What it approves
Installation of 4-Blade MT-Propeller (Model# MTV-16-1-E-C-F-R(P) / CFR240-55)
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.
This certificate issued to
Part 23 of the Federal Aviation Regulations.
Original Product -- Type Certificate Number : A9EA
1. The installation of 4-Blade MT-Propeller (Model# MTV-16-1-E-C-F-R(P) / CFR240-55) on Viking Air Limited DHC-6 Aircraft containing dual Pratt & Whitney PT6A-Series Engines to be done in accordance with Installation Instructions, Doc. No.
E-2294, 12 December 2012, Rev. 0 or later EASA approved revision, and MT-Propeller Operation & Installation Manual, Doc.
No. ATA 61-06-10 (E-610), 10 January 2012, Rev. 26 or later revision.
2. Operation must be in accordance with Aircraft Flight Manual Supplement, Doc. No E-2293, 29 November 2013, Rev. 1 or later EASA accepted revision, and is required for this installation.
3. Maintenance must be in accordance with Instruction for Continued Airworthiness, Doc. No. E-2295, 12 December 2012, Rev. 0 or later EASA approved revision.
1. The aircraft must be operated in accordance with the “Limitation” section of MT-Propeller Entwicklung GmbH Airplane Flight Manual Supplement, Doc. No E-2293, 29 November 2013, Rev. 1 or later EASA accepted revision, and is required for this installation.
2. Compatibility of this design change with previously approved modifications must be determined by the installer.
(See Continuation on Sheet 3 of 3)
MT-Propeller Entwicklung GmbH Flugplatzstrasse 1 94348 Atting Germany Make : Viking Air Limited Model : DHC-6 -1, -100, -110, -200, -210, -300, -310, -320, -400 Date of application : April 18, 2013
Date of issuance : February 18, 2014
B y direction of the A dministrator
(Signature) Gaetano Sciortino Manager New York Aircraft Certification Office
(Title)
FAA Form 8110-2-1(10-69) Page 3 of 3
Number SA03368NY Date of Issuance: February 18, 2014
Limitations and Conditions : (Continued)
3. If the holder agrees to permit another person to use the certificate to alter the product, the holder shal l give the other person written evidence of that permission
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 this modification to the Viking Air Limited DHC-6 -1, -100, -200, -300, & -400 Series is as follows:
a) The type certification basis for the Viking Air Limited DHC-6 -1, -100, -200, -300, & -400 Series as shown on TCDS A9EA for pasts not changed or not affected by the change.
b) The type certification basis for the Viking Air Limited DHC-6 -1, -100, -200, -300, & -400 Series as shown on TCDS A9EA for pasts changed or affected by the change with the following exceptions:
• For Aircraft Models: DHC-6-1, -100, & -200 Series:
o Compliance with 14 CFR 23.49, 23.51, 23.53, 23.55, 23.57, 23.59, 23.61, 23.65, 23.67, 23.75, 23.77,
23.149, and 23.1581 at Amendment 23-50, and 23.1529 at Amendment 23-26.
o Compliance with 14 CFR part 36 at Amendment 36-28.
• For Aircraft Models: DHC-6-300 Series:
o Compliance with 14 CFR 23.49 and 23.149 at Amendment 23-50, and 23.1529 at Amendment 23-26.
o Compliance with 14 CFR part 36 at Amendment 36-28.
• For Aircraft Models: DHC-6-400 Series:
o Compliance with 14 CFR 23.49, 23.65, 23.67, 23.75, 23.143, and 23.149 at Amendment 23-50; 23.161,
23.207, 23.629, 23.933, 23.1041, 23.1043, and 23.1155 at Amendment 23-7; 23.1, 23.21, 23.29, 23.33,
23.141, 23.177, 23.201, 23.203, 23.251, 23.301, 23.905, 23.907, 23.925, 23.1045, 23.1149, and 23.1153 at Amendment 23-0.
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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.