NIIN Output Data
Definition:
A DEVICE OF VARIOUS SHAPES TO BE PERMANENTLY ATTACHED TO THE STRUCTURE OF AN AIRCRAFT. IT IS DESIGNED TO PERMANENTLY MOUNT AND/OR SUPPORT AN INTEGRAL MEMBER, OR GROUP OF MEMBERS OF THE AIRFRAME IN A PROPER POSITION AND BEAR THE STRESS IMPOSED BY THE COMPONENTS BEING SUPPORTED. IT MAY HAVE MOUNTING PROVISIONS, SUCH AS SLOTS, HOLES, AND/OR ATTACHMENTS TO FACILITATE INSTALLATION. EXCLUDES ITEMS WHICH ARE PRIMARILY DESIGNED FOR DAMPENING SHOCK AND/OR VIBRATION. EXCLUDES BRACKET, ANGLE; BRACKET, DOUBLE ANGLE; BRACKET, SHELF; BRACKET, MOUNTING; AND BRACKET (1), STRUCTURAL COMPONENT, AIRCRAFT.
Reference/Part Number
Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
---|---|---|---|---|---|---|---|---|
4F22035-202A | 98897 | A | 3 | 2 | C | ZZ |
CAGE Information
Code | Company |
---|---|
98897 | LOCKHEED MARTIN CORPORATION DBA LOCK |
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 |
---|---|---|
ABPX | MATERIAL THICKNESS | 0.025 INCHES NOMINAL |
MATT | MATERIAL | ALUMINUM ALLOY 7475 |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | STRAP |
CZDJ | AIRCRAFT LOCATION | STRAP FAIL SAFE UPPER LOBE |
FEAT | SPECIAL FEATURES | MATL AL ALY 7475-T761 BARE PER STM07-121 OR AMS 4085,SPARES REPLACEMENT FOR -170A AND -186A |
CZEJ | AIRCRAFT STATION NUMBER | FS1611.910 TO FS1734.000 |
ABHP | OVERALL LENGTH | 142.000 INCHES NOMINAL |
ABMK | OVERALL WIDTH | 5.000 INCHES NOMINAL |
CZEK | AIRCRAFT MISSION DESIGN SERIES | C-5 |