# STC SA6067NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Aero Improvements, United States
- Description: Installation of an auxiliary cabin door latch pin and socket
- Applied: July 27, 1993
- Status date: February 2, 1994
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS 3A15](https://openairdocs.org/tcds/3A15), [TCDS A-777](https://openairdocs.org/tcds/A-777), [TCDS A23CE](https://openairdocs.org/tcds/A23CE), [TCDS 3A16](https://openairdocs.org/tcds/3A16), [TCDS 3A10](https://openairdocs.org/tcds/3A10)
- Certificate PDF: https://openairdocs.org/files/sha256/6c/4a/6c4a2e220f8fbe75a9f4f2a1f04917047fb1489a08feb2d52883ccc21ac33141
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C97D0B7FA409699E85256CC200569E4F.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA6067NM

## ADs that name it (0)

None.

## Approved models (71, first 50)

- Beechcraft Corporation 35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Beechcraft Corporation 35-33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation 35-A33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation 35-B33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation 35-C33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation 35-C33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation 35R ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Beechcraft Corporation 36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation 58P ([TCDS A23CE](https://openairdocs.org/tcds/A23CE))
- Beechcraft Corporation 58PA ([TCDS A23CE](https://openairdocs.org/tcds/A23CE))
- Beechcraft Corporation 58TC ([TCDS A23CE](https://openairdocs.org/tcds/A23CE))
- Beechcraft Corporation 58TCA ([TCDS A23CE](https://openairdocs.org/tcds/A23CE))
- Beechcraft Corporation 95-55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation 95-A55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation 95-B55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation 95-B55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation 95-B55B ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation 95-C55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation 95-C55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation A35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Beechcraft Corporation A36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation A36TC ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation B35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Beechcraft Corporation B36TC ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation C35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Beechcraft Corporation D35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Beechcraft Corporation D55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation D55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation E33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation E33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation E33C ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation E35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Beechcraft Corporation E55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation E55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation F33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation F33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation F33C ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation F35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Beechcraft Corporation G33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation G35 ([TCDS A-777](https://openairdocs.org/tcds/A-777))
- Beechcraft Corporation H35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation J35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation K35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation M35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation N35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation P35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation S35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation V35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation V35A ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation V35B ([TCDS 3A15](https://openairdocs.org/tcds/3A15))

All 71: https://openairdocs.org/stc/SA6067NM/models.md

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA6067NM This certificate issued to: Aero Improvements 2350 Oakleaf Canyon Road Walnut, California Part* of the * Regulations.

Original Product - Type bertificate Number: *See attached FAA Approved Model List (AML) No. SA6067NM for Make: * list of approved airplane Model: * models and applicable airworthness regulations.

Description of Type Design Change: Installation of an auxiliary cabin door latch pin and socket in accordance with Aero Improvements Master Drawing Lists on AML No. SA6067NM, dated January 19, 1994, or later FAA approved revision.

Limitations and Conditions: The approval of this modification applies to the above noted airplane model series only. This approval should not be extended to other specific airplanes of this model series on which other approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft.

w of the Federal Aviation Administration .

Date of Application: JUly 27, 1993 Jule issued: February 2, 1994 Date of Issuance: October 29, 1993 Jate uvended:

EDERAL AVIATION OMINISTRA TION Los Angeles Aircraft Certification Office Manager, Airtrame Dig Branch (Title)

47.

**FAA APPROVED MODEL LIST (AML) NO. SA6067NM**

**AERO IMPROVEMENTS FOR**

INSTALLATION OF AUXILIARY CABIN DOOR LATCH PIN & SOCKET Make: January 19, 1994 MASTER

**DRAWING LIST**

ORIGINAL CERTIFI- AML ITEM AIRPLANE MAKE MODEL AIRPLANE CERTIFICATE TYPE CATION BASIS Number Rev & Date AMENDMENT DATE 1 Cessna H,I,J,K,L, 310,310A, B C,D, E, F,G, 3A10 & Amendments in TCDS 3A10 Part 23 9328 10-13-93 "А" N, P,Q E310H, J, T310P, Q & 310J-1 2 Beech 33,А33,B33, С33, СЗЗА, Е33, Е33А, ЗА15 in TCDS 3A15 & Amendments Part 23 9334 10-30-93 NC E33C, F33 F33A, F33C G33, H35,033 K35,M35,N35 P35, S35,V35 V35A, V35B, 36,A36, A36TC, B36TC Beech 35R, F35, G35 35,A35,833 C35,D35,E35 A777 & Amendments In TCDS A77 CAR 03 9334 10-30-93 NC Beech 55,A55,B55 3A16 Part 23 9335 10-30-93 NC B55A, B55B, С55, С55А, D55, D55A, E55, E55A 5 Beech 58, 58A, 58PA 58TC, 58TCA A23CE Part 23 & Amendments 9335 10-30-93 NC in TCDS A23CE FAA Approved: Manager, Airframe Branch Los Angeles Aircraft Certification

## Every issue (1)

- February 2, 1994: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/6c/4a/6c4a2e220f8fbe75a9f4f2a1f04917047fb1489a08feb2d52883ccc21ac33141)

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