STC SA890GL

SA890GL Kaman Corporation Aircraft Wheel and Brake, LLC 1160 Center Road Avon, OH 44011 Part 23 Federal Aviation Regulations A24CE Textron Aviation Inc.

200, 200C, 200CT, 200T, A200, A200C, A200CT, B200, B200C, B200CT, B200T, B200GT, B200CGT Install Parker Hannifin Corporation, Aircraft Wheel & Brake Division Conversion Kit 199-110, revision AB, dated June 18, 2010, and if applicable, install Parker Hannifin Corporation, Aircraft Wheel & Brake Division Hot Air Manifold Kit 199-168, revision F, dated June 18, 2010, in accordance with Installation Drawing 50-79, revision N, dated June 18, 2010, or later FAA approved revisions.

1) This installation is restricted to those aircraft with standard landing gear (18x5.5 Main Wheel & Brakes).

February 13, 1985 September 19, 2022 April 16, 1985 December 15, 2010 Steven L. Lardinois Manager, Systems Section Chicago ACO Branch 3

SA890GL 3

SA890GL Date Reissued: September 19, 2022

(Continued from Page 1: Limitations and Conditions)

2) The installer must determine whether this design change is compatible with previously approved modifications.

3) 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.

4) For B200GT and B200CGT models, information regarding operation of the Brake De-lce System is contained in the Main Body of the Airplane Flight Manual. For all other models the Brake De-Ice System Airplane Flight Manual Supplement, approved on October 19, 1988, or later FAA Approved revision must be carried in the aircraft at all times.

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