What it approves
Installation of Aircraft Components, Inc. Volt and Vac Alert System, P/N 2044-1
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.
Number SA00149BO
FAA Form 8110-2 (8/13) Page 1 of 3 This certificate issued to:
Aircraft Components, Inc.
1700 Fostoria Avenue, Suite 300 Findlay, Ohio 45840 Part 23 of the Federal; Aviation Regulations.
Installation of Aircraft Components, Inc. Volt and Vac Alert System, P/N 2044-1, in accordance with Aircraft Components, Inc. Master Document List (MDL), Document Number MDL-2044, Revision 2, dated March 17, 2003, or later FAA approved revision.
1. Operation must be in accordance with the Aircraft Components, Inc. Aircraft Flight Manual Supplement (AFMS), Document Number AFMS-2044, Revision 1, FAA approved on May 15, 2003, or later FAA approved revision.
The AFMS must be carried in the aircraft during all flights.
(continued on Page 3 of 3)
Date of Application: October 18, 2001 Date reissued: February 29, 2016
Date of Issuance: June 11, 2002 Date amended: May 15, 2003
Signature Robert G. Mann
Manager, Boston Aircraft Certification Office Title See attached FAA Approved Model List (AML), Document No.
2044AML, Revision 0, dated May 15, 2003, or later FAA approved revision, for the list of approved airplane models, applicable installation data requirements, and specific limitations.
SUPPLEMENTAL TYPE CERTIFICATE, FAA FORM 8110-2 (CONTINUED)
FAA Form 8110-2 (8/13) Page 2 of 3
TRANSFER
ENDORSEMENT
To (Name of transferee)
(Address of transferee)
(Number and street)
(City, State, and ZIP Code)
From (Name of grantor)
(Address of grantor)
(Number and street)
(City, State, and ZIP Code)
Number SA00149BO February 29, 2016
FAA Form 8110-2 (8/13) Page 3 of 3 Limitations and Conditions: (continued from Page 1 of 3)
2. Maintenance must be in accordance with Aircraft Components, Inc. Instructions for Continued Airworthiness (ICA), Document Number ICA-2044, Revision 1, dated May 10, 2003, or later FAA accepted revision.
The ICA must be made available to the operator at the time of installation.
3. Compatibility of this design with previously approved modifications must be determined by the installer.
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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.
Approved models · 475
| Make | Model | Data sheet |
|---|---|---|
| Aerostar Aircraft Corporation | PA-60-600 (Aerostar 600) | A17WE |
| Aerostar Aircraft Corporation | PA-60-601 (Aerostar 601) | A17WE |
| Aerostar Aircraft Corporation | PA-60-601P (Aerostar 601P) | A17WE |
Every issue · 1
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| February 29, 2016 | Reissued, current | CertificateAML_SA00149BO |