STC SA1641SW

SA1641SW Mitsubishi Heavy Industries America, Inc.

17304 Preston Road, Suite 1270 Dallas, TX 75252 Part 10 the Civil Air Regulations A2PC Mitsubishi MU-2B-35, MU-2B-36 Installation of Sperry SPZ-200 Autopilot and STARS IVC Flight Director System according to MAI Engineering Design Summary 935A-0036, Revision G dated 6/17/76, or later FAA approved revision.

(See continuation sheet 3 of 3) January 5, 1973 March 31, 1986; August 17, 1999; January 19, 2001;

December 10, 2009; June 15, 2020; January 19, 2022 April 16, 1973 April 18, 1974; June 13, 1974; June 19, 1974; June 17, 1976 Rev. 4 S. Frances Cox Acting Manager, Fort Worth ACO Branch, Compliance & Airworthiness Division Aircraft Certification Service 3

SA1641SW 3

SA1641SW Date of Issuance: April 16, 1973 Date Amended: June 17, 1976 Date of Reissuance: January 19, 2022

Approval is limited to autopilot and flight director system and their interface with the basic aircraft.

FAA Approved Airplane Flight Manual Supplement dated April 16, 1973, is required for Sperry SPZ-200/STARS IVC Automatic Flight Control System; or Supplement dated August 29, 1973, for Sperry SPZ-200/STARS IVC Automatic Flight Control System with Automatic Rudder Trim System for Model MU-2B-35. Supplement dated March 29, 1976, is required for Sperry SPZ-200/STARS IVC Automatic Flight Control System with Automatic Rudder Trim System for Model MU-2B-36.

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

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