# STC SA04075CH - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Dynon Avionics Inc., United States - Description: Installation of Dynon EFIS-D10A EAA sales kit part number 102778-000 - Applied: December 3, 2015 - Status date: January 1, 2026 - Product: Aircraft, Small Airplane - Certification basis: Part 23 - Data sheets: [TCDS 1A15](https://openairdocs.org/tcds/1A15), [TCDS 2A13](https://openairdocs.org/tcds/2A13), [TCDS A3SO](https://openairdocs.org/tcds/A3SO), [TCDS A18SO](https://openairdocs.org/tcds/A18SO), [TCDS 3A19](https://openairdocs.org/tcds/3A19), [TCDS 3A12](https://openairdocs.org/tcds/3A12), [TCDS 3A17](https://openairdocs.org/tcds/3A17), [TCDS A13CE](https://openairdocs.org/tcds/A13CE), [TCDS A20CE](https://openairdocs.org/tcds/A20CE), [TCDS 3A13](https://openairdocs.org/tcds/3A13) - Certificate PDF: https://openairdocs.org/files/sha256/96/f2/96f2ea3ac15b502a2e592707d021f0cc21942e7333e58dbca619ea7d9184dbde - Approved model list and other attachments: [SA04075CH_AML.pdf](https://openairdocs.org/files/sha256/33/27/332730fbce17cdb87d92fe1d79088763c9e26cd39ef2e5f460914545fdfb3eb9) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128712649220260209191953.0001 - DRS record last changed: March 4, 2026 - Page: https://openairdocs.org/stc/SA04075CH ## ADs that name it (0) None. ## Approved models (111, first 50) - Piper Aircraft Inc. PA-24 ([TCDS 1A15](https://openairdocs.org/tcds/1A15)) - Piper Aircraft Inc. PA-24-250 ([TCDS 1A15](https://openairdocs.org/tcds/1A15)) - Piper Aircraft Inc. PA-24-260 ([TCDS 1A15](https://openairdocs.org/tcds/1A15)) - Piper Aircraft Inc. PA-24-400 ([TCDS 1A15](https://openairdocs.org/tcds/1A15)) - Piper Aircraft Inc. PA-28-140 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-150 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-151 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-160 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-161 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-180 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-181 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-201T ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-235 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28-236 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28R-180 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28R-200 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28R-201 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28R-201T ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28RT-201 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28RT-201T ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28S-160 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-28S-180 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - Piper Aircraft Inc. PA-32-260 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO)) - Piper Aircraft Inc. PA-32-300 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO)) - Piper Aircraft Inc. PA-32-301 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO)) - Piper Aircraft Inc. PA-32-301FT ([TCDS A3SO](https://openairdocs.org/tcds/A3SO)) - Piper Aircraft Inc. PA-32-301T ([TCDS A3SO](https://openairdocs.org/tcds/A3SO)) - Piper Aircraft Inc. PA-32-301XTC ([TCDS A3SO](https://openairdocs.org/tcds/A3SO)) - Piper Aircraft Inc. PA-32R-300 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO)) - Piper Aircraft Inc. PA-32R-301 (HP) ([TCDS A3SO](https://openairdocs.org/tcds/A3SO)) - Piper Aircraft Inc. PA-32R-301 (SP) ([TCDS A3SO](https://openairdocs.org/tcds/A3SO)) - Piper Aircraft Inc. PA-32R-301T ([TCDS A3SO](https://openairdocs.org/tcds/A3SO)) - Piper Aircraft Inc. PA-32RT-300 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO)) - Piper Aircraft Inc. PA-32RT-300T ([TCDS A3SO](https://openairdocs.org/tcds/A3SO)) - Piper Aircraft Inc. PA-32S-300 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO)) - Piper Aircraft Inc. PA-38-112 ([TCDS A18SO](https://openairdocs.org/tcds/A18SO)) - Textron Aviation Inc. 150 ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Textron Aviation Inc. 150A ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Textron Aviation Inc. 150B ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Textron Aviation Inc. 150C ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Textron Aviation Inc. 150D ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Textron Aviation Inc. 150E ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Textron Aviation Inc. 150F ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Textron Aviation Inc. 150G ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Textron Aviation Inc. 150H ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Textron Aviation Inc. 150J ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Textron Aviation Inc. 150K ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Textron Aviation Inc. 150L ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Textron Aviation Inc. 150M ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) - Textron Aviation Inc. 152 ([TCDS 3A19](https://openairdocs.org/tcds/3A19)) All 111: https://openairdocs.org/stc/SA04075CH/models.md ## 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. SA04075CH Dynon Avionics, Inc. 19825 141st PL NE Woodinville, Washington 98072 Part 23 the Federal Aviation complete certification basis *See AML *See attached FAA Approved Model List (AML) No. SA04075CH for the list of approved models and applicable airworthiness regulations. 1. Compatibility of the design change with previously approved modifications must be determined by the installer. (Continued on page 3) 12/3/2015 7/18/2016 1/1/2026 4/1/2016 7/18/2016 for Paul Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division 3 Installation of Dynon EFIS-D10A EAA sales kit part number 102778-000 per Experimental Aircraft Association Document Number TJJ-MAN-01 Rev. NR dated March 29, 2016 or later FAA Approved Revision. Regulations. See Type Certificate Data Sheet A00002AC for SA04075CH 01/01/26 3 SA04075CH 01/01/26 Limitations and Conditions (continued): 2. This Approval includes a FAA Approved Commercial Parts List, EAA Document Number JAE-CPL-01, Rev. 1, dated March 25, 2016 or later FAA approved revision. 3. Aircraft must have been fitted with a pneumatically (vacuum) powered Attitude Indicator at the time of manufacture in order to be eligible for installation of this STC. 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. --------------------------------------------------------END------------------------------------------------------ ### SA04075CH_AML.pdf **FAA APPROVED MODEL LIST (AML) NO. SA04075CH DYNON AVIONICS, INC.** FOR INSTALLATION OF EQUIPTMENT PRODUCED UNDER A COMMERCIAL PARTS LIST ISSUE DATE: April 1, 2016 **ITEM AIRCRAFT AIRCRAFT** **ORIGINAL TYPE** **CERTIFICATION BASIS** **INSTALLATION** **INSTRUCTIONS AFM AML** **MAKE MODEL CERTIFICATE NUMBER FOR** **ALTERATION NUMBER** **REVISION NO. & DATE** **SUPPLEMENT** **NUMBER/DATE** AMENDMENT DATE Page 1 of 9 1 Textron Aviation Inc. 172 172I 172A 172K 172B 172L 172C 172M 172D 172N 172E 172P 172F (USAF T-41A) 172Q 172G 172R 172H (USAF T-41A) 172S Note: These models only eligible if equipped at time of manufacture with a pneumatically driven primary attitude indicator. 3A12 As listed in TCDS 3A12 except as noted below: 14 C FR 23 Amendement 49 for the follwing. 23.301,.303,.305,.307, .1301,.1303,.1307, .1309,.1311,.1321, .1322,.1323,.1325, .1327,.1331,.1351, .1353(h),.1357,.1359, .1365,.1381 EAA Document TJJ-MAN-02 Revision NR, or later FAA approved revision. N/A April 1, 2016 **FAA APPROVED MODEL LIST (AML) NO. SA04075CH DYNON AVIONICS, INC.** FOR INSTALLATION OF EQUIPTMENT PRODUCED UNDER A COMMERCIAL PARTS LIST ISSUE DATE: April 1, 2016 **ITEM AIRCRAFT AIRCRAFT** **ORIGINAL TYPE** **CERTIFICATION BASIS** **INSTALLATION** **INSTRUCTIONS AFM AML** **MAKE MODEL CERTIFICATE NUMBER FOR** **ALTERATION NUMBER** **REVISION NO. & DATE** **SUPPLEMENT** **NUMBER/DATE** AMENDMENT DATE Page 2 of 9 2 Textron Aviation Inc. 150 150J 150A 150K 150B A150K 150C 150L 150D A150L 150E 150M 150F A150M 150G 152 150H A152 Note: These models only eligible if equipped at time of manufacture with a pneumatically driven primary attitude indicator. 3A19 As listed in TCDS 3A19 except as noted below: 14 C FR 23 Amendement 49 for the follwing. 23.301,.303,.305,.307, .1301,.1303,.1307, .1309,.1311,.1321, .1322,.1323,.1325, .1327,.1331,.1351, .1353(h),.1357,.1359, .1365,.1381 EAA Document TJJ-MAN-02 Revision NR, or later FAA approved revision. N/A April 1, 2016 **FAA APPROVED MODEL LIST (AML) NO. SA04075CH DYNON AVIONICS, INC.** FOR INSTALLATION OF EQUIPTMENT PRODUCED UNDER A COMMERCIAL PARTS LIST ISSUE DATE: April 1, 2016 **ITEM AIRCRAFT AIRCRAFT** **ORIGINAL TYPE** **CERTIFICATION BASIS** **INSTALLATION** **INSTRUCTIONS AFM AML** **MAKE MODEL CERTIFICATE NUMBER FOR** **ALTERATION NUMBER** **REVISION NO. & DATE** **SUPPLEMENT** **NUMBER/DATE** AMENDMENT DATE Page 3 of 9 3 Piper Aircraft Inc. PA-28-140 PA-28-151 PA-28-150 PA-28-161 PA-28-160 PA-28-181 PA-28-180 PA-28R-201 PA-28-235 PA-28R-201T PA-28S-160 PA-28-236 PA-28S-180 PA-28RT-201 PA-28R-180 PA-28RT-201T PA-28R-200 PA-28-201T Note: These models only eligible if equipped at time of manufacture with a pneumatically driven primary attitude indicator. 2A13 As listed in TCDS 2A13 except as noted below: 14 C FR 23 Amendement 49 for the follwing. 23.301,.303,.305,.307, .1301,.1303,.1307, .1309,.1311,.1321, .1322,.1323,.1325, .1327,.1331,.1351, .1353(h),.1357,.1359, .1365,.1381 EAA Document TJJ-MAN-02 Revision NR, or later FAA approved revision. N/A April 1, 2016 **FAA APPROVED MODEL LIST (AML) NO. SA04075CH DYNON AVIONICS, INC.** FOR INSTALLATION OF EQUIPTMENT PRODUCED UNDER A COMMERCIAL PARTS LIST ISSUE DATE: April 1, 2016 **ITEM AIRCRAFT AIRCRAFT** **ORIGINAL TYPE** **CERTIFICATION BASIS** **INSTALLATION** **INSTRUCTIONS AFM AML** **MAKE MODEL CERTIFICATE NUMBER FOR** **ALTERATION NUMBER** **REVISION NO. & DATE** **SUPPLEMENT** **NUMBER/DATE** AMENDMENT DATE Page 4 of 9 4 Piper Aircraft Inc. PA-38-112 No te: These models only eligible if equipped at time of manufacture with a pneumatically driven primary attitude indicator. A18SO As listed in TCDS A18SO except as noted below: 14 C FR 23 Amendement 49 for the follwing. 