STC SA01522WI-D

FAA Form 8110-2 (5/14) Page 1 of 3 Number: SA01522WI-D This certificate issued to: Honeywell International Inc.

21111 N 19th Ave Phoenix, Arizona 85027 Part 23 of the Federal Aviation Regulations.

Make: Socata A60EU Model: TBM 700 Serial Numbers up to and including 433 excluding 269 Description of Type Design Change:

Installation of alternate part number EFS 40 SG 465 Symbol Generator in accordance with Honeywell Master Drawing List 159-08328-0001, revision B, dated 12-9-08 or later FAA approved revision.

1) The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse affect on the airworthiness of the aircraft.

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

3) This STC has been determined to be compatible with Garmin Approved Model List STC SA01933LA, installed in accordance with FAA approved Garmin 400W Series Master Drawing List, Drawing No. 005-C0221-00, Revision D, dated 05-08-08 or later FA approved revision and/or FAA approved Garmin 500W Series Master Drawing List, Drawing No.

005-C0221-01, Revision D, dated 05-08-08 or later FAA approved revision.

Date of Application: 11-4-2008 Date Reissued: 3-25-2020 Date of Issuance: 12-12-2008 Date Amended:

By Direction of the Administrator Signature Richard B. Sleigh Title ODA Administrator, ODA-602216-NM

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

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01522WI-D

FAA Form 8110-2 (5/14) Page 3 of 3 Limitations and Conditions: (continued)

4) This STC has been determined to be compatible with DAC International STC SA10236SC installed in accordance with Master Drawing List No. 1049-000-XX, Rev E, dated March 30, 2005 or later FAA approved revision.

Certification Basis:

Based on 14 CFR §§ 21.101 and 21.115 and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this change is as follows:

a. The type certification basis for parts not changed or not affected by this change is shown on TCDS A60EU.

b. The certification basis for parts changed or affected by this change since the date of application, 11-4-2008, is determined to be:

Regulations at the latest amendment:

None.

Regulations at an intermediate amendment:

None.

Regulations at the amendment level on TCDS A60EU:

23.1301 (a) (b) (c) (d) Amdt. 23-20; 23.1309 (a)(1)(2) (c) Amdt. 23-34; 23.1322 (a) (b) (c) (d) Amdt. 23-17;

23.1329 (g) Amdt. 23-23; 23.1335 Amdt. 23-20.

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