NIIN Output Data
NIIN:
NSN:
Item Name:
STIFFENER , AIRCRAFT
Definition:
AN ITEM, GENERALLY A STRIP, DESIGNED TO STRENGTHEN AND RESIST LOADS BY ATTACHMENT TO VARIOUS COMPONENTS SUCH AS SKINS, RIBS, PYLONS, AND THE LIKE.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| 74A341121-2007 | 76301 | A | 5 | 9 | 1 | KE | ||
| 74A341121-2007 | 76823 | A | 3 | 2 | 5 | KE |
CAGE Information
| Code | Company |
|---|---|
| 76301 | BOEING COMPANY THE DBA BOEING |
| 76823 | NORTHROP GRUMMAN SYSTEMS CORPORATION |
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 |
|---|---|---|
| ABHP | OVERALL LENGTH | 5.500 INCHES NOMINAL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-9047 (6AL-4V, COND A) MIL SPEC SINGLE MATERIAL RESPONSE |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | INAVY) ANGLE, FORWARD PANEL, AFT FUS; ALSO KNOWN AS STIFFENER |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | F/A18-E/F |
| AGAV | END ITEM IDENTIFICATION | FIGHTER AIRCRAFT-FIRST (F18 E/F) |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| ABPX | MATERIAL THICKNESS | 1.500 INCHES NOMINAL |
| MATT | MATERIAL | TITANIUM |
| ABMK | OVERALL WIDTH | 2.000 INCHES NOMINAL |