# STC SA01405WI - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Mooney Airplane Company Inc., United States - Description: Installation of the Garmin GFC 700 Automatic Flight Control System and TAWS Option. - Applied: October 28, 2005 - Status date: November 17, 2006 - Product: Aircraft, Single-Engine - Certification basis: Part 21, Part 23 - Data sheets: [TCDS 2A3](https://openairdocs.org/tcds/2A3) - Certificate PDF: https://openairdocs.org/files/sha256/6e/bf/6ebf567a80298faa380f6cfeccdb90bfeb132c39d165c67623bdfd0ee536bae2 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/092733389ADCB5C1862574F100780793.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA01405WI ## ADs that name it (0) None. ## Approved models (2) - Mooney Aircraft Corporation M20M ([TCDS 2A3](https://openairdocs.org/tcds/2A3)) - Mooney Aircraft Corporation M20R ([TCDS 2A3](https://openairdocs.org/tcds/2A3)) ## 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. This certificate issued to Mooney Airplane Company, Inc. 165 Al Mooney Drive North Kerrville, Texas 78028 Part 23 of the Federal Aviation Regulations. Original Product--Type Certificate Number: 2A3 Make: Mooney Model: M20M, M20R Installation of the Garmin GFC 700 Automatic Flight Control System and TAWS Option in the Mooney M20M / M20R Aircraft in accordance with (1) Garmin Master Drawing List 005-00343-02, Revision B, dated October 6, 2006 and (2) Garmin Document No. 190-00638-00, FAA Approved Airplane Flight Manual Supplement, Revision A, dated October 6, 2006, or later FAA Approved Revision to (1) or (2). 1. M20M and M20R aircraft equipped with a G1000 Integrated Avionics System and STEC Autopilot System are eligible for this STC. 2. The modified aircraft must be maintained in accordance with the applicable Instructions for Continued Airworthiness (ICA) identified on the MDL. 3. Compatibility of this design change with previously approved modifications must be determined by the installer. 4. 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 page 3 of 3) Date reissued : November 17, 2006 Date of application: October 28, 2005 Date of issuance: October 6, 2006 Original signed by Harvey E. Nero ( Signature) Harvey E. Nero FAA Program Manager Wichita Aircraft Certification Office ( Title) FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES Number SA01405WI Date of Issuance: October 6, 2006 Date Re-issued: November 17, 2006 Certification Basis (continued from Page 1): With respect to the modifications of this STC, the applicant has complied with the following certification basis: a. The type certification basis for Mooney M20M and M20R airplanes is shown on TCDS 2A3 for parts not changed or not affected by the change. b. The certification basis for parts changed or affected by the change since the reference date of application, is based upon Part 23 as amended by Amendment 23-55. The certification basis for this modification was determined to be: Regulations at the latest Amendment 23-0 through 23-55. 14 CFR Part Amendment 14 CFR Part Amendment § 23.143(a)(b)(c) 23-50 § 23.867(a)(b) 23-49 § 23.301(a) 23-48 § 23.1301(a)(b)(c)(d) 23-20 § 23.303 - § 23.1309(a)(b)(c)(d)(e)(f) 23-49 § 23.305(a)(b) 23-45 § 23.1311(a)(b)(c) 23-49 § 23.307(a) - § 23.1321(a)(c)(e) 23-49 § 23.395(a)(1) 23-7 § 23.1322(a)(b)(c)(d)(e) 23-43 § 23.397(a)(b) 23-45 § 23.1329(a)(b)(c)(d) (e)(f)(h) 23-49 § 23.561(a)(b)(2) 23-48 § 23.1335 23-20 § 23.601 - § 23.1351(a)(g) 23-49 § 23.603(a)(b) 23-23 § 23.1353(h) 23-49 § 23.605 23-23 § 23.1357(a)(b)(c)(d) 23-43 § 23.607 - § 23.1359(a)(b)(c) 23-49 § 23.609(a)(b) - § 23.1365(a)(b)(d)(e) 23-49 § 23.611 - § 23.1367(a)(b)(c)(d) - § 23.613(a)(b)(c) 23-45 § 23.1381(a)(b) - § 23.625(a) 23-7 § 23.1431(a)(b)(e) 23-49 § 23.671(a)(b) - § 23.1525 23-45 § 23.677(a)(d) 23-49 § 23.1529 23-26 § 23.685(a)(c)(d) 23-17 § 23.1541(b)(1)(c)(2) 23-21 § 23.689(a)(1)(2)(3) (b)(c)(d)(e) 23-7 § 23.1555(a) 23-50 § 23.771(a) 23-14 § 23.1581(a)(b)(2)(c)(d)(f) 23-50 § 23.777(a)(b) 23-51 § 23.1583(h)(m) 23-50 § 23.779(a) 23-51 § 23.1585(j) 23-50 Special Conditions 23-177-SC; GFC 700 AFCS on the Mooney M20M and M20R with G1000 EFIS; Protection of Systems for High Intensity Radiated Fields (HIRF) ----------------------END-------------------- ## Every issue (3) - November 17, 2006: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/6e/bf/6ebf567a80298faa380f6cfeccdb90bfeb132c39d165c67623bdfd0ee536bae2) - November 17, 2006: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/6e/bf/6ebf567a80298faa380f6cfeccdb90bfeb132c39d165c67623bdfd0ee536bae2) - October 6, 2006: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/44/b6/44b67a32019433630e1b47d278acd63bd5048f15bbfea8f5be8eeb4ec35083f5) --- 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.