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9104M10P06 — RETAINER,TURBINE BLADE,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

9104M10P06: RETAINER,TURBINE BLADE,AIRCRAFT.

RETAINER,TURBINE BLADE,AIRCRAFT. Key specifications include material: STEEL, overall_length: 0.694 INCHES NOMINAL IN, outside_diameter: 22.854 INCHES MINIMUM AND 22.885 INCHES MAXIMUM IN, special_features: HIGH PRESSURE TURBINE ROTOR ASSY;2ND STAGE; CBORE FOR 29 HOLES EQ SP, 29 POCKETS, end_item_identification: ACFT ENG TF39, reference_data_and_literature: 2J-TF39-4, FIG 59 IND 25. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-138-5658, 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
9104M10P06
NSN: 2840-01-138-5658
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)
SPECIFICATIONS
materialSTEEL
stage_number2
overall_length0.694 INCHES NOMINAL IN
outside_diameter22.854 INCHES MINIMUM AND 22.885 INCHES MAXIMUM IN
special_featuresHIGH PRESSURE TURBINE ROTOR ASSY;2ND STAGE; CBORE FOR 29 HOLES EQ SP, 29 POCKETS
end_item_identificationACFT ENG TF39
reference_data_and_literature2J-TF39-4, FIG 59 IND 25
criticality_code_justificationAGAV
NSN2840-01-138-5658
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available RETAINER,TURBINE BLADE,AIRCRAFT TITLE COMPONENT PN 9104M10P06 MFR RETAINER,TURBINE BLADE
KEY FEATURES
•
STAGE NUMBER: 2
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
REFERENCE DATA AND LITERATURE: 2J-TF39-4, FIG 59 IND 25
•
OUTSIDE DIAMETER: 22.854 INCHES MINIMUM AND 22.885 INCHES MAXIMUM IN
•
MATERIAL: STEEL
TECHNICAL CHARACTERISTICS
STAGE NUMBER2
CRITICALITY CODE JUSTIFICATIONAGAV
REFERENCE DATA AND LITERATURE2J-TF39-4, FIG 59 IND 25
OVERALL LENGTH0.694 INCHES NOMINAL IN
OUTSIDE DIAMETER22.854 INCHES MINIMUM AND 22.885 INCHES MAXIMUM IN
SPECIAL FEATURESHIGH PRESSURE TURBINE ROTOR ASSY;2ND STAGE; CBORE FOR 29 HOLES EQ SP, 29 POCKETS
END ITEM IDENTIFICATIONACFT ENG TF39
MATERIALSTEEL
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.
2840-00-004-4242 2840-00-021-4702 2840-00-043-0981 2840-00-043-0982 2840-00-048-5261 2840-00-407-9165 2840-01-171-0875
SUBSTITUTES & CROSS-REFERENCES 1
2840PL0784431Reference document
Same NSN cross-reference
Reference document — Informative reference only
LIFECYCLE
NSN statusActive· U.S. Government catalog
Acquisition advice: Normally procured from the manufacturer (OEM)Demilitarization required — mutilation
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FREQUENTLY ASKED QUESTIONS
What is 9104M10P06?
9104M10P06 is a RETAINER,TURBINE BLADE,AIRCRAFT.
What parts can replace 9104M10P06?
There is 1 known substitute for 9104M10P06: 2840PL0784431. Substitute compatibility should be verified for your specific system.
What is the NSN for 9104M10P06?
9104M10P06 is cataloged in the U.S. Government catalog under NSN 2840-01-138-5658. This indicates validated use in U.S. government and defense supply chains.
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