STC SA1177GL

Supplemental type certificate · Paul/ Lanna Egan LLC

Holder
Paul/ Lanna Egan LLC · United States
Status
Current · Reissued
Status date
September 1, 2016
Applied
April 1, 1987
Product
Aircraft · Small Multi-Engine
Certification basis
Part 21
Data sheet
TCDS2A4

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Install Aero Medical Products Mfg., Inc. Air Ambulance Stretcher P/N 125 using Installation Kit P/N 800 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.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

3 Federal Aviation (See Type Certificate Data Sheet No. 2A4 for complete certification basis)

Install Aero Medical Products Mfg. Inc. Air Ambulance Stretcher P/N 125 using Installation Kit P/N 800 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 March 3, 2004, 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 March 29, 2004, 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 2A4 Twin Commander 680; 680-E; 680-F; 680-FL; 680-T; 680-V; 680-W; 681; 685; 690;

690A; 690B; 690C; 690D; 695A; 720 April 01, 1987

April 17, 2003

June 02, 1997; June 30, 1997 September 01, 2016 April 06, 1988; September 21, 1988;

March 07, 1989; March 29, 2004

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

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 16

MakeModelData sheet
Twin Commander Aircraft Corporation6802A4
Twin Commander Aircraft Corporation680-E2A4
Twin Commander Aircraft Corporation680-F2A4
See all 16 models

Every issue · 2

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
September 1, 2016Reissued, currentCertificate
March 29, 2004Amended, earlier issueCertificate