# STC SA1182WE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Baker Vern, United States
- Description: Rolls Royce V-1650-9A engine and Aeroproducts A542/H20-162-29M5 propeller.
- Applied: December 14, 1965
- Status date: March 22, 1966
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS LTC-11](https://openairdocs.org/tcds/LTC-11)
- Certificate PDF: https://openairdocs.org/files/sha256/fb/4d/fb4ddbd7b59cdb8eff24a79c30098980503213d7163a9fa7bf2bf00eab54e64f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/76D994DAB7278FA78625795800790DC4.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1182WE

## ADs that name it (0)

None.

## Approved models (1)

- North American Aviation Inc. Army P-51D ([TCDS LTC-11](https://openairdocs.org/tcds/LTC-11))

## What the certificate says

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

FEDERAL AVIATION AGENCY Supplemental Type Certificate

1. NAME AND ADDRESS OF APPLICANT Fern Backer 2660 E. Wardlos Road Long Beach, California 00807 FORM APPROVED, BUDGET BUREAU NO. 04-R015

**INSTRUCTIONS - SUBMIT IN TRI FLICATE TO LOCAL FAA FLIGHT STANDARDS INSPECTOR.**

**COPY WILL BE RETURNED TO APPLICANT UPON**

ISSUANCE Supplemental Type Certificate APPLIED FOR:

**AIRCRAFT ENGINE PROPELLER**

ORIGINAL MODEL DESIGNATION ARrican P-710 (North American) NEW MODEL DESIGNATION (If desired)

3. DESCRIPTION OF CHANGE Installation of Selle foyce Packard F-1650-96 engine and Aeroproducte A548/820-162-994S propeller in accordance with Vem Barker Instruction No.3 dated January 37, 2966.

Limitation of Applicability: The approval of thie change in type desigs applies to the basic North American P-D1D aircraft. This approval should not be oxtended to other specific aircraft of this nodel on which any previously approved noditications bave been incorporated unless it is firet deterined that the relationship betveen tie change sad any previously incorporated maditication will have no soverse effect on the sirvorthinese of these aircrest.

Operational Limitations: See reverse side.

Certification Basis: CA Part 6 Limited Category

• WILL DATA BE AVAILABLE FOR SALE OR RELEASE TO OTHER PERSONS? YES NO

b. WILL PARTS BE MANUFACTURED FOR SALE (Ref. CAR 1.55)1 YES NO

5. SIGNATURE AND TITLE OF APPLICANT Saf

SIGNATURE Date of Application: TITLE.

6. To be Completed by FAA NATURE AND LOCATION OF DATA Dete consisting of the above noted inctallation instructions ere filed at Aircraft Engineerine Division, TA Vester Region, Los Angeles, Calli.

ORIGINAL TYPE CERTIFICATE NO. FAA APPROVAL Org03 20700 82

ROCO L LOS Supplemental Type Certificate NO.

SIGNATURE A 1162WE (SA1182WB) Charles R. Javie, Chief DATE OF APPROVAL 5-22-66 Aircraft Engineering Division TITLE * U.S. GOVERNMENT PRINTING OFFICE: 1959 0- 509657 FORM FAA- 2417 (5-59)

Operational Limitatione: AlL ratinge and Limitations show in Spec. L--11 (page 135, Aircraft Listing) for the y-1650-7 engine are applicable to the F-1650-94 engine.

The felloving linite are applicable to the A548D1/ 820-162-280 propeller:

Dieneter - 11 it. 1. ir. maximum and minimus.

## Every issue (1)

- March 22, 1966: Issued, Current. [certificate](https://openairdocs.org/files/sha256/fb/4d/fb4ddbd7b59cdb8eff24a79c30098980503213d7163a9fa7bf2bf00eab54e64f)

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