Aircraft Stiffener, Aluminum Alloy

Part # 16B1230-214

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STIFFENER
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Overview

Aircraft Stiffener 16B1230-214 is utilized in aircraft construction, specifically located at the bulkhead and designed for the aircraft station number FS110.50. This part plays a crucial role in maintaining the structural integrity of the aircraft at its designated location. The use of aluminum alloy contributes to its lightweight yet durable properties, making it suitable for aviation applications. The stiffener is essential for reinforcing the aircraft structure, providing necessary support and stability during operation.

Features & Benefits

  • Provides reinforcement at the bulkhead location
  • Supports structural integrity at aircraft station FS110.50

Technical Information

NIIN

015974407

NSN

1560-01-597-4407

FSCG

1560

FSCG Category

Airframe Structural Components

UNSPSC Code

25201500

UNSPSC Category

Aircraft fuselage and components

Lead Time (Days)

346

Product Class Description

Aircraft stiffener

Country of Origin

United States

Manufacturer CAGE Code

NOREQ

Storage Required

No

Unit Of Measure

EA

Pieces Per Pound

0

DFAR Applicable

No

Revision Level Applicable

Yes

Product Class

252015

Material Composition

ALUMINUM ALLOY

Design Holder CAGE Code

81755

Design Holder

LOCKHEED MARTIN CORPORATION DBA LOC

Potential Alternates

1560015974407

Shipping Details

Dry Ice

No

ECCN

9A991.d

Proprietary Part

No

Hazmat

No
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