Part Number
Part Number:
NSN:
NIIN:
Item Name:
PLATE , ENGINE AFT FUSELAGE
CAGE Information
| Code | Company |
|---|---|
| 80378 | TRIUMPH AEROSTRUCTURES, LLC DBA TRIU |
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 |
|---|---|---|
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | 0.500 IN. THK,6.240 IN. W; 4 HOLES 0.4375 IN. DIA,6.780 IN. DISTANCE BETWEEN CENTERLINE OF TWO HOLES AT THE TOP ALONG L,7.080 IN. DISTANCE BETWEEN CENTERLINE OF TWO HOLES AT THE BOTTOM ALONG L,4.540 IN. DISTANCE BETWEEN HOLES ALONG W; 2.500 IN. APERTURE,2.550 IN. DISTANCE FROM EDGE ALONG L AT THE BOTTOM TO CENTERLINE OF APERTURE,5.780 IN. DISTANCE FROM EDGE ALONG W AT THE RIGHT SIDE TO CENTERLINE OF APERTURE |
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | 0.500 IN. THK,6.240 IN. W; 4 HOLES 0.4375 IN. DIA,6.780 IN. DISTANCE BETWEEN CENTERLINE OF TWO HOLES AT THE TOP ALONG L,7.080 IN. DISTANCE BETWEEN CENTERLINE OF TWO HOLES AT THE BOTTOM ALONG L,4.540 IN. DISTANCE BETWEEN HOLES ALONG W; 2.500 IN. APERTURE,2.550 IN. DISTANCE FROM EDGE ALONG L AT THE BOTTOM TO CENTERLINE OF APERTURE,5.780 IN. DISTANCE FROM EDGE ALONG W AT THE RIGHT SIDE TO CENTERLINE OF APERTURE |