What it approves
Installation of Mounting device and power supply connection for portable EFB with PIVOT cases in cockpit
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.
IMPORT ST00081IB
AEROCONSEIL 7 BOULEVARD HENRI ZIEGLER
ZAC ANDROMEDE 31700 BLAGNAC FRANCE Part 25 Title 14 Code of Federal Regulations A16WE The Boeing Company 737-600/-700/-800/-900/-900ER/-8/-9 Series
1. Installation of Mounting device and power supply connection for portable EFB with PIVOT cases in cockpit must be in accordance with Aeroconseil Master Data List Doc. No. 10003-01-A-MDL-R00, Rev.
00, dated May 18, 2021, or later EASA approved revisions.
(See Description of Type Design Change Continued on Page 3 of 3)
1. The installer must determine whether this design change is compatible with previously approved modifications.
(See Limitations and Conditions Continued on Page 3 of 3) October 20, 2022 December 8, 2022 Anthony E. Gallo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 4
IMPORT ST00081IB 4
IMPORT ST00081IB Date of Issuance: December 8, 2022
Description of Type Design Change (continued):
2. Maintenance must be in accordance with Aeroconseil Instructions for Continued Airworthiness Doc. No. 10003-01-A-ICA-F01-R00 and 10003-01-A-ICA-F02-R00, Rev. 00, dated May 12, 2021, or later EASA accepted revisions.
3. Operation must be in accordance with Aeroconseil Aircraft Flight Manual Supplement Doc. No. 10003-01-A-AFMS-F01-R00 and 10003-01-A-AFMS-F02-R00, Rev. 00, dated May 11, 2021, or later EASA approved revisions.
2. If the holder agrees to permit another person to use the certificate to alter the product, the holder shall give the other person written evidence of that permission.
3. Operation must be in accordance with the "Limitations" section of Aeroconseil Aircraft Flight Manual Supplement referenced under the Description of the Type Design section.
4. Maintenance must be in accordance with the "Airworthiness Limitations" section of Aeroconseil Instructions for Continued Airworthiness referenced under the Description of the Type Design section.
5. This STC is applicable to all serial numbers for this Make/Model aircraft.
Certification Basis:
Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48A, the certification basis for The Boeing Company Model 737-600/-700/-800/-900/-900ER/-8/-9 Series aircraft as follows:
a. The type certification basis for the aircraft is shown on TCDS A16WE for parts not changed or not affected by the change.
b. The type certification basis for the aircraft is shown on TCDS A16WE for parts changed or affected by the change plus the following 14 CFR exceptions:
(See Certification Basis Continued on Page 4 of 4) 3 4
IMPORT ST00081IB Date of Issuance: December 8, 2022
Certification Basis (continued):
14 CFR Part 25 Amendment 25-136:
§§ 25.1, 25.29, 25.301, 25.303, 25.305, 25.307, 25.321, 25.337, 25.341, 25.561,
25.562, 25.571, 25.601, 25.603, 25.605, 25.609, 25.613, 25.619, 25.625, 25.771,
25.773, 25.777, 25.785, 25.789, 25.803, 25.807, 25.809, 25.853, 25.899, 25.901,
25.1301, 25.1309, 25.1321, 25.1351, 25.1353, 25.1357, 25.1360, 25.1431, 25.1447,
25.1525, 25.1529, 25.1541, 25.1581, 25.1701, 25.1703, 25.1705, 25.1707, 25.1709,
25.1711, 25.1713, 25.1715, 25.1717, 25.1719, 25.1721, 25.1723, 25.1729 ----------END---------- 4 4
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.