PartsTable TECHNICAL DATA SHEET
NSN 1615-01-425-4920Government record, cited

Blade, Lag Shock Abs1615-01-425-4920

NSN 1615-01-425-4920 · NIIN 014254920 · Part number 423R2700-1
The Boeing Company · FSC 1615 — Helicopter Rotor Blades, Drive Mechanisms and Components · FSG 16 — Aircraft Components and Accessories · CAGE 77272
Government record, cited
NSN 1615-01-425-4920 — this item is cataloged by the U.S. Government under National Stock Number 1615-01-425-4920. Manufacturer of record part number: 423R2700-1.
Also searched as  1615-01-425-4920 · 1615014254920 · NIIN 014254920 · 01-425-4920 · FSC 1615 Helicopter Rotor Blades, Drive Mechanisms and Components · CAGE 77272 · 423R2700-1
Nearby stock numbers  ·
Features
  • Blade,lag Shock Abs — FSC 1615
  • 1 manufacturer part number on file
  • Manufacturer of record: The Boeing Company
Identification
  • NSN: 1615-01-425-4920
  • NIIN: 014254920
  • FSC: 1615 — Helicopter Rotor Blades, Drive Mechanisms and Components
  • FSG: 16 — Aircraft Components and Accessories
  • Primary part number: 423R2700-1
  • Manufacturer: The Boeing Company
General Description

The Blade,lag Shock Abs, cataloged under National Stock Number 1615-01-425-4920, is classified within Federal Supply Class 1615 (Helicopter Rotor Blades, Drive Mechanisms and Components) of the Aircraft Components and Accessories group. The manufacturer of record is The Boeing Company. The record lists 1 manufacturer part number for this item, enabling identification through both NSN and commercial part number lookups. Current acquisition status: Active.

Technical Specifications
ParameterValue
NSN1615-01-425-4920
Primary Part Number423R2700-1
Item NameBlade,lag Shock Abs
FSC / FSG1615 / 16 — Helicopter Rotor Blades, Drive Mechanisms and Components
ManufacturerThe Boeing Company
StatusACTIVE
Lifecycle & Compliance
Acquisition StatusACTIVE
DEMIL CodeDEMIL Q — CCL Item — Commerce Control List
HazardNo hazard code in the DLA record (HMIC N)
Criticality CodeF
Cross-Reference Index
Part NumberManufacturer
423R2700-1 PRIMARY The Boeing Company (USA)
No interchangeability data on file.
Other items in FSC 1615 — Helicopter Rotor Blades, Drive Mechanisms and Components
Items in the same Federal Supply class. No interchangeability or substitution relationship is implied.
1615-00-001-1399
1615-00-001-1399 · Item name not on file
1615-00-001-1400
1615-00-001-1400 · Item name not on file
1615-00-001-1774
1615-00-001-1774 · Item name not on file
1615-00-001-2675
1615-00-001-2675 · Item name not on file
1615-00-001-6441
1615-00-001-6441 · Item name not on file
1615-00-001-6442
1615-00-001-6442 · Item name not on file
1615-00-003-1146
BOLT ASSEMBLY,ROTARY WING HEAD
1615-00-003-1147
1615-00-003-1147 · Item name not on file

Frequently Asked Questions

What is NSN 1615-01-425-4920?

NSN 1615-01-425-4920 is a Blade,lag Shock Abs, manufactured by The Boeing Company, classified under FSC 1615, Helicopter Rotor Blades, Drive Mechanisms and Components. Status: active.

What part numbers are listed for NSN 1615-01-425-4920?

NSN 1615-01-425-4920 has 1 manufacturer part number on file: 423R2700-1 (The Boeing Company).

What are the specifications of 423R2700-1?

Key specifications for 423R2700-1: Special Features: DRAWING NAME=BLADE,LAG SHOCK ABSORBER ASSEMBLY; End Item Identification: HELICOPTER MODEL H-46. 0 specifications are documented in the U.S. Government catalog.

Is NSN 1615-01-425-4920 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 1615-01-425-4920?

NSN 1615-01-425-4920 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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