STIFFENER: FLAP TRAILING EDGE,

STIFFENER: FLAP TRAILING EDGE,

McFarlane Aviation

Part # MC1741-116-25=2M

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Mfr Part # MC1741-116.25

Forecastable
8130-3 Eligible
Forecastable
8130-3 Eligible
This aluminum stiffener is specifically designed for Cessna Aircrafts flap trailing edge. Made from 6061 T6 aluminum, it enhances fit and reduces stress cracks while reinforcing the structure. Its streamlined design minimizes rivet stress and deformation, contributing to the durability of the aircraft component with straightforward installation requirements.
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Boeing Distribution (formerly Aviall)

Overview

The McFarlane MC1741-116.25 Stiffener for Flap Trailing Edge is designed for Cessna Aircraft, crafted from 6061 T6 aluminum. This FAA-PMA approved stiffener features a streamlined shape that improves fit and reduces the likelihood of stress cracks. It reinforces the flap trailing edge, ensuring a straight appearance while enhancing resilience against hangar rash. The design minimizes stress around rivets, preventing cracks and deformation, thus contributing to the safety of pilots and passengers. Installation requires only a simple logbook entry.

Features & Benefits

  • Made from 6061 T6 aluminum
  • Streamlined design for improved fit
  • Reduces stress and prevents cracks
  • Enhances safety and appearance of the flap trailing edgeMcFarlane Stiffener, Flap Trailing Edge

Technical Information

FAA Approval Code

PMA

Condition

New

Country of Origin

United States

Harmonized Tariff Schedule Code

8807300010

Lead Time (Days)

30

Shelf Life

No

Forecasted

No

Shipping Details

Hazmat Code

ZND

ECCN

9A991.d

Schedule B

8807300010

8130-3 Eligible

Yes

Hazmat

No

Part Explosive

No
Buy now from
Boeing Distribution (formerly Aviall)
DISCLAIMER: Product information provided “as is.” Boeing may add, change, discontinue or remove this information at any time. Product photos may not be exact match to product delivered. See terms & conditions.