What it approves
Installation of MT-Propeller Entwicklung GmbH model MTV-27-1-E-C-F-R(G)/CFR210-58( ) or /CFR224-55( )
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 SA04633NY MT-Propeller Entwicklung GmbH Flugplatzstrasse 1 94348 Atting, Germany Part 23 Title 14 Code of Federal Regulations A14CE Textron Aviation Inc.
B100
1. Installation of MT-Propeller Entwicklung GmbH model MTV-27-1-E-C-F-R(G)/CFR210-58( ) or /CFR224-55( ) 5-blade, constant speed, full feathering, reversible propellers and spinners on Textron Aviation Inc. B100 model aircraft equipped with Honeywell TPE-331-6-252B engines or aircraft modified with FAA STC No. SA00856AT, in accordance with Master Documentation List, Doc. No. E-3224, Rev. 6, dated April 6, 2021 or later EASA approved revision.
(Description of Type Design Change Continued on Page 3 of 3)
1. The aircraft must be operated in accordance with the "Limitations" section of Airplane Flight Manual Supplement, Doc. No. E-3226, Rev. 4, dated March 17, 2021 or later EASA approved revision.
(Limitations and Conditions Continued on Page 3 of 3) August 11, 2020 May 3, 2021 Anthony E. Gallo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 3
Date o transfer:
IMPORT SA04633NY SA04633NY 3
IMPORT SA04633NY (Date of Issuance: May 3, 2021) Description of Type Design Change (continued):
2. Operation must be in accordance with Airplane Flight Manual Supplement, Doc. No.
E-3226, Rev. 4, dated March 17, 2021 or later EASA approved revision, and is required as part of this installation.
3. Maintenance must be in accordance with Instructions for Continued Airworthiness, Doc. No. E-3228, Rev. 1, dated July 30, 2019 or later EASA accepted revision, and is required as part of this installation.
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.
Certification Basis:
Based on 14 CFR §21.115 and §21.101, and FAA Order 8110.48A, the certification basis for this modification to Textron Aviation Inc. B100 aircraft is as follows:
a) The type certification basis for the Textron Aviation Inc. B100 aircraft as shown on TCDS A14CE for parts not changed or not affected by the change.
b) The type certification basis for the Textron Aviation Inc. B100 aircraft as shown on TCDS A14CE for parts changed or affected by the change with the following exceptions:
• Compliance with 14 CFR 23.1529 at Amendment 23-26.
• Compliance with 14 CFR Part 36 at Amendment 36-31.
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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 |
|---|---|---|
| Textron Aviation Inc. | B100 | A14CE |