# STC SA01141WI-D - Type: Supplemental type certificate - Status: Current, Amended - Holder: Rockwell Collins Inc, United States - Description: Modification of a single or dual Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92 control head to a Flight ID capable Collins TDR-94 or TDR-94 Mode S Transponder System installation with CTL-92E control head. - Applied: August 21, 2002 - Status date: May 24, 2006 - Product: Aircraft, Single-Engine - Certification basis: Part 3, Part 21, Part 23, Part 36 - Data sheets: [TCDS A7PC](https://openairdocs.org/tcds/A7PC), [TCDS A9EA](https://openairdocs.org/tcds/A9EA), [TCDS A21EU](https://openairdocs.org/tcds/A21EU), [TCDS A56EU](https://openairdocs.org/tcds/A56EU), [TCDS A28CE](https://openairdocs.org/tcds/A28CE), [TCDS A7CE](https://openairdocs.org/tcds/A7CE), [TCDS A16EU](https://openairdocs.org/tcds/A16EU), [TCDS A18SW](https://openairdocs.org/tcds/A18SW), [TCDS A5SW](https://openairdocs.org/tcds/A5SW), [TCDS A8SW](https://openairdocs.org/tcds/A8SW), [TCDS A59EU](https://openairdocs.org/tcds/A59EU), [TCDS A10SW](https://openairdocs.org/tcds/A10SW), [TCDS A50EU](https://openairdocs.org/tcds/A50EU), [TCDS 1A10](https://openairdocs.org/tcds/1A10), [TCDS A23SO](https://openairdocs.org/tcds/A23SO), [TCDS A8EA](https://openairdocs.org/tcds/A8EA), [TCDS 3A20](https://openairdocs.org/tcds/3A20), [TCDS A23CE](https://openairdocs.org/tcds/A23CE), [TCDS A24CE](https://openairdocs.org/tcds/A24CE), [TCDS A31CE](https://openairdocs.org/tcds/A31CE) and 2 more - Certificate PDF: https://openairdocs.org/files/sha256/40/91/4091c7c4e0be8a651be52d1258388207e68754fc1e5a5fd9dfcdc2870d52850f - Approved model list and other attachments: [SA01141WI-D.pdf](https://openairdocs.org/files/sha256/48/e4/48e4da9f01ec2ede8620579a68f21c2850575450bab38f3e9d4224bdecb8f4c9) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7FF3B082A9B0632B86257314004DE6F8.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA01141WI-D ## ADs that name it (0) None. ## Approved models (104, first 50) - AeroSpace Technologies Of Australia Pty Ltd. N22B ([TCDS A7PC](https://openairdocs.org/tcds/A7PC)) - AeroSpace Technologies Of Australia Pty Ltd. N22S ([TCDS A7PC](https://openairdocs.org/tcds/A7PC)) - B-N Group Ltd. BN-2 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU)) - B-N Group Ltd. BN-2A ([TCDS A17EU](https://openairdocs.org/tcds/A17EU)) - B-N Group Ltd. BN-2A-2 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU)) - B-N Group Ltd. BN-2A-20 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU)) - B-N Group Ltd. BN-2A-21 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU)) - B-N Group Ltd. BN-2A-26 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU)) - B-N Group Ltd. BN-2A-27 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU)) - B-N Group Ltd. BN-2A-3 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU)) - B-N Group Ltd. BN-2A-6 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU)) - B-N Group Ltd. BN-2A-8 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU)) - B-N Group Ltd. BN-2A-9 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU)) - B-N Group Ltd. BN-2B-20 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU)) - B-N Group Ltd. BN-2B-21 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU)) - B-N Group Ltd. BN-2B-26 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU)) - B-N Group Ltd. BN-2B-27 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU)) - B-N Group Ltd. BN-2T ([TCDS A17EU](https://openairdocs.org/tcds/A17EU)) - B-N Group Ltd. BN-2T-4R ([TCDS A17EU](https://openairdocs.org/tcds/A17EU)) - Bombardier Inc. DHC-6-100 ([TCDS A9EA](https://openairdocs.org/tcds/A9EA)) - Bombardier Inc. DHC-6-200 ([TCDS A9EA](https://openairdocs.org/tcds/A9EA)) - Bombardier