# STC SA8623SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Lockheed Martin Aeronautics Company
- Description: ONE-ONLY: Installation of an Executive Interior, S/N 293A-1249.
- Status date: May 8, 2007
- Data sheets: A23WE
- Certificate PDF: https://openairdocs.org/files/sha256/a5/31/a531b49a6c5901478f1eb728121a31048155199c96c06ade9c634b3129007059
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/451641D6910FA92B862572DF004E7D41.0001
- Page: https://openairdocs.org/stc/SA8623SW

## ADs that name it

None.

## Approved models (1)

- Lockheed Aircraft Corporation L-1011-385-3 (TCDS A23WE)

## 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.

Reissued to Replace Certificate Reported Lost

This Certificate issued to Lockheed Martin Aeronautics Company 86 South Cobb Drive Marietta, Georgia 30063 Part 4b of the Federal Aviation Regulations.

A23WE Lockheed

L-1011-385-3 Description of Type Design Change: Installation of an Executive Interior in aircraft serial number 293A- 1249 in accordance with Foster-Edward Aircraft Co. Inc., drawing list ER-385001, Rev. P, dated 2/26/93, or later FAA approved revision.

Limitations and Conditions: Compatibility of this modification with previously installed equipment must be determined by installer.

Date of application : August 26, 1991

Date of issuance : March 25, 1993

Date reissued : February 4, 1994, May 8, 2007

( Signature) Manager, Technical and Administrative Support Staff Los Angeles Aircraft Certification Office

NOTE:

**DO NOT DELETE THIS PAGE.**

**DO NOT ADD ANY DATA TO THIS PAGE.**

**THIS PAGE IS FOR PAGE NUMBERING PURPOSES, PLEASE DISCARD PRINTED COPY.**

Number SA00356DE

NOTE 1: Installation of STC SE00357DE is required with this modification.

NOTE 2: The following cockpit instrument must be marked accordingly:

Manifold pressure gage: 28.5 In Hg. (red line)

NOTE 3: Refer to Camarillo Aircraft Service FAA Approved Pilot’s Operating Handbook and/or Airplane Flight Manual Supplement AFMS-114-CAS, dated March 14, 2000, or later FAA approved revision, for required placards.

NOTE 4: Turbo-Flite 540 (Turbo 2000 Corp.) Master Drawing List No. TF540, Revision A, dated June 24, 1998, or later FAA approved revision; FAA Approved Airplane Flight Manual Supplement AFMS-114, Revision IR, dated October 14, 1998, or later FAA approved revision; and Instruction for Continued Airworthiness, Turbo-Flite Operations and Maintenance Manual Report 135-10, Revision none, dated March 12, 1998, or later FAA approved revision; are also approved for this installation.

- END -

## Every issue (1)

- May 8, 2007: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/a5/31/a531b49a6c5901478f1eb728121a31048155199c96c06ade9c634b3129007059)

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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.