What it approves
Installation of a up to three 28 VDC mission power busses provisions
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.
Title: (for) Christina M. Underwood Manager, East Certification Branch Compliance and Airworthiness Division Aircraft Certification Service SA04559AT MAG Aerospace 7065 Challenger Avenue Titusville, FL, 32780 Part 23 the Federal Aviation Regulations A37CE Textron Aviation Inc.
208, 208B Installation of a up to three 28 VDC mission power busses provisions in accordance with the Master Data List, 2021005-MDL-100, Revision IR, dated November 3, 2022, or later FAA approved revision.
(See Continuation Sheet 3 of 4) December 13, 2021 June 12, 2023 4
SA04559AT 4
SA04559AT Limitations and Conditions - cont.:
1. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane.
2. If the holder agrees to permit another person to use the certificate to alter the product, the holder must give the other person written evidence of that permission.
3. Instructions for Continued Airworthiness (ICA) document 2021005-ICA-1100 Rev A, dated October 11, 2022 or later FAA Approved revision and Airplane Flight Manual Supplement (AFMS) document 2021005-AFMS-001, Rev IR, dated June 9, 2023 or later FAA approved must be made available to the operator at the time of installation.
SA04559AT Certification Basis:
Based on 14 CFR 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Textron, Model 208/208B series is as follows:
a. The type certification basis for the Textron, Model 208/208B airplane is shown on TCDS A37CE 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, December 13, 2021, is based upon part 23 as amended by Amendment 23-64. Based on 14 CFR 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be:
Regulations at the latest amendment 23-0 through 23-64 § 23.21 § 23.29 § 23.303 § 23.307 § 23.601 § 23.603 § 23.605 § 23.609 § 23.619 § 23.625 § 23.1351 § 23.1357 § 23.1359 § 23.1361 § 23.1365 § 23.1367 § 23.1519 § 23.1529 § 23.1557 § 23.1581 § 23.1583
Regulations at an intermediate amendment § 23.777 § 23.1309
Regulations at the amendment level in TCDS A37CE § 23.301 § 23.305 § 23.337 § 23.613 § 23.1301
--------------------------END--------------------------- 4 4
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.