9653M35P21 — BLADE,COMPRESSOR,AIRCRAFT GAS TU

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

9653M35P21: BLADE,COMPRESSOR,AIRCRAFT GAS TU.

BLADE,COMPRESSOR,AIRCRAFT GAS TU. Key specifications include diameter: 31.305 INCHES NOMINAL IN, material: STEEL BLADE, design_type: COMPRESSOR, overall_width: 3.397 INCHES NOMINAL IN, overall_length: 30.814 INCHES MINIMUM AND 30.834 INCHES MAXIMUM IN, special_features: ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-117-2903, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.

Verify compatibility with your specific system configuration before ordering.

WHERE IT FITS

9653M35P21

NSN: 2840-01-117-2903
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)

SPECIFICATIONS

diameter	31.305 INCHES NOMINAL IN
material	STEEL BLADE
design_type	COMPRESSOR
stage_number	2
overall_width	3.397 INCHES NOMINAL IN
overall_length	30.814 INCHES MINIMUM AND 30.834 INCHES MAXIMUM IN
special_features	ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE
material_thickness	0.230 INCHES MINIMUM AND 0.561 INCHES MAXIMUM IN
end_item_identification	ACFT.ENG. TF39
engine_section_location	LOW PRESSURE COMPRESSOR
criticality_code_justification	AGAV
NSN	2840-01-117-2903

COMPONENT DIAGRAM

KEY FEATURES

•

STAGE NUMBER: 2

•

DESIGN TYPE: COMPRESSOR

•

CRITICALITY CODE JUSTIFICATION: AGAV

•

DIAMETER: 31.305 INCHES NOMINAL IN

•

ENGINE SECTION LOCATION: LOW PRESSURE COMPRESSOR

•

MATERIAL THICKNESS: 0.230 INCHES MINIMUM AND 0.561 INCHES MAXIMUM IN

TECHNICAL CHARACTERISTICS

STAGE NUMBER	2
DESIGN TYPE	COMPRESSOR
CRITICALITY CODE JUSTIFICATION	AGAV
DIAMETER	31.305 INCHES NOMINAL IN
OVERALL LENGTH	30.814 INCHES MINIMUM AND 30.834 INCHES MAXIMUM IN
OVERALL WIDTH	3.397 INCHES NOMINAL IN
ENGINE SECTION LOCATION	LOW PRESSURE COMPRESSOR
MATERIAL THICKNESS	0.230 INCHES MINIMUM AND 0.561 INCHES MAXIMUM IN
SPECIAL FEATURES	ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE
END ITEM IDENTIFICATION	ACFT.ENG. TF39

OTHER ITEMS IN FSC 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components

Items in the same Federal Supply class. No interchangeability or substitution relationship is implied.

2840-00-000-0048 2840-00-000-0049 2840-00-001-1741 2840-00-001-1743 2840-00-001-2117 2840-00-001-2284 2840-00-001-3922 2840-00-001-4903

SUBSTITUTES & CROSS-REFERENCES 4

1999M69P06Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

1999M69P02Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

1999M69P03Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

9653M35P24Same NSN cross-reference

Same NSN cross-reference

Also cataloged under this NSN

LIFECYCLE

NSN statusActive· U.S. Government catalog

Demilitarization required — critical (Q)

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FREQUENTLY ASKED QUESTIONS

What is 9653M35P21?

9653M35P21 is a BLADE,COMPRESSOR,AIRCRAFT GAS TU.

What parts can replace 9653M35P21?

There are 4 known substitutes for 9653M35P21: 1999M69P06, 1999M69P02, 1999M69P03 and 1 more. Substitute compatibility should be verified for your specific system.

What is the NSN for 9653M35P21?

9653M35P21 is cataloged in the U.S. Government catalog under NSN 2840-01-117-2903. This indicates validated use in U.S. government and defense supply chains.

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9653M35P21 — BLADE,COMPRESSOR,AIRCRAFT GAS TU

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