# STC SA2053CE-D - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Honeywell International Inc, United States - Description: 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. - Applied: December 11, 1985 - Status date: March 21, 2020 - Product: Aircraft, Small Airplane - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A37CE](https://openairdocs.org/tcds/A37CE) - Certificate PDF: https://openairdocs.org/files/sha256/a6/df/a6df21bfbb1774a48daab2d4d8071cf294633dc8479169ccdceb00fee34b7f11 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/12C4B21AEBB4C28B8625861E0074A757.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA2053CE-D ## ADs that name it (0) None. ## Approved models (2) - Textron Aviation Inc. 208 ([TCDS A37CE](https://openairdocs.org/tcds/A37CE)) - Textron Aviation Inc. 208B ([TCDS A37CE](https://openairdocs.org/tcds/A37CE)) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can 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. ------------------------------------------------------------------------------------END-------------------------------------------------------------------------------- ## Every issue (2) - March 21, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/a6/df/a6df21bfbb1774a48daab2d4d8071cf294633dc8479169ccdceb00fee34b7f11) - February 28, 2000: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/c7/8f/c78f4094629fc7f26649e275b7c1be40f04b1eb8c6690068e51d35dd88be6964) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.