Part Number
Definition:
A FLEXIBLE INFLATABLE RUBBER COMPONENT OF AN AIRCRAFT DEICING SYSTEM. IT IS DESIGNED TO BE ATTACHED TO THE LEADING EDGE OF AN AIRFOIL AND BE EXPANDED BY INFLATION TO BREAK OFF SURFACE ICE.
CAGE Information
| Code | Company |
|---|---|
| 03481 | BFGOODRICH CO THE AEROSPACE DIV ENGI |
Federal Supply Class
Title
AIRCRAFT HYDRAULIC, VACUUM, AND
Inclusions:
INCLUDES HYDRAULIC AND PNEUMATIC ACCUMULATORS, PUMPS, MOTORS, ACTUATING CYLINDERS, AND FILTERS; DE-ICING BOOTS; FLUID TYPE DE-ICING PUMPS, VALVES AND FILTERS; VACUUM SYSTEM OIL SEPARATORS; PNEUMATIC PRESSURIZATION EQUIPMENT OTHER THAN THAT FOR PRESSURIZING CABINS AND COMPARTMENTS.
Exclusions:
EXCLUDES JET ENGINE HYDRAULIC COMPONENTS (FSC 2840); VALVES SPECIFICALLY DESIGNED FOR AIR CONDITIONING, HEATING, VENTILATING, CABIN PRESSURIZING, AND THERMAL DE-ICING (FSC 1660); VALVES SPECIFICALLY DESIGNED FOR USE WITH AIRCRAFT ENGINES (FSC 2840); GUIDED MISSILES AND GUIDED MISSILE ENGINES (FSC 1338), LANDING GEAR (FSC 1620), WHEEL AND BRAKE SYSTEM COMPONENTS (FSC 1630); OXYGEN BREATHING SYSTEM COMPONENTS (FSC 1660); IN-FLIGHT REFUELING SYSTEM HYDRAULIC COMPONENTS (FSC 1680); SPECIFICALLY DESIGNED HYDRAULIC POWER STEERING SYSTEM COMPONENTS (FSC 1620).
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| FEAT | SPECIAL FEATURES | FIRST BREAK TO SECOND BREAK; INSTALL FLAT PATTERN; 102.187 IN. LG; 39.625 IN. W/FIRST END, 37.750 IN. W/SECOND END; CURVED FORM W/TAPERED EDGES:0.423 CU FT AIR CAP. A OR B PORTS; TUBE AREA FILLED W/1.000 IN. CHORDWISE; TWO 1.250 IN. DIA MANIFOLD TUBES EACH W/ONE 0.750 IN. AIR CONNECTOR |