STC SA966CE

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 3 SA966CE Curry Aviation, LLC 616 N. Palmetto Street Leesburg, FL 34748 Civil Air Regulations.3* Installation of STOL Kit (wing leading edge cuffs, drooped tips, and stall fences). Data required:

1. FAA Approved STOL-Craft Drawing List No. 3, dated November 8, 1973 or April 30, 1986 or later FAA approved revision, for Models 210L, T210L, 210M, T210M, 210N, T210N, previously modified by STC SA760NW.

(continued on page 3)

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

2. Models 210N, T210N, P210N: eligible for installation of de-icer boots over the leading edge cuffs provided the airplane has factory installed provisions for de-icing.

(continued on page 3)

for Paul Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service Textron Aviation (Cessna) 210G, H, J, K, L, M, N;

T210G, H, J, K, L, M, N;

P210N 5/25/1977, 12/16/2022 5/25/78, 4/25/80, 2/8/82, 4/20/82, 4/30/88, 10/6/88, 4/17/92, 1/14/99 October 23, 1973 January 14, 1974 3A21

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):

3 SA966CE

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 3 of 3 Date reissued: 12/16/2022

Certification Basis (cont'd):

Civil Air Regulations effective May 15, 1956, and paragraph 3.112 as amended October 1, 1959.

Type Design Change (cont'd):

2. FAA Approved STOL-Craft Drawing List No. 3, dated October 6, 1998, or later FAA approved revision, for Models 210N, T210N, P210N, is required for installation of the de-icer boots over the leading edge cuff.

3. FAA Approved Airplane Flight Manual Supplement (AFMS), dated April 25, 1980, or later FAA approved revision, is required for Models 210N, T210N, Serial No. 21062955 and On, when this modification in installed.

4. FAA Approved Airplane Flight Manual Supplement (AFMS), dated or April 20, 1982, or later FAA approved revision, is required for Models 210N, T210N, Serial No. P21000151 and On when this modification in installed.

5. FAA Approved Airplane Flight Manual Supplement (AFMS), dated April 25, 1980, revised October 5, 1988, or later FAA approved revision, is required equipment for the Models 210N, T210N airplanes previously equipped with de-icer boots.

6. FAA Approved Airplane Flight Manual Supplement (AFMS), dated April 20, 1982, revised October 4, 1988, or later FAA approved revision, is required equipment for the Model P210N airplanes previously equipped with de-icer boots.

Limitation and Conditions (cont'd ):

3. Model T210N: eligible for this modification if previously modified by STC SA760NW.

4. Models 210K, L, M, N and T210K, L, M, N: eligible for this modification if previously modified by STC SA1202CE.

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