STC SH1415SO

IMPORT SH1415SO Magellan Aerospace 660 Berry Street Winnipeg, MB Canada R3C 2S4 Part 29 Title 14 Code of Federal Regulations H4SW Bell Textron Inc.

412, 412CF, 412EP Configuration #1 - Installation P/N 364-83300-5 (Standard Skid Gear) or P/N 364-83300-7 (High Skid Gear)

1. Installation of a Wire Strike Protection System must be in accordance with Bristol Aerospace Limited Drawing List EM105301, Issue F, Transport Canada Civil Aviation (TCCA) approved June 30, 2011, or later TCCA approved revision.

1. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

(See continuation sheet 3) July 28, 1980 April 21, 1995, June 14, 2001, January 25, 2024 February 24, 1983 September 29, 1994, March 7, 1995, March 25, 2002, March 27, 2024 Anthony E. Gallo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 3

IMPORT SH1415SO SH1415SO 3

IMPORT SH1415SO Date Amended: March 27, 2024 Date Reissued: January 25, 2024

Description of Type Design Change (continued):

Configuration #1 (continued)

2. Maintenance must be in accordance with Bristol Aerospace Limited Maintenance Manual Supplement PM-965-041, Issue C, dated April 17, 2007, or later TCCA accepted revision.

Configuration #2 - Installation P/N 364-83100-19

1. Installation of a Wire Strike Protection System must be in accordance with Bristol Aerospace Limited Drawing List EM104802, Issue A, TCCA approved September 14, 1999, or later TCCA approved revision.

2. Maintenance must be in accordance Bristol Aerospace Limited Installation Instructions document ER82737, Issue H, dated December 6, 1995, or later TCCA accepted revision.

2. The installer must determine whether this design change is compatible with previously approved modifications.

3. This STC is applicable to all serial numbers for this Make and Models.

----------END---------- 3 3