| Hint | Answer | % Correct |
|---|---|---|
| Max. Weight in Baggage Area (lbs) (Utility Category) | 0 | 0%
|
| max. fuel imbalance: | 10 | 0%
|
| 1000 during cruise and descent | 0%
| |
| Min. Octane Fuel | 100 / 100LL | 0%
|
| Minimum Octane | 100 / 100LL | 0%
|
| Vfe | 102 | 0%
|
| Usable Fuel (gal) | 108 | 0%
|
| Vlo (retracting) | 109 | 0%
|
| Fuel Capacity (gal) | 110 | 0%
|
| Vfe | 111 | 0%
|
| Vo (at 2550 lbs) | 113 | 0%
|
| Max. Oil Pressure (psi) | 115 | 0%
|
| Vo at 2870 | 115 | 0%
|
| Max. Oil Pressure | 115 | 0%
|
| Vno | 125 | 0%
|
| Yellow Band | 125-154 | 0%
|
| Vo at 3800 | 135 | 0%
|
| Vle | 140 | 0%
|
| Vlo (extending) | 140 | 0%
|
| Negative Load Factor (Normal Category) | -1.5 | 0%
|
| Negative Load Factor | -1.5 | 0%
|
| Vne | 154 | 0%
|
| Red Line | 154 | 0%
|
| Vno | 169 | 0%
|
| Yellow Band | 169-202 | 0%
|
| Max. Demonstrated Crossinwd (kts) | 17 | 0%
|
| Negative Load Factor (Utility Category) | -1.7 | 0%
|
| Max. Demonstrated Crosswind | 17 | 0%
|
| Nose Gear Tire Pressure (psi) | 18 | 0%
|
| Takeoff Power (hp) | 180 | 0%
|
| Rated HP | 180 | 0%
|
| max. airspeed engaged: | 190 | 0%
|
| Positive Load Factor (with flaps) | 2 | 0%
|
| Minimum Safe Oil (qt) | 2 | 0%
|
| E-Battery Min. Volts (Ground) | 20 | 0%
|
| Max. Weight in Baggage Area (lbs) (Normal Category) | 200 | 0%
|
| Max. Weight in Baggage Area (lbs) | 200 | 0%
|
| windmilling and gear / flaps up | 200 | 0%
|
| 200 during approach | 0%
| |
| Vne | 202 | 0%
|
| Upper Red Line | 202 | 0%
|
| Max. Takeoff Weight (lbs) (Utility Category) | 2130 | 0%
|
| Max. Landing Weight (lbs) (Utility Category) | 2130 | 0%
|
| Max. Ramp Weight (lbs) (Utility Category) | 2138 | 0%
|
| E-Battery Min. Volts | 23.3 | 0%
|
| E-Battery Min. Volts (Flight) | 23.3 | 0%
|
| Battery Volts | 24 | 0%
|
| Main Gear Tire Pressure (psI) | 24 | 0%
|
| Max. Oil Temperature | 245 | 0%
|
| Max. Oil Temperature | 245 | 0%
|
| Min. Oil Pressure (psi) | 25 | 0%
|
| Min. Oil Pressure | 25 | 0%
|
| Battery Min. Volts | 25 | 0%
|
| gear down / flaps up | 250 | 0%
|
| Max. Takeoff Weight (lbs) (Normal Category) | 2550 | 0%
|
| Max. Landing Weight (lbs) (Normal Category) | 2550 | 0%
|
| Max. Ramp Weight (lbs) (Normal Category) | 2558 | 0%
|
| Takeoff RPM | 2700 | 0%
|
| Rated RPM | 2700 | 0%
|
| Alternator Volts | 28 | 0%
|
| Aspen Battery Life | 30 min | 0%
|
| Aspen Battery Life | 30 min | 0%
|
| Battery Max. Volts | 32 | 0%
|
| E-Battery Max. Volts | 32 | 0%
|
| Wing Span (ft) | 35.5 | 0%
|
| Positive Load Factor (Normal Category) | 3.8 | 0%
|
| Positive Load Factor (no flaps) | 3.8 | 0%
|
| Max. Takeoff Weight (lbs) | 3800 | 0%
|
| Max. Landing Weight (lbs) | 3800 | 0%
|
| Max. Ramp Weight (lbs) | 3816 | 0%
|
| Wing Span | 38 ft 6.6 in | 0%
|
| Wheel Ply | 4 | 0%
|
| min. altitude engaged: | 400 during takeoff | 0%
|
| Positive Load Factor (Utility Category) | 4.4 | 0%
|
| White Band | 45-102 | 0%
|
| Usable Fuel (gal) | 48 | 0%
|
| gear down / flaps 25 | 490 | 0%
|
| Engine Specs | 4 cylinder | 0%
|
| G5 Battery Life | 4 hours | 0%
|
| G5 Battery Life | 4 hours | 0%
|
| Max. Fuel Capacity (gal) | 50 | 0%
|
| Nose Gear Pressure (psi) | 50 | 0%
