STC SA2053CE-D

Supplemental type certificate · Honeywell International Inc

Holder
Honeywell International Inc · United States
Status
Current · Reissued
Status date
March 21, 2020
Applied
December 11, 1985
Product
Aircraft · Small Airplane
Certification basis
Part 21, Part 23
Data sheet
TCDSA37CE

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

What it approves

Install KAP 100 single axis, KAP 150 two axis, or KFC 150 two axis flight control system with optional third(yaw) axis and/or optional KAS-297B vertical speed and altitude selector.

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 Page 1 of 3 FAA Form 8110-2 (5/14)

Number: SA2053CE-D This certificate issued to: Honeywell International Inc.

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

Original Product – Type Certificate Number: Make: Cessna Model:

A37CE 208, 208A, 208B

Installation of the Bendix/King KAP100 single axis, KAP150 two axis, or KFC150 two axis Flight Control System with optional third (yaw) axisand/or optional KAS297BVertical Speed and Altitude Selector.

(See continuation Sheet for Required Data)

1. This approval should not be extended to other specific airplanesof this model on which other previously approved modificationsare incorporated, unlessit isdetermined that the interrelationship between this change any any of those other previously approved modificationswill introduce no adverse effect upon the airworthinessof that airplane.

(See Continuation Sheet for additional Limitationsand Conditions)

Date of Application: 12-11-85

Date of Issuance: 2-28-86 Date Reissued: 2-28-00, 3-21-20

Date Amended: 10-13-86, 1-20-89, 5-12-89, 10-30-89, 4-10-92, 9-14-92, 3-3-94

Signature

Title Richard B. Sleigh ODA Administrator, ODA-602216-NM

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 2 of 3 FAA Form 8110-2 (5/14)

To (Name and address of transferee)

From (Name and address of grantor)

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

(Continuation Sheet) Number: SA2053CE-D

REQUIRED DATA (continued):

Field Installations KAP100 Single Axis Flight Control System

1. Master Drawing List 155-9346-00, Rev. 4, dated 1-4-94.

2. Airplane Flight Manual Supplement 006-0448-00, Revision 1, dated 3-3-94.

KAP150 and KFC150 Two Axis Flight Control System with or without optional third (yaw) axis

1. Master Drawing List 155-9346-00, Rev. 4, dated 1-4-94.

2. Airplane Flight Manual Supplement 006-0448-01, Revision 2, dated 3-3-94.

Optional KAS297BVertical Speed and Altitude Selector

1. Master Drawing List 155-9346-00, Rev. 4, dated 1-4-94.

2. Airplane Flight Manual Supplement 006-0448-02, Revision 1, dated 3-3-94.

Cessna Factory Installation KAP150 and KFC150 Two Axis Flight Control System with or without optional third (yaw) axis

1. Master Drawing List 155-9346-01Rev. 8, dated 4-3-92.

2. Airplane Flight Manual Supplement 006-0448-01, Revision 1, dated 10-13-86.

3. Cessna Factory Airplane Flight Manual Supplement D1324-1-13, Rev. 16, approved 9-14-92may be used in lieu of AFMS 006-0448-01for KAP150 systems only.

4. Cessna Factory Airplane Flight Manual Supplement D1336-13, Rev. 6, approved 4-10-92may be used in lieu of AFMS 006-0448-01for 150 systems only.

Optional KAP297BVertical Speed and Altitude Selector

1. Master Drawing List 155-9346-01Rev. 8, dated 4-3-92.

2. Airplane Flight Manual Supplement 006-0448-02dated 2-28-86.

3. Cessna Factory Airplane Flight Manual Supplement D1336-13, Rev. 6, approved 4-10-92may be used in lieu of AFMS 006-0448-02for KFC150 systemswith KAS297B only.

4. Cessna Factory Airplane Flight Manual Supplement D1324-1-13, Rev. 16, approved 9-14-92may be used in lieu of AFMS 006-0448-02for KAP150 systemswith KAS297B only.

Later FAA approved revisionsto above listed data are incorporated without further revisionsto the Supplemental Type Certificate.

LIMITATIONSAND CONDITIONS(continued)

2. This modification hasbeen shown to be compatible with Model 208 Airplane equipped with Wipline Model 8000 Floats.

Operation of the system(s) isapproved when these floatsare installed in accordance with STCNumber SA1311GL. This approval islimited to the Model 208 airplane only.

3. 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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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 · 2

MakeModelData sheet
Textron Aviation Inc.208A37CE
Textron Aviation Inc.208BA37CE

Every issue · 2

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

DateStatusFiles
March 21, 2020Reissued, currentCertificate
February 28, 2000Reissued, earlier issueCertificate