Part Number
Definition:
AN ADAPTER DESIGNED TO SUPPORT/POSITION AIRCRAFT COMPONENTS DURING INSTALLATION/REMOVAL. IT IS USED IN CONJUNCTION WITH LIFT TRAILERS, HYDRAULIC JACKS AND THE LIKE. EXCLUDES ITEMS HAVING A MORE SPECIFIC NAME.
CAGE Information
| Code | Company |
|---|---|
| 43999 | BOEING COMPANY THE DBA BOEING DIV DE |
Federal Supply Class
Title
AIRCRAFT GROUND SERVICING EQUIPM
Inclusions:
INCLUDES ENERGIZERS; ENGINE PREHEATERS; MOORING ASSEMBLIES; WHEEL CHOCKS; BEACHING EQUIPMENT; AILERON, ELEVATOR, AND RUDDER LOCKS; PASSENGER LOADING RAMPS; MAINTENANCE PLATFORMS; AIRCRAFT MAINTENANCE AND BOARDING LADDERS; AIRCRAFT MAINTENANCE SLINGS AND HOISTS; AIRCRAFT FIN TILTING JACKS; AIRFIELD SPECIALIZED LIFT TRUCKS AND TRAILERS; FITTED COVERS FOR AIRFRAME COMPONENTS; AIRCRAFT ENGINE COVERS.
Exclusions:
EXCLUDES AIRFIELD SPECIALIZED TRUCKS AND TRAILERS DESIGNED PRIMARILY FOR TRANSPORTING AIRCRAFT ASSEMBLIES (FSC 1740); MAINTENANCE STANDS DESIGNED FOR SUPPORT OF AIRCRAFT ASSEMBLIES DURING REPAIR OR OVERHAUL (FSC 4920); TEST STANDS (FSC 4920); GENERAL PURPOSE JACKS (FSC 5120); SLINGS (FSC 3940), AND HOISTS (FSC 3950); TRAILERS (FSC 2330), LIQUID OXYGEN, AIRCRAFT SERVICING (FSC 1660).
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| FCLS | FUNCTIONAL CLASSIFICATION | HH-5.1 |
| FEAT | SPECIAL FEATURES | C/O HYDRALIC JACK WITH POSITIONING HEADS; MAX HEIGHT OF JACK 65.000 IN. ; COLLAPSIBLE LADDER |
| SUPP | SUPPLEMENTARY FEATURES | JACK ASSY MOUNTED ON HORIZONAL TRACK ASSY; ADAPTER HAS PROTECTIVE RAILS TO KEEP MAINTENANCE PERSONNEL FROM FALLING WHEN ADAPTER ASSY RAISED TO MAX HEIGHT OF 160.750 IN. FROM GROUND |
| ABHP | OVERALL LENGTH | 48.000 INCHES NOMINAL |
| ABMK | OVERALL WIDTH | 62.000 INCHES NOMINAL |
| ALBY | USAGE DESIGN | WEAPONS SYSTEM COMPONENT |
| ABKW | OVERALL HEIGHT | 45.000 INCHES NOMINAL |
| ZZZV | FSC APPLICATION DATA | B1-B ACFT AGE. |
| ABSX | ATTACHMENT METHOD | BOLTED |
| FTLD | FUNCTIONAL DESCRIPTION | USED TO GAIN ACCESS TO TRAPEZOIDAL DOORS FOR INSTALLATION/REMOVAL OF LRU COMPONENTS |