STC SA4405SW

United £tatu of amtrica Bepartment of transportation—federal aoiation administration Supplemental t^pe Certificate SA4405SW S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 nx.<^^/t<!^z4il«jp«y^,<^^^ Civil Air 3A15 Beech F33A, A36, A36TC Installation of S-TEC System 60 Pitch Stabilization System, Model ST-053 with Optional Autotrlm System according to Bulletin No. 156, Revision 2, dated 11-11-81 and Master Drawing List No. 9249, Revision B, dated 11-11-81, or later FAA approved revision.

866 Continuation Sheet, P&g6 2, Of thlS ?TC w .tyiMt/ MflV 5 1981 June 30, 1981 10/23/81; 2/3/82 Revision 2 Don P. Watson (Slgnalure) Acting Chief, Aircraft Certification —Division———————————————————(Title)

( FAA FOKM 8110-2 (10-68)

tinted $tattt of Bepartmcnt of transportation— ,fE(Jeral aviation administration ^upplemental l^pe Certificate(Continuation &heet) SA4405SW Revision 2 Limitations and Conditions:

1. Pilot's Operating Handbook and FAA< Approved Airplane Flight Manual Supplement P/N 8951 dated June 30, 1981, is required for Beech Models A36 and F33A with S-TEC System 60 Pitch Stabilization System, Model ST-053 without optional autotrlm system.

OR Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement P/N 8951-1 dated October 23, 1981, is required for Beech Models A36 and F33A with S-TEC System 60 Pitch Stabilization System, Model ST-053 with or without optional autotrlm system.

OR Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement P/N 8951-2 dated February 3, 1982, is required for Beech Models F33A, A36, and A36TC with S-TEC System 60 Pitch Stabilization System, Model ST-053 with or without optional autotrlm system.

2. Compatibility of this modification with other previously approved modifications must be determined by the installer.

FAA FORM 8110-2-1 (1O-69) PAGE 2 OF 2 PAGES