# STC SA01306WI-D - Type: Supplemental type certificate - Status: Current, Amended - Holder: Rockwell Collins Inc, United States - Description: Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation. - Applied: December 17, 2004 - Status date: February 28, 2007 - Product: Aircraft, Single-Engine - Certification basis: Part 21 - Data sheets: [TCDS A7PC](https://openairdocs.org/tcds/A7PC), [TCDS A17EU](https://openairdocs.org/tcds/A17EU), [TCDS A9EA](https://openairdocs.org/tcds/A9EA), [TCDS A21EU](https://openairdocs.org/tcds/A21EU), [TCDS A56EU](https://openairdocs.org/tcds/A56EU), [TCDS A1WI](https://openairdocs.org/tcds/A1WI), [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 A10SW](https://openairdocs.org/tcds/A10SW), [TCDS A2PC](https://openairdocs.org/tcds/A2PC), [TCDS A59EU](https://openairdocs.org/tcds/A59EU), [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) and 5 more - Certificate PDF: https://openairdocs.org/files/sha256/ec/13/ec13ea6ad5a46aad174f148c21d441dbdaf44f3f1b249e723fa474e7f9ddca79 - Approved model list and other attachments: [SA01306WI-D_AML.pdf](https://openairdocs.org/files/sha256/5d/6d/5d6db7b9cca6d73a32c61d81706b5b52b536e2a0e2e02b7ba0589b906d1f4f77) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0B197BF4CD49A76E862572D700616CCB.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA01306WI-D ## ADs that name it (0) None. ## Approved models (105, 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)) - Cessna Aircraft Company 425 ([TCDS A7CE](https://openairdocs.org/tcds/A7CE)) - Cessna Aircraft Company 441 ([TCDS A28CE](https://openairdocs.org/tcds/A28CE)) - Cessna Aircraft Company 525 ([TCDS A1WI](https://openairdocs.org/tcds/A1WI)) - 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)) - M7 Aerospace LP SA226-TC ([TCDS A8SW](https://openairdocs.org/tcds/A8SW)) - M7 Aerospace LP SA227-AC (C-26A) ([TCDS A8SW](https://openairdocs.org/tcds/A8SW)) - M7 Aerospace LP SA227-AT ([TCDS A5SW](https://openairdocs.org/tcds/A5SW)) - M7 Aerospace LP SA227-BC (C-26A) ([TCDS A8SW](https://openairdocs.org/tcds/A8SW)) - M7 Aerospace LP SA227-CC ([TCDS A18SW](https://openairdocs.org/tcds/A18SW)) - M7 Aerospace LP SA227-DC (C-26B) ([TCDS A18SW](https://openairdocs.org/tcds/A18SW)) - M7 Aerospace LP SA227-PC ([TCDS A8SW](https://openairdocs.org/tcds/A8SW)) - M7 Aerospace LP SA227-TT ([TCDS A5SW](https://openairdocs.org/tcds/A5SW)) - Mitsubishi Heavy Industries Ltd. MU-2B-25 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW)) - Mitsubishi Heavy Industries Ltd. MU-2B-25 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC)) - Mitsubishi Heavy Industries Ltd. MU-2B-26 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW)) - Mitsubishi Heavy Industries Ltd. MU-2B-26 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC)) - 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-35 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC)) - Mitsubishi Heavy Industries Ltd. MU-2B-36 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW)) - Mitsubishi Heavy Industries Ltd. MU-2B-36 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC)) All 105: https://openairdocs.org/stc/SA01306WI-D/models.md ## What the certificate says This is OCR from the scanned FAA certificate. OCR can misread letters and numbers. