Va 90 106 105 100. Vne 146 164 155 162. Vno 145 115 130 139. Vfe 10° 130 90 140 164. Vlo 140 146 131 110. Vle 164 106 130 146. Vs 50 55 48 42. Vso 50 55 42 44. Vx 67 70 55 56. Vy 84 65 75 80. Vr 55 60 59 62. Vapp (Flap DN) 60-70 55-65 50-60 70-80. Vglide 105 73 59 69. Max Cross Wind 18 15 19 13. Tipo de combustible 100/130 97/100 130. Capacidad combustible total 66 62. Capacidad combustible usable 66 62. Presión de combustible Minima (PSI) 0.5 2.2 1.2 2.5. Presión de Combustible Máxima (PSI) Red Arc 8 7.2 6. Peso máximo TAKEOFF (LBS) 2650 2550 1650 1320. Maximum Baggage (LBS) 55 200 190 180. MCP Reason HP o BHP 180 160 140 200. Maximum RPM 2700 2650 5500 2900. Static RPM Maximum 2500 4700 2700 2100. Static RPM Minimum 2100 2400 1950 2000. Cilinder Head MAXIMUM Temperature (F°) 500 200. Cilinder Head MINIMUM Temperature (F°) 200 500 350 400. Oil MAXIMUM Temperature (°F) 245 100 246 112. Oil MINIMUM Temperature (°F) 100 102 130 98. OIL MAXIMUM Pressure (PSI) 115 102 112 116. Oil MINIMUM Pressure (PSI) 25 12 14 26. Spin 106 Prohibido 113 90. Steep Turns 90 106 105 115. Lazy Eights 106 90 105 Prohibido. Chandelles 90 106 Prohibido 115. Engine failure during takeoff run:
Throttle Full Idle. Engine failure during takeoff run:
Brakes Apply Brake. Engine failure during takeoff run:
Wing Flaps Retract 10°. Engine failure during takeoff run:
Mixture Full Rich Idle CUT-OFF. Engine failure during takeoff run:
Ignition Switch Start OFF. Engine failure during takeoff run:
Master Switch ON OFF. Engine failure immediately after takeoff:
Airspeed
70 KIAS (FLAPS UP) 65 KIAS (FLAPS DN) 65 KIAS (FLAPS UP) 60 KIAS (FLAPS DN). Engine failure immediately after takeoff:
MIXTURE FULL RICH IDLE CUTOFF. Engine failure immediately after takeoff:
FUEL SELECTOR VALVE BOTH OFF. Engine failure immediately after takeoff:
IGNITION SWITCH START OFF. Engine failure immediately after takeoff:
WINGS FLAP RETRACT AS REQUIERED. Engine failure during flight:
AIRSPEED 75 79. Engine failure during flight:
CARBURATOR HEAT ON OFF . Engine failure during flight:
FUEL SELECTOR VALVE BOTH CHECK TANK. Engine failure during flight:
MIXTURE FULL RICH IDLE CUTOFF. Engine failure during flight:
IGNITION SWITCH BOTH (OR START IF PROPELLER IS STOPED) START (OR BOTH IF PROPELLER IS STOPED). Engine failure during flight:
PRIMER IN AND LOCKED AS NEEDED. FIRE DURING START ON GROUND:
CRANKING CONTINUE STOP. IF ENGINE STARTS:
POWER
1700 RPM FOR A FEW MINUTES 2100 RPM FOR A FEW MOMENTS. IF ENGINE STARTS:
ENGINE SHUTDOWN AND INSPECT FOR DAMAGE USE EXTINGUISHER. IF ENGINE FAILS TO START:
THROTTLE FULL OPEN IDLE CUTOFF. IF ENGINE FAILS TO START:
MIXTURE FULL RICH IDLE CUTOFF. IF ENGINE FAILS TO START:
CRANKING STOP CONTINUE. IF ENGINE FAILS TO START:
EXTINGUISHER OBTAIN USE. IF ENGINE FAILS TO START:
ENGINE SECURE RESTART. IF ENGINE FAILS TO START:
MASTER SWITCH OFF ON. IF ENGINE FAILS TO START:
IGNITION SWITCH OFF ON. IF ENGINE FAILS TO START:
FUEL SELECTOR VALVE OFF BOTH. IF ENGINE FAILS TO START:
FIRE EXTINGUISH EVACUATE. IF ENGINE FAILS TO START:
FIRE DAMAGE INSPECT RESTART THE ENGINE. ENGINE FIRE IN FLIGHT:
MIXTURE FULL RICH IDLE CUTOFF. ENGINE FIRE IN FLIGHT:
FUEL SELECTOR VALVE OFF BOTH. ENGINE FIRE IN FLIGHT:
MASTER SWITCH OFF ON. ENGINE FIRE IN FLIGHT:
CABIN HEAT AND AIR ON OFF. ENGINE FIRE IN FLIGHT:
AIRSPEED 105 KIAS 73. ENGINE FIRE IN FLIGHT:
FORCED LANDING EXECUTE USE THE CLOSEST RUNWAY.
