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160D611637-33 — PLATE,STRUCTURAL,AIRCRAFT

✓ Government record, cited
— · COMPONENT
PRODUCT OVERVIEW

160D611637-33: PLATE,STRUCTURAL,AIRCRAFT.

The PLATE,STRUCTURAL,AIRCRAFT is a the manufacturer industrial component. Key specifications include material: ALUMINUM ALLOY, overall_width: 2.000 INCHES NOMINAL IN, overall_length: 6.000 INCHES NOMINAL IN, special_features: MANUFACTURED SUGGESTED NAME(SHIM-LAMINATED); DIMENSIONS ARE STOCKSIZE; ADDITIONAL WS 0.00; NHA 160D611103, aircraft_location: WS23.00 AND 66.00, material_thickness: 0.090 INCHES NOMINAL IN. This part is cataloged in the U.S.

Government catalog under NSN 1560-01-490-9679, 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
160D611637-33
NSN: 1560-01-490-9679
FSC: 1560 — Airframe Structural Components
CAGE: 79RG9 — NORTHROP GRUMMAN SYSTEMS CORPORATION (USA)
SPECIFICATIONS
materialALUMINUM ALLOY
overall_width2.000 INCHES NOMINAL IN
overall_length6.000 INCHES NOMINAL IN
special_featuresMANUFACTURED SUGGESTED NAME(SHIM-LAMINATED); DIMENSIONS ARE STOCKSIZE; ADDITIONAL WS 0.00; NHA 160D611103
aircraft_locationWS23.00 AND 66.00
material_thickness0.090 INCHES NOMINAL IN
aircraft_mission_design_seriesA-10
material_document_and_classificationAMS4013 ASSN STD SINGLE MATERIAL RESPONSE
NSN1560-01-490-9679
COMPONENT DIAGRAM
COMPONENT MAIN IC EDGE CONNECTOR No detailed specs available PLATE,STRUCTURAL,AIRCRAFT TITLE COMPONENT PN 160D611637-33 MFR PLATE,STRUCTURAL,AIRCR
KEY FEATURES
•
MATERIAL DOCUMENT AND CLASSIFICATION: AMS4013 ASSN STD SINGLE MATERIAL RESPONSE
•
MATERIAL THICKNESS: 0.090 INCHES NOMINAL IN
•
AIRCRAFT LOCATION: WS23.00 AND 66.00
•
MATERIAL: ALUMINUM ALLOY
•
AIRCRAFT MISSION DESIGN SERIES: A-10
TECHNICAL CHARACTERISTICS
MATERIAL DOCUMENT AND CLASSIFICATIONAMS4013 ASSN STD SINGLE MATERIAL RESPONSE
OVERALL LENGTH6.000 INCHES NOMINAL IN
OVERALL WIDTH2.000 INCHES NOMINAL IN
MATERIAL THICKNESS0.090 INCHES NOMINAL IN
SPECIAL FEATURESMANUFACTURED SUGGESTED NAME(SHIM-LAMINATED); DIMENSIONS ARE STOCKSIZE; ADDITIONAL WS 0.00; NHA 160D611103
AIRCRAFT LOCATIONWS23.00 AND 66.00
MATERIALALUMINUM ALLOY
AIRCRAFT MISSION DESIGN SERIESA-10
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 1
160D611637-17Reference document
Same NSN cross-reference
Reference document — Secondary reference
LIFECYCLE
NSN statusActive· U.S. Government catalog
Acquisition advice: Insurance item — stocked against contingency demandNo demilitarization required
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FREQUENTLY ASKED QUESTIONS
What is 160D611637-33?
160D611637-33 is a PLATE,STRUCTURAL,AIRCRAFT.
What parts can replace 160D611637-33?
There is 1 known substitute for 160D611637-33: 160D611637-17. Substitute compatibility should be verified for your specific system.
What is the NSN for 160D611637-33?
160D611637-33 is cataloged in the U.S. Government catalog under NSN 1560-01-490-9679. This indicates validated use in U.S. government and defense supply chains.
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