EQUIPMENT AND ALTERNATE MISSION CONFIGURATION EQUIPMENT STORED ON BOARD THE AIRCRAFT.
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| CZDJ | AIRCRAFT LOCATION | WING, FLAP |
| BWJF | SIDE FOR WHICH DESIGNED | BOTH SIDES |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/12 FED SPEC SINGLE MATERIAL RESPONSE |
| MATT | MATERIAL | ALUMINUM ALLOY 7075 |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | F/A-18A/C |
| AGAV | END ITEM IDENTIFICATION | F-18 FIGHTER AIRCRAFT |