STC SA00353BO

Number SA00353BO

FAA Form 8110-2 (5/14) Page 1 of 3 This certificate issued to:

Flight Enhancements, LLC 47 Oakcrest Road Oxford, CT 06478 Part 23 of the Federal; Aviation Regulations.

Installation of an Auto Lean system in accordance with Flight Enhancements document number AL- TLD-002 Revision 2 or later FAA approved revision.

1. Operation must be in accordance with Flight Enhancements Corp. Aircraft Flight Manual Supplement (AFMS) Document number AL-AFM-002, Revision 2, FAA approved on January 12, 2017, 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: April 21, 2014 Date reissued: April 10, 2017

Date of Issuance: May 15, 2015 Date amended: January 12, 2017

Signature Nicholas Faust

Acting Manager, Boston Aircraft Certification Office Title See attached FAA Approved Model List (AML), Document No. AL- AML-002, Revision IR, or later FAA approved revision, for the list of approved airplane models, applicable installation data requirements, and specific limitations.

FAA Form 8110-2 (5/14) Page 2 of 3

To (Name and address of transferee) Name:

Address (Number and Street, City, State, and ZIP Code):

From (Name and address of grantor) Name:

Address (Number and Street, City, State, and ZIP Code):

(Continuation Sheet) Number SA00353BO

FAA Form 8110-2 (5/14) Page 3 of 3

Limitations and Conditions: (continued from Page 1 of 3)

2. Maintenance must be in accordance with Instructions for Continued Airworthiness (ICA), Document number AL-IM-002, Revision 2, dated November 30, 2016, or later FAA accepted revision.

The ICA must be made available to the operator at the time of installation.

3. Operation of the Auto Lean system is prohibited during takeoff and landing.

4. Compatibility of this design with previously approved modifications must be determined by the installer.

Certification Basis:

Based on 14 CFR § 21.115 and § 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48, the certification basis for the AML identified Make and Model aircraft is as follows:

a. The type certification basis for parts not changed or not affected by the change is shown on the applicable TCDS.

b. The modification certification basis for parts changed or affected by the change since the reference application date, April 21, 2014, is based upon part 23 as amended by Amendment 23-62 as follows:

Regulations at the latest amendment 23-0 through 23-62

23.301(a), 23.305, 23.561(a)(3), 23.773(a)(2), 23.779(b)(1), 23.781(b), 23.867(b),

23.1141(c). 23.1147(a)(2), 23.1301, 23.1309(a)(2)(b)(c)(3)(d), 23.1322, 23.1357, 23.1367,

23.1521, 23.1529, 23.1541, 23.1581, 23.1583(m), 23.1585(j) Regulations at an intermediate amendment None Regulations at the amendment level in the applicable TCDS None ------------------------------------------------------------END-------------------------------------------------------