# STC SA2753CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Walter Timothy Miller, United States
- Description: Installation of flap actuated landing gear warning system.
- Applied: August 6, 1991
- Status date: October 5, 2023
- Product: Aircraft, Small Airplane
- Data sheets: [TCDS A-777](https://openairdocs.org/tcds/A-777)
- Certificate PDF: https://openairdocs.org/files/sha256/a7/b5/a7b514a4c3a899e59d13ca93463400f892e564262dcd51bacc81331582cd5093
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135752197420240422161821.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA2753CE

## ADs that name it (0)

None.

## Approved models (9)

- Raytheon Aircraft Company 35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company 35R ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company A35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company B35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company C35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company D35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company E35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company F35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Raytheon Aircraft Company G35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

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)

## Every issue (1)

- October 5, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/a7/b5/a7b514a4c3a899e59d13ca93463400f892e564262dcd51bacc81331582cd5093)

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