# STC SA1541GL

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Paul/ Lanna Egan LLC
- Description: Install Egan Aviation air ambulance stretcher P/N 125 using installation kit P/N 801.
- Status date: September 1, 2016
- Data sheets: A5SW, A5SW, A5SW, A5SW, A5SW, A5SW, A5SW
- Certificate PDF: https://openairdocs.org/files/sha256/31/a9/31a9891d5760d41d059978f83c04750d45b2cc527e0f9cb99219dedb67d12ec7
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/CD54CA10AD3BB4E48625811D006957A2.0001
- Page: https://openairdocs.org/stc/SA1541GL

## ADs that name it

None.

## Approved models (7)

- Fairchild Aircraft Corporation SA226-AT (TCDS A5SW)
- Fairchild Aircraft Corporation SA226-T (TCDS A5SW)
- Fairchild Aircraft Corporation SA226-T(B) (TCDS A5SW)
- Fairchild Aircraft Corporation SA227-AT (TCDS A5SW)
- Fairchild Aircraft Corporation SA227-TT (TCDS A5SW)
- Fairchild Aircraft Corporation SA26-AT (TCDS A5SW)
- Fairchild Aircraft Corporation SA26-T (TCDS A5SW)

## 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.

23 Federal Aviation (See Type Certificate Data Sheet No. A5SW for complete certification basis)

Install Aero Medical Products Mfg., Inc. Air Ambulance Stretcher P/N 126 using Installation Kit P/N 805 in accordance with Installation and Operating Instructions, Form EA 109K, dated April 23, 2001, or later FAA approved revisions. The Medical Oxygen System Kit P/N 807 is an FAA approved option. The Inverter/Pump Kit No. 812 may be installed in accordance with Inverter/Pump Installation Instructions, EA Form 170, dated June 9, 2001, or later FAA approved revisions.

1. FAA Approved Aircraft Flight Manual Supplement dated November 19, 2001, or later FAA approved revisions required.

2. Prior to the first flight of each modified aircraft, and after each change to any of the Communication, Navigational, or Med Pack equipment, a ground EMI test must be conducted in accordance to EA Form 173, dated November 15, 1993. A copy of EA Form 173 must be kept with the aircraft records.

3. FAA Approved Aircraft Maintenance Manual Supplement dated November 19, 2001, or later FAA approved revisions required.

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

5. 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.

Paul/ Lanna Egan LLC 6534 Tanglewood Dr. NE Saint Petersburg, FL 33702 A5SW Fairchild Aircraft SA226-AT; SA226-T; SA226-T(B); SA227-AT; SA227-TT; SA26-AT;

SA26-T November 15, 1990

December 12, 1990

April 29, 1994; May 01, 1997;

September 1, 2016 November 19, 2001

Original Signed By:

Karol Mordasiewicz

(Signature) Karol Mordasiewicz Manager, Airframe & Administrative Branch Chicago Aircraft Certification Office

(Title)

FAA FORM 8110-2-1(10-69) PAGE 2 of 2 PAGES

## Every issue (1)

- September 1, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/31/a9/31a9891d5760d41d059978f83c04750d45b2cc527e0f9cb99219dedb67d12ec7)

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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.