STC SA1854WE

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

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Title SA1854WE Sabreliner Aviation, LLC 1390 Highway H Perryville, MO 63775 4b Civil Air Regulations. (See T.C. Data Sheet A2WE) 2 A2WE NA-265 Installation of aft ballast, optional large capacity batteries, heavy duty landing gear assemblies, and extended center of gravity limits. Modifications shall be in accordance with:

(1) "Sealed Equipment List" dated December 18, 1968, (Pages 2.5 through 2.9 contained in TFD 68-1180).

(2) Sealed Rockwell International corporation Drawings 282-053201-30 "B," 282-300019 "B," 282-300457 "B," and 282-311010 "A."

(3) Sealed Rockwell International Engineering Orders 13070, 13073, and 13572, or FAA approved revision.

Rockwell International The approval of this change in type design applies to the model NA-265 only. 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 the other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane. This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight in the fuselage. The center of gravity limits are contained on pages 2.2 and 2.4 of Rockwell International TFD 68-1180 dated December 18, 1968.

FAA Approved Aifplane Flight Manual MA-61-3 Supplement No. 1 dated December 20, 1968 is required.

December 18, 1968 July 23, 1973; June 30, 1983; March 7, 2014 December 20, 1968 Grant E. Youngdahl Program Manager Wichita Aircraft Certification Office

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

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