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| Aviation Gas weight per gallon |
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| Max Baggage Compartment Weight |
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| Max fuel quantity RV12 in Gallons |
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| Empty Weight for RV12 239VA |
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| Payload (Max TO - Full Fuel) |
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| 100 HP 5,800 RPM 5 mins max |
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| Unusable Fuel for Vx Climb |
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| Unusable Fuel for other climbs |
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| Flight Operations Allowed? |
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| Day / Night VFR. No IFR / IMC or Flight in Known Icing. |
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| Caution Range of Operations - speed |
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| Maximum Direct Crosswind Component |
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| Aerobatics - intentional spins |
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| Max seat loading pilot / passenger? |
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| 300 lbs per seat (W&B Permitting) |
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| Tach Norm Operating Range |
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| Max Cold Oil Pressure (red line) |
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| Fuel Pressure Normal Range |
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| 2.2 - 7.2 PSI (5.8 with other pump) |
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| 7.2 PSI (5.8 with other pump) |
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| Max pitch up, prolonged ops, with what amount of fuel could lead to fuel starvation? |
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Definition
| 8 degrees, 4 gallons or less |
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Term
| What is the caution related to the Master Switch? |
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Definition
| Not to be switched off with the engine running except in case of emergency. Damage to Voltage Regulator could result. |
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Term
| Fire while starting? (contained to inlet area) |
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Definition
Keep Cranking Engine Choke - Off Throttle - Open Fuel - Off Fire Continues: All Electrical Off / Evacuate |
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Term
| Low Voltage Discharge Light On |
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Definition
Non Essential Elec Equip Off Avionics Switch Off - EFIS / GPS will continue to operate Land as soon as possible |
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| High Voltage of ____ requires what? |
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Definition
15 Volts - indicates runaway generator - Master - OFF - 30A Main Bus Fuse - Pull / Remove ASAP - Non Essential Elec Equipment Off - Avionics Switch Off (EFIS/ GPS will continue) - Land as soon as possible |
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Term
| Engine Failure on Takeoff |
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Definition
Runway Remaining: Maintain Flying Speed - 60 KIAS (55 min) Throttle Closed Land ahead - brake.
No Runway Remaining - Fuel Shuttoff - check on - Choke - Check Open - Push - Ignition Switches - Both On - Fuel Pump - Check Fuse |
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| Engine Failure - Off airport landing |
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Definition
Speed 60 Flaps Full Down Fuel Shut-off - OFF Ignition Switches - OFF Master Switch - OFF Land at minimum speed possible |
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Maintain Airspeed – 60 KIAS (55 KIAS minimum) Ignition Switches – BOTH ON Fuel Pump – CHECK FUSE (illuminated if blown) Fuel Shut-Off Valve – CHECK ON - DOWN Choke – CHECK OPEN - PUSH If restart not possible, change throttle and/or choke settings in attempt to restart Follow “Forced Landing Procedure” if unable to restart |
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- Rotax 912ULS - 4 Cylinder, horizontally opposed - Air Cooled w liquid cooled cylinder heads - Dual Carburetors - Dual Spark Plugs - 2 Independent Electronic Ignition Systems |
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Gear driven Sensenich model 2A0R5R70E, composite two blade, fixed ground adjustable pitch with a 70 inch/177.8 cm. diameter. |
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| What is unique to Flaps / Ailerons? |
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Definition
The full span ailerons and flaps are combined into one unit called flaperons. An internal mechanical mixer allows the ailerons, via torque rods, to “droop” performing the function of flaps. |
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Stabilator and Ruder are cable controlled. Trim Tab - DC Motor |
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| EFIS (Electronic Flight Instrument System) |
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| What is the limiting factor for an RV12, Takeoff or Landing distance? |
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Definition
| Takeoff Distance. An RV-12 can takeoff from any given runway, it can, when properly flown, easily land on that same runway. |
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| During high ambient temp conditions, what should be done during preflight ref the fuel pump? |
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Definition
| Run the fuel pump for 5 mins to flush the fuel lines and minimize the potential for vapor lock. |
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| Under normal pre-flight conditions, how long is the fuel pump allowed to run? |
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Definition
