1-100-620-01 — SHAFT,TURBINE,AIRCRAFT GAS TURBI

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

1-100-620-01: SHAFT,TURBINE,AIRCRAFT GAS TURBI.

SHAFT,TURBINE,AIRCRAFT GAS TURBI. Key specifications include material: STEEL OVERALL, overall_length: 28.030 INCHES NOMINAL IN, hardness_rating: 34.0 ROCKWELL C MINIMUM AND 37.0 ROCKWELL C MAXIMUM OVERALL, material_document_and_classification: AMS 6362 ASSN STD SINGLE MATERIAL RESPONSE AND AMS 6265 ASSN STD SINGLE MATERIAL RESPONSE OVERALL. This part is cataloged in the U.S.

Government catalog under NSN 2840-00-981-6997, 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

1-100-620-01

NSN: 2840-00-981-6997
FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
CAGE: 78U39 — OZARK AEROWORKS LLC (USA)

SPECIFICATIONS

material	STEEL OVERALL
overall_length	28.030 INCHES NOMINAL IN
hardness_rating	34.0 ROCKWELL C MINIMUM AND 37.0 ROCKWELL C MAXIMUM OVERALL
material_document_and_classification	AMS 6362 ASSN STD SINGLE MATERIAL RESPONSE AND AMS 6265 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
NSN	2840-00-981-6997

COMPONENT DIAGRAM

KEY FEATURES

•

HARDNESS RATING: 34.0 ROCKWELL C MINIMUM AND 37.0 ROCKWELL C MAXIMUM OVERALL

•

MATERIAL DOCUMENT AND CLASSIFICATION: AMS 6362 ASSN STD SINGLE MATERIAL RESPONSE AND AMS 6265 ASSN STD SINGLE MATERIAL RESPONSE OVERALL

•

MATERIAL: STEEL OVERALL

TECHNICAL CHARACTERISTICS

HARDNESS RATING	34.0 ROCKWELL C MINIMUM AND 37.0 ROCKWELL C MAXIMUM OVERALL
MATERIAL DOCUMENT AND CLASSIFICATION	AMS 6362 ASSN STD SINGLE MATERIAL RESPONSE AND AMS 6265 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
OVERALL LENGTH	28.030 INCHES NOMINAL IN
SPECIAL FEATURES	TAPERED OD; 3.67 MIN 3.675 MAX IN. LARGEST OD; FIRST END; EXT SPLINES; 19 TEETH; 30 DEG PRESSURE ANGLE; 1.248 MIN 1.25 MAX IN. OD; 1.1675 IN. NOM PITCH DIA; 1.88 MIN 2.44 MAX IN. LG SPLINES; 0.267 MIN 0.272 MAX IN. DISTANCE FROM FIRST END TO SPLINES; SCEOND END; EXT SPLINES; 13 TEETH; 30 DEG PRESSURE ABGLE; 1/162 MIN 1.167 MAX IN. OD; 1.0833 IN. NOM PITCH DIA; 2.12 MIN 2.26 MAX IN. LG SPLINES; 0.96 IN. NOM DISTANCE FROM SECOND END TO SPLINES; FIRST END; INT THD; 0.625 IN.-18 UNF 2B THD; 0.88 MIN 0.92 MAX IN. DP THD; 0.267 MIN 0.272 MAX IN. DISTANCE FROM FIRST END TO THD; SECOND END; INT THD; 0.625 IN.-18 UNF 2B THD; 0.65 MIN 0.69 MAX IN. DP THD COUNTERSUNK 60 DEG TO 0.72 IN. NOM DIA IN
MATERIAL	STEEL OVERALL

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

No substitute or cross-reference records for this part.

LIFECYCLE

NSN statusActive· U.S. Government catalog

Acquisition advice: Normally procured from the manufacturer (OEM)Demilitarization required — mutilation + specific procedure

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FREQUENTLY ASKED QUESTIONS

What is 1-100-620-01?

1-100-620-01 is a SHAFT,TURBINE,AIRCRAFT GAS TURBI.

What is the NSN for 1-100-620-01?

1-100-620-01 is cataloged in the U.S. Government catalog under NSN 2840-00-981-6997. This indicates validated use in U.S. government and defense supply chains.

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1-100-620-01 — SHAFT,TURBINE,AIRCRAFT GAS TURBI

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