Part Number
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.
CAGE Information
Code | Company |
---|---|
0YCM5 | BAE SYSTEMS TECHNOLOGY SOLUTIONS & S |
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 | 6.375 INCHES MINIMUM AND 6.405 INCHES MAXIMUM |
SFTT | SURFACE TREATMENT | PRIMER AND PAINT |
ABNM | THICKNESS | 0.063 INCHES NOMINAL |
STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-P-53022 TY I MIL SPEC 1ST TREATMENT RESPONSE AND MIL-C-46168 COLOR 37038 MIL SPEC 2ND TREATMENT RESPONSE |
MATT | MATERIAL | ALUMINUM ALLOY 6061 |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-250/AA ASSN STD SINGLE MATERIAL RESPONSE |
ABMK | OVERALL WIDTH | 5.750 INCHES MINIMUM AND 5.770 INCHES MAXIMUM |
CZDJ | AIRCRAFT LOCATION | AQ-36 LPCR |
CZEK | AIRCRAFT MISSION DESIGN SERIES | C-130 |