| 2 mins. If low battery voltage, start engine, run for 5 mins at 2,000 rpm. |
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| Main landing Gear Proper Inflation? |
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- Master and both ignition switches off - Remove Oil Cap from Tank Cover - Turn prop in direction of rotation - several turns. - Check Oil Level - Replace cap |
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| Nose Landing Gear Proper Inflation? |
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| Purpose of Throttle Return Springs |
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Definition
1) Keep the two carburetors balanced, ensuring equal power right to left (takes slack out of cables). 2) Ensures that carbs fail to power on, should cables break. |
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| Where does cabin heat come from? |
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Definition
| Ducted over the coolant heat exchanger and into the cabin. |
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| Stall Warning comes on how many knots before stall? |
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| In calm wind, aerodynamic steering on the ground with Rudder is possible to what speed? |
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| Terrain Proximity colors - red and yellow designate what? |
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| Red, terrain +/- 100' of your current altitude. Yellow, more than +/- 100' of your current altitude. |
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| Heading number at the top of direction arc in the map? |
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| Magenta - GPS derived data - it is ground track. |
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| How do you exit map panning mode? |
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Definition
| Press the center of the right button. |
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Coolant/Cylinder Head Temperature* Normal in Cruise (green arc) 150 to 230 F Caution Range (yellow arc) 230 to 248 F Maximum (red line) 248 F |
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Oil Temperature Minimum 120 F Normal in Cruise 190 to 230 F Caution Range (yellow arc) 230 F to 248 F Maximum (red line) 248 F |
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Oil Pressure Minimum at Idle (red line) 12 psi Minimum at Cruise 29 psi Maximum at Cruise 73 psi Maximum – Cold (red line) 100 psi Minimum at Idle (red line) 12 psi |
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Exhaust Gas Temperature Maximum Cruise 1560 F Maximum Take-Off 1616 F |
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Tachometer Caution Range (yellow arc) 1400 to 1800 RPM Normal Range (green arc) 1800 to 5500 RPM Caution Range (yellow arc) 5500 to 5800 RPM Maximum (red line) 5800 RPM |
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| What Type of Coolant should be used? |
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Definition
| 1:1 Water / Ethylene Glycol |
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| What is the difference in oil quantity between min and max lines on oil dipstick? |
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| What is an acceptable RPM range for engine warmup? |
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Definition
1,800 - 2.500 RPM until Oil Temp Reaches 120F |
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| MAG Check performed at what RPM? |
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| Max differential on MAG Check? |
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| What is the reduction ration of the gear box? |
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| What is the time limit for engaging the starter? |
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Definition
| 10 seconds, followed by 2 minute cool down. |
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| For inflight re-start, when should the starter be used? |
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Definition
| If the propeller quits windmilling. It will not windmill below 80 KIAS. |
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Term
| What speed should not be exceeded in Turbulence? |
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Definition
| 108 KIAS, for comfort better to consider 90 KIAS |
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Term
| What flight control should not be used during stall recovery? |
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Definition
| Ailerons, instead use the rudder to maintain lateral control. |
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| Self Tests should be completed every 3 mos, i/a/w manufacturer's manual |
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| What is the approach speed on short final with full flaps on a short field approach? |
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| Is it possible to be within the allowed c.g. range on takeoff, but to be out of c.g. limits at landing? |
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Definition
Yes - Fuel burn moves CG Forward. If you have no baggage and two heavy occupants, i.e. 220 lbs each, you can be in CG @ 82.65 at takeoff and landing with only 3 gallons of fuel, you would be at 80.37 with forward limit of 80.49. If you set a personal limit of not landing with less than 4 gallons, you will remain in limits at all times. Fuel burn moves CG Forward. |
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| Difference between ELSA and SLSA? |
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Definition
SLSA - 100% factory built, can be used for instruction and rental. "Special" airworthiness ELSA - Experimental Airworthiness, not eligible for rental / flight instruction. |
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At what RPM will the Skyview system give an audible warning that the canopy is not latched? |
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