# STC SA01234WI-D - Type: Supplemental type certificate - Status: Current, Issued - Holder: Honeywell International Inc, United States - Description: Installation of Bendix/King KMH 880 Multi-Hazard Awareness System or Bendix/King KGP 560 General Aviation Enhanced Ground Proximity Warning System (GA-EGPWS). - Applied: April 16, 2004 - Status date: April 6, 2020 - Product: Aircraft, Small Airplane - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A00009CH](https://openairdocs.org/tcds/A00009CH) - Certificate PDF: https://openairdocs.org/files/sha256/d2/82/d28203787f412f1bb418cbb294ee856b7871fc772567bd97cbbb671e085c5e24 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DA9BA90A4F04DC00862585DE006C7772.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA01234WI-D ## ADs that name it (0) None. ## Approved models (2) - Cirrus Design Corporation SR20 ([TCDS A00009CH](https://openairdocs.org/tcds/A00009CH)) - Cirrus Design Corporation SR22 ([TCDS A00009CH](https://openairdocs.org/tcds/A00009CH)) ## 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 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 Original Product – Type Certificate Number: Make: By Direction of the Administrator Signature Title 3 SA01234WI-D Honeywell International Inc. 21111 N 19th Ave Phoenix, Arizona 85027 Federal Aviation Regulations.23 Installation of the Bendix/King KMH 880 Multi-Hazard Awareness System or the Bendix/King KGP 560 General Aviation Enhanced Ground Proximity Warning System (GA-EGPWS). REQUIRED DATA: 1. Master Drawing List 159-08303-0001, Revision B, dated 4-14-2004; 2. For KMH 880 installations, Airplane Flight Manual Supplement 006-10317-0001, Revision -, dated 4-16-2004, 3. For KGP 560 installations, Airplane Flight Manual Supplement 006-10317-0000, Revision -, dated 4-16-2004. Later FAA approved revisions to the above listed data are incorporated without further revision to this Supplemental 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. Richard B. Sleigh ODA Administrator, ODA-602216-NM Cirrus Design Corporation SR20, SR22 4-6-20201-16-2004 4-16-2004 A00009CH 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 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 A00009CH. 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. 23.301 All 23-48 23.1309 a(1)(2), b 23-49 23.303 23-0 23.1321 a, c, e 23-49 23.305 23-45 23.1322 All 23-43 23.307 23-0 23.1331 a 23-43 23.337 23-48 23.1351 a, b 23-49 23.561 e 23-48 23-1357 All 23-43 23.573 a(1)(2)(3)(4) 23-48 23.1365 a, b, d, e 23-49 23.603 All 23-23 23.1367 23-0 23.605 a 23-23 23.1381 23-0 23.607 b 23-48 23.1431 a, b, e 23-49 23.609 All 23-0 23.1501 23-21 23.613 All 23-45 23.1529 23-26 23.627 23-0 23.1541 a2, b 23-21 23.1301 All 23-20 Regulations at an intermediate amendment none Regulations at the amendment level shown on TCDS none ------------------------------------------------------------------------------------END------------------------------------------------------------------------------------ SA01234WI-D ## Every issue (2) - April 6, 2020: Issued, Current. [certificate](https://openairdocs.org/files/sha256/d2/82/d28203787f412f1bb418cbb294ee856b7871fc772567bd97cbbb671e085c5e24) - April 16, 2004: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/19/cc/19cc617978703450655e72f4883e0796acfb62a5d7e62a9baa16397e1016d719) --- 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.