2840-33-210-6419

Aircraft Gas Turbine Engine Front Frame Strut

2840332106419 332106419 TP290139 TP290146

A rigid piece designed to resist pressure in the direction of its length. It is positioned between the inner and outer rings and is a main component of a FRAME, FRONT, AIRCRAFT GAS TURBINE ENGINE. View more Aircraft Gas Turbine Engine Front Frame Strut

2840-33-210-6419 STRUT,FRONT FRAME,AIRCRAFT GAS TURBINE ENGINE 2840332106419 332106419

Managed by Spain
NSN Created on 4 Dec 2012
Data Last Changed
January 2023
NATO Update Count
1
NATO Data Quality
2840-33-210-6419 STRUT,FRONT FRAME,AIRCRAFT GAS TURBINE ENGINE 2840332106419 332106419 1/1
NSN 2840-33-210-6419 (Generic Image) 1/1

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2840-33-210-6419 2840332106419 332106419,TP290139,TP290146
TP290139 TP290146 A rigid piece designed to resist pressure in the direction of its length.
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,TP290139,TP290146 TP290139TP290146 A rigid piece designed to resist pressure in the direction of its
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Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components from Spain (ES)
Aircraft Gas Turbine Engine Airflow Baffle M541A3361200RNCC: 3 | RNVC: 2 | DAC: 1 5 Jun 2013 2840-33-210-6419

2840-33-210-6419 Demil Restrictions 2840-33-210-6419

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

2840-33-210-6419 is a Aircraft Gas Turbine Engine Front Frame Strut

2840-33-210-6419 End Users End Users 2840-33-210-6419

Germany (ZG)

2840-33-210-6419 Manufacturers Approved Sources 2840-33-210-6419

Part Number
Manufacturer
Status
TP290139
8338B - Industria De Turbo Propulsores (Active)
Primary Buy
RNCC 3 RNVC 2 DAC 1
TP290146
8338B - Industria De Turbo Propulsores (Active)
Secondary Buy
RNCC 5 RNVC 2 DAC 1

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