STC SA4209NM-D

Historical

Supplemental type certificate · Hollingsead International

Holder
Hollingsead International · United States
Status
Historical · Surrendered
Status date
June 18, 2009
Applied
June 24, 1992
Product
Aircraft · Large Multi-Engine
Certification basis
Part 21, Part 25
Data sheet
TCDSA6WE

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

What it approves

Interior reconfiguration.

What the certificate saysOCR

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: SA4209NM-D Certificate This certificate issued to: Hollingsead International SURRENDERED Ventura, California 93003 2226 Goodyear Avenue on . 6-18-09 Certifies that the change in the type design for the following product with the limitation's and condition's therefor as specified hereen meets the airerthiness requirement's of Part 25 of the Federal Aviation Regulations.

Original Product Type Certificate Number AGWE Make: McDonnell Douglas Model: MD-83 Description of Type Design Change: Interior reconfiguration of the McDonnell Douglas MD-83 airplane in accordance with Lucas Aviation documentation:

Master Drawing List, R34-1, Rev. B, Dated 28 July 1992, or later FAA approved revisions Airplane Flight Manual Supplement R34-7, Rev. NC, Dated 27 July 1992, or later FAA approved revisions Limitations and Conditions: Aircraft modified in accordance with this STC must be operated in accordance with Approved Flight Manual Supplement R34-7, Rev. N/C or later FAA approved revision.

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 25-66. 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.

i it lead the poling date which i de bis chen valeted ty the this met Federal Aviation Administration .

Date of Application: June 24, 1992 Date Reissued: April 12, 1995; December 16, 1996;

April 1, 1998; August 1, 2005; May 7, 2007 Date of Issuance: August 1, 1992 Date Amended:

By Direction of the Administrator FERAL AVAT Carlto K. Woo (Signature) Manager, Technical & Administrative Support TOMANS TRAD 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) trom (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):

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 · 2

MakeModelData sheet
McDonnell Douglas CorporationDC-9-83A6WE
McDonnell Douglas CorporationDC-9-83 (MD-83)A6WE

Every issue · 3

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

DateStatusFiles
June 18, 2009Surrendered, earlier issueCertificate
May 7, 2007Reissued, earlier issueCertificate
August 1, 2005Reissued, earlier issueCertificate