# STC ST10163SC-D

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: American Airlines Inc, United States
- Description: Rearrange Aircraft Interior to 16 F/C and 124 T/C Cabin and 3 Galley.
- Applied: August 11, 2006
- Status date: October 1, 2006
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE)
- Certificate PDF: https://openairdocs.org/files/sha256/ca/05/ca05f812e620bd33c20849dcb6d4c3b9ebbb72eeeb8095d10b8f9ab8a51c1640
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/09C4ACBAF280E4718625785D007532BE.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/ST10163SC-D

## ADs that name it (0)

None.

## Approved models (2)

- The Boeing Company DC-9-82 (MD-82) ([TCDS A6WE](https://openairdocs.org/tcds/A6WE))
- The Boeing Company 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 ST 101635C-D This certificate issued to: 3900 N. Mingo Road American Airlines, Inc.

Engineering Dept., MD 208 Tulsa, Oklahoma 74116 Certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airvorthiness neguirements of Part 25 of the Federal Aviation Regulations:

Original Product - Typebertificate Numben: AGWE Make: McDonnell Douglas Model: DC-9-82, -83* Description of Type Design Change: *Reference AA DAS Approved Report K3207- SNER, Rev Basic or latest DAS -700094-SW approved revision for authorized aircraft Rearrange Aircraft Interior to 16 F/C and 124 T/C Cabin and 3 Galley in accordance with Master Data List K3207-MDL, Rev Original dated October 1, 2006, and Airplane Flight Manual Supplement K3207-AFMS, Revision Basic or later DAS-700094-SW approved revision.

This approval should not be incorporated in any aircraft of this specific model until compatibility of this modification with previously approved modifications has been determined by the installer. 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.

Limitations and Conditions: continued on page 3 of 3

Date of Application: August 11, 2006 Date Reissued:

Date of Issuance: October 1, 2006 Date Amended:

FEDERAL AVIATION C. E. Williams OMINISTRA DAS-700094-SW Administrator ( Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number ST 101635C-D Certification Basis:

Based on 14 CFR 21.115 and 21.101, and the FAA policy for non-significant changes in FAA Order 8110.48, the certification basis for the McDonnell Douglas Model DC-9-82, -83 series aircraft for the change is as follows:

a. The Type Certification basis for McDonnell Douglas Model DC-9-82, 83 series airplanes is shown on TCDS A6WE for parts not changed or not affected by the

b. The certification basis for parts changed or affected by the change since the reference date of application, August 11, 2006 is based upon Part 25, as amended by Amendment 25-116. Based on 14 CFR 21.115 and 21.101, and the FAA policy for non significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be:

Regulations at the latest amendment 25-0 through 25-116:

25.21 (a)1, 25.29, 25.301, 25.303, 25.305(a-c), 25.307, 25.562, 25.601, 25.603, 25.605(a),

25.609, 25.611, 25.785(b-k), 25.787(a-b), 25.793, 25.810, 25.815, 25.817, 25.851,

25.869(a)4, 25.981(a)3,(b), 25.1301, 25.1309(a),(b),(d), (g), 25.1357(a),(c), 25.1415,

25.1441, 25.1445, 25.1450, 25.1529, 25.1541, 25.1561(b),(c), 25.1581 (a)2, 25.1583(c)1,(c)2,

25.1585(a)2.

Regulations at an intermediate amendment:

25.803(c) - Admt 46, 25.853 - Admt 83, 25.1351(a) - Admt 41,

25.1353(a),(b), (d) - Admt 42, 25.1411 - Admt 79, 25.1423 - Admt 79 Regulations at the amendment level in TCDS A6WE:

25.561, 25.607, 25.613, 25.625, 25.789, 25.791, 25.807, 25.809, 25.811, 25.812, 25.813,

25.1431 (a), (c), 25.1439, 25.1447, 25.1557(a) ---END--

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

## Every issue (1)

- October 1, 2006: Issued, Current. [certificate](https://openairdocs.org/files/sha256/ca/05/ca05f812e620bd33c20849dcb6d4c3b9ebbb72eeeb8095d10b8f9ab8a51c1640)

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