Inc. DHC-6-300 ([TCDS A9EA](https://openairdocs.org/tcds/A9EA)) - British Aerospace (Scotland) Jetstream 3201 ([TCDS A56EU](https://openairdocs.org/tcds/A56EU)) - British Aerospace (Scotland) Jetstream Series 3101 ([TCDS A21EU](https://openairdocs.org/tcds/A21EU)) - Dornier Luftfahrt GmbH Dornier 228-100 ([TCDS A16EU](https://openairdocs.org/tcds/A16EU)) - Dornier Luftfahrt GmbH Dornier 228-101 ([TCDS A16EU](https://openairdocs.org/tcds/A16EU)) - Dornier Luftfahrt GmbH Dornier 228-200 ([TCDS A16EU](https://openairdocs.org/tcds/A16EU)) - Dornier Luftfahrt GmbH Dornier 228-201 ([TCDS A16EU](https://openairdocs.org/tcds/A16EU)) - Dornier Luftfahrt GmbH Dornier 228-202 ([TCDS A16EU](https://openairdocs.org/tcds/A16EU)) - Dornier Luftfahrt GmbH Dornier 228-212 ([TCDS A16EU](https://openairdocs.org/tcds/A16EU)) - Fairchild Aircraft Corporation SA226-TC ([TCDS A8SW](https://openairdocs.org/tcds/A8SW)) - Fairchild Aircraft Corporation SA227-AC (C-26A) ([TCDS A8SW](https://openairdocs.org/tcds/A8SW)) - Fairchild Aircraft Corporation SA227-AT ([TCDS A5SW](https://openairdocs.org/tcds/A5SW)) - Fairchild Aircraft Corporation SA227-BC (C-26A) ([TCDS A8SW](https://openairdocs.org/tcds/A8SW)) - Fairchild Aircraft Corporation SA227-CC ([TCDS A18SW](https://openairdocs.org/tcds/A18SW)) - Fairchild Aircraft Corporation SA227-DC (C-26B) ([TCDS A18SW](https://openairdocs.org/tcds/A18SW)) - Fairchild Aircraft Corporation SA227-PC ([TCDS A8SW](https://openairdocs.org/tcds/A8SW)) - Fairchild Aircraft Corporation SA227-TT ([TCDS A5SW](https://openairdocs.org/tcds/A5SW)) - Industrie Aeronautiche e Meccaniche P-180 ([TCDS A59EU](https://openairdocs.org/tcds/A59EU)) - Mitsubishi Heavy Industries Ltd. MU-2B-25 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW)) - Mitsubishi Heavy Industries Ltd. MU-2B-26 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW)) - Mitsubishi Heavy Industries Ltd. MU-2B-26A ([TCDS A10SW](https://openairdocs.org/tcds/A10SW)) - Mitsubishi Heavy Industries Ltd. MU-2B-35 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW)) - Mitsubishi Heavy Industries Ltd. MU-2B-36 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW)) - Mitsubishi Heavy Industries Ltd. MU-2B-36A ([TCDS A10SW](https://openairdocs.org/tcds/A10SW)) - Mitsubishi Heavy Industries Ltd. MU-2B-40 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW)) - Mitsubishi Heavy Industries Ltd. MU-2B-60 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW)) - Piaggio Aero Industries S.p.A. P-180 ([TCDS A59EU](https://openairdocs.org/tcds/A59EU)) - Pilatus Aircraft Limited PC-7 ([TCDS A50EU](https://openairdocs.org/tcds/A50EU)) - Raytheon Aircraft Company 1900C (C-12J) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) All 104: https://openairdocs.org/stc/SA01141WI-D/models.md ## What the certificate says Some pages are OCR from the scanned FAA certificate. OCR can misread letters and numbers. **FAA APPROVED MODEL LIST (AML) NO. SA01141WI-D** **ROCKWELL COLLINS, INC.** FOR MODIFICATION OF A SINGLE OR DUAL COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH CTL-92 CONTROL HEAD TO A FLIGHT ID CAPABLE COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH COLLINS CTL-92E CONTROL HEAD IN PART 23 AIRCRAFT Issue Date: 02/2 4/03 **ORIGINAL** **CERTIFICATION** **INSTALLATION** **INSTRUCTIONS** **ITEM** **AIRCRAFT MAKE** **AIRCRAFT MODEL TYPE** **CERTIFICATE NUMBER BASIS FOR** **ALTERATION** **DRAWING INDEX NO.** **REVISION NO.** AND DATE [1] AFM **SUPPLEMENT** **NUMBER/DATE AML** **AMENDMENT DATE** Aerospace Technologies of Australia PTY Ltd N22B N22S A7PC FAR 21.29 and FAR 23, effective February 1, 1965, including Amendments 23- 1 to 23-9, and additional requirements in TCDS A7PC 992-4435-001 Rev A, 09/15/05 09/15/05 [1] Or later FAA approved revision Page 2 of 21 FAA APPROVED MODEL LIST (AML) NO. SA01141WI-D **ROCKWELL COLLINS, INC.