National Stock Number (NSN) 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 |
---|---|---|---|---|---|---|---|---|
4F72634-107A | 26512 | A | 5 | 9 | 5 | SB | ||
4F72634-107A | 98897 | A | 3 | 2 | 2 | SB |
CAGE Information
Code | Company |
---|---|
26512 | NORTHROP GRUMMAN SYSTEMS CORPORATION |
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 |
---|---|---|
CZEJ | AIRCRAFT STATION NUMBER | FUSELAGE STA 1084.00 TO 1128.00 |
CZDJ | AIRCRAFT LOCATION | PANEL-LOWER FWD MLG FAIRING |
CZEK | AIRCRAFT MISSION DESIGN SERIES | C-5B |
MATT | MATERIAL | GLASS FIBER AND PLASTIC POLYURETHANE |
FEAT | SPECIAL FEATURES | M/F: PREIMPREGNATED GLASS FABRIC PER STM22-4CL FORM I CLASS 1 USING MIL-C-9084 TYPE VIII B FABRIC AND FOAM HIGH TEMP, POLYURETHANE 6-8LBS MAX PER CUBIC FOOT. GENERAL PLASTICS MFG CO NO. FR7600 SERIES OR EQUIV |