STC SA00377BO

Number SA00377BO

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

BE Aerospace, Inc DBA SMR Technologies, Inc 93 Nettie Fenwick Rd Fenwick, WV 26202-4000

Part 23 of the Federal; Aviation Regulations.

Description of Type Design:

Installation of pneumatic de-icer timer kit in accordance with applicable installation instructions as specified on AML.

Limitations and Conditions: (continued on page 3 of 3)

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

2. Instructions for Continued Airworthiness, 13-33-089, revision 2, dated June 28, 2016, or later FAA accepted revision are required with this installation.

Date of Application: June 25, 2013 Date reissued:

Date of Issuance: March 20, 2017 Date amended:

Signature Nicholas Faust

Acting Manager, Boston Aircraft Certification Office Title See attached FAA Approved Model List (AML) Document Number SA00377BO, Revision IR, or later FAA approved revision for the list of approved airplane models, applicable installation data, 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 SA00377BO March 20, 2017

FAA Form 8110-2 (8/13) Page 3 of 3

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

3. A copy of this certificate and FAA Approved Model List (AML) No. SA00377B, dated March 20, 2017 or later FAA approved revision must be maintained as part of the permanent records for the modified aircraft.

4. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

5. This modification is not compatible with the Garmin G1000 system, and will not be used in any aircraft with that system.

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 aircraft listed on the AML is as follows:

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

b. The modification certification basis for parts changed or affected by the change since the reference application date, June 25, 2013, part 23 as amended by Amendment 23-62 as follows:

Regulations at the latest amendment 23-00 through 23-62

23.301 (a)(b)(c)(d), 23.303, 23.305(a)(b), 23.601, 23.603(a1,2,3)(b), 23.605(a)(b), 23.867, 23.1301,

23.1309 (a) (b) (c), 23.1357, 23.1359 (c) 23.1365 (a) (d) (e) (f). 23.1367, 23.1416 (b) (c), 23.1419,

23.1529, 23.1555 (a), 23.1585 (a)

If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

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