NIIN Output Data
Definition:
A PREFORMED ITEM OF VARIOUS SHAPES, AND CONTOURS, WHICH MAY HAVE A SANDWICH OR HONEYCOMB CORE BONDED TO A METALLIC OR NONMETALLIC FACING MATERIAL. IT IS USED TO ENCLOSE INTEGRAL PORTIONS OF THE FUSELAGE OR TO FORM PARTITIONS OR SECTIONS WITHIN A WING, EMPENNAGE, FUSELAGE, NACELLE OR CREW COMPARTMENT. IT MAY HAVE MOUNTING PROVISIONS SUCH AS PREDRILLED HOLES TO FACILITATE INSTALLATION, BUT WILL HAVE NO ITEMS ATTACHED TO IT EXCEPT BRACKET (S) OR OTHER SECURING DEVICES TO ACCOMMODATE ITS OWN MOUNTING OR SUPPORT. IT MAY BE MOUNTED BY MEANS OF FASTENERS, BONDING OR WELDING. EXCLUDES PANEL, INTERIOR LINING, AIRCRAFT; COVER ACCESS; COVER, ACCESS, AIRCRAFT; FLOOR (1), AIRCRAFT; CORE MATERIAL, CELLULAR, STRUCTURAL.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| 4W12030-204A | 98897 | A | 5 | 9 | 2 | MB | ||
| 4W12030-234A | 98897 | A | 5 | 9 | 2 | MB | ||
| 4W12060-240A | 59213 | A | 5 | 2 | 5 | ZZ | ||
| 4W12030-240A | 98897 | A | 3 | 2 | 2 | MB | ||
| 4W12030-240A | 0TZ71 | A | 5 | 2 | 5 | ZZ | ||
| 4W12030-240A | 9U679 | A | 5 | 2 | 5 | ZZ | ||
| 4W12030-240A | 29183 | A | 5 | 2 | 5 | ZZ | ||
| 4W12030-240A | 99115 | A | 5 | 2 | 5 | ZZ | ||
| 4W12030-240A | 1B6R3 | A | 5 | 2 | 5 | ZZ |
CAGE Information
| Code | Company |
|---|---|
| 0TZ71 | WESTLAKE HARDWARE NO 2 |
| 98897 | LOCKHEED MARTIN CORPORATION DBA LOCK |
| 59213 | AERO COMPONENTS INC |
| 9U679 | CPI AEROSTRUCTURES INC. DBA CPI AERO |
| 29183 | G. S. E. DYNAMICS INC. |
| 99115 | HONEYCOMB COMPANY OF AMERICA INC. |
| 1B6R3 | MRA SYSTEMS INC. DBA MIDDLE RIVER AI |
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 |
|---|---|---|
| MATT | MATERIAL | ALUMINUM ALLOY 7075 AND TITANIUM ALLOY |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/12 FED SPEC 1ST MATERIAL RESPONSE AND MIL-T-9046 MIL SPEC 2ND MATERIAL RESPONSE |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | C-5A |
| CZEJ | AIRCRAFT STATION NUMBER | FS1024 TO FS1084 |