Piper Arrow PA 28 RT-201T (Turbo) - Checkout Sheet
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1 Piper Arrow PA 28 RT-201T (Turbo) - Checkout Sheet Name Date CFI 1. List the following speeds: VX (gear up, flaps up) Best Angle of Climb Speed (gear down, flaps up) VY (gear up, flaps up) Best Rate of Climb Speed (gear down, flaps up) VS0 Stall speed (dirty) VS1 Stall speed (clean) VA (at 2900 lbs) Maneuvering Speed no full abrupt control movements above this speed (at 1893 lbs) VNE Never Exceed Speed do not exceed this speed in any configuration VNO Maximum Structural Cruising Speed do not exceed this speed except in smooth air, and only with caution VFE Maximum Flaps Extended Speed do not exceed this speed with flaps extended VLE Maximum Landing Gear Extended Speed do not exceed this speed with the landing gear extended What is the Maximum Landing Gear Extension Speed? This speed should not be exceeded when extending the landing gear. What is the Maximum Landing Gear Retraction Speed? This speed should not be exceeded when retracting the landing gear. What is the Turbulent Air Operating Speed? What is the Maximum Demonstrated Crosswind Velocity? 2. Maximum Weights Maximum Takeoff Weight Maximum Landing Weight
2 Maximum Ramp Weight 3. Weight and Balance Problem Determine if the aircraft is within weight and CG limits. Calculate this by using the aircraft POH. Weight Arm Moment Basic Empty Weight ,918 Pilot & Front Passenger ,590 Rear Passenger ,620 Fuel (50 6lb/gal) ,500 Baggage ,280 Totals What is the aircraft gross weight? What is the aircraft CG? Is the aircraft within limitations? 4. Determine the takeoff distance over a 50-ft obstacle and the liftoff speed with the given information: PA 6,095 ft MSL, OAT = 23⁰C, Gross weight = 2,700 b, Headwind = 5 kts. (Use page 5-13, Figure 5-5 in aircraft POH) 5. Determine the fuel burn and distance to climb with the following given information: Maximum gross weight, gear retracted, climb knots, no wind, takeoff PA = 3,795 ft MSL and OAT = 25⁰C, Cruise PA = 8,450 ft MSL and OAT = 6⁰C. (Use page 5-19, Figure 5-17 in aircraft POH) 6. Determine the landing distance and approach airspeed over a 50-ft obstacle with the following given information: Destination PA = 525 ft MSL and OAT = 18⁰C, Landing weight = 2,580 lbs, no wind. (Use page 5-30, Figure 5-35 in aircraft POH) 7. Fuel and Oil What is the fuel capacity for this aircraft? Total: gal. Total Useable: gal. What is the minimum octane fuel this aircraft can use? What is the engine oil capacity?
3 8. Performance What is the Engine Model Number? _ Maximum rated Horsepower? Maximum Rotation Speed (RPM)? What is the maximum takeoff weight? What is the normal main oleo strut extension? What is the maximum magneto drop? The maximum magneto difference? You should avoid continuous engine operation between and RPM and below. Why should prolonged idling at low RPM be avoided? What is the Service Ceiling for this aircraft? 9. Emergency Procedures & Failures 1. List the emergency procedure for Engine Fire During Start: 2. List the emergency procedure for Engine Fire In Flight: 3. List the emergency procedure for Engine Fire In Flight (During Cruise): 4. List the emergency procedure for Emergency Approach to Landing:
4 5. What are the prop over-speed procedures? 6. What are the (5) steps to spin recovery? 7. In the power off emergency landing pattern, downwind altitude is how many feet? 8. At best glide speed, a wind-milling engine, prop full decrease, the aircraft will travel miles for each 1,000 feet of altitude loss. 9. How is an alternator failure detected? 10. What are the corrective steps for an alternator failure? 10. General Questions 1. Which documents must be carried aboard the aircraft?
5 2. What documents must you carry with you? 3. What are the (3) most probable causes for engine roughness? 4. How is the engine primed? 5. What is the maximum starter cranking and resting periods? 6. The gear unsafe horn will activate if the throttle is reduced below. 7. What is the gear up rate of climb at 2,750 lbs, 15⁰C, at sea level? fpm. 8. What is the flaps up takeoff distance at 2,750 lbs, 20⁰C, at sea level, lift off is at 71 kts, with wind? _ feet 9. At 75% power, GPH is approximately. 10. If the OAT is 10⁰C, PA is 3,000 ft, TAS is. 11. Who is responsible for determining that the aircraft is airworthy before flight? Completed Date CFI Chief Flight Instructor CFI Remarks
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