STC SA3366NM

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

(See Continuation Sheet Page 3 of 3 Pages) Page 1 of 3 SA3366NM Raisbeck Engineering Inc.

2811 South 102nd Street, Suite 100 Tukwila, WA 98168 Part 23 the Federal Aviation Regulations A24CE Beechcraft 200, 200C, 200CT, 200T, A200 (C-12A), A200 (C-12C), A200C (UC-12B), A200CT (C-12D), A200CT (FWC 12D), A200CT (C 12F), A200CT (RC 12D), A200CT (RC-12G), A200CT (RC 12H), A200CT (RC-12K), A200CT (RC 12P), A200CT (RC-12Q) B200, B200C, B200CT, B200T, B200CGT, B200C (C 12F), B200C (UC 12M), B200C (C 12R), B200C (UC 12F), B200GT Installation of the Ram Air Recovery System in accordance with Raisbeck Engineering Drawing List R81-1001, Revision K, dated February 1, 2008, or later Federal Aviation Administration approved revision.

March 11, 1986 March 31, 2014; September 1, 2023 April 30, 1986 November 21, 1997; November 23, 1999;

February 1, 2008 for Manager, West Certification Branch Approval of this change in type design applied to the above model aircraft only. This approval should not be extended to other aircraft of this model on which other previously approved modifications have been incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this certificate must be maintained as part of the permanent record of the modified aircraft.

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

Page 2 of 3 SA3366NM

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number:

End Page 3 of 3 Limitations and Conditions continued:

SA3366NM Additionally, if the airplane is modified in accordance with STC SA2698NM-S (Quiet Turbofan Propellers) a copy of the Airplane Flight Manual Supplement 99-117, Revision A, dated February 1, 2008, or later FAA Approved revision, shall be maintained as part of the permanent records for the modified aircraft.

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.