# STC SA1072GL

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: McFarlane Aviation Inc, United States
- Description: Installation of cooling shroud on engine driven dry air pumps.
- Applied: July 21, 1986
- Status date: November 21, 2017
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 2A13](https://openairdocs.org/tcds/2A13)
- Certificate PDF: https://openairdocs.org/files/sha256/3f/81/3f816b0e314237720a89be7fd813fa8d205eecef1719991d84d1f706b14abcc3
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/88FB919E7C10CA6C862582490066E561.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1072GL

## ADs that name it (0)

None.

## Approved models (18)

- Piper Aircraft Inc. PA-28-140 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-150 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-151 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-160 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-161 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-180 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-181 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-201T ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-235 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28-236 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28R-180 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28R-200 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28R-201 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28R-201T ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28RT-201 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28RT-201T ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28S-160 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- Piper Aircraft Inc. PA-28S-180 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))

## 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.

3 Federal Aviation

(See Type Certificate Data Sheet 2A13 for complete certification basis.)

Installation of a Cooling Shroud on engine driven dry air pumps in accordance with Aero Cables Report No. 8, Revision 01, dated December 29, 2006, or later FAA approved revision.

1) The installer must determine whether this design change is compatible with previously approved modifications.

2) If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission.

McFarlane Aviation, Inc.

696 E. 1700 Road Baldwin City, KS 66006

2A13 The New Piper Aircraft, Inc.

PA-28-140, -150, -151, -160, -161, -180, -181, -235, -236, -201T;

PA-28S-160, -180; PA-28R-180, -200, -201, -201T;

PA-28RT-201, 201T July 21, 1986

October 9, 1986

March 19, 2004; June 15, 2004 ;

November 21, 2017 October 28, 1986; May 1, 2007

Original Signed By:

Monica L. Nemecek

(Signature) Monica L. Nemecek Acting Manager, Airframe and Administrative Services Section Chicago ACO Branch

(Title)

## Every issue (2)

- November 21, 2017: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/3f/81/3f816b0e314237720a89be7fd813fa8d205eecef1719991d84d1f706b14abcc3)
- May 1, 2007: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/05/ad/05ad590f9f3dd9bc0b43c6f4ed8d93b4c54db40ad978e29df5753c2a94f6a808)

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