An aircraft is loaded 110 pounds over maximum certificated gross weight. If fuel (gasoline) is drained to bring the aircraft weight within limits, how much fuel should be drained?

Which would provide the greatest gain in altitude in the shortest distance during climb after takeoff?

After takeoff, which airspeed would the pilot use to gain the most altitude in a given period of time?

What effect does high density altitude, as compared to low density altitude, have on propeller efficiency and why?

Which combination of atmospheric conditions will reduce aircraft takeoff and climb performance?

What effect does high density altitude have on aircraft performance?

What effect, if any, does high humidity have on aircraft performance?

If an emergency situation requires a downwind landing, pilots should expect a faster

(Refer to Fig 36) What is the expected fuel consumption for a 1,000 NM flight under the following conditions:

Pressure Altitude: 8,000 ft

Temperature: 22^o C

Manifold Pressure: 20.8” Hg

Wind: Calm

(Refer to Fig 36) What fuel flow should a pilot expect at 11,000 ft on a standard day with 65% max continuous power?

(Refer to Fig 36) Determine the approximate manifold pressure setting with 2450 RPM to achieve 65% max continuous power at 6,500 ft with a temperature 36^o F higher than standard

(Refer to Fig 37) What is the headwind component for a landing on Runway 18 if the tower reports the wind as 220 degrees at 30 knots

(Refer to Fig 37) Determine the maximum wind velocity for a 45 degrees crosswind if the maximum crosswind component for the airplane is 25 knots

(Refer to Fig 37) What is the maximum wind velocity for a 30 deg crosswind if the maximum crosswind component for the airplane is 12 kt?

(Refer to Fig 37) With a reported wind of North at 20 kt, which runway (6, 29, or 32) is acceptable for use for an airplane with a 13-kt max crosswind component?

(Refer to Fig 37) With a reported wind of South at 20 kt, which runway (10, 14, or 24) is appropriate for an airplane with a 13-kt max crosswind component?

(Refer to Fig 37) What is the crosswind component for a landing on Runway 18 if the tower reports the wind as 220 degrees at 30 knots?

(Refer to Fig 39) Determine the approximate ground roll distance

Pressure Altitude: Sea Level

Headwind: 4 Knots

Temperature: Standard

(Refer to Fig 39) Determine the total distance required to land over a 50 foot obstacle

Pressure Altitude: 7,500 feet

Headwind: 8 Knots

Temperature: 32^o F

Runway: Hard Surface

(Refer to Fig 39) Determine the total distance required to land over a 50 foot obstacle

Pressure Altitude: 5,000 feet

Headwind: 8 Knots

Temperature: 41^o F

Runway: Hard Surface

(Refer to Fig 39) Determine the approximate ground roll distance

Pressure Altitude: 5,000 feet

Headwind: Calm

Temperature: 101^o F

(Refer to Fig 39) Determine the total distance required to land over a 50 foot obstacle

Pressure Altitude: 3,750 feet

Headwind: 12 Knots

Temperature: Standard

(Refer to Fig 41) Determine the total distance required for takeoff to clear a 50 foot obstacle

OAT: Standard

Pressure Altitude: 4,000 feet

Takeoff Weight: 2,800 lb

Headwind component: Calm

(Refer to Fig 41) Determine the total distance required for takeoff to clear a 50 foot obstacle

OAT: Standard

Pressure Altitude: Sea Level

Takeoff Weight: 2,700 lb

Headwind component: Calm

(Refer to Fig 41) Determine the approximate ground roll distance required for takeoff

OAT: 101^o F

Pressure Altitude: 2,000 feet

Takeoff Weight: 2,750 lb

Headwind component: Calm

(Refer to Fig 41) Determine the approximate ground roll distance required for takeoff

OAT: 90^o F

Pressure Altitude: 2,000 feet

Takeoff Weight: 2,500 lb

Headwind component: 20 knots

Given (Table Above)

The CG is located how far aft of datum?

(Refer to Figs 33 and 34) What is the max amount of baggage that can be carried when the airplane is loaded as follows:

Front Seat Occupants: 387 lb

Rear Seat Occupants: 293 lb

Fuel: 35 gallons

(Refer to Figs 33 and 34) Determine if the aircraft weight and balance is within limits:

Front Seat Occupants: 415 lb

Rear Seat Occupants: 110 lb

Fuel, Main Tanks: 44 gallons

Fuel, Aux Tanks: 19 gallons

Baggage: 32 lb

(Refer to Fig 35) What is the maximum amount of baggage that may be loaded aboard the airplane for the CG to remain within the moment envelope?

Empty Weight = 1350 lb

Empty MOM/1000 = 51.5 lb-in

Pilot/Front Passenger = 250 lb

Rear Passengers = 400 lb

Fuel (30 gallons)

(Refer to Fig 35) Determine the moment of the airplane and determine which category is applicable

Empty Weight = 1350 lb

Empty MOM/1000 = 51.5 lb-in

Pilot/Front Passenger = 310 lb

Rear Passengers = 96 lb

Fuel (38 gallons)

(Refer to Fig 35) What is the maximum amount of fuel that may be aboard the airplane at takeoff if loaded as follows?

Empty Weight = 1350 lb

Empty MOM/1000 = 51.5 lb-in

Pilot/Front Passenger = 340 lb

Rear Passengers = 310 lb

Baggage = 45 lb

(Refer to Fig 35) Determine the moment with the following data:

Empty Weight = 1350 lb

Empty MOM/1000 = 51.5 lb-in

Pilot/Front Passenger = 340 lb

Fuel = Capacity (Std Tanks)

(Refer to Fig 35) Determine the moment with the following data

Empty Weight = 1350 lb

Empty MOM/1000 = 51.5 lb-in

Pilot/Front Passenger = 380 lb

Fuel (48 gallons) = 288 lb

(Refer to Figs 33 and 34) Which action can adjust the airplane’s weight to maximum gross weight and the CG within limits for takeoff?

Front Seat Occupants: 425 lb

Rear Seat Occupants: 300 lb

Fuel, Main Tanks: 44 gallons

(Refer to Figs 33 and 34) What effect does a 35-gallon fuel burn (main tanks) have on the weight and balance if the airplane weighed 2,890 lb and the MOM/100 was 2,452 at takeoff

(Refer to Figs 33 and 34) With the airplane loaded as follows, what action can be taken to balance the airplane?

Front Seat Occupants: 411 lb

Rear Seat Occupants: 100 lb

Fuel, Main Tanks: 44 gallons

(Refer to Fig 62) If 50 pounds of weight is located at Point X and 100 pounds at Point Z, how much weight must be located at Point Y to balance the plank?

(Refer to Fig 61) How should the 500-pound weight be shifted to balance the plank on the fulcrum?