** FOR MODIFICATION OF A SINGLE OR DUAL COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH CTL-92 CONTROL HEAD TO A FLIGHT ID CAPABLE COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH COLLINS CTL-92E CONTROL HEAD IN PART 23 AIRCRAFT Issue Date: 0 2/24/03 **ORIGINAL** **CERTIFICATION** **INSTALLATION** **INSTRUCTIONS** **ITEM** **AIRCRAFT MAKE** **AIRCRAFT MODEL TYPE** **CERTIFICATE NUMBER BASIS FOR** **ALTERATION** **DRAWING INDEX NO.** **REVISION NO.** AND DATE [1] AFM **SUPPLEMENT** **NUMBER/DATE AML** **AMENDMENT DATE** Beech Aircraft Corporation **58P 58PA 58TC 58TCA** A23CE Part 23 of the Federal Aviation Regulations, effective February 1, 1965, and Amendments 1 through 12, and additional requirements in TCDS A23CE 992-4435-001 Rev A, 09/15/05 09/15/05 [1] Or later FAA approved revision Page 3 of 21 FAA APPROVED MODEL LIST (AML) NO. SA01141WI-D **ROCKWELL COLLINS, INC.** FOR MODIFICATION OF A SINGLE OR DUAL COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH CTL-92 CONTROL HEAD TO A FLIGHT ID CAPABLE COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH COLLINS CTL-92E CONTROL HEAD IN PART 23 AIRCRAFT Issue Date: 0 2/24/03 **ORIGINAL** **CERTIFICATION** **INSTALLATION** **INSTRUCTIONS** **ITEM** **AIRCRAFT MAKE** **AIRCRAFT MODEL TYPE** **CERTIFICATE NUMBER BASIS FOR** **ALTERATION** **DRAWING INDEX NO.** **REVISION NO.** AND DATE [1] AFM **SUPPLEMENT** **NUMBER/DATE AML** **AMENDMENT DATE** Beech Aircraft Corporation Bombardier Inc. F90 (Twin Otter) DHC-6-100 DHC-6-200 DHC-6-300 A31CE A9EA FAR Part 23 dated February 1, 1965, as amended through 23-16, and additional requirements in TCDS A31CE CAR 3 dated May 15, 1956 and Amendments 3-1 to 3-8, and additional requirements in TCDS A9EA 992-4435-001 992-4435-001 Rev A, 09/15/05 Rev A, 09/15/05 09/15/05 09/15/05 [1] Or later FAA approved revision Page 4 of 21 FAA APPROVED MODEL LIST (AML) NO. SA01141WI-D **ROCKWELL COLLINS, INC.** FOR MODIFICATION OF A SINGLE OR DUAL COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH CTL-92 CONTROL HEAD TO A FLIGHT ID CAPABLE COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH COLLINS CTL-92E CONTROL HEAD IN PART 23 AIRCRAFT Issue Date: 0 2/24/03 **ORIGINAL** **CERTIFICATION** **INSTALLATION** **INSTRUCTIONS** **ITEM** **AIRCRAFT MAKE** **AIRCRAFT MODEL TYPE** **CERTIFICATE NUMBER BASIS FOR** **ALTERATION** **DRAWING INDEX NO.** **REVISION NO.** AND DATE [1] AFM **SUPPLEMENT** **NUMBER/DATE AML** **AMENDMENT DATE** 5 British Aerospace Regional Aircraft Jetstream Model 3101 A21EU FAR 21.29 and FAR 23, effective February 1, 1965, including Amendments 23-1 through 23-3, and additional requirements in TCDS A21EU 992-4435-001 Rev A, 09/15/05 09/15/05 [1] Or later FAA approved revision Page 5 of 21 FAA APPROVED MODEL LIST (AML) NO. SA01141WI-D **ROCKWELL COLLINS, INC.** FOR MODIFICATION OF A SINGLE OR DUAL COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH CTL-92 CONTROL HEAD TO A FLIGHT ID CAPABLE COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH COLLINS CTL-92E CONTROL HEAD IN PART 23 AIRCRAFT Issue Date: 0 2/24/03 **ORIGINAL** **CERTIFICATION** **INSTALLATION** **INSTRUCTIONS** **ITEM** **AIRCRAFT MAKE** **AIRCRAFT MODEL TYPE** **CERTIFICATE NUMBER BASIS FOR** **ALTERATION** **DRAWING INDEX NO.** **REVISION NO.** AND DATE [1] AFM **SUPPLEMENT** **NUMBER/DATE AML** **AMENDMENT DATE** British Aerospace Regional Aircraft Jetstream Model 3201 A56EU FAR 21.29 and FAR Part 23, effective February 1, 1965, including Amendments 23-1 through 23-34, and additional requirements in TCDS A56EU 992-4435-001 Rev A, 09/15/05 09/15/05 [1] Or later FAA approved revision **FAA APPROVED MODEL LIST (AML) NO. SA01141WI-D** **ROCKWELL COLLINS, INC.