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Part Number

Part Number:
NSN:
NIIN:
Item Name:
SEAL , AIR , AIRCRAFT GAS TURBINE EN

Definition:

A RIGID METALLIC ITEM, GENERALLY CIRCULAR. IT MAY BE FORMED OF SEGMENTED ARCS. IT IS DESIGNED TO PREVENT LEAKAGE OF AIR IN AN ENGINE, GAS TURBINE, AIRCRAFT. IT MAY BE OF VARIOUS CROSS-SECTIONAL SHAPES. IT MAY HAVE MOUNTING FACILITIES. IT MAY ACT AS A SPACER BUT ITS PRIMARY FUNCTION IS AS AN AIR SEAL.

CAGE Information

Code Company
07482 GENERAL ELECTRIC COMPANY DBA GE DIV

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
ABPX MATERIAL THICKNESS 0.008 INCHES NOMINAL
ABPX MATERIAL THICKNESS 0.008 INCHES NOMINAL
MDCL MATERIAL DOCUMENT AND CLASSIFICATION AMS 5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
CZCJ STAGE NUMBER 1
FEAT SPECIAL FEATURES T.O. 2J-TF39-4;TURBINE NOZZLE ASSY
CZBJ ENGINE SECTION LOCATION HIGH PRESSURE TURBINE
AGAV END ITEM IDENTIFICATION ACFT ENG TF-39
MATT MATERIAL NICKEL ALLOY OVERALL
ABMK OVERALL WIDTH 0.135 INCHES MINIMUM AND 0.145 INCHES MAXIMUM
ABHP OVERALL LENGTH 1.765 INCHES MINIMUM AND 1.785 INCHES MAXIMUM

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