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1386M88P04 — SUPPORT,TURBINE NOZZLE,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

1386M88P04: SUPPORT,TURBINE NOZZLE,AIRCRAFT.

SUPPORT,TURBINE NOZZLE,AIRCRAFT. Key specifications include material: STEEL, overall_length: 2.465 INCHES MINIMUM AND 2.469 INCHES MAXIMUM IN, inside_diameter: 3.126 INCHES NOMINAL IN, outside_diameter: 33.550 INCHES MINIMUM AND 33.570 INCHES MAXIMUM IN, mounting_hole_diameter: 0.274 INCHES MINIMUM AND 0.283 INCHES MAXIMUM IN, mounting_hole_quantity: 79. This part is cataloged in the U.S.

Government catalog under NSN 2840-01-307-6359, 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
1386M88P04
NSN: 2840-01-307-6359
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 07482 — GENERAL ELECTRIC COMPANY (USA)
SPECIFICATIONS
materialSTEEL
overall_length2.465 INCHES MINIMUM AND 2.469 INCHES MAXIMUM IN
inside_diameter3.126 INCHES NOMINAL IN
outside_diameter33.550 INCHES MINIMUM AND 33.570 INCHES MAXIMUM IN
mounting_hole_diameter0.274 INCHES MINIMUM AND 0.283 INCHES MAXIMUM IN
mounting_hole_quantity79
end_item_identificationACFT ENG F110G129
criticality_code_justificationAGAV
NSN2840-01-307-6359
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available SUPPORT,TURBINE NOZZLE,AIRCRAFT TITLE COMPONENT PN 1386M88P04 MFR SUPPORT,TURBINE NOZZLE
KEY FEATURES
•
MOUNTING HOLE QUANTITY: 79
•
CRITICALITY CODE JUSTIFICATION: AGAV
•
MOUNTING HOLE DIAMETER: 0.274 INCHES MINIMUM AND 0.283 INCHES MAXIMUM IN
•
OUTSIDE DIAMETER: 33.550 INCHES MINIMUM AND 33.570 INCHES MAXIMUM IN
•
INSIDE DIAMETER: 3.126 INCHES NOMINAL IN
•
MATERIAL: STEEL
TECHNICAL CHARACTERISTICS
MOUNTING HOLE QUANTITY79
CRITICALITY CODE JUSTIFICATIONAGAV
MOUNTING HOLE DIAMETER0.274 INCHES MINIMUM AND 0.283 INCHES MAXIMUM IN
OVERALL LENGTH2.465 INCHES MINIMUM AND 2.469 INCHES MAXIMUM IN
OUTSIDE DIAMETER33.550 INCHES MINIMUM AND 33.570 INCHES MAXIMUM IN
INSIDE DIAMETER3.126 INCHES NOMINAL IN
END ITEM IDENTIFICATIONACFT ENG F110G129
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 2
KDS 2840-4003Reference document
Same NSN cross-reference
Reference document — Secondary reference
1386M88P03Same 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 1386M88P04?
1386M88P04 is a SUPPORT,TURBINE NOZZLE,AIRCRAFT.
What parts can replace 1386M88P04?
There are 2 known substitutes for 1386M88P04: KDS 2840-4003, 1386M88P03. Substitute compatibility should be verified for your specific system.
What is the NSN for 1386M88P04?
1386M88P04 is cataloged in the U.S. Government catalog under NSN 2840-01-307-6359. This indicates validated use in U.S. government and defense supply chains.
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✓ PartsTable — the parts reference. Every fact cited to its source.
PartsTable Design LLC · partstable.com
U.S. Government catalog: edition PUBLOGDVD v12.0.0 (OCT 2026), edition date 2026-10-01, retrieved 2026-10-18.
PartsTable commercial catalog: edition Unified commercial catalog snapshot through 2026-09-28, edition date not on file, retrieved 2026-09-28.