23.301,.303,.305,.307, .1301,.1303,.1307, .1309,.1311,.1321, .1322,.1323,.1325, .1327,.1331,.1351, .1353(h),.1357,.1359, .1365,.1381 EAA Document TJJ-MAN-02 Revision NR, or later FAA approved revision. N/A April 1, 2016 **FAA APPROVED MODEL LIST (AML) NO. SA04075CH DYNON AVIONICS, INC.** FOR INSTALLATION OF EQUIPTMENT PRODUCED UNDER A COMMERCIAL PARTS LIST ISSUE DATE: April 1, 2016 **ITEM AIRCRAFT AIRCRAFT** **ORIGINAL TYPE** **CERTIFICATION BASIS** **INSTALLATION** **INSTRUCTIONS AFM AML** **MAKE MODEL CERTIFICATE NUMBER FOR** **ALTERATION NUMBER** **REVISION NO. & DATE** **SUPPLEMENT** **NUMBER/DATE** AMENDMENT DATE Page 5 of 9 5 Textron Aviation Inc. 182 182K 182A 182L 182B 182M 182C 182N 182D 182P 182E 182Q 182F 182R 182G R182 182H T182 182J TR182 182S T182T 182T Note: These models only eligible if equipped at time of manufacture with a pneumatically driven primary attitude indicator. 3A13 As listed in TCDS 3A13 except as noted below: 14 C FR 23 Amendement 49 for the follwing. 23.301,.303,.305,.307, .1301,.1303,.1307, .1309,.1311,.1321, .1322,.1323,.1325, .1327,.1331,.1351, .1353(h),.1357,.1359, .1365,.1381 EAA Document TJJ-MAN-02 Revision NR, or later FAA approved revision. N/A July 18, 2016 **FAA APPROVED MODEL LIST (AML) NO. SA04075CH DYNON AVIONICS, INC.** FOR INSTALLATION OF EQUIPTMENT PRODUCED UNDER A COMMERCIAL PARTS LIST ISSUE DATE: April 1, 2016 **ITEM AIRCRAFT AIRCRAFT** **ORIGINAL TYPE** **CERTIFICATION BASIS** **INSTALLATION** **INSTRUCTIONS AFM AML** **MAKE MODEL CERTIFICATE NUMBER FOR** **ALTERATION NUMBER** **REVISION NO. & DATE** **SUPPLEMENT** **NUMBER/DATE** AMENDMENT DATE Page 6 of 9 6 Textron Aviation Inc. 177 177A 177B Note: These models only eligible if equipped at time of manufacture with a pneumatically driven primary attitude indicator. A13CE As listed in TCDS A13CE except as noted below: 14 C FR 23 Amendement 49 for the follwing. 23.301,.303,.305,.307, .1301,.1303,.1307, .1309,.1311,.1321, .1322,.1323,.1325, .1327,.1331,.1351, .1353(h),.1357,.1359, .1365,.1381 EAA Document TJJ-MAN-02 Revision NR, or later FAA approved revision. N/A July 18, 2016 7 Textron Aviation Inc. 177RG No te: These models only eligible if equipped at time of manufacture with a pneumatically driven primary attitude indicator. A20CE As listed in TCDS A20CE except as noted below: 14 C FR 23 Amendement 49 for the follwing. 23.301,.303,.305,.307, .1301,.1303,.1307, .1309,.1311,.1321, .1322,.1323,.1325, .1327,.1331,.1351, .1353(h),.1357,.1359, .1365,.1381 EAA Document TJJ-MAN-02 Revision NR, or later FAA approved revision. N/A July 18, 2016 **FAA APPROVED MODEL LIST (AML) NO. SA04075CH DYNON AVIONICS, INC.** FOR INSTALLATION OF EQUIPTMENT PRODUCED UNDER A COMMERCIAL PARTS LIST ISSUE DATE: April 1, 2016 **ITEM AIRCRAFT AIRCRAFT** **ORIGINAL TYPE** **CERTIFICATION BASIS** **INSTALLATION** **INSTRUCTIONS AFM AML** **MAKE MODEL CERTIFICATE NUMBER FOR** **ALTERATION NUMBER** **REVISION NO. & DATE** **SUPPLEMENT** **NUMBER/DATE** AMENDMENT DATE Page 7 of 9 8 Textron Aviation Inc. 175 175A 175B 175C P172D R172E (USAF T-41B) (USAF T-41C or D) R172F (USAF T-41D) R172G (USAF T-41C / D) R172H (USAF T-41D) R172J R172K 172RG Note: These models only eligible if equipped at time of manufacture with a pneumatically driven primary attitude indicator. 