What it approves
Installation of Crew Rest Curtains in the forward cabin to provide Class 2 Crew Rest Compartments
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.
FAA Form 8110-2 (5/14) Page 1 of
Part of the
Signature
Title 25 ST00159NY American Airlines, Inc.
3900 N. Mingo Road Engineering Dept., MD 208 Tulsa, Oklahoma 74116 Federal Aviation Regulations.
767-200 Series
1. Installation of Crew Rest Curtains in the forward cabin to provide Class 2 Crew Rest Compartments in accordance with US Airways Master Data List No 12P25A0922 initial release, dated September 30, 2013.
2. FAA accepted Instructions for Continued Airworthiness. Report No. 13-9, Rev A, dated August 27, 2013.
1. This STC does not require a revised Electrical Wiring Interconnection System (EWIS) Instruction for Continued Airworthiness.
2. The Installer must determine whether this design change is compatible with previously approved modifications.
3. 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.
The Boeing Company April 5, 2013 October 3, 2013 A1NM September 17, 2015 Raymond Reinhardt Acting Manager, New York Aircraft Certification Office 3
FAA Form 8110-2 (5/14) Page 2 of
To (Name and address of transferee)
From (Name and address of grantor)
ST00159NY 3
FAA Form 8110-2 (5/14) Page 3 of
Date Reissued: September 17, 2015
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 Boeing Model 767-200 series is as follows:
a. The type certification basis for Boeing Model 767 series airplanes is shown on TCDS A1NM 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, April 5, 2013, is based upon Part 25, as amended by Amendment 25-136 and Part 26. 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:
25.30l(a)(b)(c), 25.303, 25.601, 25.815, 25.1529, 25.1541 (a)(b)
Regulations at an intermediate amendment None
Regulations at the amendment level in TCDS A1NM
25.305 (a)(b), 25.307 (a), 25.561 (a)(b)(c), 25.603 (a)(b), 25.605, 25.611, 25.613 (a)(b)(c)(d)(e), 25.625 (a),
25.785 (c.2), 25.789, 25.791, 25.803 (a), 25.811 (d), 25.812 (d), 25.813 (a)(d), 25.853 (a)(b),
25.1301(a)(b)(c)(d), 25.1447 (c)
CFR Part 26 26.47 (b) Amdt 26-1 ----------END---------- ST00159NY 3
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| The Boeing Company | 767-200 Series | A1NM |