# STC SA2095SO

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: American Airlines Inc, United States
- Description: Reconfiguration of passenger seating to a 4F/59Y Mixed Class configuration
- Applied: January 13, 1987
- Status date: December 30, 2015
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A20EU](https://openairdocs.org/tcds/A20EU)
- Certificate PDF: https://openairdocs.org/files/sha256/42/97/4297bf68d19c179680e6efc83abc2613ba2cf747c2fbf1c76f30ce9e0dcd8ff5
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E20CDDAB04396EE386257F6B00591182.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2095SO

## ADs that name it (0)

None.

## Approved models (2)

- Fokker Services F.28 Mark 0100 ([TCDS A20EU](https://openairdocs.org/tcds/A20EU))
- Fokker Services F.28 Mark 1000 ([TCDS A20EU](https://openairdocs.org/tcds/A20EU))

## 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.

FAA Form 8110-2 (5/14) Page 1 of

Part of the

Signature

Title SA2095SO American Airlines, Inc.

3900 N. Mingo Road Engineering Dept., MD 208 Tulsa, Oklahoma 74116 Federal Aviation Regulations.

1. Reconfiguration of F.28 Mark 1000 passenger seating to a 4F/59Y Mixed Class configuration in accordance with US Airways Drawing 5J2540257, Rev B, dated January 31, 1994 and installation of a soft class divider in accordance with US Airways Drawing 5E2540447, dated January 27, 1993.

2. Amendment dated April 14, 1997: The modification directs the reconfiguration of the F.28 Mark 0100 passenger seating configuration. The new configuration is 12F/85Y. The configuration change is defined by US Airways top drawing 5F2540638, Rev A, dated April 14, 1997.

1. The installer must determine whether this design change is compatible with previously approved modifications.

2. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

3. Use of the 5F25400638-l configuration is contingent upon successful completion of the testing required by US Airways Engineering Test Report No. 02-08-92, rev C or later FAA approved revision.

Gaetano Sciortino Manager New York Aircraft Certification Office Fokker Services B.V.

F.28 Mark 1000 and F.28 Mark 0100 December 4, 2015, December 30, 2015 August 15, 1989, January 15, 1992, March 18, 1993, January 31, 1994, April 14, 1997 January 13, 1987 April 24, 1987 A20EU 2 “Reissued on December 4, 2015, to supersede the original STC, which has been lost or misplaced.”

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee)

From (Name and address of grantor)

2 SA2095SO

## Every issue (2)

- December 30, 2015: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/42/97/4297bf68d19c179680e6efc83abc2613ba2cf747c2fbf1c76f30ce9e0dcd8ff5)
- December 4, 2015: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/00/f6/00f6434849ddb5bd0a36ed3460b43991a1e79c866d26018e6e59c0aec5d7f323)

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