** FOR MODIFICATION OF A SINGLE OR DUAL COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH CTL-92 CONTROL HEAD TO A FLIGHT ID CAPABLE COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH COLLINS CTL-92E CONTROL HEAD IN PART 23 AIRCRAFT Issue Date: 02/24/03 **ORIGINAL** **CERTIFICATION** **INSTALLATION** **INSTRUCTIONS** **ITEM** **AIRCRAFT MAKE** **AIRCRAFT MODEL TYPE** **CERTIFICATE NUMBER BASIS FOR** **ALTERATION** **DRAWING INDEX NO.** **REVISION NO.** AND DATE [1] AFM **SUPPLEMENT** **NUMBER/DATE AML** **AMENDMENT DATE** Cessna Aircraft Company 425 A7CE Part 3 of the Civil Air Regulations dated May 15, 1956, as amended by 3-1 through 3-6, 3-8, and additional requirements in TCDS A7CE 992-4435-001 Rev A, 09/15/05 09/15/05 [1] Or later FAA approved revision Page 7 of 21 FAA APPROVED MODEL LIST (AML) NO. SA01141WI-D **ROCKWELL COLLINS, INC.** FOR MODIFICATION OF A SINGLE OR DUAL COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH CTL-92 CONTROL HEAD TO A FLIGHT ID CAPABLE COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH COLLINS CTL-92E CONTROL HEAD IN PART 23 AIRCRAFT Issue Date: 02/24/03 **ORIGINAL** **CERTIFICATION** **INSTALLATION** **INSTRUCTIONS** **ITEM** **AIRCRAFT MAKE** **AIRCRAFT MODEL TYPE** **CERTIFICATE NUMBER BASIS FOR** **ALTERATION** **DRAWING INDEX NO.** **REVISION NO.** AND DATE [1] AFM **SUPPLEMENT** **NUMBER/DATE AML** **AMENDMENT DATE** Cessna Aircraft Company 441 A28CE Part 23 of the Federal Aviation Regulations effective February 1, 1965, as amended by 23-1 through 23-14, and additional requirements in TCDS A28CE 992-4435-001 Rev A, 09/15/05 09/15/05 [1] Or later FAA approved revision Page 8 of 21 FAA APPROVED MODEL LIST (AML) NO. SA01141WI-D **ROCKWELL COLLINS, INC.** FOR MODIFICATION OF A SINGLE OR DUAL COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH CTL-92 CONTROL HEAD TO A FLIGHT ID CAPABLE COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH COLLINS CTL-92E CONTROL HEAD IN PART 23 AIRCRAFT Issue Date: 02/24/03 **ORIGINAL** **CERTIFICATION** **INSTALLATION** **INSTRUCTIONS** **ITEM** **AIRCRAFT MAKE** **AIRCRAFT MODEL TYPE** **CERTIFICATE NUMBER BASIS FOR** **ALTERATION** **DRAWING INDEX NO.** **REVISION NO.** AND DATE [1] AFM **SUPPLEMENT** **NUMBER/DATE AML** **AMENDMENT DATE** Dornier Luftfahrt GMBH Dornier 228-100 Dornier 228-101 Dornier 228-200 Dornier 228-201 Dornier 228-202 Dornier 228-212 A16EU FAR 23, effective February 1, 1965, including Amendments 23-1 through 23-23, and additional requirements in TCDS A16EU 992-4435-001 Rev A, 09/15/05 09/15/05 [1] Or later FAA approved revision Page 9 of 21 FAA APPROVED MODEL LIST (AML) NO. SA01141WI-D **ROCKWELL COLLINS, INC.** FOR MODIFICATION OF A SINGLE OR DUAL COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH CTL-92 CONTROL HEAD TO A FLIGHT ID CAPABLE COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH COLLINS CTL-92E CONTROL HEAD IN PART 23 AIRCRAFT Issue Date: 02/24/03 **ORIGINAL** **CERTIFICATION** **INSTALLATION** **INSTRUCTIONS** **ITEM** **AIRCRAFT MAKE** **AIRCRAFT MODEL TYPE** **CERTIFICATE NUMBER BASIS FOR** **ALTERATION** **DRAWING INDEX NO.** **REVISION NO.** AND DATE [1] AFM **SUPPLEMENT** **NUMBER/DATE AML** **AMENDMENT DATE** Fairchild Aircraft Corporation Fairchild Aircraft Inc. SA227-AT SA227-TT SA226TC SA227-AC SA227-PC SA227-BC (C-26A) A5SW A8SW CAR 3 effective May 15, 1956, through Amendments 3-8, and additional requirements in TCDS A5SW FAR 23 effective February 1, 1965, through Amendments 23-6, and additional requirements in TCDS A8SW 992-4435-001 992-4435-001 Rev A, 09/15/05 Rev A, 09/15/05 09/15/05 09/15/05 [1] Or later FAA approved revision Page 10 of 21 FAA APPROVED MODEL LIST (AML) NO. SA01141WI-D **ROCKWELL COLLINS, INC.