PartsTable TECHNICAL DATA SHEET
NSN 2840-00-898-9124Government record, cited

Disk and Shaft, Axial Compressor,2840-00-898-9124

NSN 2840-00-898-9124 · NIIN 008989124 · Part number 1-100-287-04
Rolls-Royce Deutschland Ltd & Co Kg · FSC 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components · FSG 28 — Engines, Turbines, and Components · CAGE D0272
Government record, cited
NSN 2840-00-898-9124 — this item is cataloged by the U.S. Government under National Stock Number 2840-00-898-9124. Manufacturer of record part number: 1-100-287-04.
Also searched as  2840-00-898-9124 · 2840008989124 · NIIN 008989124 · 00-898-9124 · FSC 2840 Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components · CAGE D0272 · 1-100-287-04
Nearby stock numbers  ·
Features
  • Disk and Shaft,axial Compressor, — FSC 2840
  • General Characteristics Item Description: STEEL AMS6382,ROCKWELL C SCALE 34 MIN,37 MAX HARDNESS,4.922 IN. MIN,4.946 IN. MAX O/A LG,TAPERED OD DISK,5.927 IN. MIN,5.937 IN. MAX LARGEST OD,5.872 IN. MIN,5.882 IN. MAX SMALLEST OD,0.922 IN. MIN,0.924 IN. MAX W,31 BLADE GROOVES EQUALLY SPACED ON OD,FIRST END,3.456 IN. MIN,3.466 IN. MAX LG FROM SHAFT END TO DISK,SECOND END,0.544 IN. MIN,0.556 IN. MAX LG FROM HUB END TO DISK,4.4180 IN. MIN,4.4185 IN. MAX LARGEST HUB OD,10 HOLES DRILLED LONGITUDINALLY THROUGH HUB,0.319 IN. MIN,0.323 IN. MAX DIA,COUNTERBORED 0.533 IN. MIN,0.543 IN. MAX DIA BY 0.220 IN. DEPTH,HOLES EQUALLY SPACED ON 3.560 IN. NOM BOLT CIRCLE DIA,FIRST END FIRST COMPLEMENT,EXTERNAL THD 1.750 IN. -16 UN CL 3A THD,0.356 IN. MIN,0.376 IN. MAX THD LG (INCL THD RELIEF),FIRST END SECOND COMPLEMENT,EXTERNAL SPLINE,45 TEETH,30 DEG PRESSURE ANGLE,0.163 IN. MIN,0.173 IN. MAX SPLINE LG,1.9137 IN. MIN,19167 IN. MAX OD,1.8750 IN. NOM PITCH DIA,0.506 IN. MIN,0.526 IN. MAX DISTANCE FROM SHAFT END TO SPLINE A
  • 1 manufacturer part number on file
  • Manufacturer of record: Rolls-Royce Deutschland Ltd & Co Kg
Identification
  • NSN: 2840-00-898-9124
  • NIIN: 008989124
  • FSC: 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
  • FSG: 28 — Engines, Turbines, and Components
  • Primary part number: 1-100-287-04
  • Manufacturer: Rolls-Royce Deutschland Ltd & Co Kg
General Description

The Disk and Shaft,axial Compressor,, cataloged under National Stock Number 2840-00-898-9124, is classified within Federal Supply Class 2840 (Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components) of the Engines, Turbines, and Components group. The manufacturer of record is Rolls-Royce Deutschland Ltd & Co Kg. Government technical data includes 1 specification, cited from the U.S. Government catalog. The record lists 1 manufacturer part number for this item, enabling identification through both NSN and commercial part number lookups. 1 additional reference document (drawings, advisory and superseded references) is recorded in the U.S. Government catalog. Current acquisition status: Active.

