What it approves
Installation of cross aisle curtains, a Pre-Recorded Announcement Machine (PRAM) with associated wiring, forward windscreens, first class and main cabin seats with associated wiring, a hanging soft divider, a mid-cabin closet, a window plug, a sidewall literature pocket.
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
ST11269DS American Airlines, Inc., Maintenance and Engineering (M&E) Division, 3900 North Mingo Road, MD 537/TUL Tulsa, Oklahoma 74116 25 14, Code of Federal Regulations A28NM Airbus A320-214/-232 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 the permission.
(Limitations and Conditions continued on page 3 of 4) 11/10/2025 06/19/2026 ODA-700094-SW STC Administrator 4 In accordance Master Data List 104937-MDL Revision NEW dated 15 June 2026, or later FAA Approved Revision: Installation of cross aisle curtains, a Pre-Recorded Announcement Machine (PRAM) with associated wiring, forward windscreens, first class and main cabin seats with associated wiring, a hanging soft divider, a mid-cabin closet, a window plug, a sidewall literature pocket. Serial Number Effectivity Report 104937-SNER Revision NEW, dated 19 August 2025, or later FAA Approved Revision.
ST11269DS 06/19/2026 ST11269DS 4
ST11269DS 06/19/2026 Limitations and Conditions, Continued:
This STC is contingent on the concurrent installation of the following service bulletins:
- Airbus Service Bulletin SB25-1CJW – Install XL Fixed Bins and Adapt Cabin For An A320,
- Airbus Service Bulletin SB25-1CPK – Emergency Equipment and ELTs, and
- Diehl Service Bulletin SBA- 25-37559– Lavatories Refresh
The Instructions for Continued Airworthiness, 104937-ICA, Revision B, or later FAA Accepted revision shall be made available to the operator at the time of installation. The aircraft shall be maintained in accordance with the applicable Instructions for Continued Airworthiness.
A revised EWIS ICA is not required for this STC. An AFMS is not required for this STC.
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 Airbus Model A320-214 / -232 aircraft for the change is as follows:
a. The Type Certification basis for Airbus Model A320-214 / -232 airplanes is shown on TCDS A28NM for parts not changed or not affected by the change.
b. The certification basis for parts changed or affected by the change since the reference date of application, November 10, 2025, is based upon Part 25, as amended by Amendment 25-153 and Part 26 as amended by Amendment 26-7. 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 25-153:
25.301, 25.303, 25.562(a)(c)(2)(4)(5)(6)(7)(8), 25.601, 25.603, 25.605, 25.609, 25.619, 25.789(a), 25.791, 25.793,
25.815, 25.817, 25.853(a)(d), 25.856(a), 25.1316(b), 25.1317(b), 25.1421, 25.1423(c), 25.1438(b), 25.1501,
25.1529, 25.1541, 25.1561(b)(c)
Regulations at an intermediate amendment level:
25.869(a)(4) Amendment 25-72, 25.981(a)(3)(d), Amendment 25-125
Regulations at the amendment level in TCDS A28NM:
25.21(a)(1), 25.29, 25.305(a)(b), 25.307(a), 25.365(e)(f)(g), 25.561, 25.611, 25.613, 25.625, 25.785(a)(b)(d) (e)(h)
(1) (i)(1)(3), 25.787(a)(b), 25.803(a), 25.811(b)(d)(3), 25.812(d)(e)(1) (h)(k)(1)(2), 25.813(a)(b)(c)(d)(e), 25.851(a)
(1)(2), 25.1301(a)(b)(c)(d), 25.1307(c), 25.1309(a)(b)(d)(e)(f)(g), 25.1351(a), 25.1353(a)(b), 25.1357(a)(c)(g),
25.1411(a)(1)(b) (e)(f), 25.1415(d), 25.1431(a)(c), 25.1447(a)(c)(1), 25.1557(a)(c), 25.1583(c)(2)
(CERTIFICATION BASIS CONTINUED ON PAGE 4)
ST11269DS 06/19/2026 Certification Basis, continued:
Special Conditions:
FAA Special Conditions 25-375-SC, "Special Conditions: Airbus A318, A319, A320 and A321 Series Airplanes:
Inflatable Restraints", dated November 12, 2008
FAA Special Conditions 25-671-SC, "Special Conditions: Airbus A318, A319, A320 and A321 Series Airplanes:
Non-Rechargeable Lithium Battery Installations", dated May 16, 2017; SC1, SC2, SC3, SC4, SC5, SC6
Issue Paper:
FAA Issue Paper S-1 for Installed Non-Rechargeable Lithium Batteries Means of Compliance, dated May 19, 2019 Transport Airplane Position Paper, TAPP-25.1353-1, for non-rechargeable lithium batteries in AmSafe NexGen Electronic Module Assemblies
14 CFR Part 26 Regulations Based on 14 CFR §21.101(g), applicable provisions of 14 CFR part 26 are included in the certification basis. For any future 14 CFR part 26 amendments, the holder of this STC must demonstrate compliance with the applicable sections. As of the issuance of this STC, compliance has been found for the following regulations 14 CFR § 26.11
(c) Amendment 26-7.
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.