|
| Max. Cylinder Head Temperature | 500 | 0%
|
| Green Band | 50-125 | 0%
|
| gear down / flaps 40 | 525 | 0%
|
| Main Gear Pressure (psi) | 55 | 0%
|
| White Band | 55-111 | 0%
|
| Vmca | 56 | 0%
|
| Lower Red Line | 56 | 0%
|
| Green Band | 57-169 | 0%
|
| Nose Tire Ply | 6 | 0%
|
| Alternator Max. Amps (Ground) | 60 | 0%
|
| Alternator Max. Amps (Flight) | 65 | 0%
|
| Alternator Amps | 70 | 0%
|
| Straight Propeller Diameter Min. (in) | 72 | 0%
|
| Scimitar Propeller Diameter Min. (in) | 72.5 | 0%
|
| Straight Propeller Diameter Max. (in) | 74 | 0%
|
| Scimitar Propeller Diameter Max. (in) | 74 | 0%
|
| Propeller Diameter Max. (in) | 76 | 0%
|
| Propeller Diameter Min. (in) | 76 | 0%
|
| Max. Oil Capacity (qt) | 8 | 0%
|
| Oil Capacity (qt) | 8 | 0%
|
| Main Tire Ply | 8 | 0%
|
| 80 all other times | 0%
| |
| Vxse | 82 | 0%
|
| Vx | 82 | 0%
|
| Vsse | 82 | 0%
|
| Vyse | 88 | 0%
|
| Blue Line | 88 | 0%
|
| Vy | 88 | 0%
|
| min. airspeed engaged: | 90 during approach | 0%
|
| Vo (at 1917 lbs) | 98 | 0%
|
| affected engine | 0%
| |
| ailerons neutral | 0%
| |
| ailerons neutral | 0%
| |
| air cooled | 0%
| |
| Strut Type | air-oil / oleo | 0%
|
| Strut Type | air-oil / oleo | 0%
|
| airspeed 135 | 0%
| |
| airspeed 76 | 0%
| |
| airspeed 76 | 0%
| |
| airspeed 88 | 0%
| |
| airspeed at least 88 | 0%
| |
| airspeed at least 88 | 0%
| |
| alt air open | 0%
| |
| alt air open | 0%
| |
| alt air open | 0%
| |
| alt air open | 0%
| |
| alternator off | 0%
| |
| alternators off | 0%
| |
| bank 2, 3 into op engine | 0%
| |
| bank 2, 3 into op engine | 0%
| |
| bank 45 | 0%
| |
| bank 45 | 0%
| |
| battery off | 0%
| |
| battery off | 0%
| |
| battery off | 0%
| |
| below 140 gear down | 0%
| |
| brakes as needed | 0%
| |
| brakes as required | 0%
| |
| brakes as required | 0%
| |
| brakes maximum | 0%
| |
| cabin heat off | 0%
| |
| autopilot approved for: | cat 1 precision and non precision | 0%
|
| climb speed 88 | 0%
| |
| Straight Propeller Type | constant speed | 0%
|
| Scimitar Propeller Type | constant speed | 0%
|
| Prohibited for: | coupled OEI go around | 0%
|
| cowl flap as required | 0%
| |
| cowl flaps open | 0%
| |
| direct drive | 0%
| |
| directional control maintain | 0%
| |
| directional control maintain | 0%
| |
| directional control maintain | 0%
| |
| directional control maintain | 0%
| |
| directional control maintain | 0%
| |
| must be disengaged: | during takeoff and landing | 0%
|
| E battery arm | 0%
| |
| e battery arm | 0%
| |
| electrical load reduce | 0%
| |
| emergency descent | 0%
| |
| emergency descent | 0%
| |
| emergency descent | 0%
| |
| evacuate | 0%
| |
| evacuate | 0%
| |
| extinguish | 0%
| |
| extinguish | 0%
| |
| extinguish | 0%
| |
| extinguish | 0%
| |
| flaps 102 | 0%
| |
| flaps as needed | 0%
| |
| flaps as needed | 0%
| |
| flaps up | 0%
| |
| flaps up | 0%
| |
| fuel pump as required | 0%
| |
| fuel pump off | 0%
| |
| fuel pump off | 0%
| |
| fuel pump on | 0%
| |
| fuel pump on | 0%
| |
| fuel pump on | 0%
| |
| fuel pumps off | 0%
| |
| fuel pumps on | 0%
| |
| fuel quantity check | 0%
| |
| fuel selector off | 0%
| |