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA01306WI-D This certificate issued to: Rockwell Collins, Inc. 400 Collins Road NE, MS 164-100 Cedar Rapids, IA 52498 Purt "of the " Porqulations. Original Product - Type Cerlificate Number : * *See attached FAA Approved Model List (AML) Make: No. SA01306WI-D for list of approved airplane models Model: and applicable airworthiness regulations. Description of Type Design Change: Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. SA01306WI-D, Revision -, or later FAA approved revision. Limitations and Conditions: (1) Prior FAA approved installation of a Collins ALT-50A part numbers 622-3201-001/-002/-011 or ALT-55B part numbers 622-2855-001/-002/-011/-012 is a prerequisite to this STC. (2) For aircraft installations utilizing two radio altimeters, both radio altimeters must be replaced; Intermixing of new radio altimeters with legacy radio altimeters is not approved. (3) Approval of this change in type design applies to the above model aircraft only. (4) Compatibility of this design change with previously approved modifications must be determined by the installer. (5) A copy of this Certificate and FAA Approved Model List (AML) No. SA01306WI-D issued February 7, 2005, or later FAA approved revision, must be maintained as part of the permanent records for the modified aircraft. (6) 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. Date of Application: December 17, 2004 Date Reissued: Date of Issuance: February 7, 2005 Date Amended: FEDERAL AVIATION By Direction of the Administrator in Gale 8. Bohn (Signature) TOMNISTRATO Administrator, DAS-500864-CE (Title) ### SA01306WI-D_AML.pdf This is OCR from the scanned FAA attachment. OCR can misread letters and numbers. **FAA APPROVED MODEL LIST (AML) NO. SA01306WI-D ROCKWELL COLLINS, INC.** FOR MODIFICATION OF COLLINS ALT-50A OR ALT-55B RADIO ALTIMETER SYSTEM INSTALLATION TO A COLLINS ALT-1000 OR ALT-4000 RADIO ALTIMETER SYSTEM INSTALLATION IN PART 23 AIRCRAFT Issue Date: February 7, 2005 **ORIGINAL CERTIFICATION INSTALLATION** TYPE BASIS INSTRUCTIONS AFM AML AIRCRAFT AIRCRAFT CERTIFICATE FOR DRAWING REVISION NO. SUPPLEMENT AMENDMENT ITEM MAKE MODEL NUMBER ALTERATION INDEX NO. AND DATE (1] NUMBER/DATE DATE Aerospace N22B A7PC TCDS A7PC RCA-0095-001 Rev A, 02/28/07 N/A 02/28/07 Technologies N22S Revision 4 of Australia March 31, 1989 PTY Ltd. 2 BN Group BN-2, BN-2A A17EU TCDS A17EU RCA-0095-001 Rev A, 02/28/07 N/A 02/28/07 Ltd. BN-2A-6 Revision 16 BN-2A-8 December 9, 2002 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 3 Bombardier (Twin Otter) AgEA TCDS A9EA RCA-0095-001 Rev A, 02/28/07 N/A 02/28/07 Inc. DHC-6-100 Revision 11 DHC-6-200 June 20, 2000 DHC-6-300 [1] Or later FAA approved revision Page 1 of 7 **FAA APPROVED MODEL LIST (AML) NO. SA01306WI-D ROCKWELL COLLINS, INC.** MODIFICATION OF COLLINS ALT-50A OR ALT-55B RADIO ALTIMETER SYSTEM INSTALLATION TO A COLLINS ALT-1000 OR ALT-4000 RADIO ALTIMETER SYSTEM INSTALLATION IN PART 23 AIRCRAFT Issue Date: February 7, 2005 **ORIGINAL CERTIFICATION INSTALLATION** TYPE BASIS INSTRUCTIONS AFM AML AIRCRAFT AIRCRAFT CERTIFICATE FOR DRAWING REVISION NO. SUPPLEMENT AMENDMENT ITEM MAKE MODEL NUMBER ALTERATION INDEX NO. AND DATE !! NUMBER/DATE DATE British Jetstream A21EU TCDS A21EU RCA-0095-001 Rev A, 02/28/07 N/A 02/28/07 Aerospace Series 3101 Revision 16 Regional October 6, 2003 Aircraft 5 British (Jetstream A56EU TCDS A56EU 02/28/07 Aerospace Aircraft Limited) Revision 5 Regional Jetstream October 6, 2003 Aircraft Model 3201 6 Cessna 425 A7CE TCDS A7CE RCA-0095-001 Rev A, 02/28/07 NA 02/28/07 Aircraft Revision 45 Company July 12, 2002 7 Cessna 441 A28CE TCDS A28CE RCA-0095-001 Rev A, 02/28/07 02/28/07 Aircraft Revision 12 Company September 22, 2003 8 Cessna 525 A1WI TCDS A1WI RCA-0095-001 Rev A, 02/28/07 NA 02/28/07 Aircraft Revision 13 Company December 10, 2004 [1] Or later FAA approved revision Page 2 of 7 **FAA APPROVED MODEL LIST (AML) NO. SA01306WI-D ROCKWELL COLLINS, INC.** FOR MODIFICATION OF COLLINS ALT-50A OR ALT-55B RADIO ALTIMETER SYSTEM INSTALLATION TO A COLLINS ALT-1000 OR ALT-4000 RADIO ALTIMETER SYSTEM INSTALLATION IN PART 23 AIRCRAFT Issue Date: February 7, 2005 **ORIGINAL CERTIFICATION INSTALLATION** TYPE BASIS INSTRUCTIONS AFM AML AIRCRAFT AIRCRAFT CERTIFICATE FOR DRAWING REVISION NO. SUPPLEMENT AMENDMENT ITEM MAKE MODEL NUMBER ALTERATION INDEX NO. AND DATE (1) NUMBER/DATE DATE 9 Dornier Dornier 228-100 A16EU TCDS A16EU RCA-0095-001 Rev A, 02/28/07 N/A 02/28/07 Luftfahrt Dornier 228-101 Revision 8 GMBH Dornier 228-200 October 23, 1990 Dornier 228-201 Dornier 228-202 Dornier 228-212 10 Piaggio P-180 A59EU TCDS A59EU RCA-0095-001 Rev A, 02/28/07 NIA 02/28/07 Aero Revision 10 Industries May 14, 2003 S.P.A. 11 M7 (Fairchild A5SW TCDS A5SW RCA-0095-001 Rev A, 02/28/07 NA 02/28/07 Aerospace Aircraft Revision 26 LP Incorporated) August 24, 2004 SA227-AT SA227-TT 12 M7 (Fairchild A8SW TCDS A8SW RCA-0095-001 Rev A, 02/28/07 N/A 02/28/07 Aerospace Aircraft Revision 22 LP Incorporated) August 24, 2004 SA226-TC SA227-AC SA227-PC SA227-BC (C-26A) [1] Or later FAA approved revision Page 3 of 7 **FAA APPROVED MODEL LIST (AML) NO. SA01306WI-D ROCKWELL COLLINS, INC.** FOR MODIFICATION OF COLLINS ALT-50A OR ALT-55B RADIO ALTIMETER SYSTEM INSTALLATION TO A COLLINS ALT-1000 OR ALT-4000 RADIO ALTIMETER SYSTEM INSTALLATION IN PART 23 AIRCRAFT Issue Date: February 7, 2005 **ORIGINAL CERTIFICATION INSTALLATION** TYPE BASIS INSTRUCTIONS AFM AML AIRCRAFT AIRCRAFT CERTIFICATE FOR DRAWING REVISION NO. SUPPLEMENT AMENDMENT ITEM MAKE MODEL NUMBER ALTERATION INDEX NO. AND DATE "] NUMBER/DATE DATE 13 M7 (Fairchild Aircraft A18SW TCDS A18SW RCA-0095-001 Rev A, 02/28/07 N/A 02/28/07 Aerospace Incorporated) Revision 4 LP SA227-CC August 24, 2004 SA227-DC (C-26B) 14 Mitsubishi MU-2B-25 A2PC TCDS A2PC RCA-0095-001 Rev A, 02/28/07 NIA 02/28/07 Heavy MU-2B-26 Revision 16 Industries MU-2B-35 June 30, 1975 Ltd. MU-2B-36 15 Mitsubishi MU-2B-25 A10SW TCDS A10SW RCA-0095-001 Rev A, 02/28/07 NA 02/28/07 Heavy MU-2B-26 Revision 14 Industries MU-2B-35 August 25, 2003 Ltd. MU-2B-36 MU-2B-26A MU-2B-36A MU-2B-40 MU-2B-60 16 Pilatus PC-7 A50EU TCDS A5OEU RCA-0095-001 Rev A, 02/28/07 NIA 02/28/07 Aircraft Ltd. Revision 2 July 1, 1996 [1] Or later FAA approved revision Page 4 of 7 **FAA APPROVED MODEL LIST (AML) NO. SA01306WI-D ROCKWELL COLLINS, INC.