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 * Regulations.
Configuration 1 (GPS without WAAS):
Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module in accordance with VoiceFlight Systems VFS101 Master Document List, document no. VFS101-MDL001, revision C, dated December 20, 2011.
Configuration 2 (GPS with WAAS):
Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module in accordance with VoiceFlight Systems VFS101 Master Document List (WAAS), document no. VFS101-MDL002, revision C, dated December 20, 2011.
Configuration 1:
1. VoiceFlight Systems LLC VFS101 Instructions for Continued Airworthiness, VFS101-ICA, revision J, dated December 19, 2011, is required for this installation.
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. Make: * Model: * Date reissued: November 18, 2010
Date amended: June 27, 2011, January 9, 2012
( Signature) Michele Maurer Acting 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 2 of 2
Number SA02717NY Date Amended: January 9, 2012
2. VoiceFlight Systems LLC VFS101 Pilot’s Guide, VFS101-PMAN, revision F, dated November 10, 2010 is required for this installation.
3. The VFS101 must interface with an existing Garmin GNS 430 or Garmin GNS 530. The installation of the Garmin 430/530 is not approved by this STC.
4. Acceptable GPS installations are limited to a single Garmin 430, dual Garmin 430, single Garmin 530, dual Garmin 530, or a single Garmin 430 plus a single Garmin 530.
5. 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.
6. Installation not approved for aircraft with a Maximum Certificated Gross Takeoff Weight of 6,000 pounds or more.
7. The installer must determine whether this design change is compatible with previously approved modifications.
8. 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.
Configuration 2:
1. VoiceFlight Systems LLC VFS101 (WAAS) Instructions for Continued Airworthiness, VFS101-ICA2, revision D, dated December 19, 2011, is required for this installation.
2. VoiceFlight Systems LLC VFS101 Pilot’s Guide (WAAS), VFS101-PMAN2, revision B, dated May 11, 2011 is required for this installation.
3. The VFS101 must interface with an existing Garmin GNS 430W or Garmin GNS 530W. The installation of the Garmin 430W/530W is not approved by this STC.
4. Acceptable GPS installations are limited to a single Garmin 430W, dual Garmin 430W, single Garmin 530W, dual Garmin 530W, or a single Garmin 430W plus a single Garmin 530W.
5. 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.
6. Installation not approved for aircraft with a Maximum Certificated Gross Takeoff Weight of 6,000 pounds or more.
7. The installer must determine whether this design change is compatible with previously approved modifications.
8. 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:
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---
ADs that name this STC · 0
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Approved models · 681
Every issue · 3
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| January 9, 2012 | Amended, earlier issue | CertificateApproved model list |
| June 27, 2011 | Amended, earlier issue | Certificate |
| July 21, 2009 | Issued, earlier issue | Certificate |