STC SA00304BO

Number SA00304BO

FAA Form 8110-2 (8/13) Page 1 of 3 This certificate issued to:

Approach Aviation 30 Sheffield Terrace Marlborough, MA 01752 Part 3 of the Civil Air Regulations.

Original Product - Type Certificate Number: 3A15 Make: Beechcraft Corporation Model: 36, A36

Installation of an extended baggage compartment in accordance with Approach Aviation Master Document List (MDL), Document BE36-MASTERDWGLIST, Revision B, dated May 20, 2016, or later FAA approved revision.

1. Operation must be in accordance with Approach Aviation Aircraft Flight Manual Supplement (AFMS), Document BE36-AFMS-001, Revision A, dated October 06, 2010, FAA approved on December 17, 2010, 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 02, 2010 Date reissued: May 23, 2016

Date of Issuance: December 23, 2010 Date amended:

Signature Robert G. Mann

Manager, Boston Aircraft Certification Office Title

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 SA00304BO May 23, 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 Approach Aviation Instructions for Continued Airworthiness (ICA), Document BE36-ICA-001, Revision A, dated October 06, 2010, or later FAA accepted revision.

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

3. Eligible for installation only on Beechcraft Corporation model 36 and model A36, serial numbers E-1 through E-1370.

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 Beechcraft Corporation model 36 and model A36 aircraft is as follows:

a. The type certification basis for parts not changed or not affected by the change is shown on TCDS 3A15.

b. The modification certification basis for parts changed or affected by the change since the reference application date, September 02, 2010, is based upon CAR 3 as amended on May

15. 1956, as follows:

Regulations at the latest amendment May 15, 1956, through 3-8

3.171, 3.172, 3.173, 3.174, 3.291, 3.292, 3.293, 3.294, 3.295, 3.296, 3.301, 3.302, 3.307,

3.386, 3.392 NOTE: Findings of compliance were also made to 14 CFR as follows:

part 23 through amendment 23-59: 23.1529, 23.1583, 23.1585, 23.1587, 23.1589 part 25 through amendment 25-129: 25.853(a), F25-1 Regulations at an intermediate amendment None Regulations at the amendment level in TCDS 3A15 None ------------------------------------------------------------END-------------------------------------------------------