What it approves
Installation of Class II Electronic Flight Bag System Provisions in accordance with ASM Top Drawing List 5699-0001-00, Revision G, dated August 23, 2010, or later FAA approved revision. FAA approved Airplane Flight Manual Supplement No. 5699-2160-00, Revision IR, dated July 21, 2010 or later FAA approved revision is required.
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.
Part 25 of the Federal Aviation Regulations.
Description of Type Design Change: Installation of Class II Electronic Flight Bag System Provisions in accordance with ASM Top Drawing List 5699-0001-00, Revision G, dated August 23, 2010, or later FAA approved revision. FAA approved Airplane Flight Manual Supplement No. 5699-2160-00, Revision IR, dated July 21, 2010 or later FAA approved revision is required.
Limitations and Conditions: The installer must determine whether this design change is compatible with previously approved modifications. 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.
Aircraft Systems & Manufacturing 302 Toledo Trail Georgetown, TX 78628 A6WE Make : McDonnell Douglas Model : DC-9-51, DC-9 -83, DC-9-81, -82, -87, MD-88, MD-90-30 Date of application : September 30, 2009
Date of issuance : August 20, 2010
( Signature) S. Frances Cox Manager, Special Certification Office Southwest Region
( Title)
FAA Form 8110-2-1(10-69) Page 2 of 3
FAA Form 8110-2-1(10-69) Page 3 of 3
Number ST10979SC Date of Issuance: August 20, 2010
Certification Basis: The aircraft certification basis for the DC-9/MD-88/-90 is per the Type Certification Data Sheet A6WE, revision 26, dated November 1, 2001, Amendments 25-1 through 25-70 and Amendments through 25-123 as applicable to this modification and noted below.
Part 25, Subpart B – Flight
25.29 (b) Amdt 25-72
Part 25, Subpart C – Structure
25.305 Amdt 25-86, 25.307 Amdt 25-72, 25.365 (a)(b)(d) Amdt 25-87, 25.561 (a)(b)(c)(d) Amdt 25-91
Part 25, Subpart D – Design and Construction
25.613 Amdt 25-112, 25.625 Amdt 25-72, 25.773 (a)(1) Amdt 25-121, 25.869 (a)(1) Amdt 25-113
25.899 (a)(b)(1) Amdt 25-123
Part 25, Subpart F – Equipment
25.1301 (a) Amdt 25-123, 25.1307 (c) Amdt 25-72, 25.1309 (b)(c)(d)(e) Amdt 25-123, 25.1316 Amdt 25-80
25.1351 (a) Amdt 25-72, 25.1353 (a)(b)(1-4) Amdt 25-123, 25.1357 (a)(b)(e) Amdt 25-123, 25.1431 (a)(b)(c) Amdt 25-113
Part 25, Subpart G – Operating Limitations and Information
25.1581 Amdt 25-72, 25.1583 Amdt 25-105
Part 26, Continued Airworthiness and Safety Improvements for Transport Category Airplanes Subpart B – Enhanced Airworthiness Program for Airplane Systems
26.11 Amdt 26-0
26.47 Amdt 26-1
26.49 Amdt 26-1
------------------------------------------------------------------------END---------------------------------------------------- ------------- -----
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.