STC SA2753CE

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. A-777 for complete certification basis).

Original Product --T ype 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 modifications 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 sup port 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 A-777 M ake : Beech Aircraft Corporation M odel : 35, A35, B35, C35, D35, E35, F35, G35, 35R Date reissued : May 11, 1995; May 7, 1997;

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

By d ir ection 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

Dat e of issuance : August 21, 1991

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

Transfer the ownership of Supplemental Type Certificate Number

to (Name of transferee)

(Address of transferee) (Number and street)

(City, State, and ZIP code)

from (Name of grantor) (Print of type)

(Address of grantor) (Number and street)

(City, State, and ZIP code)