** FOR MODIFICATION OF COLLINS ALT-50A OR ALT-55B RADIO ALTIMETER SYSTEM INSTALLATION TO A COLLINS ALT-1000 OR ALT-4000 RADIO ALTIMETER SYSTEM INSTALLATION IN PART 23 AIRCRAFT Issue Date: February 7, 2005 **ORIGINAL CERTIFICATION INSTALLATION** TYPE BASIS INSTRUCTIONS AFM AML AIRCRAFT AIRCRAFT CERTIFICATE FOR DRAWING REVISION NO. SUPPLEMENT AMENDMENT ITEM MAKE MODEL NUMBER ALTERATION INDEX NO. AND DATE! NUMBER/DATE DATE 17 The New PA-23 1A10 TCDS 1A10 RCA-0095-001 Rev A, 02/28/07 N/A 02/28/07 Piper Revision 50 Aircraft, Inc. September 10, 2003 18 The New PA-31T2 ASEA TCDS A8EA RCA-0095-001 Rev A, 02/28/07 N/A 02/28/07 Piper Revision 22 Aircraft, Inc. February 25, 2004 19 The New PA-42 A23SO TCDS A23SO RCA-0095-001 Rev A, 02/28/07 N/A 02/28/07 Piper PA-42-720 Revision 16 Aircraft, Inc. PA-42-1000 June 21, 2004 20 Raytheon C90 3A20 TCDS 3A20 RCA-0095-001 Rev A, 02/28/07 N/A 02/28/07 Aircraft C9OA Revision 62 Company C90GT December 7, 2005 E90 21 Raytheon B100 A14CE TCDS A14CE RCA-0095-001 Rev A, 02/28/07 NIA 02/28/07 Aircraft Revision 36 Company December 26, 2003 22 Raytheon (Beech) A23CE TCDS A23CE RCA-0095-001 Rev A, 02/28/07 N/A 02/28/07 Aircraft 58₽ Revision 14 Company 58PA April 15, 1996 58TC 58TCA [1] Or later FAA approved revision Page 5 of 7 **FAA APPROVED MODEL LIST (AML) NO. SA01306WI-D ROCKWELL COLLINS, INC.** FOR MODIFICATION OF COLLINS ALT-50A OR ALT-55B RADIO ALTIMETER SYSTEM INSTALLATION TO A COLLINS ALT-1000 OR ALT-4000 RADIO ALTIMETER SYSTEM INSTALLATION IN PART 23 AIRCRAFT Issue Date: February 7, 2005 **ORIGINAL CERTIFICATION INSTALLATION** TYPE BASIS INSTRUCTIONS AFM AML AIRCRAFT AIRCRAFT CERTIFICATE FOR DRAWING REVISION NO. SUPPLEMENT AMENDMENT ITEM MAKE MODEL NUMBER ALTERATION INDEX NO. AND DATE !!! NUMBER/DATE DATE 23 Raytheon 200 A24CE TCDS A24CE RCA-0095-001 Rev A, 02/28/07 N/A 02/28/07 Aircraft A200C (UC-12B) Revision 88 Company 200C, B200 November 3, 2004 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) 300 300LW B300 B300C 1900C (C-12J) 1900D [1] Or later FAA approved revision Page 6 of 7 **FAA APPROVED MODEL LIST (AML) NO. SA01306WI-D ROCKWELL COLLINS, INC.** FOR MODIFICATION OF COLLINS ALT-50A OR ALT-55B RADIO ALTIMETER SYSTEM INSTALLATION TO A COLLINS ALT-1000 OR ALT-4000 RADIO ALTIMETER SYSTEM INSTALLATION IN PART 23 AIRCRAFT Issue Date: February 7, 2005 **ORIGINAL CERTIFICATION INSTALLATION** TYPE BASIS INSTRUCTIONS AFM AML AIRCRAFT AIRCRAFT CERTIFICATE FOR DRAWING REVISION NO. SUPPLEMENT AMENDMENT ITEM MAKE MODEL NUMBER ALTERATION INDEX NO. AND DATE! NUMBER/DATE DATE 24 Raytheon (Beech) A31CE TCDS A31CE RCA-0095-001 Rev A, 02/28/07 N/A 02/28/07 Aircraft F90 Revision 7 Company April 15, 1996 25 Twin 680 2A4 TCDS 2A4 RCA-0095-001 Rev A, 02/28/07 N/A 02/28/07 Commander 690A Revision 46 Aircraft 690C April 3, 2000 Corporation 690D 695 695A 695B [1] Or later FAA approved revision FAA Approved: Quen & Bota Aeministrator, DAS-500864-CE Amended: January 17, 2006, February 28, 2007 Page 7 of 7 ## Every issue (3) - February 28, 2007: Amended, Current. [certificate](https://openairdocs.org/files/sha256/ec/13/ec13ea6ad5a46aad174f148c21d441dbdaf44f3f1b249e723fa474e7f9ddca79), [SA01306WI-D_AML.pdf](https://openairdocs.org/files/sha256/5d/6d/5d6db7b9cca6d73a32c61d81706b5b52b536e2a0e2e02b7ba0589b906d1f4f77) - January 17, 2006: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/24/6a/246a04152b54909462adf1fec1ffa432b0bf588fa0cc6ef99292975f4c24b84f) - February 7, 2005: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/ec/13/ec13ea6ad5a46aad174f148c21d441dbdaf44f3f1b249e723fa474e7f9ddca79), [SA01306WI-D.pdf](https://openairdocs.org/files/sha256/ec/13/ec13ea6ad5a46aad174f148c21d441dbdaf44f3f1b249e723fa474e7f9ddca79) --- 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.