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74A314377-2005 — FORMER,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

74A314377-2005: FORMER,AIRCRAFT.

The FORMER,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 7075, overall_width: 17.000 INCHES NOMINAL IN, overall_length: 22.000 INCHES NOMINAL IN, special_features: CONSISTS OF 1 FORMER,3 BEARINGS;3.0 IN THICK IN, aircraft_location: NLG FWD FUSELAGE DOOR MACHANISM, aircraft_station_number: Y230.20. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-600-2170, 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
74A314377-2005
NSN: 1560-01-600-2170
FSC: 1560 — Airframe Structural Components
CAGE: 76301 — THE BOEING COMPANY DIV DEFENSE (USA)
SPECIFICATIONS
materialALUMINUM ALLOY 7075
overall_width17.000 INCHES NOMINAL IN
overall_length22.000 INCHES NOMINAL IN
special_featuresCONSISTS OF 1 FORMER,3 BEARINGS;3.0 IN THICK IN
aircraft_locationNLG FWD FUSELAGE DOOR MACHANISM
aircraft_station_numberY230.20
side_for_which_designedRIGHT SIDE
aircraft_mission_design_seriesF/A18A
material_document_and_classificationMMS-159 FED SPEC SINGLE MATERIAL RESPONSE
NSN1560-01-600-2170
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available FORMER,AIRCRAFT TITLE COMPONENT PN 74A314377-2005 MFR FORMER,AIRCRAFT
KEY FEATURES
•
AIRCRAFT STATION NUMBER: Y230.20
•
MATERIAL DOCUMENT AND CLASSIFICATION: MMS-159 FED SPEC SINGLE MATERIAL RESPONSE
•
AIRCRAFT LOCATION: NLG FWD FUSELAGE DOOR MACHANISM
•
MATERIAL: ALUMINUM ALLOY 7075
•
SIDE FOR WHICH DESIGNED: RIGHT SIDE
TECHNICAL CHARACTERISTICS
AIRCRAFT STATION NUMBERY230.20
MATERIAL DOCUMENT AND CLASSIFICATIONMMS-159 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH22.000 INCHES NOMINAL IN
OVERALL WIDTH17.000 INCHES NOMINAL IN
SPECIAL FEATURESCONSISTS OF 1 FORMER,3 BEARINGS;3.0 IN THICK IN
AIRCRAFT LOCATIONNLG FWD FUSELAGE DOOR MACHANISM
MATERIALALUMINUM ALLOY 7075
SIDE FOR WHICH DESIGNEDRIGHT SIDE
AIRCRAFT MISSION DESIGN SERIESF/A18A
OTHER ITEMS IN FSC 1560 — Airframe Structural Components
Items in the same Federal Supply class. No interchangeability or substitution relationship is implied.
1560-00-000-0047 1560-00-001-1849 1560-00-001-1850 1560-00-001-1851 1560-00-001-2368 1560-00-001-2478 1560-00-001-2479 1560-00-001-2480
SUBSTITUTES & CROSS-REFERENCES

No substitute or cross-reference records for this part.

LIFECYCLE
NSN statusActive· U.S. Government catalog
Demilitarization required — mutilation + specific procedure
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FREQUENTLY ASKED QUESTIONS
What is 74A314377-2005?
74A314377-2005 is a FORMER,AIRCRAFT.
What is the NSN for 74A314377-2005?
74A314377-2005 is cataloged in the U.S. Government catalog under NSN 1560-01-600-2170. This indicates validated use in U.S. government and defense supply chains.
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