Beechcraft T-34B Mentor

Beechcraft T-34B Mentor — T-34Btest NAME : Date: CFI: Grade: Engine model number is HP Max RPM Engine Oil Capacity is Minimum Fuel Octane is Maximum Takeoff Weight is Required Onboard Documents are Main Strut Extension is Maximum Mag. Drop is Best Rate of Climb Airspeed is VNE is Maximum Gear Extension Speed is? Clean Stall Speed is Maximum Gear Retraction Speed is Minimum Oil Pressure is Total Usable Fuel is Maximum Demonstrated Crosswind is Avoid Continuous Engine RPM Operation Between Engine Restart Procedures are Power off Emergency Glide Speed is Prop overspeed procedures are Spin Recovery Procedure is In the Emergency Landing Pattern downwind altitude is At best glide speed, windmilling engine, the T-34 will travel ______ miles for each 1000 feet of altitude. The basic steps in an engine failure situation are (list 5): 1. 2. 3. 4. 5. The first step in an engine fire emergency is How is an alternator failure detected? What are alternator failure corrective steps Most probable causes for engine roughness are How do you prime the engine? Maximum starter cranking period is Recommend final approach airspeed with flaps full is The landing gear horn will operate if the throttle is reduced below What is the average rate of climb at sea level, 75 deg F, 2985 Lbs? What is the Takeoff Distance, 2985 lbs, 50 deg F, sea level? At max range power setting of 19”/1900 RPM, 5000 ft, max gross wt, what is CAS and fuel flow? ________________ and . Determine if the aircraft is within weight and CG limits. Given: Item Weight Arm Moment BEW 2236.8 85.6 191470.6 P/P 180.0 87.0 Rear Pax 180.0 138.0 Fuel (50 gal x 6) 300.0 80.0 Oil 22.5 46.0 Aircraft within weight and CG limits. Determine the takeoff distance over a 50’ obstacle and liftoff airspeed. Given: Air Temp: 50 deg F Pressure Alt: sea level Weight: 2975 lbs Headwinds: 0 kts Takeoff distance: Liftoff airpseed: What is the specific range (nm/lb fuel) at 5000 ft, 2775 lbs., TAS 125? Specific range: Determine landing distance and approach airspeed over a 50’ obstacle. Given: Landing Wt. 2975 Lbs. Flaps: 100 % Dn. Pressure Alt: Sea Level Headwinds: Zero Landing distance: Approach airspeed: