PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR BEECHCRAFT BARON 58, 58A, G58

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SAMPLE D’Shannon Products, LTD Document No: P/N-58-Supp-1 1309 County Road 134 Beechcraft Baron 58, 58A, G58 Buffalo, MN 55313 Revision A Date: __________________ Page 1 of 5 PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT FOR BEECHCRAFT BARON 58, 58A, G58 REG. NO. ______________________ SER. NO. ______________________ This supplement must be attached to the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual when a V/G SYSTEM is installed in accordance with STC(s) SA4016NM. The information contained herein supplements or supersedes the basic handbook only in those areas listed herein. For limitations, procedures, and performance information not contained in this supplement, consult the basic Pilot's Operating Handbook and FAA Approved Airplane Flight Manual. SAMPLE D’Shannon Products, LTD Document No: P/N-58-Supp-1 1309 County Road 134 Beechcraft Baron 58, 58A, G58 Buffalo, MN 55313 Revision A Date: __________________ Page 2 of 5 LOG OF REVISIONS Revision Description FAA Approved IR Original Issue 03-15-88 A Added G58 model Baron; Modernized Document SAMPLE D’Shannon Products, LTD Document No: P/N-58-Supp-1 1309 County Road 134 Beechcraft Baron 58, 58A, G58 Buffalo, MN 55313 Revision A Date: __________________ Page 3 of 5 LOG OF PAGES Page No. Revision No. Date 1 A 8/19/2014 2 A 8/19/2014 3 A 8/19/2014 4 A 8/19/2014 5 A 8/19/2014 SAMPLE D’Shannon Products, LTD Document No: P/N-58-Supp-1 1309 County Road 134 Beechcraft Baron 58, 58A, G58 Buffalo, MN 55313 Revision A Date: __________________ Page 4 of 5 GENERAL The V/G System Consists of 107 vortex generators affixed to the wings and vertical stabilizer. The purpose of the V/G system is to reduce stall and Vmca speeds through control of boundary layer airflow Although the V/G System reduces stall and Vmca speeds, the pilot is encouraged to fly by reference to the performance specifications in the original Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual to provide an increased margin of safety. LIMITATIONS 1. 103 vortex generators constitute the minimum requirement. If less than 107 vortex generators are in place, the aircraft must be operated in accordance with the original Pilot’s Operating Handbook and FAA Approved Airplane Flight Manual. 2. Change all references to Vmca values in and on placards to: 74 KCAS 3. AIRSPEED INDICATOR MARKINGS: KCAS WHITE ARC 68-122 RED RADIAL 74 BLUE RADIAL 100 GREEN ARC 74-195 YELLOW ARC 195-223 RED RADIAL 223 WHITE TRIANGLE 152 EMERGENCY PROCEDURES: EMERGENCY AIRSPEEDS: AIR MINIMUM CONTROL SPEED (Vmca) 74 KIAS NORMAL PROCEDURES AIRSPEEDS FOR SAFE OPERATION: AIR MIINIMUM CONTROL SPEED (Vmca) 74 KIAS PERFORMANCE SEE FOLLOWING PERFORMANCE CHART SAMPLE D’Shannon Products, LTD Document No: P/N-58-Supp-1 1309 County Road 134 Beechcraft Baron 58, 58A, G58 Buffalo, MN 55313 Revision A Date: __________________ Page 5 of 5 STALL SPEEDS – ZERO THRUST Weight in Pounds Angle of Bank in Degrees Stall Speed in Knots CAS Note 1. THE MAXIMUM ALTITUDE LOSS EXPERIENCED WHILE CONDUCTING STALLS IN ACCORDANCE WITH CAR 3120 WAS 400 FEET 2. A NORMAL STALL RECOVERY TECHNIQUE MAY BE USED 3. POWER IDLE CONDITIONS WILL INCREASE THE ZERO THRUST STALL SPEEDS BY APPROXIMATELY ONE KNOT AT FLAPS DOWN AND TWO KNOTS AT FLAPS UP FLAPS UP FLAPS DOWN