** FOR MODIFICATION OF A SINGLE OR DUAL COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH CTL-92 CONTROL HEAD TO A FLIGHT ID CAPABLE COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH COLLINS CTL-92E CONTROL HEAD IN PART 23 AIRCRAFT Issue Date: 02/24/03 **ORIGINAL** **CERTIFICATION** **INSTALLATION** **INSTRUCTIONS** **ITEM** **AIRCRAFT MAKE** **AIRCRAFT MODEL TYPE** **CERTIFICATE NUMBER BASIS FOR** **ALTERATION** **DRAWING INDEX NO.** **REVISION NO.** AND DATE [1] AFM **SUPPLEMENT** **NUMBER/DATE AML** **AMENDMENT DATE** 12 Fairchild Aircraft Inc. SA227-CC SA227-DC (C-26B) A18SW FAR Part 23 through Amendment 23-34 plus Amendment 23-39; FAR Part 36, SFAR 27 through Amendment 5, and additional requirements in TCDS A18SW 992-4435-001 Rev A, 09/15/05 09/15/05 [1] Or later FAA approved revision **FAA APPROVED MODEL LIST (AML) NO. SA01141WI-D** **ROCKWELL COLLINS, INC.** FOR MODIFICATION OF A SINGLE OR DUAL COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH CTL-92 CONTROL HEAD TO A FLIGHT ID CAPABLE COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH COLLINS CTL-92E CONTROL HEAD IN PART 23 AIRCRAFT Issue Date: 02/24/03 **ORIGINAL** **CERTIFICATION** **INSTALLATION** **INSTRUCTIONS** **ITEM** **AIRCRAFT MAKE** **AIRCRAFT MODEL TYPE** **CERTIFICATE NUMBER BASIS FOR** **ALTERATION** **DRAWING INDEX NO.** **REVISION NO.** AND DATE [1] AFM **SUPPLEMENT** **NUMBER/DATE AML** **AMENDMENT DATE** Industrie Aeronautich Meccaniche P-180 A59EU Federal Aviation Regulations – 14 CFR Part 23, effective February 1, 1965, including Amendments 23-1 through 23-33, and additional requirements in TCDS A59EU 992-4435-001 Rev A, 09/15/05 09/15/05 [1] Or later FAA approved revision **FAA APPROVED MODEL LIST (AML) NO. SA01141WI-D** **ROCKWELL COLLINS, INC.** FOR MODIFICATION OF A SINGLE OR DUAL COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH CTL-92 CONTROL HEAD TO A FLIGHT ID CAPABLE COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH COLLINS CTL-92E CONTROL HEAD IN PART 23 AIRCRAFT Issue Date: 02/24/03 **ORIGINAL** **CERTIFICATION** **INSTALLATION** **INSTRUCTIONS** **ITEM** **AIRCRAFT MAKE** **AIRCRAFT MODEL TYPE** **CERTIFICATE NUMBER BASIS FOR** **ALTERATION** **DRAWING INDEX NO.** **REVISION NO.** AND DATE [1] AFM **SUPPLEMENT** **NUMBER/DATE AML** **AMENDMENT DATE** Mitsubishi Heavy Industries Ltd. Mitsubishi Heavy Industries Ltd. MU-2B-36 MU-2B-26 MU-2B-25 MU-2B-35 MU-2B-26 MU-2B-36 MU-2B-26A MU-2B-40 MU-2B-36A MU-2B-60 A2PC A10SW CAR 3 dated May 15, 1956, including Amendments 3-1 through 3-8, and additional requirements in TCDS A2PC CAR 3 dated May 15, 1956, including Amendments 3-1 through 3-8, and additional requirements in TCDS A10SW 992-4435-001 992-4435-001 Rev A, 09/15/05 Rev A, 09/15/05 09/15/05 09/15/05 [1] Or later FAA approved revision Page 13 of 21 FAA APPROVED MODEL LIST (AML) NO. SA01141WI-D **ROCKWELL COLLINS, INC.** FOR MODIFICATION OF A SINGLE OR DUAL COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH CTL-92 CONTROL HEAD TO A FLIGHT ID CAPABLE COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH COLLINS CTL-92E CONTROL HEAD IN PART 23 AIRCRAFT Issue Date: 02/24/03 **ORIGINAL** **CERTIFICATION** **INSTALLATION** **INSTRUCTIONS** **ITEM** **AIRCRAFT MAKE** **AIRCRAFT MODEL TYPE** **CERTIFICATE NUMBER BASIS FOR** **ALTERATION** **DRAWING INDEX NO.** **REVISION NO.** AND DATE [1] AFM **SUPPLEMENT** **NUMBER/DATE AML** **AMENDMENT DATE** Piaggio Aero Industries S.p.A. Pilatus Aircraft Ltd. P-180 PC-7 A59EU A50EU 14 CFR Part 23 effective February 1, 1965, including Amendments 23-1 through 23-33, and additional requirements in TCDS A59EU 14 CFR Part 23 effective February 1, 1965, including Amendments 23-1 through 23-16, and additional requirements in TCDS A50EU 992-4435-001 992-4435-001 Rev A, 09/15/05 Rev A, 09/15/05 09/15/05 09/15/05 [1] Or later FAA approved revision Page 14 of 21 FAA APPROVED MODEL LIST (AML) NO. SA01141WI-D **ROCKWELL COLLINS, INC.