Beechcraft T-34B Mentor — T-34Btest NOT FOR FLIGHT — source fidelity: unreviewed | operational review: none | completeness: full Source: Beechcraft/T-34B Mentor/T-34Btest.txt Rights: licensed Checklist hash: 21a2c41db469b915328fcfc83cca5945c9384cb313a8d0b30cca75db8a5d9e2e Verify against the aircraft's own approved documentation before use. ======================================================================== BEECHCRAFT T-34B MENTOR — T-34BTEST ----------------------------------- ** NOTE: NAME : Date: ** NOTE: 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: