18-14 — IGNITER,SPARK,GAS TURBINE ENGINE

✓ Government record, cited

— · MRO · MRO_GENERAL

PRODUCT OVERVIEW

18-14: IGNITER,SPARK,GAS TURBINE ENGINE.

IGNITER,SPARK,GAS TURBINE ENGINE. Key specifications include shape: ROUND, height: 0.328 INCHES NOMINAL IN, length: 18.000 INCHES NOMINAL IN, material: RUBBER SYNTHETIC BASIC, sterility: NONSTERILE, base_style: MINIATURE SCREW. This part is cataloged in the U.S.

Government catalog under NSN 5310-00-054-3328, 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

MRO→ MRO_GENERAL→ 18-14

NSN: 5310-00-054-3328
NIINs: 000543328, 001000329, 001433170, 001860519, 002411172, 002440756, 004486680, 005294896, 005803435, 006401054, 006816879, 007176455, 011041188, 011740892, 011833000, 011924712, 012477735, 012849403, 015834467
FSC: 5310 — Nuts and Washers
CAGE: 78189 — ITW SHAKEPROOF AUTOMOTIVE PRODUCTS (USA)

SPECIFICATIONS

shape	ROUND
height	0.328 INCHES NOMINAL IN
length	18.000 INCHES NOMINAL IN
material	RUBBER SYNTHETIC BASIC
sterility	NONSTERILE
base_style	MINIATURE SCREW
body_style	PLAIN, SOLID
body_width	6.125 INCHES MAXIMUM IN
bore_style	PLAIN BOTH ENDS
bulb_style	T (TUBULAR)
shaft_type	ROUND SINGLE ACTUATOR
teeth_type	SINGLE HELIX
NSN	5310-00-054-3328

COMPONENT DIAGRAM

KEY FEATURES

•

HARDNESS RATING: 89.0 ROCKWELL B MINIMUM AND 94.0 ROCKWELL B MAXIMUM

•

STYLE DESIGNATOR: FLAT EXTERNAL TEETH

•

OUTSIDE DIAMETER: 0.494 INCHES MINIMUM AND 0.510 INCHES MAXIMUM IN

•

MATERIAL THICKNESS: 0.023 INCHES MINIMUM AND 0.028 INCHES MAXIMUM IN

•

DEPARTURE FROM CITED DESIGNATOR: AS MODIFIED BY MATERIAL COMPOSITION AND FINISH

•

NONDEFINITIVE SPEC/STD DATA: 2 TYPE AND 2 STYLE

•

SURFACE TREATMENT: NICKEL OVERALL

•

MATERIAL: COPPER ALLOY OVERALL

TECHNICAL CHARACTERISTICS

HARDNESS RATING	89.0 ROCKWELL B MINIMUM AND 94.0 ROCKWELL B MAXIMUM
STYLE DESIGNATOR	FLAT EXTERNAL TEETH
OUTSIDE DIAMETER	0.494 INCHES MINIMUM AND 0.510 INCHES MAXIMUM IN
MATERIAL THICKNESS	0.023 INCHES MINIMUM AND 0.028 INCHES MAXIMUM IN
DEPARTURE FROM CITED DESIGNATOR	AS MODIFIED BY MATERIAL COMPOSITION AND FINISH
NONDEFINITIVE SPEC/STD DATA	2 TYPE AND 2 STYLE
SURFACE TREATMENT	NICKEL OVERALL
MATERIAL	COPPER ALLOY OVERALL
HOLE DIAMETER	0.255 INCHES MINIMUM AND 0.267 INCHES MAXIMUM IN

SUBSTITUTES & CROSS-REFERENCES 3

N413P25EReference document

Same NSN cross-reference

Reference document — Advisory reference — outside the item-of-supply concept

N0413P00025EReference document

Same NSN cross-reference

Reference document — Advisory reference — outside the item-of-supply concept

FFW100Reference document

Same NSN cross-reference

Reference document — Identification reference

LIFECYCLE

NSN statusCancelled· U.S. Government catalog

Acquisition advice: Normally procured from the manufacturer (OEM)No demilitarization required

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FREQUENTLY ASKED QUESTIONS

What is 18-14?

18-14 is a IGNITER,SPARK,GAS TURBINE ENGINE. It is classified as a MRO (MRO_GENERAL).

What parts can replace 18-14?

There are 3 known substitutes for 18-14: N413P25E, N0413P00025E, FFW100. Substitute compatibility should be verified for your specific system.

What is the NSN for 18-14?

18-14 is cataloged in the U.S. Government catalog under NSN 5310-00-054-3328. This indicates validated use in U.S. government and defense supply chains.

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18-14 — IGNITER,SPARK,GAS TURBINE ENGINE

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