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204-70045-363 — LONGERON

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

204-70045-363: LONGERON.

The LONGERON is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY 2024, overall_width: 3.700 INCHES NOMINAL IN, overall_length: 74.500 INCHES NOMINAL IN, special_features: HEAT TREAT T62; FINISH SRF-2.30, aircraft_location: LOWER FORWARD,COWL PANEL ASSY-ENGINE NACELLE, material_thickness: 0.050 INCHES NOMINAL IN. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-110-6516, 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
204-70045-363
NSN: 1560-01-110-6516
FSC: 1560 — Airframe Structural Components
CAGE: 81205 — THE BOEING COMPANY DIV DEFENSE (USA)
SPECIFICATIONS
materialALUMINUM ALLOY 2024
overall_width3.700 INCHES NOMINAL IN
overall_length74.500 INCHES NOMINAL IN
special_featuresHEAT TREAT T62; FINISH SRF-2.30
aircraft_locationLOWER FORWARD,COWL PANEL ASSY-ENGINE NACELLE
material_thickness0.050 INCHES NOMINAL IN
side_for_which_designedLEFT SIDE
aircraft_mission_design_seriesE-3A A
material_document_and_classificationQQ-A-250/5-0 FED SPEC SINGLE MATERIAL RESPONSE
NSN1560-01-110-6516
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available LONGERON TITLE COMPONENT PN 204-70045-363 MFR LONGERON
KEY FEATURES
•
MATERIAL DOCUMENT AND CLASSIFICATION: QQ-A-250/5-0 FED SPEC SINGLE MATERIAL RESPONSE
•
MATERIAL THICKNESS: 0.050 INCHES NOMINAL IN
•
AIRCRAFT LOCATION: LOWER FORWARD,COWL PANEL ASSY-ENGINE NACELLE
•
MATERIAL: ALUMINUM ALLOY 2024
•
SIDE FOR WHICH DESIGNED: LEFT SIDE
TECHNICAL CHARACTERISTICS
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-250/5-0 FED SPEC SINGLE MATERIAL RESPONSE
OVERALL LENGTH74.500 INCHES NOMINAL IN
OVERALL WIDTH3.700 INCHES NOMINAL IN
MATERIAL THICKNESS0.050 INCHES NOMINAL IN
SPECIAL FEATURESHEAT TREAT T62; FINISH SRF-2.30
AIRCRAFT LOCATIONLOWER FORWARD,COWL PANEL ASSY-ENGINE NACELLE
MATERIALALUMINUM ALLOY 2024
SIDE FOR WHICH DESIGNEDLEFT SIDE
AIRCRAFT MISSION DESIGN SERIESE-3A A
OTHER ITEMS IN FSC 1560 — Airframe Structural Components
Items in the same Federal Supply class. No interchangeability or substitution relationship is implied.
1560-00-003-1977 1560-00-003-3257 1560-00-004-4244 1560-00-005-7280 1560-00-006-0576 1560-00-006-6538 1560-00-007-9578 1560-00-009-4192
SUBSTITUTES & CROSS-REFERENCES

No substitute or cross-reference records for this part.

LIFECYCLE
NSN statusActive· U.S. Government catalog
Acquisition advice: Insurance item — stocked against contingency demandDemilitarization required — critical (Q)
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FREQUENTLY ASKED QUESTIONS
What is 204-70045-363?
204-70045-363 is a LONGERON.
What is the NSN for 204-70045-363?
204-70045-363 is cataloged in the U.S. Government catalog under NSN 1560-01-110-6516. This indicates validated use in U.S. government and defense supply chains.
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