Part Number
Definition:
A MECHANICAL DEVICE LOCATED IN THE EXHAUST AREA OF A JET ENGINE ON LARGE AIRPLANES. IT IS DESIGNED TO DEFLECT THE ENGINE FAN OR EXHAUST GASES FORWARD TO INCREASE THE DESCENT ANGLE IN FLIGHT, OR TO DECREASE THE LANDING SPEED ON THE GROUND. IT CAN TAKE THE FORM OF PIVOTING CLAMSHELL DOORS, CASCADE VANES (DIVERTERS); TRANSLATING SLEEVES; BLOCKER DOORS, OR THE LIKE. WHEN NOT IN USE IT MUST BE STREAMLINED TO THE CONFIGURATION OF THE ENGINE NACELLE.
CAGE Information
| Code | Company |
|---|---|
| 07482 | GENERAL ELECTRIC COMPANY DBA GE DIV |
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 |
|---|---|---|
| ZZZY | REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATD BY LOCKHEED SOURCE CONTROL DWG NO. 4P94200-109E |
| ZZZY | REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATD BY LOCKHEED SOURCE CONTROL DWG NO. 4P94200-109E |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | C-5 |