** FOR MODIFICATION OF A SINGLE OR DUAL COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH CTL-92 CONTROL HEAD TO A FLIGHT ID CAPABLE COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH COLLINS CTL-92E CONTROL HEAD IN PART 23 AIRCRAFT Issue Date: 02/24/03 **ORIGINAL** **CERTIFICATION** **INSTALLATION** **INSTRUCTIONS** **ITEM** **AIRCRAFT MAKE** **AIRCRAFT MODEL TYPE** **CERTIFICATE NUMBER BASIS FOR** **ALTERATION** **DRAWING INDEX NO.** **REVISION NO.** AND DATE [1] AFM **SUPPLEMENT** **NUMBER/DATE AML** **AMENDMENT DATE** Pilatus Britten- Norman Limited BN-2, BN-2A BN-2A-6 BN-2A-8 BN-2A-2 BN-2A-9 BN-2A-3 BN-2A-20 BN-2A-21 BN-2A-26 BN-2A-27 BN-2B-20 BN-2B-21 BN-2B-26 BN-2B-27 BN-2T BN-2T-4R A17EU FAR 21.29 and FAR 23, effective February 1, 1965, including Amendments 23-1, and additional requirements in TCDS A17EU 992-4435-001 Rev A, 09/15/05 09/15/05 [1] Or later FAA approved revision **FAA APPROVED MODEL LIST (AML) NO. SA01141WI-D** **ROCKWELL COLLINS, INC.** FOR MODIFICATION OF A SINGLE OR DUAL COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH CTL-92 CONTROL HEAD TO A FLIGHT ID CAPABLE COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH COLLINS CTL-92E CONTROL HEAD IN PART 23 AIRCRAFT Issue Date: 02/24/03 **ORIGINAL** **CERTIFICATION** **INSTALLATION** **INSTRUCTIONS** **ITEM** **AIRCRAFT MAKE** **AIRCRAFT MODEL TYPE** **CERTIFICATE NUMBER BASIS FOR** **ALTERATION** **DRAWING INDEX NO.** **REVISION NO.** AND DATE [1] AFM **SUPPLEMENT** **NUMBER/DATE AML** **AMENDMENT DATE** The New Piper Aircraft, Inc. The New Piper Aircraft, Inc. PA-23 PA-31T2 1A10 A8EA CAR 3 dated November 1, 1949, including Amendments 3-1 through 3-9, and additional requirements in TCDS 1A10 CAR 3 effective May 15, 1956, through Amendment 3-8, and additional requirements in TCDS A8EA 992-4435-001 992-4435-001 Rev A, 09/15/05 Rev A, 09/15/05 09/15/05 09/15/05 [1] Or later FAA approved revision **FAA APPROVED MODEL LIST (AML) NO. SA01141WI-D** **ROCKWELL COLLINS, INC.** FOR MODIFICATION OF A SINGLE OR DUAL COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH CTL-92 CONTROL HEAD TO A FLIGHT ID CAPABLE COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH COLLINS CTL-92E CONTROL HEAD IN PART 23 AIRCRAFT Issue Date: 02/24/03 **ORIGINAL** **CERTIFICATION** **INSTALLATION** **INSTRUCTIONS** **ITEM** **AIRCRAFT MAKE** **AIRCRAFT MODEL TYPE** **CERTIFICATE NUMBER BASIS FOR** **ALTERATION** **DRAWING INDEX NO.** **REVISION NO.** AND DATE [1] AFM **SUPPLEMENT** **NUMBER/DATE AML** **AMENDMENT DATE** The New Piper Aircraft, Inc. PA-42 PA-42-720 PA-42-1000 A23SO Federal Aviation Regulations Part 23 effective February 1, 1965, including Amendments 23- 14, 23-16, 23-17, 23-18, 23-20, 23- 21, 23-23, 23-26, and additional requirements in TCDS A23SO 992-4435-001 Rev A, 09/15/05 09/15/05 [1] Or later FAA approved revision Page 17 of 21 FAA APPROVED MODEL LIST (AML) NO. SA01141WI-D **ROCKWELL COLLINS, INC.** FOR MODIFICATION OF A SINGLE OR DUAL COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH CTL-92 CONTROL HEAD TO A FLIGHT ID CAPABLE COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH COLLINS CTL-92E CONTROL HEAD IN PART 23 AIRCRAFT Issue Date: 02/24/03 **ORIGINAL** **CERTIFICATION** **INSTALLATION** **INSTRUCTIONS** **ITEM** **AIRCRAFT MAKE** **AIRCRAFT MODEL TYPE** **CERTIFICATE NUMBER BASIS FOR** **ALTERATION** **DRAWING INDEX NO.** **REVISION NO.