# STC SA01418WI-D - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Honeywell International Inc, United States - Description: Installation of the Bendix/King KFC 225 Automatic Flight Control System: Required Data. - Applied: April 13, 2006 - Status date: March 25, 2020 - Product: Aircraft, Small Airplane - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A00011LA](https://openairdocs.org/tcds/A00011LA) - Certificate PDF: https://openairdocs.org/files/sha256/64/01/6401f5a00340e34fe1a31a6906d9de1eacd0e5d996010509565479914418a33a - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/89C3924CD1142121862585E4005B2FC9.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA01418WI-D ## ADs that name it (0) None. ## Approved models (2) - GA 8 Airvan (Pty) Ltd GA8 ([TCDS A00011LA](https://openairdocs.org/tcds/A00011LA)) - GA 8 Airvan (Pty) Ltd GA8-TC320 ([TCDS A00011LA](https://openairdocs.org/tcds/A00011LA)) ## 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. FAA Form 8110-2 (5/14) Page 1 of 4 Number: SA01418WI-D This certificate issued to: Honeywell International Inc. 21111 N 19th Ave Phoenix, Arizona 85027 Part 23 of the Federal Aviation Regulations. Original Product – Type Certificate Number: Make: GA8 Airvan (Pty) Ltd A00011LA Model: GA8 and GA8-TC320 Description of Type Design Change: Installation of the Bendix/King KFC 225 Automatic Flight Control system. REQUIRED DATA: For the GA8 model Master Drawing List 159-08311-0001, Revision E, dated 12-19-2006 or Later FAA approved revision. For the GA8-TC320 model Master Drawing List 159-08311-0001, Revision G, dated 1-2-2012 or later FAA approved revision. 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 affect on the airworthiness of the aircraft. 2) If the holder agrees to permit another person to use this ce rtificate to alter the product, the holder shall give the other person written evidence of that permission. 3) This approval is limited to GA 8 aircraft serial numbers GA8-00-004 and subsequent and GA8-TC320 aircraft serial numbers GA8-TC320-08-130 and subsequent that are eligible for a U.S. Type Certificate. (continued on page 3) Date of Application: 4-13-2006 Date Reissued: 9-1-2009; 4-27-2018; 3-25-2020 Date of Issuance: 1-19-2007 Date Amended: 1-16-2012 By Direction of the Administrator Signature Title Richard B. Sleigh ODA Administrator, ODA-602216-NM FAA Form 8110-2 (5/14) Page 2 of 4 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: SA01418WI-D FAA Form 8110-2 (5/14) Page 3 of 4 Limitations and Conditions: (continued) 4) This approval is compatible with the cargo pod part number GA8-255004-17 when installed in accordance with Gippsland Aeronautics Service Bulletin SB-GA8-2004-14. 5) Airplane Flight Manual Suppl ement, Honeywell part number 006-10320-0000, Revision -, dated 1-19-2007, or later FAA approved revision, is required for the operation of the GA8 model aircraft. Airplane Flight Manual Supplement 006-10320-0000, Revision A, dated 1-16-2012, or later FAA approved revision, is required for the operation of the GA8-TC320 model aircraft. 6) Instructions for Continued Airworthiness, contained in Honey well Document 006-20038-0000, revision E, or later FAA accepted revision, must be made available to the operator at the time of installation in the GA8 model. Instructions for Continued Airworthiness, contained in Honeywell Document 006-20038-0000, revision F, or later FAA accepted revision, must be made available to the operator at the time of installation in the GA8-TC320 model. 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 this change is as follows: a. The certification basis for parts changed or affected by this change since the date of application, 4-13-2006, is determined to be: Regulations at the latest amendment: None. Regulations at an intermediate amendment: None. (continued on page 4) United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01418WI-D FAA Form 8110-2 (5/14) Page 4 of 4 Certification Basis: (continued) Regulations at the amendment level on TCDS A00011LA: 23.143 (a), (c) Amdt. 23-5; 23.301 (a), (b), (c), (d) Amdt. 23-48; 23.303 Amdt. 23-0; 23.305 (a), (b) Amdt. 23-45; 23.307 (a), (b) Amdt. 23-0; 23.337 (a)(1), (b)(1) Amdt. 23-48; 23.561 (e) Amdt. 23-48; 23.572 (a)(1) Amdt. 23-48; 23.601 Amdt. 23-0; 23.603 (a), (b)Amdt. 23-23; 23.605 (a)Amdt. 23-23; 23.607 (b) Amdt. 23-48; 23.609 (a), (b) Amdt. 23-0; 23.611 Amdt. 23-48; 23.613 (a), (b), (c), (d) Amdt. 23-45; 23.627 Amdt. 23-0; 23.671 (a), (b) Amdt. 23-0; 23.675 (c) Amdt. 23-17; 23.677 (d) Amdt. 23-49; 23.681 (a)(1)(2) Amdt. 23-0; 23.685 (a), (b), (c), (d) Amdt. 23-17; 23.689 (a)(2)(3), (b), (c) Amdt. 23-7; 23.771 (a) Amdt. 23-14; 23.773 (a)(2) Amdt. 23-45; 23.777 (a), (b) Amdt. 23-51; 23.779 (a)(2) Amdt. 23-51; 23.1301 (a), (b), (c), (d) Amdt. 23-20; 23.1303 (b), (f) Amdt. 23-49; 23.1309 (a)(1)(2), (b)(1)(2)(3)(4), (c)(1), (e) Amdt. 23-49; 23.1311 (a)(1)(2)(5)(6) Amdt. 23-49; 23.1321 (a), (c), (e) Amdt. 23-49; 23.1322 (a), (b), (c), (d), (e) Amdt. 23-43; 23.1325 (a) (b)(1)(2)(i) Amdt. 23-50; 23.1327 (a)(1)(2) Amdt. 23-20; 23.1329 (a)(1)(2), (b), (d), (e), (f), (g), (h) Amdt. 23-49; 23.1331 (a), (b) Amdt. 23-43; 23.1335 Amdt. 23-20; 23.1351 (a)(1)(2)(i) Amdt. 23-49; 23.1357 (a)(c) Amdt. 23-43; 23.1365 (a), (b), (d), (e), (f) Amdt. 23-49; 23.1367 (a), (b), (c), (d) Amdt. 23-0; 23.1381 (a), (b), (c) Amdt. 23-0; 23.1431 (a), (b), (e) Amdt. 23-49; 23.1501 (a), (b) Amdt. 23-21; 23.1529 Amdt. 23-26; 23.1541 (a), (b), (c)(2) Amdt. 23-21; 23.1555 (a), (b), (e)(2) Amdt. 23-50; 23.1581 (a)(1)(2), (b)(1)(3), (c), (d), (f) Amdt. 23-50; 23.1583 (m) Amdt. 23-50; 23.1585 (a)(1), (j) Amdt. 23-50 -------------------------------------------------------------------------- END ------------------------------------------------------------------------- ## Every issue (4) - March 25, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/64/01/6401f5a00340e34fe1a31a6906d9de1eacd0e5d996010509565479914418a33a) - April 27, 2018: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/47/4e/474e0ac455415b6631ab16c6638b68edda412c39f5707fbe96881040a6bc8aac) - January 16, 2012: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/5e/5c/5e5c2e90f609e61bbc359e8ca9167c5b0233bd7e9d81ccf38c0745ad867a5f64) - January 19, 2007: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/89/f2/89f2a34ef573c8976cdc0892333e1857132a0d1131472609d606af29243a003f) --- 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.