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NSN 1560-01-481-2955Government record, cited

Plate, Structural, Aircraft1560-01-481-2955

NSN 1560-01-481-2955 · NIIN 014812955
FSC 1560 — Airframe Structural Components · FSG 15 — Aircraft and Airframe Components
Government record, cited
Also searched as  1560-01-481-2955 · 1560014812955 · NIIN 014812955 · 01-481-2955 · FSC 1560 Airframe Structural Components · E10-20511 · E10-20511-23
Nearby stock numbers  ·
Features
  • Plate,structural,aircraft — FSC 1560
  • Aircraft Station Number: NS50.42
  • Surface Treatment Document and Classification: MIL-C-81706 MIL SPEC 1ST TREATMENT RESPONSE AND MIL-P-85582 MIL SPEC 2ND TREATMENT RESPONSE
  • Relationship to Similar Equipment: SIMILAR TO LOCKHEED (36659) P/N 803416-23, DOOR ASSEMBLY
  • Criticality Code Justification: AGAV
  • Material Document and Classification: QQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE
  • Material Thickness: 1.670 INCHES MINIMUM AND 1.730 INCHES MAXIMUM IN
  • Aircraft Location: MID-TAILPIPE, INBOARD NACELLE
Identification
  • NSN: 1560-01-481-2955
  • NIIN: 014812955
  • FSC: 1560 — Airframe Structural Components
  • FSG: 15 — Aircraft and Airframe Components
General Description

The Plate,structural,aircraft, cataloged under National Stock Number 1560-01-481-2955, is classified within Federal Supply Class 1560 (Airframe Structural Components) of the Aircraft and Airframe Components group. Government technical data includes 9 specifications, cited from the U.S. Government catalog. 2 additional reference documents (drawings, advisory and superseded references) are recorded in the U.S. Government catalog. Current acquisition status: Active.

Technical Specifications
ParameterValue
NSN1560-01-481-2955
Item NamePlate,structural,aircraft
FSC / FSG1560 / 15 — Airframe Structural Components
StatusACTIVE
Aircraft Station NumberNS50.42
Surface Treatment Document and ClassificationMIL-C-81706 MIL SPEC 1ST TREATMENT RESPONSE AND MIL-P-85582 MIL SPEC 2ND TREATMENT RESPONSE
Relationship to Similar EquipmentSIMILAR TO LOCKHEED (36659) P/N 803416-23, DOOR ASSEMBLY
Criticality Code JustificationAGAV
Material Document and ClassificationQQ-A-250/5 FED SPEC SINGLE MATERIAL RESPONSE
Material Thickness1.670 INCHES MINIMUM AND 1.730 INCHES MAXIMUM IN
Aircraft LocationMID-TAILPIPE, INBOARD NACELLE
MaterialALUMINUM ALLOY 2024
Aircraft Mission Design SeriesP-3 ALL
Lifecycle & Compliance
Acquisition StatusACTIVE
DEMIL CodeDEMIL Q — CCL Item — Commerce Control List
HazardPossible hazard — SDS may be required (DLA HMIC P)
Criticality CodeY
Cross-Reference Index
No manufacturer part numbers on file in the U.S. Government catalog.
Reference documents
ReferenceMeaning
E10-20511 D/9 Drawing number reference only
U.S. Government activity
E10-20511-23 3/2 Design control — primary reference
U.S. Government activity

Frequently Asked Questions

What is NSN 1560-01-481-2955?

NSN 1560-01-481-2955 is a Plate,structural,aircraft, classified under FSC 1560, Airframe Structural Components. Status: active.

What are the specifications of 1560-01-481-2955?

Key specifications for 1560-01-481-2955: Aircraft Station Number: NS50.42; Surface Treatment Document and Classification: MIL-C-81706 MIL SPEC 1ST TREATMENT RESPONSE AND MIL-P-85582 MIL SPEC 2ND TREATMENT RESPONSE; Relationship to Similar Equipment: SIMILAR TO LOCKHEED (36659) P/N 803416-23, DOOR ASSEMBLY; Criticality Code Justification: AGAV. 9 specifications are documented in the U.S. Government catalog.

Is NSN 1560-01-481-2955 hazardous material?

Possible hazard — SDS may be required (DLA HMIC P). Hazard information on this page is shown exactly as it appears in the DLA record.

What is the DEMIL code for NSN 1560-01-481-2955?

NSN 1560-01-481-2955 has DEMIL Code Q. Demilitarization may be required before disposal or transfer to non-military entities.

Sources

U.S. Government catalog: edition PUBLOGDVD v12.0.0 (OCT 2026), edition date 2026-10-01, retrieved 2026-10-16.

U.S. Government catalog: edition PUBLOGDVD v12.0.0 (OCT 2026), edition date 2026-10-01, retrieved 2026-10-18.

✓ Data cited from the U.S. Government catalog; commercial cross-references from OEM and certified industry sources.
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