STC SA00194BO

Number SA00194BO

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. Landing Gear Warning System for Amphibian Aircraft, P/N 2042, in accordance with Aircraft Components, Inc. Master Document List (MDL), Document Number as referenced on the AML, or later FAA approved revision.

1. Operation must be in accordance with the Aircraft Components, Inc. Aircraft Flight Manual Supplement (AFMS), Document Number as referenced on the AML, 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: September 21, 2001 Date reissued: February 29, 2016

Date of Issuance: March 01, 2004 Date amended: July 21, 2005

Signature Robert G. Mann

Manager, Boston Aircraft Certification Office Title See attached FAA Approved Model List (AML), Document No.

2042-AML, Revision 0, 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 SA00194BO 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 as referenced on the AML, 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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