Aircraft Performance Memory Items

GIVEN: Empty weight 1271lb Empty weight 102.4 Pilot and copilot 360lb Cargo 340lb Fuel 37 gal Will the CG remain within limits after 30 gallons of fuel has been used in flight?. Yes, the CG will remain within limits. N/A.

What is the standard temperature at 10.000ft?. -5C. N/A.

When diverting to an alternate airport because of an emergency, pilots should. Apply rule of thumbs computation, estimates, and other appropriate shortcuts to divert to the new course as soon as possible. N/A.

GIVEN: Total weight 3037lb CG location stattion 68.8 Fuel consuption 12.7 GHP Fuel CG station 68.0 After 1 hour 45 minutes of flight time, the CG would be located at station. 68.83. N/A.

GIVEN: Empty weight 1271lb Empty weight moment 102.04 Pilot and copilot 260lb Rear and passenger 120lb Cargo 60lb Fuel 37 Gal Under these conditions, the CG is determined to be located. within the CG envelope. N/A.

GIVEN: Temperature 75F Pressure altitude 6000ft Weight 2.900lb Headwind 20kts To safety takeoff over a 50foot obstacle in 1000 feet, what weight reduction is necessary?. 300 pounds. N/A.

GIVEN: Airport pressure altitude 2000ft Airport temperature 20C Cruise pressure altitude 10000 ft Cruise temperature 0C What will be the fuel, time, and distance required to climb to cruise altitude under the given conditions?. 5 gallons, 9 minutes, 13NM. N/A.

If the tower reported surface wind is 010 at 18 knots, what is the crosswind component for a Rwy 08 landing?. 17 knots. N/A.

GIVEN: Empty weight 1271lb Empty weight moment 102.04 Pilot and copilot 400lb Rear seat passenger 140lb Cargo100lb Fuel 37Gal Is the airplane loaded within limits?. Yes, the weight and CG is within limits. N/A.

What effect, if any, would a change in ambient temperature or air density have on gas turbine engine performance ?. As temperature increases, thrust decreases. N/A.

When computing weight and balance, the basic empty weight includes the weight of the airframe, engine, and all installed optional equipment. Basic empty weight also includes. the unusable fuel, full operating fluids, and full oil. N/A.

What effect does an uphill runway slope have on takeoff performance?. Increase takeoff distance. N/A.

At higher elevation airports the pilot should know that indicated airspeed. will be unchanged, but groundspeed will be faster. N/A.

When conducting a go-around, the pilot must be aware that. the airplane is trimmed for a power off condition, and application of takeoff power will cause the nose to rise rapidly. N/A.

Which type of approach and landing is recommeded during gusty wind conditions?. A power on approach and power on landing. N/A.

The performance tables of an aircraft for takeoff and climb are based on. Pressure/density altitude. N/A.

What is the headwind component for a Rwy 13 takeoff if the surface wind is 190 at 15 knots?. 7 knots. N/A.

Whatis the approximate glide distance if you are operating at 8000 feet?. 12NM. N/A.

When turbulance is encoutered during the approach to a landing, what action is recommended and for what primary reason?. Increase the airspeed slighty above normal approach speed to attain more positive control. N/A.

What is the approximate glide distance if you are operating at 5500 feet?. 8 NM. N/A.

A proper corsswind landing on a runway requires that, at the moment of touchdown, the. direction of motion of the airplane and its longitudinal axis be parallel to the runway. N/A.

GIVEN: Airport pressure altitude 4000ft Airport temperature 12C Cruise pressure altitude 9000ft Cruise temperature -4C What will be the distance required to climb to cruise altitude under the given conditions?. 8.5 miles. N/A.

The CG of an aircraft can be determined by which of th following methods?. Dividing total moment by total weight. N/A.

What is the standard temperture at 20.000 feet?. -25C. N/A.

An aircraft is loaded with a ramp weight of 3650 ponds and having a CG of 94.0 approximately how much baggage woud have to be moved from the rear baggage area at station 180 to the forward baggage area at station 40 in order to move the CG to 92.0?. 52.14 pounds. N/A.

Rwy 30 is being used for landing. Which surface wind would exceed the airplanes crosswind capability of 0.2 V(S), if V(SO) is 60 knots?. 260 at 20 ktos. N/A.

If all index units are positive when computing weight and balance, the location of the datum would be at the. nose, or out in front of the airplane. N/A.

The surface wind is 180 at 25 knots. What is the crosswind component for a Rwy 13 landing?. 19 knots. N/A.

With regard to the technique required for a crosswind correction on takeoff, a pilot should use. rudder as required to maintain directional control, aileron pressure into the wind, and higher than normal lift-off airspeed in both conventional and nosewheel type airplane. N/A.

GIVEN: Total weight 4137lb CG location station 67.8 Fuel consumption 13.7 GPH Fuel CG station 68 After 1 hour 30 minutes of flight ime, the CG would be located at station. 67.79. N/A.

An airplane is loaded to a gross weight of 4800 pounds, with three pieces of luggage in the rear baggage compartment. The CG is located 98 inches aft of datum, which is 1 inch aft of limits. If luggage which weighs 90 pounds is moved from the rear baggage compartment (145 inches aft of datum) to the front compartment (45 inches aft of datum), what is the new CG?. 96.13 inches aft of datum. N/A.

Baggage weighing 90 pounds is placed in a normal categoryairplanes baggage compartment which is placarded at 100 pounds. If this airplane is subjected to a positive load factor of 3.5 Gs, the total load of the baggage would be. 315 pounds and would not be excessive. N/A.

If you experince an engine failure in a sinfle engine aircraft after takeoff, you should. establish the proper glide attitude. N/A.