What it approves
Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module
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 * of the * R egulations.
Original Product -- Type Certificate N umber: *
Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module in accordance with VoiceFlight Systems VFS101 Master Document List, document no. VFS101-MDL003, revision D, dated March 4, 2014, or later FAA approved revisions.
VoiceFlight Systems LLC Airplane Flight Manual Supplement, document number VFS101-AFMS, Revision A, FAA approved on March 5, 2014 is required as part of this installation.
The aircraft is to be maintained in accordance with VoiceFlight Systems LLC VFS101 Instructions for Continued Airworthiness, VFS101-ICA3, revision D, dated March 3, 2014.
Limitations and Conditions
1. The VFS101 must interface with one or two existing Garmin 400/500 Series (Non-WAAS) GPS units, or with one or two existing Garmin 400W/500W Series (WAAS) GPS units. The installation of the Garmin GPS units is not approved by this STC.
VoiceFlight Systems LLC 105 Jordan Road Troy, NY 12180 * See attached FAA Approved Model List (AML), Document No.
SA02717NY for the list of approved airplane models and applicable airworthiness regulations. M ake: * M odel: * Date reissued: November 18, 2010
Date amended: June 27, 2011, January 9, 2012, January 30, 2013, September 17, 2013, March 5, 2014
B y direction of the A dministrator
(Signature) Gaetano Sciortino Manager New York Aircraft Certification Office
(Title)
Date of application: November 21, 2006
Date of issuance: July 21, 2009
FAA Form 8110-2-1(10-69) Page 3 of 3
N umber SA02717NY Date Amended: March 5, 2014
Limitations and Conditions: (Continued)
2. The VFS101 must interface with an audio panel with an available un-switched input having a nominal input impedance of no less then 500 Ohms. The installation of the audio panel is not approved by this STC.
3. The installer must determine whether this design change is compatible with previously approved modifications.
4. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other pers on written evidence of that permission.
Certification Basis:
The certification basis for the changed aircraft as described in this certificate is as follows:
a. The type certification basis as shown on the TCDS (see AML, Document No. SA02717NY) for all areas not affected by the change.
b. The certification basis for parts changed or affected by the change since the reference date of application, November 21, 2006, is as shown on the TCDS (see AML, Document No. SA02717NY). In addition, the holder of this certificate has complied with 14 CFR Part 23 as amended by Amendment 23-54.
The following lists the Federal Aviation Regulations complied with through Amendment Level 23-54
23.301 23.303 23.305 23.307 23.333 23.337 23.471 23.561 23.601 23.603
23.605 23.609 23.611 23.613 23.619 23.625 23.777 23.853 23.863 23.1182
23.1301 23.1309 23.1357 23.1359 23.1365 23.1367 23.1431 23.1529 23.1585 ---END---
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Every issue · 1
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| Date | Status | Files |
|---|---|---|
| March 5, 2014 | Amended, current | CertificateApproved model list |