C172RG  systems/procedures quiz:

Fuel

  The fuel tanks have a usable capacity of ___ gallons; ___ gallons if filled to the bottom edge of the fuel filler collar.  
  At 75% power, the engine burns approximately ___gph, and at 65%  ___gph.  
  The fuel selector has positions ___, ___ , -___ and ___.  In flight, the ___ position should be used, except during ____.  The ____ selector position should be used when fueling the aircraft, or parking on a slope.  
  The airplane is equipped with an electric fuel pump, which is used if _____. 
  During preflight, fuel should be drained from ___, ___, ___ and ___.

Flaps

Vfe is ___ knots.  Up to ___ degrees of flaps may be used up below ___ knots.  __ degrees of flaps may be used for takeoffs at gross weights below ___lbs. The use of flaps for takeoff will ___.

Gear

Vlo is __ knots. Vle is ___ knots.  There are __ landing gear position indicator lights. The gear is hydraulically activated. Hydraulic pressure is maintained by an ___ pump.  The hydraulic fluid reservoir and dip-stick is located ___.  Hydraulic pressure can also by provided by ___, but can only be used to ___ the gear.  The gear horn should sound if either ___ or ___.

What is the procedure if the gear fails to retract?  ___
What is the procedure if the gear fails to extend? ___

W&B

With full fuel and oil, the airplane has a cabin load of ___ lbs.   The baggage compartment may carry up to ___ lbs, including at most __ lbs in the "hat-shelf" area.


Speeds

Va (at max gross) is ___ knots  (IAS)
Best rate of climb (sea-level) is ___ knots and ___ knots at 10000 feet.
Best angle of climb speed (Sea-level) is ___ knots and ___ knots at 10000 feet.
Best glide speed (at MGW) is ___ knots, with zero wind you have a glide ratio of about __ to one. 
For a short field takeoff, you should climb at __ knots, retracting the gear when ____.

Electrical

What is the procedure if the LOW-VOLTAGE warning light illuminates? ___

Performance

The service ceiling is  ____ feet.
At sea-level, max gross weight, no wind, temp 20C, the takeoff ground roll is ___ feet, and the distance over a 50 ft obstacle is ___ feet.
At 6000MSL, max gross weight, no wind, temp 20C, the takeoff ground roll is ___ feet, and the distance over a 50 ft obstacle is ___ feet. After takeoff, the max ROC is ___ fpm at an airspeed of __ knots.

At sea-level, max gross weight, no wind, temp 20C, the landing ground roll is ___ feet, and the distance over a 50 ft obstacle is ___ feet.
At 6000MSL, max gross weight, no wind, temp 20C, the landing ground roll is ___ feet, and the distance over a 50 ft obstacle is ___ feet.