# STC SA4202NM-D

- Type: Supplemental type certificate
- Status: Historical, Surrendered
- Holder: Hollingsead International, United States
- Description: Interior reconfiguration.
- Applied: January 8, 1992
- Status date: June 18, 2009
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE)
- Certificate PDF: https://openairdocs.org/files/sha256/55/3a/553ab5d824b4c7dee7e545d82ed25539758f39149da95aaf6951c29ed83c66ce
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/47442B1AD0B3AE9F8625760000749167.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA4202NM-D

## ADs that name it (0)

None.

## Approved models (2)

- McDonnell Douglas Corporation DC-9-83 ([TCDS A6WE](https://openairdocs.org/tcds/A6WE))
- McDonnell Douglas Corporation DC-9-83 (MD-83) ([TCDS A6WE](https://openairdocs.org/tcds/A6WE))

## 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: SA4202NM-D Certificate This certificate issued to: Hollingsead International SURRENDERED 2226 Goodyear Avenue 6/8-09 Ventura, California 93003 on Certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereen meet's the airworthiness requirement's of Part 25 of the Federal Aviaticn Regulations.

Original Product Type Cerlificate Number AGWE Make: McDONNELL DOUGLAS Model: MD-83 Description of Type Design Change: Interior reconfiguration of a McDonnell Douglas MD-83 airplane in accordance with Lucas Aviation documentationo MDL R30-1 Rev. N/C dated 2/10/92, or later FAA approved revision o DWG. 30000-5,-1,-7,-3 Rev. N/C dated 2/10/92, 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. All of the above interior furnishings meet the heat release requirement (65/65) and smoke emission requirement

(200) of § 25.853 (a-1), amendment 25-67. 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: January 8, 1992 Date Reissued: April 12, 1995; December 16, 1996;

April 1, 1998; August 1, 2005; May 7, 2007 Date of Issuance: February 10, 1992 Date Amended: April 7, 1992; April 28, 1992 By Direction of the Administrator alto K. Woo (Signature) Manager, Technical & Administrative Support TOMNISTRAND 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 (3)

- June 18, 2009: Surrendered, Historical. [certificate](https://openairdocs.org/files/sha256/55/3a/553ab5d824b4c7dee7e545d82ed25539758f39149da95aaf6951c29ed83c66ce)
- May 7, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/76/0b/760bac1179f9f026926c01a29bd4f091b0a53258a969ec060b8a972b20c8aa20)
- August 1, 2005: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/b3/57/b357fce9135958a47981e16f27bf3f899e84bd659a346fa78873ce7b83fc6271)

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