Supplemental type certificate · Honeywell International Inc

Holder
Honeywell International Inc · United States
Status
Current · Issued
Status date
April 6, 2020
Applied
June 7, 2005
Product
Aircraft · Small Airplane
Certification basis
Part 21
Data sheet
TCDS3A21

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of a Roll Disable System for Bendix/King KFC 225 Automatic Flight Control System.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property oft h eS T C holder.

FAA Form 8110-2 (5/14) Page 1 of This certificate issued to:

Part of the

Signature

Title 3 SA01363WI-D Honeywell International Inc.

21111 N 19th Ave Phoenix, Arizona 85027 Federal Aviation Regulations.23 Installation of a Roll Disable System for the Bendix/King KFC 225 Automatic Flight Control System:

REQUIRED DATA:

(1) Master Drawing List 159-08309-0001, Revision D, dated 11-29-2005; and

(2) Airplane Flight Manual Supplement 006-10310-0001, Revision -, dated 12-2-2005.

Later FAA approved revisions to the above listed data are incorporated without further revision to this Supplemental Type Certificate.

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 effect upon the airworthiness of the aircraft.

2. 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.

(See continuation sheet) Richard B. Sleigh ODA Administrator, ODA-602216-NM Cessna 210L, T210L, 210M, T210M, 210N, T210N 4-6-20206-7-2005 12-2-2005 3A21

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property oft h eS T C holder.

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

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

The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property oft h eS T C holder.

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

3 Limitations and Conditions: (continued)

3. Airplanes to be altered in accordance with this Supplemental Type Certificate must first have the KFC 225 Automatic Flight Control System installed in accordance with Supplemental Type Certificate SA01362WI-D.

4. Airplanes to be altered in accordance with this Supplemental Type Certificate must be owned by the United States government. If ownership of the airplane should change from the United States government, the alteration including the Airplane Flight Manual Supplement 006-10310-0001 must be removed from the airplane, and the Airplane Flight Manual Supplement 006-10310-0000 must be inserted into the Pilot’s Operating Handbook prior to the ownership transfer. Contact the local FAA FSDO for assistance in confirming government ownership.

Certification Basis:

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

a. The certification basis for parts not changed or not affected by this change is shown on TCDS 3A21.

listed on AML Number, 159-08293-0002.

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

Regulations at the latest amendment Section Amdt. Section Amdt.

23.601 - 23.1331 a, b, c 23-43

23.603 a, b 23-23 23.1351 a(1)(2i) 23-49

23.605 a 23-23 - 23.1365 a, b, d, e 23-49

23.607 a 23-48 23.1367 a, b, c, d -

23.609 a - 23.1501 a, b 23-21

23.611 23-48 23.1529 23-26

23.771 a 23-14 23.1541 a(1)(2), b(1)(2),c(2) 23-21

23.773 a(2) 23-45 - 23.1555 a 23-50

23.777 a, b 23-51 23.1581 a(1)(2)(3),b(1)(3), c, d, f 23-50

23.1301 a, b, c, d 23-20 23.1583 m 23-50

23.1309 a(1)(2), b(1)(2)(3)(4), c(1),e 23-49 23.1585 a(1)(2)(3)(4)(5)(6), j 23-50

23.1322 c, d, e 23-43 Regulations at an intermediate amendment none Regulations at the amendment level shown on TCDS none ------------------------------------------------------------------------------------END------------------------------------------------------------------------------------ SA01363WI-D

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 6

MakeModelData sheet
Textron Aviation Inc.210L3A21
Textron Aviation Inc.210M3A21
Textron Aviation Inc.210N3A21
Textron Aviation Inc.T210L3A21
Textron Aviation Inc.T210M3A21
Textron Aviation Inc.T210N3A21

Every issue · 2

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
April 6, 2020Issued, currentCertificate
December 2, 2005Issued, earlier issueCertificate