Technical Specifications
ParameterValue
NSN2840-00-898-9124
Primary Part Number1-100-287-04
Item NameDisk and Shaft,axial Compressor,
FSC / FSG2840 / 28 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
ManufacturerRolls-Royce Deutschland Ltd & Co Kg
StatusACTIVE
General Characteristics Item DescriptionSTEEL AMS6382,ROCKWELL C SCALE 34 MIN,37 MAX HARDNESS,4.922 IN. MIN,4.946 IN. MAX O/A LG,TAPERED OD DISK,5.927 IN. MIN,5.937 IN. MAX LARGEST OD,5.872 IN. MIN,5.882 IN. MAX SMALLEST OD,0.922 IN. MIN,0.924 IN. MAX W,31 BLADE GROOVES EQUALLY SPACED ON OD,FIRST END,3.456 IN. MIN,3.466 IN. MAX LG FROM SHAFT END TO DISK,SECOND END,0.544 IN. MIN,0.556 IN. MAX LG FROM HUB END TO DISK,4.4180 IN. MIN,4.4185 IN. MAX LARGEST HUB OD,10 HOLES DRILLED LONGITUDINALLY THROUGH HUB,0.319 IN. MIN,0.323 IN. MAX DIA,COUNTERBORED 0.533 IN. MIN,0.543 IN. MAX DIA BY 0.220 IN. DEPTH,HOLES EQUALLY SPACED ON 3.560 IN. NOM BOLT CIRCLE DIA,FIRST END FIRST COMPLEMENT,EXTERNAL THD 1.750 IN. -16 UN CL 3A THD,0.356 IN. MIN,0.376 IN. MAX THD LG (INCL THD RELIEF),FIRST END SECOND COMPLEMENT,EXTERNAL SPLINE,45 TEETH,30 DEG PRESSURE ANGLE,0.163 IN. MIN,0.173 IN. MAX SPLINE LG,1.9137 IN. MIN,19167 IN. MAX OD,1.8750 IN. NOM PITCH DIA,0.506 IN. MIN,0.526 IN. MAX DISTANCE FROM SHAFT END TO SPLINE A
Lifecycle & Compliance
Acquisition StatusACTIVE
DEMIL CodeDEMIL B — Remove Demilitarization Key Points
HazardNo hazard code in the DLA record (HMIC N)
Criticality CodeX
Cross-Reference Index
Part NumberManufacturer
1-100-287-04 Rolls-Royce Deutschland Ltd & Co Kg (DEU)
Reference documents
ReferenceMeaning
1-100-287-04 3/2 Design control — primary reference
U.S. Government activity
No interchangeability data on file.
Other items in FSC 2840 — Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
Items in the same Federal Supply class. No interchangeability or substitution relationship is implied.
2840-00-000-0048
ENGINE,AIRCRAFT,TURBO-SHAFT
2840-00-000-0049
MODIFICATION KIT,ENGINE
2840-00-001-1741
CASE AND NOZZLE ASSEMBLY,TURBINE
2840-00-001-1743
2840-00-001-1743 · Item name not on file
2840-00-001-2117
2840-00-001-2117 · Item name not on file
2840-00-001-2284
2840-00-001-2284 · Item name not on file
2840-00-001-3922
2840-00-001-3922 · Item name not on file
2840-00-001-4903
SEAL,AIR,AIRCRAFT GAS TURBINE EN

Frequently Asked Questions

What is NSN 2840-00-898-9124?

NSN 2840-00-898-9124 is a Disk and Shaft,axial Compressor,, manufactured by Rolls-Royce Deutschland Ltd & Co Kg, classified under FSC 2840, Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components. Status: active.

What part numbers are listed for NSN 2840-00-898-9124?

NSN 2840-00-898-9124 has 1 manufacturer part number on file: 1-100-287-04 (Rolls-Royce Deutschland Ltd & Co Kg).

What are the specifications of 1-100-287-04?

Key specifications for 1-100-287-04: General Characteristics Item Description: STEEL AMS6382,ROCKWELL C SCALE 34 MIN,37 MAX HARDNESS,4.922 IN. MIN,4.946 IN. MAX O/A LG,TAPERED OD DISK,5.927 IN. MIN,5.937 IN. MAX LARGEST OD,5.872 IN. MIN,5.882 IN. MAX SMALLEST OD,0.922 IN. MIN,0.924 IN. MAX W,31 BLADE GROOVES EQUALLY SPACED ON OD,FIRST END,3.456 IN. MIN,3.466 IN. MAX LG FROM SHAFT END TO DISK,SECOND END,0.544 IN. MIN,0.556 IN. MAX LG FROM HUB END TO DISK,4.4180 IN. MIN,4.4185 IN. MAX LARGEST HUB OD,10 HOLES DRILLED LONGITUDINALLY THROUGH HUB,0.319 IN. MIN,0.323 IN. MAX DIA,COUNTERBORED 0.533 IN. MIN,0.543 IN. MAX DIA BY 0.220 IN. DEPTH,HOLES EQUALLY SPACED ON 3.560 IN. NOM BOLT CIRCLE DIA,FIRST END FIRST COMPLEMENT,EXTERNAL THD 1.750 IN. -16 UN CL 3A THD,0.356 IN. MIN,0.376 IN. MAX THD LG (INCL THD RELIEF),FIRST END SECOND COMPLEMENT,EXTERNAL SPLINE,45 TEETH,30 DEG PRESSURE ANGLE,0.163 IN. MIN,0.173 IN. MAX SPLINE LG,1.9137 IN. MIN,19167 IN. MAX OD,1.8750 IN. NOM PITCH DIA,0.506 IN. MIN,0.526 IN. MAX DISTANCE FROM SHAFT END TO SPLINE A. 1 specification is documented in the U.S. Government catalog.

Is NSN 2840-00-898-9124 hazardous material?

No hazard code in the DLA record (HMIC N). Hazard information on this page is shown exactly as it appears in the DLA record.

What is the DEMIL code for NSN 2840-00-898-9124?

NSN 2840-00-898-9124 has DEMIL Code B. 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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