STC SA01141WI-D

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