What it approves
Installation of Satcom System
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 SA04461NY SAAB Aktiebolag SE-581 88 Linkoeping Linkoeping, Sweden Federal Aviation Regulations.
1. Installation of Satcom System in accordance with SAAB Aktiebolag Master Data List Doc. No. TDM19-05-0-LEP Revision D, dated January 31st, 2020, or later EASA approved revisions.
2. Aircraft operation in accordance with SAAB Aktiebolag Operating Instructions Doc. No. TDM19-05-4-Olp1, Revision A, dated March 1st, 2019, and TDM19-05-4-Olp2, Revision A, dated March 1st, 2019, or later EASA approved revisions.
3. Maintenance in accordance with SAAB Aktiebolag Instructions for Continued Airworthiness Doc. No. TDM19-05-4-ICA Revision C, dated January 28, 2020, or later EASA accepted revisions.
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 the certificate to alter the product, the holder shall give the other person written evidence of that permission.
3. Must adhere to the Airworthiness Limitations section of SAAB Aktiebolag Instructions for Continued Airworthiness Doc. No. TDM19-05-4-ICA, Revision C, dated January 28, 2020, or later EASA accepted revisions.
Anthony A. Gallo Acting Manager New York ACO Branch Textron Aviation Inc.
B200GT, A100, 200, 300, 190 July 19, 2019 February 25, 2020 IMPORT A24CE 3
FAA Form 8110-2 (5/14) Page 2 of
To (Name and address of transferee)
From (Name and address of grantor)
3 SA04461NY
FAA Form 8110-2 (5/14) Page 3 of
3 Date of issuance: February 25, 2020
4. This change is only applicable to Beech 200GT with Fusion avionics
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 8110.48, the certification basis for the Beechcraft B200GT A100, 200, 300, 190is as follows:
a. The type certified basis for parts not changed or not affected by the change is shown on TCDS A24CE.
b. The modification certification basis for parts changed or affected by the change since the reference application date is shown on TCDS A24CE with the following exceptions to the airworthiness regulations:
The following paragraph(s) at a later amendment:
23.301, 23.303, 23.305, 23.307, 23.561, 23.571, 23.603, 23.609, 23.613, 23.771, 23.773, 23.777,
23.853, 23.1301, 23.1309, 23.1322, 23.1351, 23.1357, 23.1359, 23.1365, 23.1367, 23.1381,
23.1431, 23.1529, 23.1541, 23.1585 from CS 23 at amendment 4.
END SA04461NY
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.