What it approves
Installation of 4-blade propeller MTV-16-1-E-C-F/CFL225-37a in accordance with EASA approved MT Propeller Installation Instruction Doc. No. E-1953, Original Issue, dated August 20, 2010. The following MT Propeller documents are required with this installation: EASA approved Airplane Flight Manual Supplement Doc. No. E-1952-2, Original Issue, dated August 20, 2010 and Instructions for Continued Airworthiness Doc. No. E-1954, Revised August 20, 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.
CAR 3 Part 23 of the Federal Regulations.
Installation of 4-blade propeller MTV-16-1-E-C-F/CFL225-37a in accordance with EASA approved MT Propeller Installation Instruction Doc. No. E-1953, Original Issue, dated August 20, 2010. The following MT Propeller documents are required with this installation: EASA approved Airplane Flight Manual Supplement Doc. No. E-1952-2, Original Issue, dated August 20, 2010 and Instructions for Continued Airworthiness Doc. No. E-1954, Revised August 20, 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. A8EA Make: Piper Aircraft Inc.
Model: PA-31P Date reissued:
( Signature) Anthony Socias Manager New York Aircraft Certification Office
( Title)
Date of application: April 8, 2010
Date of issuance: May 3, 2011
FAA Form 8110-2-1(10-69) Page 2 of 2
Number SA02959NY 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 Piper Aircraft Inc. Model PA-31P Aircraft Type Certified under TCDS NO. A8EA for parts not changed or not affected by the change.
The type certification basis for Piper Aircraft Inc. Model PA-31P Aircraft Type Certified under TCDS NO. A8EA for parts changed or affected by the change with the following 14 CFR exceptions:
CAR 3.712 Amendment 3-8
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
23.49 Amendment 23-21
23.51 Amendment 23-34
23.65 Amendment 23-34
23.67 Amendment 23-34
23.75 Amendment 23-34
23.77 Amendment 23-34
23.149 Amendment 23-21
23.201 Amendment 23-14
23.207 Amendment 23-7
23.251 Amendment 23-7
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
23.1041 Amendment 23-7
23.1043 Amendment 23-7
23.1047 Amendment 23-21
23.1305 Amendment 23-34
23.1501 Amendment 23-21
23.1513 Amendment 23-0
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 36-28
………………………..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 |
|---|---|---|
| Piper Aircraft Inc. | PA-31P | A8EA |