# STC SA2-1016

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Staggerwing Museum Foundation Inc., United States
- Description: Recertification under subparts B &G of CAR 3 and installation of SA4-120 airspeed system, SA4-21, fuel system, and SA-2-523, stabilizer angle of incidence change and elevator seal strips.
- Applied: December 22, 1961
- Status date: October 6, 2006
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A-757](https://openairdocs.org/tcds/A-757)
- Certificate PDF: https://openairdocs.org/files/sha256/3d/bb/3dbb6063a3683b4a78f384930184b18ef0a330657230d11c10b6e89ec4f1b2f6
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/89B9F24307917E16862574F1006BBB0F.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2-1016

## ADs that name it (1)

- [AD 65-03-01](https://openairdocs.org/ad/65-03-01): Gap Seal Strips · Recertification under subparts B &G of CAR 3 and installation… (Staggerwing Museum Foundation STC SA2-1016 or 7 others). Named in the applicability

## Approved models (1)

- Hawker Beechcraft Corporation C18S ([TCDS A-757](https://openairdocs.org/tcds/A-757))

## 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.

This certificate issued to: Staggerwing Museum Foundation, Inc.

560 Old Shelbyville Hwy Tullahoma, TN 37388

Part * of the Civil Air Regulations. * Subparts B & G of CAR 3.

Original Product - Type Certificate Number : 757 Make : Beech Model : C18S

Re-certification under subparts B & G of CAR 3 and installation of SA4-120 airspeed system, SA4-21, fuel system, and SA2-523, stabilizer angle of incidence change and elevator seal strips in accordance with Airline Training, Inc. Data List No. 10018 dated 05/01/60.

Airline Training, Inc. FAA approved Airplane Flight Manual Supplement dated 07/12/60 required.

Airworthiness compatibility of this STC with all other major changes to the standard original model(s) shown above should be confirmed prior to installation of this STC. 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.

Date of issuance : December 22, 1961

Date reissued : December 9, 1966; August 15, 1968;

February 26, 1990; October 6, 2006 Date amended :

Original signed by Robert D. Adamson

( Signature) Robert D. Adamson Program Manager Wichita Aircraft Certification Office (Title)

## Every issue (1)

- October 6, 2006: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/3d/bb/3dbb6063a3683b4a78f384930184b18ef0a330657230d11c10b6e89ec4f1b2f6)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.