STC SA2551CE

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the proper ty of the STC holder.

FAA Form 8110-2 (5/14) Page 1 of This certificate issued to:

Part of the Original Product – Type Certificate Number: Make:

By Direction of the Administrator Signature Title 2 SA2551CE Curry Aviation, LLC 616 N. Palmetto Street Leesburg, FL 34748 Civil Air Regulations.3 Establishes the compatibility to install the flap actuated aileron droop system per STC SA1689WE, and the wing leading edge cuffs, drooped tips and stall fences per STC SA910CE.

1. Compatibility of this design with previously approved modification must be determined by the installer.

2. Before installation, the aircraft must be previously modified by STC SA1689WE.

3. Before installation, the aircraft must be previously modified by STC SA910CE.

for Paul Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service Textron Aviation (Cessna) 172, A, B, C, D, E, F, G, H, I, K, L, M, N, P 12/16/2022October 19, 1989 October 27, 1989 3A12

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the proper ty of the STC holder.

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

2 SA2551CE