| fuel selector off | 0%
| |
| fuel selector off | 0%
| |
| fuel selector on | 0%
| |
| fuel selector on, cross feed | 0%
| |
| fuel selectors off | 0%
| |
| fuel selectors off | 0%
| |
| fuel selectors on | 0%
| |
| fuel selector switch tanks | 0%
| |
| fuel selector switch tanks | 0%
| |
| - | full feathering | 0%
|
| - | full feathering | 0%
|
| full forward | 0%
| |
| full forward | 0%
| |
| Max. Manifold Pressure | full throttle | 0%
|
| gear up | 0%
| |
| gear up | 0%
| |
| gear verify down | 0%
| |
| heat defrost off | 0%
| |
| heat defrost off | 0%
| |
| horizontally opposed | 0%
| |
| - | hydraulically actuated | 0%
|
| - | hydraulically actuated | 0%
|
| inop alternator off | 0%
| |
| inop cowl flaps closed | 0%
| |
| inop engine identify and verify | 0%
| |
| inop engine identify and verify | 0%
| |
| inop fuel pump off | 0%
| |
| inop fuel selector off | 0%
| |
| inop left mag off then on | 0%
| |
| inop mags off | 0%
| |
| inop mixture idle | 0%
| |
| inop prop feather | 0%
| |
| inop right mag off then on | 0%
| |
| inop throttle idle | 0%
| |
| Left Engine Model # | IO-360-B1G6 | 0%
|
| Engine Model # | IO-360-B4A | 0%
|
| land as soon as possible | 0%
| |
| land as soon as possible | 0%
| |
| land as soon as practical | 0%
| |
| land as soon as practical | 0%
| |
| land power off | 0%
| |
| land straight ahead | 0%
| |
| land straight ahead | 0%
| |
| left mag off then on | 0%
| |
| Right Engine Model # | LIO-360-B1G6 | 0%
|
| locate landing area | 0%
| |
| Engine Manufacturer | Lycomming | 0%
|
| mags off | 0%
| |
| manual gear | 0%
| |
| mayday | 0%
| |
| mayday | 0%
| |
| mixture as required | 0%
| |
| mixture full | 0%
| |
| mixture full | 0%
| |
| mixture full | 0%
| |
| mixture idle | 0%
| |
| mixture idle | 0%
| |
| mixture idle | 0%
| |
| mixture idle | 0%
| |
| mixture rich | 0%
| |
| mixture rich | 0%
| |
| mixtures idle | 0%
| |
| naturally aspirated | 0%
| |
| no flaps 125 | 0%
| |
| obstacles avoid | 0%
| |
| oil pressure check | 0%
| |
| oil temperature check | 0%
| |
| max. autopilot engage limits: | pitch +-50 | 0%
|
| power as required | 0%
| |
| prop feather | 0%
| |
| props full | 0%
| |
| props full | 0%
| |
| props full | 0%
| |
| right mag off then on | 0%
| |
| roll +-75 | 0%
| |
| rudder neutral | 0%
| |
| rudder neutral | 0%
| |
| Rudder opposite | 0%
| |
| rudder opposite | 0%
| |
| safe airspeed | 0%
| |
| safe airspeed | 0%
| |
| secure | 0%
| |
| secure | 0%
| |
| secure | 0%
| |
| secure | 0%
| |
| Propeller Manufacturer | Sensenich | 0%
|
| shallow turns | 0%
| |
| smooth back pressure | 0%
| |
| smooth backpressure | 0%
| |
| starter continue to engage | 0%
| |
| start switch continue cranking | 0%
| |
| throttle full | 0%
| |
| throttle full | 0%
| |
| throttle idle | 0%
| |
| throttle idle | 0%
| |
| throttle idle | 0%
| |
| throttle idle | 0%
| |
| throttles full | 0%
| |
| throttles full | 0%
| |
| throttles idle | 0%
| |
| throttles idle | 0%
| |
| throttles idle | 0%
| |
| throttles idle | 0%
| |
| If stall warning system is inop: | USP will not activate in altitude critical modes | 0%
|
| vents closed | 0%
| |
| vents open | 0%
|