Please note: Due to this product's length and required packing material, the estimated freight charge quoted at the time of checkout will not be correct. Additional shipping and crating charges on top of the quoted freight charge will also apply. For an accurate estimate of actual shipping costs, please email your address and preferred ship method to our Shipping department at shipping@mcfarlaneaviation.com. This product can ONLY ship domestically via FedEx Express services (not including FedEx Ground) due to the length. Please contact our Shipping department for international shipping options. |
Flap Trailing Edge Stiffener for Cessna Aircraft
New streamline shape and improved fit to reduce stress cracks.
FAA-PMA Stiffener made of 6061 T6 Aluminum material.
Logbook entry is all that is required.
What is the purpose of a flap trailing edge stiffener?
McFarlane's stiffeners are streamlined and have the correct angle.
Original stiffeners deform the skins, resulting in cracks, strain in the corrugation, and stress around the rivet heads.
Early airplanes did not have a stiffener, but it can be added.
New Improved Fit to Reduce Skin Stress
Our new McFarlane 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 concentration in the skin corrugations and near the rivets making cracks less likely. McFarlane has improved the stiff ener angle as compared to other brand of triangle stiffeners.
New Streamline Shape
Our new design smoothly transitions from the skin surface to a blunt trailing edge without an unsightly bulb and resultant drag found on common trailing edge stiffeners. The new shape even weighs less than other bulky stiffeners.
Instructions for Continued Airworthiness
OEM Part Number | McFarlane Part Number | Comment |
1220100-27 | MC1741-116.25 | |
1220100-28 | MC1741-116.25 | |
1220100-37 | MC1741-116.25 | |
1220100-48 | MC1741-116.25 | |
1220100-49 | MC1741-116.25 | |
1741-116.25 | MC1741-116.25 |
Make | Series | Model | Beginning S/N | Ending S/N | Quantity Per Aircraft | Location | Eligibility Chart |
Cessna | 206 | 206 | 206-0001 | 206-0275 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | 206H | 20608001 | 206999999 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | P206 | P206-0002 | P206-0160 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | P206A | P206-0161 | P206-0306 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | P206B | P206-0307 | P206-0419 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | P206C | P206-0420 | P206-0519 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | P206D | P206-0520 | P206-0603 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | P206E | P20600604 | P20600647 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | T206H | T20608001 | T206999999 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | TP206A | P206-0191 | P206-0306 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | TP206B | P206-0307 | P206-0419 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | TP206C | P206-0420 | P206-0519 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | TP206D | P206-0520 | P206-0603 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | TP206E | P20600604 | P20600647 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | TU206A | U206-0487 | U206-0656 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | TU206B | U206-0657 | U206-0914 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | TU206C | U206-0915 | U206-1234 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | TU206D | U206-1235 | U206-1444 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | TU206E | U20601445 | U20601700 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | TU206F | U20601701 | U20602199 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | TU206F | U20602200 | U20603521 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | TU206G | U20603522 | U20607020 | 2 | Wing Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | U206 | U206-0276 | U206-0437 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | U206A | U206-0438 | U206-0656 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | U206B | U206-0657 | U206-0914 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | U206C | U206-0915 | U206-1234 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | U206D | U206-1235 | U206-1444 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | U206E | U20601445 | U20601700 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | U206F | U20601701 | U20602199 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | U206F | U20602200 | U20603521 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 206 | U206G | U20603522 | U20607020 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 207 | 207 | 20700001 | 20700362 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 207 | 207A | 20700363 | 20700788 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 207 | T207 | 20700001 | 20700362 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 207 | T207A | 20700363 | 20700788 | 2 | Flap Trailing Edge Stiffener | 1743 |
Cessna | 210 | 210D | 21058221 | 21058510 | 2 | Flap Trailing edge Stiffener | 1743 |
Cessna | 210 | 210E | 21058511 | 21058715 | 2 | Flap Trailing edge Stiffener | 1743 |
Cessna | 210 | 210F | 21058716 | 21058818 | 2 | Flap Trailing edge Stiffener | 1743 |
Cessna | 210 | T210F | T210-0001 | T210-0197 | 2 | Flap Trailing edge Stiffener | 1743 |
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Please verify product details for suitability for your application.