# STC SA4065SW

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Aero Logistics Intl
- Description: Metal chip detector in engine oil.
- Status date: December 4, 1979
- Data sheets: 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, 3A19, 3A19
- Certificate PDF: https://openairdocs.org/files/sha256/eb/a0/eba02bdbc495a61f8ee40d7ad1fb9f57eee97a624d6f51b6d7762e0ef124d586
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2ECB364CEF99CDB685256CC2000C6087.0001
- Page: https://openairdocs.org/stc/SA4065SW

## ADs that name it

None.

## Approved models (18)

- Cessna Aircraft Company 150 (TCDS 3A19)
- Cessna Aircraft Company 150A (TCDS 3A19)
- Cessna Aircraft Company 150B (TCDS 3A19)
- Cessna Aircraft Company 150C (TCDS 3A19)
- Cessna Aircraft Company 150D (TCDS 3A19)
- Cessna Aircraft Company 150E (TCDS 3A19)
- Cessna Aircraft Company 150F (TCDS 3A19)
- Cessna Aircraft Company 150G (TCDS 3A19)
- Cessna Aircraft Company 150H (TCDS 3A19)
- Cessna Aircraft Company 150J (TCDS 3A19)
- Cessna Aircraft Company 150K (TCDS 3A19)
- Cessna Aircraft Company 150L (TCDS 3A19)
- Cessna Aircraft Company 150M (TCDS 3A19)
- Cessna Aircraft Company 152 (TCDS 3A19)
- Cessna Aircraft Company A150K (TCDS 3A19)
- Cessna Aircraft Company A150L (TCDS 3A19)
- Cessna Aircraft Company A150M (TCDS 3A19)
- Cessna Aircraft Company A152 (TCDS 3A19)

## 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.

<-Sl6au£a&<rn4/.

United grata of amrrica Bepartment of ^Transportation — Jpedcral Situation administration upplemental 'Cgpe Certificate SA4065SW Aero LogtsticB International P. 0. Box 34395 Dallas, Texas 75234 Project A4365SW-S AAB-214 ,<^^/i^z^^ ^ 3 j&& Civil Air 3A19 CessnaCessna 150,A,B,C,D,E,F.G,H,J,K, A150K, L, M, A150M, 152. A152 A150L, installation of metal chip detector in engine oil according to Drawings 11-150-01 dated 12/29/78; 11-150-10 dated 12/29/78;

11-150-21 dated 1/20/79; 11-150-40, Revision A dated 10/5/79; 11-150-35 dated 10/27/78; and 11-150-50 dated 4/14/79, or later FAA approved revision.

Aircraft must be placarded according to Drawing 11-150-50.

Compatibility of this modification with other previously approved modifications must be determined by the installer.

January 30, 1979 December 4, 1979 (Signature) Don P. Watson Chief, Engineering and Manufacturing Branch (Title)

**FAA FOKM 8II0-2 (10-68)**

## Every issue (1)

- December 4, 1979: Issued, Current. [certificate](https://openairdocs.org/files/sha256/eb/a0/eba02bdbc495a61f8ee40d7ad1fb9f57eee97a624d6f51b6d7762e0ef124d586)

---
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.