** AND DATE [1] AFM **SUPPLEMENT** **NUMBER/DATE AML** **AMENDMENT DATE** Raytheon Aircraft Company C90, C90A C90GT E90 3A20 CAR 3 effective May 15, 1956, with Amendments 3-1, 3-2, 3-8, and additional requirements in TCDS 3A20 992-4435-001 Rev A, 09/15/05 05/24/06 [1] Or later FAA approved revision Page 18 of 21 FAA APPROVED MODEL LIST (AML) NO. SA01141WI-D **ROCKWELL COLLINS, INC.** FOR MODIFICATION OF A SINGLE OR DUAL COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH CTL-92 CONTROL HEAD TO A FLIGHT ID CAPABLE COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH COLLINS CTL-92E CONTROL HEAD IN PART 23 AIRCRAFT Issue Date: 02/24/03 **ORIGINAL** **CERTIFICATION** **INSTALLATION** **INSTRUCTIONS** **ITEM** **AIRCRAFT MAKE** **AIRCRAFT MODEL TYPE** **CERTIFICATE NUMBER BASIS FOR** **ALTERATION** **DRAWING INDEX NO.** **REVISION NO.** AND DATE [1] AFM **SUPPLEMENT** **NUMBER/DATE AML** **AMENDMENT DATE** Raytheon Aircraft Corporation 200 A200C (UC-12B) 200C, B200 B200C (C-12F) or (UC-12F) or (UC-12M) or (C-12R) A200 (C-12A) or (C-12C) 200T, 200CT A200CT (C-12D) or (FWC-12D) or (RC-12D) or (C-12F) or (RC-12G) or (RC-12H) B200T, B200CT A200CT (RC-12K) or (RC-12P) A24CE FAR Part 23, effective February 1, 1965, including Amendments 23-1 through 23-9, 23-11, and additional requirements in TCDS A24CE 992-4435-001 Rev A, 09/15/05 N/A 05/24/06 [1] Or later FAA approved revision Page 19 of 21 FAA APPROVED MODEL LIST (AML) NO. SA01141WI-D **ROCKWELL COLLINS, INC.** FOR MODIFICATION OF A SINGLE OR DUAL COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH CTL-92 CONTROL HEAD TO A FLIGHT ID CAPABLE COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH COLLINS CTL-92E CONTROL HEAD IN PART 23 AIRCRAFT Issue Date: 02/24/03 **ORIGINAL** **CERTIFICATION** **INSTALLATION** **INSTRUCTIONS** **ITEM** **AIRCRAFT MAKE** **AIRCRAFT MODEL TYPE** **CERTIFICATE NUMBER BASIS FOR** **ALTERATION** **DRAWING INDEX NO.** **REVISION NO.** AND DATE [1] AFM **SUPPLEMENT** **NUMBER/DATE AML** **AMENDMENT DATE** Raytheon Aircraft Corporation Raytheon Aircraft Corporation 300 300LW B300 (BE-350) B300C A24CE A24CE FAR Part 23, effective February 1, 1965, including Amendments 23-1 through 23-9, 23-11, and additional requirements in TCDS A24CE FAR Part 23 effective February 1, 1965, as amended by Amendments 23-1 through 23-34, and additional requirements in TCDS A24CE 992-4435-001 992-4435-001 Rev A, 09/15/05 Rev A, 09/15/05 N/A N/A 09/15/05 09/15/05 [1] Or later FAA approved revision **FAA APPROVED MODEL LIST (AML) NO. SA01141WI-D** **ROCKWELL COLLINS, INC.** FOR MODIFICATION OF A SINGLE OR DUAL COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH CTL-92 CONTROL HEAD TO A FLIGHT ID CAPABLE COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH COLLINS CTL-92E CONTROL HEAD IN PART 23 AIRCRAFT Issue Date: 02/24/03 **ORIGINAL** **CERTIFICATION** **INSTALLATION** **INSTRUCTIONS** **ITEM** **AIRCRAFT MAKE** **AIRCRAFT MODEL TYPE** **CERTIFICATE NUMBER BASIS FOR** **ALTERATION** **DRAWING INDEX NO.** **REVISION NO.** AND DATE [1] AFM **SUPPLEMENT** **NUMBER/DATE AML** **AMENDMENT DATE** Raytheon Aircraft Company 1900C (C-12J) 1900D A24CE FAR Part 23, effective February 1, 1965, including Amendments 23-1 through 23-9, 23-11, and additional requirements in TCDS A24CE 992-4435-001 Rev A, 09/15/05 09/15/05 [1] Or later FAA approved revision **FAA APPROVED MODEL LIST (AML) NO. SA01141WI-D ROCKWELL COLLINS, INC.