# STC SA4182NM-D

- Type: Supplemental type certificate
- Status: Historical, Surrendered
- Holder: Hollingsead International Inc, United States
- Description: Reconfiguration of the Lockheed Model L-1011-385-1-14 Airplane.
- Applied: November 6, 1989
- Status date: June 18, 2009
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A23WE](https://openairdocs.org/tcds/A23WE)
- Certificate PDF: https://openairdocs.org/files/sha256/b8/94/b89450740cacea8b55bdb2efe077395d8b02bc2ae59ad32af378435e0fe74b4f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/FB28520AAC2CF14F862575EC0067BE56.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA4182NM-D

## ADs that name it (0)

None.

## Approved models (1)

- Lockheed Aircraft Corporation L-1011-385-1-14 ([TCDS A23WE](https://openairdocs.org/tcds/A23WE))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA4182NM-D SURRENDERED Certificate This certificate issued to: Hollingsead International on 6-18-09 2226 Goodyear Avenue Ventura, California 93003 Part 25 of the Federal Aviation Poequlations.

Original Product Type Certificate Number A23WE Make: Lockheed Model: L-1011-385-1-14 Description of Type Design Change: Reconfiguration of the Lockheed Model L-1011-385-1-14 Airplane in accordance with Tracor Aviation, Inc. Index List IL-223-001, Interior Reconfiguration Air Transat L-1011-385-1-14, Rev. N/C, dated 12/1/89 or later FAA approved revision.

Limitations and Conditions: This approval should not be incorporated on any certificated product of this model on which other approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those previously incorporated modifications will not introduce any adverse effect upon the airworthiness of the certificated product. A copy of this STC must be included in the permanent records of the modified aircraft. AFM supplement R05-6, Rev. N/C, dated 12/1/89 or later FAA approved revisions are required as part of this installation. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

Date of Application: November 6, 1989 Date of Issuance: December 20, 1989

**HE AL AVARI**

TOMANSTRATD Date Reissued: June 20, 1991; April 12, 1995;

December 16, 1996; April 1, 1998; August 1, 2005 May 7, 2007 Date Amended:

By Direction of the Administrator Carlt K. Woe (Signature) Manager, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office (Title)

TRANSFER ENDORSEMENT Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transfer) (Number and street) (City, State, and Zip code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City; State, and Zip code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

## Every issue (2)

- June 18, 2009: Surrendered, Historical. [certificate](https://openairdocs.org/files/sha256/b8/94/b89450740cacea8b55bdb2efe077395d8b02bc2ae59ad32af378435e0fe74b4f)
- August 1, 2005: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/93/52/935223bbd94cdaaac82f3f7784eb1867e05bc8a0708b506c70cf0fc8471f412a)

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