STC SA04192NY

SA04192NY Honeywell International Inc. (Bendix King) 21111 N. 19th Avenue Phoenix, AZ 85027 23 Federal Aviation Regulations See attached FAA Approved Model List (AML), Document No. 89800009-037, Rev IR, or later FAA approved revision for the list of approved airplane models, applicable installation data requirements and specific limitations.

KFD 900 Primary Flight Display System in accordance with documents: (1) Aerospace Design & Compliance LLC. Master Data List, 89000009-031, Revision IR, dated April 29, 2020, or later FAA approved revision. (2) Bendix King Instructions for Continued Airworthiness (ICA), 89800009-012 Rev 2, date August 11, 2022, or later FAA accepted revision. The ICA and its contents must be incorporated into the operator's maintenance program. (3) Bendix King Aircraft Flight Manual Supplement (AFMS), 89800009-031, Rev 0, dated November 9, 2022, or later FAA approved revision.

(See Continuation Sheet Page 3 for Limitations and Conditions) March 5, 2020 March 2, 2023 May 8, 2023 April 29, 2020 November 11, 2022 Timothy Trank ODA administrator, ODA-602216-NM 3

SA04192NY 3

SA04192NY Date Amended: 11/11/2022 Date re-issued: 03/02/2023, 05/08/2023

Limitations and Conditions (cont):

1. The installer must determine whether this design change is compatible with previously approved modifications.

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

3. This STC is applicable to all serial numbers for the Make and Models listed on AML No. 89800009-037.

4. Installation of KFD 900 System is approved for Class I and II airplanes only.

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the the FAA Approved Model List (AML) No. 89800009-037 is as follows:

(1) The type certification basis for all Models included in AML No. 89800009-037 is included in the applicable TCDS as listed in the FAA approved AML for parts not changed or not affected by the change.

(2) The certification basis for parts changed or affected by the change since the reference date of application March 5, 2020, is in accordance with Title 14 CFR Part 23 amdt 23-62, except for the following earlier amendments:

23.1301 amdt 23-20

23.1309 amdt 23-49

23.1431 amdt 23-49 ----------END---------- 3 3