369A1406-3 — GUIDE,SPRING,MAIN ROTOR

✓ Government record, cited

— · COMPONENT

PRODUCT OVERVIEW

369A1406-3: GUIDE,SPRING,MAIN ROTOR.

The GUIDE,SPRING,MAIN ROTOR is a the manufacturer industrial component. This part is cataloged in the U.S. Government catalog under NSN 1615-00-181-4236, 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

369A1406-3

NSN: 1615-00-181-4236
FSC: 1615 — Helicopter Rotor Blades, Drive Mechanisms and Components
CAGE: 8V613 — THE BOEING COMPANY (USA)

SPECIFICATIONS

Part Number	369A1406-3
NSN	1615-00-181-4236

COMPONENT DIAGRAM

KEY FEATURES

•

GENERAL CHARACTERISTICS ITEM DESCRIPTION: STEEL,MIL-S-6758 COMP 4130 COND N OR STEEL,CORROSION RESISTANT MIL-H-6867 COMP 17-4PH,PASSIVATED PER HP4-B,SHAPE,FLANGED SLEEVE,DIM.,0.850 IN. NOM LG,2.178 IN. MIN,2.179 IN. MAX FLANGE OD,0.130 IN. NOM FLANGE W,0.970 IN. MIN,1.000 IN. MAX FLANGE 1ST STEP OD,0.110 IN. NOM FLANGE 1ST STEP W,0.417 IN. MIN,0.427 IN. MAX ACROSS HEX FLATSON BODY,0.610 IN. OM BODY LG,0.255 IN. MIN,0.265 IN. MAX BODY ID,0.700 IN. NOM FLANGE COUNTERBORE DIA BY 0.150 IN. DEEP,1.940 IN. DISTANCE ACROSS FLATS ON FLANGE,RIGHT HOLES 0.390 IN. DIA ON FLANGE EQUALLY SPACED ON 1.500 IN. BOLT CIRCLE DIA,ONE GROOVE ON FLANGE RIGHT FACE 0.060 IN. W,0.030 IN. DEEP AND 1.426 IN. DIA IN

TECHNICAL CHARACTERISTICS

GENERAL CHARACTERISTICS ITEM DESCRIPTION

STEEL,MIL-S-6758 COMP 4130 COND N OR STEEL,CORROSION RESISTANT MIL-H-6867 COMP 17-4PH,PASSIVATED PER HP4-B,SHAPE,FLANGED SLEEVE,DIM.,0.850 IN. NOM LG,2.178 IN. MIN,2.179 IN. MAX FLANGE OD,0.130 IN. NOM FLANGE W,0.970 IN. MIN,1.000 IN. MAX FLANGE 1ST STEP OD,0.110 IN. NOM FLANGE 1ST STEP W,0.417 IN. MIN,0.427 IN. MAX ACROSS HEX FLATSON BODY,0.610 IN. OM BODY LG,0.255 IN. MIN,0.265 IN. MAX BODY ID,0.700 IN. NOM FLANGE COUNTERBORE DIA BY 0.150 IN. DEEP,1.940 IN. DISTANCE ACROSS FLATS ON FLANGE,RIGHT HOLES 0.390 IN. DIA ON FLANGE EQUALLY SPACED ON 1.500 IN. BOLT CIRCLE DIA,ONE GROOVE ON FLANGE RIGHT FACE 0.060 IN. W,0.030 IN. DEEP AND 1.426 IN. DIA IN

OTHER ITEMS IN FSC 1615 — Helicopter Rotor Blades, Drive Mechanisms and Components

Items in the same Federal Supply class. No interchangeability or substitution relationship is implied.

1615-00-056-4862 1615-00-420-7841 1615-00-446-7576 1615-00-458-8376 1615-00-621-1853 1615-00-629-4445 1615-00-689-6306 1615-00-689-6307

SUBSTITUTES & CROSS-REFERENCES

No substitute or cross-reference records for this part.

LIFECYCLE

NSN statusActive· U.S. Government catalog

No demilitarization required

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FREQUENTLY ASKED QUESTIONS

What is 369A1406-3?

369A1406-3 is a GUIDE,SPRING,MAIN ROTOR.

What is the NSN for 369A1406-3?

369A1406-3 is cataloged in the U.S. Government catalog under NSN 1615-00-181-4236. This indicates validated use in U.S. government and defense supply chains.

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369A1406-3 — GUIDE,SPRING,MAIN ROTOR

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