# STC SA466SW

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Mitchell Industries Inc
- Description: Installation of Mitchell pitch trim Model AK147.
- Status date: January 14, 1965
- Data sheets: 1A15, 1A15, 1A15, A1EA
- Certificate PDF: https://openairdocs.org/files/sha256/78/4e/784ed8cfd76e74dde6874e38a748fbd9c6ebea5882fed78f1fbe66346d719904
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/AD00294A344918B186257E1F0049B6D4.0001
- Page: https://openairdocs.org/stc/SA466SW

## ADs that name it

None.

## Approved models (4)

- Piper Aircraft Inc. PA-24 (TCDS 1A15)
- Piper Aircraft Inc. PA-24-250 (TCDS 1A15)
- Piper Aircraft Inc. PA-24-400 (TCDS 1A15)
- Piper Aircraft Inc. PA-30 (TCDS A1EA)

## 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.

**FEDERAL AVIATION AGENCY**

1. NAME AND ADDRESS OF APPLICANT Mitehell Industrie., Inc.

Municipal Airport P. O. Box 610 Mineral Welle, Te«a« 74067 FORM APPROVED, BUDGET BUREAU NO. 04-R015

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

**COPY WILL BE RETURNED TO APPLICANT UPON**

**ISSUANCE**

2. SUPPLEMENTAL TYPE CERTIFICATE APPLIED FOR:

lyl AIRCRAFT I I ENGINE [~~l PROPELLER ORIGINAL MODEL DESIGNATION nt. *A Piper PA.24. PA*24.2SOr PA.zifiOO, NEW MODEL DESIGNATION (If demited)

3. DESCRIPTION OF CHANGE Installation of Mitchell Pitch Trim Model AK147 in accordance with Mitchell Industrie*, Inc. Bulletin No. 260 dated 12-21-64 and eubeequent F.A. A. approved bulletin* and/ or •upplemantt .

**WILL DATA BE AVAILABLE FOR SALE OR RELEASE TO**

b. WILL PARTS BE MANUFACTURED FOR SALE (Ret. CAR

**5. SIGNATURE AND TITLE OF APPLICANT 12-21-64**

DATE OF APPLICATION OTHER PERSONS? Ljd YES I— J NO 1 .55)1 CXl YES F~~l NO /) / I a / "*~) ^/^ /K&Ss**S ' jd%%^<£r<'-'-r<'*+ — -

SIGNATURE Vice President TITLE

6. To be Completed by FAA

NATURE AND LOCATION OF DATA Data lifted in Item 3 above on file at SW-210.

Applicable regulation* seat aa original certification.

**ORIGINAL TYPE CERTIFICATE NO. FAA API 1A15 & A1KA SUPPLEMENTAL TYPE CERTIFICATE NO.**

SA4668W ;

DATE OF APPROVAL B. *t 1-14-65 -SMfi =ROVAL ^ ' ?/) ° <L^ / /6=^^t^£^o^ ^f^> J^J^ )

SI GNATURE ^^^ , Slaughter f . Knginaerinf and Manufacturing Branch ___Tl TLE * U.S. GOVERNMENT PRINTING OFFICE : 1959 O—509657 FORM FAA-2417 (5-59)

## Every issue (1)

- January 14, 1965: Issued, Current. [certificate](https://openairdocs.org/files/sha256/78/4e/784ed8cfd76e74dde6874e38a748fbd9c6ebea5882fed78f1fbe66346d719904)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.