STC SA2754CE

certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon m eets the airworth iness requirements of Part 3 of the Federal Aviation R egulations .(See Type Certificate Data Sheet No. 3A15 for complete certification basis).

Original Product --Type Certificate N umber :

Installation of a flap actuated landing gear warning system in accordance with Platte Valley Aero Installation Instructions BZ-001, no revision, or BZ-002, no revision, or later FAA approved revisions.

1) Compatibility of this design change with previously approved modificati ons must be determined by the installer.

2) 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.

This certificat e and the support ing data which is the basis for approval shall remain in effect until surrendered, suspend ed, revoked or a termination date is otherwise established by the A dministrator of the F ederal A viation A dministr ation.

Walter Timothy Miller 2188 Canyonville Drive Henderson, NV 89044 3A15 M ake : Beech Aircraft Corporation M odel : 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, E33C, F33, F33A, F33C, G33, H35, J35, K35, M35, P35, S35, V35, V35A, V35B, 36, A36, A36TC, and B36TC Date reissued : May 11, 1995; May 7, 1997;

October 5, 2023 Date ame nded : October 7, 1991

B y d irection of the A dministr ator

(Signature) Paul (Vu) Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service

(Title)

Date of application : August 6, 1991

Date of issuance : August 21, 1991

FAA FORM 8110-2-1(10-69) PAGE 2 of 2 PAGES

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from (Name of grantor) (Print of type)

(Address of grantor) (Number and street)

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