STC ST00163NY

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

Part of the

Signature

Title ST00163NY American Airlines, Inc.

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

1. Installation of B/E Aerospace 15 Minutes Duration Gaseous Oxygen Container in Lavatory in accordance with US Airways Master Data List No. 32P35A1104 (initial release, dated October 10, 2014) or later FAA approved revision, FAA accepted Instructions for Continued Airworthiness Report No 14-8 Revision A, dated September 17, 2014, or later FAA accepted revision, and FAA approved EWIS Instructions for Continued Airworthiness Report Impact No. 14-10, Revision New, dated August 20, 2014, or later FAA approved revision.

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.

Anthony Gallo Acting Manager New York Aircraft Certification Office Airbus A319-100 Series A320-200 Series A321-200 Series October 30, 2015 August 28, 2015 May 2, 2014 October 10, 2014 A28NM 3

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

To (Name and address of transferee)

From (Name and address of grantor)

3 ST00163NY

FAA Form 8110-2 (5/14) Page 3 of

3 Date Reissued: October 30, 2015

Certification Basis:

Based on 14 CFR 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for Airbus Models: A319-100, A320-200, A321-200 series is as follows:

a. The type certification basis for Airbus Model A319-100, A320-200, A321-200 series airplanes is shown in TCDS A28NM for part not changed or affected by the change.

b. The certification basis for parts changed or affected by the change since the reference date of application, May 2, 2014 is based upon Part 25, as amended by Amendment 25-137 and Part 26. Based on 14 CFR 21.115 and 21.101, and the FAA policy for 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 25-137

25.301 (a)(b)(c), 25.303,25.305 (a)(b), 25.307 (a), 25.561 (a)(b)(c)(d), 25.601, 25.603 (a)(b)(c), 25.605 (a),

25.607 (a)(b)(c), 25.611, 25.613 (a)(b)(c), 25.625 (a), 25.789 (a), 25.853 (a)( e), 25.1301 (a)(b),

25.1309 (a)(b)(d)(e)(f), 25.1351 (a), 25.1353 (a)( c), 25.1357 (a)( e), 25.1431 (a), 25.1438 (a), 25.1441 (a)(b),

25.1445 (a), 25.1447 (a)(c,l), 25.1449, 25.1453 (a)(b), 25.1529

Regulations at an intermediate amendment None.

Regulations at the amendment level in TCDS A46NM None.

Equivalent Safety Findings exist with respect to the following Regulations:

For Airbus Models A319-100, A320-200, A321-200:

25.1441 (c) Oxygen equipment & supply in accordance with ELOS Memo AT10288IB-T-S-6

25.1443 (c) Minimum mass flow of supplemental oxygen in accordance with ELOS Memo AT10288IB-T-S-5

CFR Part 26

26.11 (c) Amdt 26-0, 26.47 (b) Amdt 26-1

----------END---------- ST00163NY