3A17 As listed in TCDS 3A17 except as noted below: 14 C FR 23 Amendement 49 for the follwing. 23.301,.303,.305,.307, .1301,.1303,.1307, .1309,.1311,.1321, .1322,.1323,.1325, .1327,.1331,.1351, .1353(h),.1357,.1359, .1365,.1381 EAA Document TJJ-MAN-02 Revision NR, or later FAA approved revision. N/A July 18, 2016 **FAA APPROVED MODEL LIST (AML) NO. SA04075CH DYNON AVIONICS, INC.** FOR INSTALLATION OF EQUIPTMENT PRODUCED UNDER A COMMERCIAL PARTS LIST ISSUE DATE: April 1, 2016 **ITEM AIRCRAFT AIRCRAFT** **ORIGINAL TYPE** **CERTIFICATION BASIS** **INSTALLATION** **INSTRUCTIONS AFM AML** **MAKE MODEL CERTIFICATE NUMBER FOR** **ALTERATION NUMBER** **REVISION NO. & DATE** **SUPPLEMENT** **NUMBER/DATE** AMENDMENT DATE Page 8 of 9 9 Piper Aircraft, Inc PA-24 PA-24-250 PA-24-260 PA-24-400 No te: These models only eligible if equipped at time of manufacture with a pneumatically driven primary attitude indicator. 1A15 As listed in TCDS 1A15 except as noted below: 14 C FR 23 Amendement 49 for the follwing. 23.301,.303,.305,.307, .1301,.1303,.1307, .1309,.1311,.1321, .1322,.1323,.1325, .1327,.1331,.1351, .1353(h),.1357,.1359, .1365,.1381 EAA Document TJJ-MAN-02 Revision NR, or later FAA approved revision. N/A July 18, 2016 **FAA APPROVED MODEL LIST (AML) NO. SA04075CH DYNON AVIONICS, INC.** FOR INSTALLATION OF EQUIPTMENT PRODUCED UNDER A COMMERCIAL PARTS LIST ISSUE DATE: April 1, 2016 **ITEM AIRCRAFT AIRCRAFT** **ORIGINAL TYPE** **CERTIFICATION BASIS** **INSTALLATION** **INSTRUCTIONS AFM AML** **MAKE MODEL CERTIFICATE NUMBER FOR** **ALTERATION NUMBER** **REVISION NO. & DATE** **SUPPLEMENT** **NUMBER/DATE** AMENDMENT DATE Page 9 of 9 NOTE: FAA Approved Commercial Parts List, EAA Document Number JAE-CPL-01, Revison 1, Dated March 25, 2016 or later FAA approved revision is applicable to all models listed above. = FAA APPROVED: for Paul Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service Issued: April 1, 2016 Amended: July 18, 2016 Reissued: January 1, 2026 10 Piper Aircraft, Inc PA-32-260 PA-32R-301 (SP) PA-32-300 PA-32R-301 (HP) PA-32S-300 PA-32R-301T PA-32R-300 PA-32-301 PA-32RT-300 PA-32-301T PA-32RT-300T PA-32-301FT PA-32-301XTC Note: These models only eligible if equipped at time of manufacture with a pneumatically driven primary attitude indicator. A3SO As listed in TCDS A3SO except as noted below: 14 CFR 23 Amendement 49 for the follwing. 23.301,.303,.305,.307, .1301,.1303,.1307, .1309,.1311,.1321, .1322,.1323,.1325, .1327,.1331,.1351, .1353(h),.1357,.1359, .1365,.1381 EAA Document TJJ-MAN-02 Revision NR, or later FAA approved revision. N/A July 18, 2016 ## Every issue (2) - January 1, 2026: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/96/f2/96f2ea3ac15b502a2e592707d021f0cc21942e7333e58dbca619ea7d9184dbde), [SA04075CH_AML.pdf](https://openairdocs.org/files/sha256/33/27/332730fbce17cdb87d92fe1d79088763c9e26cd39ef2e5f460914545fdfb3eb9) - July 18, 2016: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/cd/b5/cdb5b11033c096ad4ef13d533d6d76453d162cb695cc78dd7189d631b8b52792), [AML_SA04075CH.pdf](https://openairdocs.org/files/sha256/11/58/11584e9387af1eab1e221d5665cc9eb491ce9155e155e0b988c141f4e6fe559b) --- 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.