STC SA83RM

FAA Form 8110-2 (5/14) Page 1 of 3

Reissued on July 31, 2017 to supersede the original STC, which has been lost or misplaced.

Number: SA83RM

Part 21/25 of the Federal Aviation Regulations.

RESTRICTED CATEGORY

Original Product – Type Certificate Number: A22CE Make: Cessna Model: 500

Increased Ramp and Takeoff Weights for Restricted Category operation, in accordance with Branson Aircraft Corporation Airplane Flight Manual Supplement, FAA approved October 22, 1976, or later FAA approved supplement.

Date of Application: September 01, 1976 Date Reissued: 7/21/81; 12/24/97; 9/8/05; 7/31/17 Date of Issuance: October 22, 1976 Date Amended:

Signature

Title Jim Grigg Manager, Fort Worth A CO Branch, Compliance & Airworthiness Division Sierra Industries, Ltd.

122 Howard Langford Drive Uvalde, TX 78801

FAA Form 8110-2 (5/14) Page 2 of 3

Transfer the ownership of Supplemental Type Certificate Number: SA83RM

To (Name and address of transferee)

From (Name and address of grantor)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA83RM

FAA Form 8110-2 (5/14) Page 3 of 3

Date of Issuance: October 22, 1976 Date of Reissuance: July 31, 2017

1. Eligible for Cessna Model 500 serial numbers 500-0303 and up, and -0071 thru -0302 incorporating SB32-23, and -0001 thru -0070 incorporating SB32-1 and SB32-23, provided it is determined that the operation permitted by this Supplemental Type Certificate is compatible with later changes to this model.

2. Increased Ramp and Takeoff Weights may only be used for Restricted Category operation.

3. FAA approved Flight Manual Supplement dated October 22, 1976 or later FAA approved revision is required.

4. This approval should not be extended to aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft.

5. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

-END-

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA83RM

FAA Form 8110-2 (5/14) Page 4 of 3