STC SA2073CE-D

FAA Form 8110-2 (5/14) Page 1 of 3 Number: SA2073CE-D This certificate issued to: Honeywell International Inc.

21111 N 19th Ave Phoenix, Arizona 85027 Part 4b of the Civil Air Regulations.

Make: Rockwell International A2WE Model: NA-265-65 Description of Type Design Change:

Installation of Bendix/King EFS 10 Electronic Flight Instrument System (5 tube), dual KFC 400 Automatic Flight Control System, dual KAD 480 Air Data System, dual KNS 660 Flight Management System, KHF 950HF Comm System and MLS 21 Microwave Landing System.

This STC requires prior or concurrent installation of the following:

1) A third altimeter meeting the requirements specified in FAR 25.1303(b)(2).

2) A third attitude indicator m eeting the requirements specified in FAR 25.1303(b)(4).

(See continuation sheet) 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.

Date of Application: 9-8-86 Date Reissued: 2-28-95; 2-28-00; 3-27-20 Date of Issuance: 3-14-88 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: SA2073CE-D

FAA Form 8110-2 (5/14) Page 3 of 3 Description of Type Design Change: (continued) REQUIRED DATA:

(1) Bendix/King Master Drawing List 155-9382-00, Rev.3 dated 2- 15-88 and (2) Bendix/King Airplane Flight Manual Supplements

(a) 006-0461-00 dated 3-14-88 for KFC 400, (b) 006-0472-00 dated 3-14-88 for KNS 660, (c) 006-0473-00 dated 3-14-88 for EFS 10, (d) 006-0474-00 dated 3-14-88 for KAD 480, (e) 006-0475-00 dated 3-14-88 for KHF 950 and (f) 006-0476-00 dated 3-14-88 for MLS 21 or later approved revision to (1), (2)(a), (b), (c), (d), (e), or (f).

Limitations and Conditions: (continued) KNS 660 Pilot’s Guide No. 006-8407-00 or later revision is required.

For the Bendix/King EFS 10 above, compliance has been shown with the following sections of FAR Part 25:

25.1301 (amend. 25-38)

25.1303(b) (amend. 25-38)

25.1309 (amend. 25-41)

25.1321(a)(b)(d)(e) (amend. 25-41)

25.1322 (amend. 25-38)

25.1331 (amend. 25-41)

25.1333 (amend. 25-41)

25.1335 (amend. 25-41)

25.1523 (amend. 25-3) Installation in the airplane was evaluated in accordance with CAR 4b (amendments 4b-1 thru 4b-9 and additional items noted on TC Data Sheet A2WE).

This approval included evaluation of the interface between the Bendix/King EFS 10, KFC 400, KAD 480, KNS 660, RDS 86 and CC 2024F.

This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of these other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane.

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