• Wishlists
  • 877-477-7823
  • Contact Us
 
 
THE AVIATION SUPERSTORE FOR ALL YOUR AIRCRAFT & PILOT NEEDS | 877-4-SPRUCE
Thumbs 1
Thumbs 1

CESSNA FLAP TRAILING EDGE STIFFENER

From $86.75 to $157.75
Description Part Number Price Buy
FLAP TRAILING EDGE STIFFNER 79.5 05-00046 $86.75
Quantity
FLAP TRAILING EDGE STIFFNER 116.25" 05-07237 $157.75
Quantity
Subtotal $0.00
Add to Wishlist

Overview

Improved Fit to Reduce Skin Stress
The stiffeners are accurately shaped to the same angle that the top and bottom skins come together to completely eliminate the bending stress due to riveting the skins together. This prevents stress concentrations in the skin corrugations and near the rivets, making cracks less likely.

Streamline Shape
The design smoothly transitions from the skin surface to a blunt trailing edge. It maintains the flap's natural airfoil shape by eliminating the unsightly bulb and resultant drag found on common trailing edge stiffeners.

What is the purpose of a flap trailing edge stiffener?
    Reinforce the flap trailing edge to make it more resilient to hangar rash.
    Ensure a straight trailing edge. Without a stiffener, the trailing edge tends to have a "wavy" appearance where the top and bottom skin rivet together.
    Reduce stress in the flap skins and prevent cracks around the rivets. Without a stiffener of the proper shape, the skin must abruptly bend where the top and bottom skins rivet together.
    Provide a blunt surface to protect the foreheads of unsuspecting pilots and passengers.

Application Chart

Application Chart
Aircraft
Serial Number
Part No.
150
All
10-94001 79.5
152
All
10-94001 79.5
170
All
10-94001 79.5
172
All
10-94001 79.5
175
All
10-94001 79.5
180
All
10-94001 79.5
182
All
10-94001 79.5
185
All
10-94001 79.5
188
All
10-94001 79.5
206
All
10-94001 116
207
All
10-94001 116

Reviews

Q&A

Q: What are the length and width of each unit shipped?

The length of each unit shipped is 79.5" long. The manufacturer could not provide any width information. We were able to obtain the STC and Technical Supplement. Please review it by clicking here.

View in Catalog

View Image View in Catalog