STC SA2781CE

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

Part of the

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Title 1965, plus amendments and special conditions as listed on the type data sheet except FAR 25.1001 as * SA2781CE Textron Aviation Inc.

One Cessna Boulevard Wichita, KS 67215 25 Federal Aviation Regulations effective February 1, Cessna 560 * amended by Amendment 25-57.

3 A22CE Increases the maximum gross weight by 400 lbs in accordance with Cessna Engineering Change Record 029365, dated December 3, 1991, or later FAA approved revision, which results in a maximum design ramp weight of 16,500 lbs and maximum design takeoff weight of 16,300 lbs. The maximum landing weight of 15,200 lbs remains unchanged.

1. Airplanes are eligible for this modification only when the 12,200 lbs zero fuel weight option per ECR 26053 has been incorporated.

2. The FAA approved Airplane Flight Manual Supplement dated December 6, 1991, or later FAA approved revision is required equipment when this modification is installed.

(see continuation sheet 3 of 3) April 27, 2017 January 7, 1992 July 30, 1991 December 6, 1991 Mark Fuller STC ODA administrator ODA-100129-CE

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

To (Name and address of transferee)

From (Name and address of grantor)

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

Date of Issuance: December 6, 1991 Date Amended: January 7, 1992 Date Reissued: April 27, 2017

3. This approval should not be extended to other specific airplanes 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 will introduce no adverse effect upon the airworthiness of that airplane.

-- END -- 3 SA2781CE