What it approves
Installation of propeller MTV-27-1-E-C-F-R(P)/CFR225-55f in accordance with MT Propeller Installation Instruction Doc. No. E-1879, Original Issue, dated October 25, 2010. The following MT Propeller documents are required with this installation: EASA Approved Airplane Flight Manual Supplement Doc. No. E-1878, Original Issue, dated October 25, 2010 and Instruction for Continued Airworthiness Doc. No. E-1880, Original Issue, dated October 25, 2010.
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 23 of the Federal Regulations.
Installation of propeller MTV-27-1-E-C-F-R(P)/CFR225-55f in accordance with MT Propeller Installation Instruction Doc. No. E- 1879, Original Issue, dated October 25, 2010. The following MT Propeller documents are required with this installation:
EASA Approved Airplane Flight Manual Supplement Doc. No. E-1878, Original Issue, dated October 25, 2010 and Instruction for Continued Airworthiness Doc. No. E-1880, Original Issue, dated October 25, 2010.
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 this certificate to alter a product, the holder must give the other person written evidence of that permission.
MT- Propeller Entwicklung GmbH FlugplatzstraBe 1 94348 Atting, Germany No. A60EU Make: SOCATA Model: TBM 700 A, B, C1, C2, N Date reissued:
( Signature) Anthony Socias Manager New York Aircraft Certification Office
( Title)
Date of application: February 14,, 2011
Date of issuance: May 26, 2011
FAA Form 8110-2-1(10-69) Page 2 of 2
Number SA02958NY Issuance date: May 3, 2011
Certification Basis:
Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for changes that are not significant in FAA Order 8110.48, the certification basis for this modification are as follows:
The type certification basis for the SOCATA TBM 700 A, B, C1, C2, N Aircraft as shown on TCDS A60EU for parts not changed or not affected by the change.
The type certification basis for the SOCATA TBM 700 A, B, C1, C2, N Aircraft as shown on TCDS A60EU for parts changed or affected by the change with the following 14 CFR exceptions:
23.1 Amendment 23-34
23.21 Amendment 23-0
23.29 Amendment 23-21
23.33 Amendment 23-0
23.45 Amendment 23-34
23.51 Amendment 23-34
23.65 Amendment 23-34
23.75 Amendment 23-34
23.77 Amendment 23-34
23.201 Amendment 23-14
23.207 Amendment 23-7
23.251 Amendment 23-0
23.629 Amendment 23-31
23.867 Amendment 23-7
23.901 Amendment 23-34
23.905 Amendment 23-29
23.907 Amendment 23-0
23.925 Amendment 23-0
23.929 Amendment 23-14
23.933 Amendment 23-34
23.937 Amendment 23-7
23.1041 Amendment 23-7
23.1043 Amendment 23-0
23.1045 Amendment 23-7
23.1305 Amendment 23-34
23.1419 Amendment 23-14
23.1501 Amendment 23-21
23.1521 Amendment 23-21
23.1529 Amendment 23-26
23.1541 Amendment 23-21
23.1549 Amendment 23-28
23.1559 Amendment 23-21
23.1581 Amendment 23-34
23.1583 Amendment 23-34
23.1587 Amendment 23-34
14 CFR Section 36 Amendment 36-1
………………………..END…………………….
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 |
|---|---|---|
| SOCATA | TBM 700 | A60EU |