** FOR MODIFICATION OF A SINGLE OR DUAL COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH CTL-92 CONTROL HEAD TO A FLIGHT ID CAPABLE COLLINS TDR-94 OR TDR-94D MODE S TRANSPONDER SYSTEM INSTALLATION WITH COLLINS CTL-92E CONTROL HEAD IN PART 23 AIRCRAFT Issue Date: 02/24/03 **INSTALLATION** **INSTRUCTIONS** **ORIGINAL CERTIFICATION** TYPE BASIS AFM AML AIRCRAFT AIRCRAFT CERTIFICATE FOR DRAWING REVISION NO. SUPPLEMENT AMENDMENT ITEM MAKE MODEL NUMBER ALTERATION INDEX NO. AND DATE!" NUMBER/DATE DATE 27 Twin 680 2A4 CAR 3 effective 992-4435-001 Rev A, 09/15/05 N/A 09/15/05 Commander November 1, 1949, Aircraft through Corporation Amendment 3-12, and additional requirements in TCDS 2A4 28 Twin 690A 2A4 CAR 3 dated May 992-4435-001 Rev A, 09/15/05 N/A 09/15/05 Commander 690C 15, 1956, including Aircraft 695 Amendments 3-3, Corporation 695A 3-4, 3-6, and 690D additional 695B requirements in TCDS 2A4 [1] Or later FAA approved revision FAA Approved: Administrator, DAS-500864-CE Amended: May 14, 2003, September 15, 2005, May 24, 2006 Page 21 of 21 ### SA01141WI-D.pdf This is OCR from the scanned FAA attachment. OCR can misread letters and numbers. United States of America Department of Transportation - Federal Abiation Administration Supplemental Type Certificate Number SA01141W1-D This certificate, isued to Rockwell Collins, Inc. 400 Collins Road NE, MS 164-100 Cedar Rapids, IA 52498 cerlifies that the change in the lype design for the following product with the limitations and conditions therefor us specified hereon meets the airworthiness requirements of Part "of the " Reqululions. Criginal Product Type Certificate Number : * *See attached FAA Approved Model List (AML) Make : * No. SA01141 WI-D for list of approved airplane models Model : * and applicable airworthiness regulations. Descriplion of Type Design Change: Modification of a single or dual Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92 control head to a Flight ID capable Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92E control head in accordance with Collins Installation Instructions as listed on AML No. SA01141 WI-D, Revision -, or later FAA approved revision. Limitations and Conditions: (1) This STC is not applicable to existing installations utilizing a TDR-90 Mode C transponder. (2) Approval of this change in type design applies to the above model aircraft only. (3) Compatibility of this design change with previously approved modifications must be determined by the installer. (4) A copy of this Certificate and FAA Approved Model List (AML) No. SA01141 WI-D issued February 24, 2003, or later FAA approved revision, must be maintained as part of the permanent records for the modified aircraft. (5) 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 This certificate and the supporting data which is the basis for approval shall remuin in effect until surrendered, suspended, revcked, or a termination date is otherwise established by the Administrater of the Federal Avialica Administration. Dule of upplication: August 21, 2002 Dule reissurel: Dule of istance: February 24, 2003 Date unended : FEDERAL AVIATION John 8. Botan By direction of the Administrator (Signature) TOMINSTRATOR Joken S. Bohn Administrator, DAS-500864-CE (Title) Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both. FAA FORM 8110-2 (10-68) PAGE 1 This certificate may be transferred in accordance with FAR 21.47. ## Every issue (3) - May 24, 2006: Amended, Current. [certificate](https://openairdocs.org/files/sha256/40/91/4091c7c4e0be8a651be52d1258388207e68754fc1e5a5fd9dfcdc2870d52850f), [SA01141WI-D.pdf](https://openairdocs.org/files/sha256/48/e4/48e4da9f01ec2ede8620579a68f21c2850575450bab38f3e9d4224bdecb8f4c9) - September 15, 2005: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/48/e4/48e4da9f01ec2ede8620579a68f21c2850575450bab38f3e9d4224bdecb8f4c9), [SA01141WI-D.pdf](https://openairdocs.org/files/sha256/40/91/4091c7c4e0be8a651be52d1258388207e68754fc1e5a5fd9dfcdc2870d52850f) - May 14, 2003: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/48/e4/48e4da9f01ec2ede8620579a68f21c2850575450bab38f3e9d4224bdecb8f4c9) --- 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.