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9687M92G14 — SUPPORT,TURBINE NOZZLE,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

9687M92G14: SUPPORT,TURBINE NOZZLE,AIRCRAFT.

SUPPORT,TURBINE NOZZLE,AIRCRAFT. Key specifications include material: STEEL, overall_length: 12.568 INCHES NOMINAL IN, inside_diameter: 25.035 INCHES MINIMUM AND 25.055 INCHES MAXIMUM IN, outside_diameter: 28.233 INCHES NOMINAL IN, mounting_hole_diameter: 0.345 INCHES MINIMUM AND 0.346 INCHES MAXIMUM IN, mounting_hole_quantity: 32. This part is cataloged in the U.S.

Government catalog under NSN 2840-00-563-9154, 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
9687M92G14
NSN: 2840-00-563-9154
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)
SPECIFICATIONS
materialSTEEL
overall_length12.568 INCHES NOMINAL IN
inside_diameter25.035 INCHES MINIMUM AND 25.055 INCHES MAXIMUM IN
outside_diameter28.233 INCHES NOMINAL IN
mounting_hole_diameter0.345 INCHES MINIMUM AND 0.346 INCHES MAXIMUM IN
mounting_hole_quantity32
end_item_identificationENGINE,AIRCRAFT,TURBOFAN,MODEL TF39GE1A
criticality_code_justificationAGAV
NSN2840-00-563-9154
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available SUPPORT,TURBINE NOZZLE,AIRCRAFT TITLE COMPONENT PN 9687M92G14 MFR SUPPORT,TURBINE NOZZLE
KEY FEATURES
•
MOUNTING HOLE QUANTITY: 32
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
MOUNTING HOLE DIAMETER: 0.345 INCHES MINIMUM AND 0.346 INCHES MAXIMUM IN
•
OUTSIDE DIAMETER: 28.233 INCHES NOMINAL IN
•
INSIDE DIAMETER: 25.035 INCHES MINIMUM AND 25.055 INCHES MAXIMUM IN
•
MATERIAL: STEEL
TECHNICAL CHARACTERISTICS
MOUNTING HOLE QUANTITY32
CRITICALITY CODE JUSTIFICATIONAGAV
MOUNTING HOLE DIAMETER0.345 INCHES MINIMUM AND 0.346 INCHES MAXIMUM IN
OVERALL LENGTH12.568 INCHES NOMINAL IN
OUTSIDE DIAMETER28.233 INCHES NOMINAL IN
INSIDE DIAMETER25.035 INCHES MINIMUM AND 25.055 INCHES MAXIMUM IN
END ITEM IDENTIFICATIONENGINE,AIRCRAFT,TURBOFAN,MODEL TF39GE1A
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.
2840-00-000-0048 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 1
2840PL0844149Reference document
Same NSN cross-reference
Reference document — Informative reference only
LIFECYCLE
NSN statusActive· U.S. Government catalog
Demilitarization required — mutilation
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FREQUENTLY ASKED QUESTIONS
What is 9687M92G14?
9687M92G14 is a SUPPORT,TURBINE NOZZLE,AIRCRAFT.
What parts can replace 9687M92G14?
There is 1 known substitute for 9687M92G14: 2840PL0844149. Substitute compatibility should be verified for your specific system.
What is the NSN for 9687M92G14?
9687M92G14 is cataloged in the U.S. Government catalog under NSN 2840-00-563-9154. This indicates validated use in U.S. government and defense supply chains.
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