# STC ST00201AT

- Type: Supplemental type certificate
- Status: Current, Surrendered
- Holder: Pemco Aeroplex Inc, United States
- Description: Reconfiguration of passenger interior.
- Applied: March 30, 1993
- Status date: August 4, 2009
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A28NM](https://openairdocs.org/tcds/A28NM)
- Certificate PDF: https://openairdocs.org/files/sha256/49/0b/490b2b72f9c2cf882b6e7367c26d20e86567c3f39f22211ae6f2d17de5ea5f1a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1C20369A795D92A186257742006FD49B.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/ST00201AT

## ADs that name it (0)

None.

## Approved models (1)

- Airbus A320 Series ([TCDS A28NM](https://openairdocs.org/tcds/A28NM))

## 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 Added Notes at Surrender:

Future unsafe conditions existing in the product can Number STO0201AT result in an airworthiness directive requiring correction of the unsafe condition before further flight. If there is no entity to comply with 14 CFR This certificate issued to: Pemso World Air Services an unsafe condition might resultin permanently 21.99(a), Required désign changes, the existence of 100 Pemco Drive grounding of the aircran.

Dothan, AL 36303 Replacement parts might not be available in the future.

Purt ¿ Poegulutions.

Original Product - Type Certificule Number: A28NM Description of Type Design Change: This modification will allew the recon iguration of pasener opterfer in Airbus 320 aircraft series in accordance with Pemco Aeroplex Drawing List, "Interior Arrangement Airbus A320" 2620, Bevision B, dated December 8, 1993, or later FAA approved revision.

Bimitutions und Complitions "This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determine by the installer that the interrelationship between this change and any other previously approved modifications wiN produce no adverse effect upon the airworthiness of that airplane. This determination should include consideration of signficant changes in weight distribution such as an increase in the fixed disposable weight in the (See continuation sheet 3 of 3) supporting dutu which is the busis for upproval shall remain in effect until suspen ad, revoled or a terminution dute is otherwise estublished by the Administrator of the " Administration.

Dute /upplicution: March 30, 1993 Date Reissued: 06/29/98; 11/5/99; 6/27/07 Dute umendeil: 12/ 17/93 Date of Issuance: April 21, 1993 By Direction of the Administrator FEDERAL AVIATION Signatur Melvin D. Taylor * Manager, ACE-115A TOMINISTRATIO Atlanta Aircraft Certification Office (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST00201AT ED Date of Issuance: April 21, 1993 Date Amended: December 17, 1993 SURRENDER Limitations and Conditions: (Continued):

agrees to permit another person to use this certificate to alter the product, the holder shall give the oth person written evidence of that permission."

FAA FORM 8110-2-1 (10-69) PAGE 3 of 3 PAGES

## Every issue (1)

- August 4, 2009: Surrendered, Current. [certificate](https://openairdocs.org/files/sha256/49/0b/490b2b72f9c2cf882b6e7367c26d20e86567c3f39f22211ae6f2d17de5ea5f1a)

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