STC SA00378BO

Number SA00378BO

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

Cirrus Design Corp.

4515 Taylor Circle Duluth, MN 55811 Part 23 of the Federal Aviation Regulations.

Original Product - Type Certificate Number: A00009CH Make: Cirrus Design Corporation Model: SR20 S/N 20-2339 and subsequent SR22 S/N 22-4435 and subsequent SR22T S/N 22T-1460, 1471, 1473, and subsequent

Installation of integrated wingtip exterior light assemblies in accordance with Whelen drawing 90775 Rev – or later FAA approved revision.

See Page 3

Date of Application: February 17, 2016 Date reissued: March 9, 2017

Date of Issuance: December 28, 2016 Date amended:

Signature Nicholas Faust

Acting 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 SA00378BO March 9, 2017

FAA Form 8110-2 (8/13) Page 3 of 3 Limitations and Conditions:

1. Operation of the SR20 must be in accordance with the Airplane Flight Manual Supplement (AFMS), Whelen Document 11934-S56, Original Issue or later FAA approved revision. The AFMS must be carried in the aircraft during all flights.

2. Operation of the SR22 and SR22T must be in accordance with the AFMS, Whelen Document 13772-158, Original Issue or later FAA approved revision. The AFMS must be carried in the aircraft during all flights.

3. Maintenance for this modification to the SR20 must be in accordance with the instructions in Whelen document 20_IICAW_ST02044BO-A dated December 1, 2016. The instructions in 20_IICAW_ST02044BO-A dated December 1, 2016 must be incorporated into the Cirrus Aircraft Maintenance Manual for the SR20.

4. Maintenance for this modification to the SR22 and SR22T must be in accordance with the instructions in Whelen document 22_IICAW_ST02044BO-A dated December 1, 2016. The instructions in 22_IICAW_ST02044BO-A dated December 1, 2016 must be incorporated into the Cirrus Aircraft Maintenance Manual for the SR22 / SR22T.

5. 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 Make 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 is shown on the applicable TCDS.

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