The Cover,strut Pad, cataloged under National Stock Number 2840-00-427-8027, is classified within Federal Supply Class 2840 (Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components) of the Engines, Turbines, and Components group. Government technical data includes 1 specification, cited from the U.S. Government catalog. 1 additional reference document (drawings, advisory and superseded references) is recorded in the U.S. Government catalog. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 2840-00-427-8027 |
| Item Name | Cover,strut Pad |
| FSC / FSG | 2840 / 28 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components |
| Status | ACTIVE |
| General Characteristics Item Description | CRES,AMS5510,2.250 IN. MIN,2.252 IN. MAX LG,1.300 IN. MIN,1.320 IN. MAX W,0.201 IN. MIN,0.211 IN. MAX,DIA OF HOLES LOCATEDON 0.960 IN. BY 1.840 IN. CENTERS IN |
| Acquisition Status | ACTIVE |
| DEMIL Code | DEMIL A — No Demilitarization Required |
| Hazard | No hazard code in the DLA record (HMIC N) |
| Criticality Code | X |
| Reference | Meaning |
|---|---|
| 3029T69P01 | 3/2 Design control — primary reference U.S. Government activity |
NSN 2840-00-427-8027 is a Cover,strut Pad, classified under FSC 2840, Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components. Status: active.
Key specifications for 2840-00-427-8027: General Characteristics Item Description: CRES,AMS5510,2.250 IN. MIN,2.252 IN. MAX LG,1.300 IN. MIN,1.320 IN. MAX W,0.201 IN. MIN,0.211 IN. MAX,DIA OF HOLES LOCATEDON 0.960 IN. BY 1.840 IN. CENTERS IN; End Item Identification: J-85 AIRCRAFT ENGINE. 1 specification is documented in the U.S. Government catalog.
No hazard code in the DLA record (HMIC N). Hazard information on this page is shown exactly as it appears in the DLA record.
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.