National Stock Number (NSN) Output Data
Definition:
A RIGID ITEM, FABRICATED FROM A HEAT RESISTANT ALLOW, WITH OR WITHOUT INSULATION MATERIAL ADDED. DESIGNED TO PROTECT PARTS, AREAS OR SYSTEMS OF AN ENGINE, GAS TURBINE, AIRCRAFT FROM EXCESSIVE HEAT DAMAGE. SEE ALSO INSULATION BLANKET, THERMAL, AIRCRAFT GAS TURBINE ENGINE.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| 9194758 | 98748 | A | 3 | 2 | 2 | MB |
CAGE Information
| Code | Company |
|---|---|
| 98748 | AIR FORCE UNITED STATES DEPARTMENT O |
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 |
|---|---|---|
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5536 ASSN STD SINGLE MATERIAL RESPONSE OVERALL |
| FEAT | SPECIAL FEATURES | 40 HOLES,.085-.095 DIA EQUALLY SPACED |
| ABMZ | DIAMETER | 9.902 INCHES MINIMUM AND 9.908 INCHES MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | J57-43WB & J57-59W ENGINES; TO. 2J-J57-54 |
| MATT | MATERIAL | NICKEL ALLOY OVERALL |
| CRTL | CRITICALITY CODE JUSTIFICATION | AGAV |
| ABHP | OVERALL LENGTH | 1.315 INCHES MINIMUM AND 1.355 INCHES MAXIMUM |
| CZBJ | ENGINE SECTION LOCATION | COMBUSTION CHAMBER |