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Part Number:
NSN:
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Item Name:
SUMP , OIL , AIRCRAFT GAS TURBINE EN

Definition:

A CHAMBER SURROUNDING THE MAIN BEARINGS FOR A SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. THE CHANBER IS USED TO COLLECT LUBRICATING FLUID FOR RECIRCULATION.

CAGE Information

Code Company
93596 KERNS MANUFACTURING CORP.

Federal Supply Class

Title

GAS TURBINES AND JET ENGINES, AI

Inclusions:

INCLUDES COMPRESSOR AND TURBINE ROTORS; BLADES; COMBUSTION CHAMBER; ACCESSORY GEAR BOX; AFTERBURNER; EXHAUST CONE; RESERVOIRS, HYDRAULIC; TANK, OIL.

Exclusions:

EXCLUDES OIL, AIR, ANTI-ICING, AND HYDRAULIC REGULATORS, VALVES, AND PUMPS SPECIALLY DESIGNED FOR GAS TURBINES AND JET ENGINES (FSC 2995); CONTROL ASSEMBLIES, PUSH-PULL (FSC 2995); ENGINE MOUNTED CONTROL ASSEMBLIES (FSC 2995); FUEL SYSTEM COMPONENTS (FSC 2915); ENGINE ELECTRICAL SYSTEM COMPONENTS (FSC 2925); ENGINE COOLING SYSTEM COMPONENTS (FSC 2935); ENGINE AIR/OIL CLEANER/FILTER/STRAINERS (FSC 2945).

Characteristics (Decoded)

MRC Requirements Statement Clear Text Reply
FEAT SPECIAL FEATURES T.O. 2J-J85-94, FIG 7, IND 28; 2ND END DIA. 5.560
MDCL MATERIAL DOCUMENT AND CLASSIFICATION AMS4117 ASSN STD 1ST MATERIAL RESPONSE OVERALL OR AMS4065 ASSN STD 2ND MATERIAL RESPONSE OVERALL
CRTL CRITICALITY CODE JUSTIFICATION ABPX AND ABMZ AND ABHP AND FEAT
CXCY PART NAME ASSIGNED BY CONTROLLING AGENCY ORIGINAL NAME SUMP,FRONT FRAME
ABPX MATERIAL THICKNESS 0.070 INCHES MINIMUM AND 0.090 INCHES MAXIMUM
MATT MATERIAL ALUMINUM OVERALL
AGAV END ITEM IDENTIFICATION J85-GE-21/21A/21B AIRCRAFT GAS TURBINE ENGINE
ABHP OVERALL LENGTH 2.868 INCHES MINIMUM AND 2.872 INCHES MAXIMUM
ABMZ DIAMETER 6.300 INCHES NOMINAL
CZBJ ENGINE SECTION LOCATION COMPRESSOR

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