Part Number
Definition:
A RIGID ITEM OF VARIOUS SHAPES PERMANENTLY ATTACHED TO A STRUCTURE OF AN AIRCRAFT, DESIGNED TO PROVIDE ACCESS FOR INSPECTION, SERVICE, REPLACEMENT OF COMPONENTS AND/OR ADJUSTMENTS. IT IS DESIGNED TO BE ATTACHED BY MEANS OF HINGES OR SIMILAR DEVICE. IT MAY INCLUDE SELF-CLOSING FEATURES AND HAVE A QUICK RELEASE OR OTHER TYPE LATCHING TO PERMIT ACCESS WITH A MINIMUM OF EFFORT. IT MAY INCLUDE AN OBSERVATION WINDOW. EXCLUDES COVER, ACCESS; COVER ACCESS, AIRCRAFT; DOOR, ACCESS; DOOR, AIRCRAFT AND ALL DOORS NOT SPECIFICALLY DESIGNED TO PROVIDE ACCESS FOR THE PURPOSES LISTED ABOVE.
CAGE Information
| Code | Company |
|---|---|
| 76301 | BOEING COMPANY THE DBA BOEING |
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 |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | AIRCRAFT MODEL F-18 |
| ADPB | DISTANCE BETWEEN HOLE CENTERLINE AND FIRST HOLE ALONG WIDTH | 3.900 INCHES NOMINAL |
| ABMW | PERIPHERAL SHAPE STYLE | RECTANGLE, TWO HOLES |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A25015,COND T81 FED SPEC SINGLE MATERIAL RESPONSE |
| ABGL | WIDTH | 6.220 INCHES NOMINAL |
| CBBL | FEATURES PROVIDED | OBSERVATION FACILITY |
| ABRY | LENGTH | 2.250 INCHES NOMINAL |
| AAGR | CROSS-SECTIONAL SHAPE STYLE | FLAT |
| ADQB | SECURING DEVICE TYPE | HINGE |
| ADPD | DISTANCE FROM FIRST HOLE CENTERLINE TO END ALONG WIDTH | 0.950 INCHES NOMINAL |
| ADPR | BODY THICKNESS | 0.080 INCHES NOMINAL |
| ADNU | CORNER RADIUS | 0.210 INCHES NOMINAL |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |