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O.A.T : ISA + 15°C
Pressure Altitude: 0 ft
Aeroplane Mass: 3400 lbs
Flaps: up
Speed: 100 KIAS
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Item mass (lb) |
Arm (in) |
Moment (lb x in) |
|
Empty mass |
1,495.0 |
101.4 |
151,593.0 |
Pilot and passenger |
380.0 |
64.0 |
|
Fuel |
30 US Gal |
96.0 |
|
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pressure altitude 6,000 ft
temperature 20°C above standard
power setting 60%
wind calm
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pressure altitude 4,000 ft
temperature 20°C below standard
power setting 60%
wind calm
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pressure altitude |
8,000 ft |
temperature |
20°C below standard |
power setting |
55% |
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I On the ground the aircraft would be tail heavy and passenger or crew movement or fuel usage could make it tip up.
II The flying controls would be too sensitive increasing the risk of a tail strike at rotation.
III The tendency to stall would increase and it may be impossible to achieve “hands off” balanced flight.
IV Recovery from a spin would be much more difficult.
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pressure altitude 8,000 ft
temperature 20°C below standard
power setting 55%
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pressure altitude 0 ft
temperature 15°C
mass 2300 lb
wind calm
surface tarmac
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pressure altitude |
0 ft |
temperature |
standard |
mass |
1900 lb |
wind |
calm |
surface |
grass, dry |
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pressure altitude 3,000 ft
temperature 20°C
mass 2200 lb
wind calm
surface grass, dry
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pressure altitude 2,000 ft
temperature 40°C
mass 2100 lb
wind tail 4 kt
surface tarmac
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pressure altitude |
2,000 ft |
temperature |
30°C |
mass |
2100 lb |
wind |
head 18 kt |
surface |
grass, dry |
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pressure altitude |
4,000 ft |
temperature |
15°C |
mass |
2300 lb |
wind |
calm |
surface |
asphalt |
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Item |
Mass (lb) |
Moment/1000 (lb x in) |
|
Empty mass |
1,350 |
51.5 |
|
Pilot and front passenger |
250 |
||
Rear passengers |
400 |
||
Fuel |
30 US gal. |
||
Baggage |
|||
Oil |
8 qt |
-0.2 |
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A Take-off Mass of = 2353 lbs
A calculated C of G for departure = 89.75 inches aft of the datum
An estimated fuel burn = 200 lbs with a C of G 85.00 inches aft of datum.
The position of the C of G on landing will be?
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pressure altitude |
1,000 ft |
temperature |
10°C |
mass |
2300 lb |
wind |
tail 10 kt |
surface |
tarmac |
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16 min
Item |
Mass (lb) |
Moment/1000 (lb x in) |
Empty mass |
1,350 |
51.5 |
Pilot and front passenger |
340 | |
Fuel (full std. tanks) |
||
Oil |
8 qt |
-0.2 |
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Weight (LB) |
Arm (IN) |
Moment (LB-IN) |
|
Empty weight |
1,495.0 |
101.4 |
151,593.0 |
Pilot and passengers |
380.0 |
64.0 |
— |
Fuel (30 gal usable-no-reserve) |
— |
96.0 |
— |
|
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Item |
Mass (lb) |
Moment/1000 (lb x in) |
|
Empty mass |
1,350 |
51.5 |
|
Pilot and front passenger |
340 |
||
Rear passengers |
310 |
||
Baggage |
45 |
||
Oil |
8qt | -02 | |
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pressure altitude |
1,500 ft |
temperature |
30°C |
mass |
2300 lb |
wind |
calm |
surface |
tarmac |
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QNH 1025 hPa
temperature -4°C
elevation 3,850 ft
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I The stalling speed decreases, which is a negative factor.
II Range and endurance decrease, which are negative factors.
III The stall risk increases, which is a negative factor.
IV Stick forces increase, which is a negative factor.
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pressure altitude |
0 ft |
temperature |
0°C |
mass |
2300 lb |
wind |
head 18 kt |
surface |
grass, dry |
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Given:
O.A.T: ISA +15°C
Pressure Altitude: 0 ft
Aeroplane Mass: 2940 lbs
Tailwind component: 10 kt
Flaps: Landing position (down) Runway: Tarred and Dry
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1 – file an ATC flight plan
2 – modify an active ATC flight plan
3 – cancel an active ATC flight plan
4 – close an active ATC flight plan Which of the following combinations contains all of the correct statements?
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pressure altitude |
1,000 ft |
temperature |
30°C |
mass |
2300 lb |
wind |
head 9 kt |
surface |
tarmac |
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Given:
O.A.T: ISA
Pressure Altitude: 1000 ft
Aeroplane Mass: 3500 lbs
Tailwind component: 5 kt
Flaps: Landing position (down)
Runway: Tarred and Dry
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Have a higher stalling speed.
Have a reduced maximum level flight speed.
Have increased range and endurance.
Have a reduced rate of climb and operating ceiling.
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Given:
Pressure altitude: 4000 ft
O.A.T.: 5°C
Aeroplane mass: 3530 lbs
Headwind component: 15 kt
Flaps: Approach setting
Runway: tarred and dry
Landing gear: down
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O.A.T: 30°C
Pressure Altitude: 1000 ft
Aeroplane Mass: 3450 lbs
Tailwind component: 2.5 kt
Flaps: up
Runway: Tarred and Dry
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Time (mins) Fuel (gal) Distance (nm)
a. 3 0.7 4
b. 18 3.7 25
c. 12 2.3 17
d. 15 3.0 21
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O.A.T: ISA Pressure
Altitude: 4000 ft
Headwind component: 5 kt
Flaps: up
Runway: Tarred and Dry
Factored runway length: 2000 ft
Obstacle height: 50 ft
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O.A.T: -7°C
Pressure Altitude: 7000 ft
Aeroplane Mass: 2950 lbs
Headwind component: 5 kt
Flaps: Approach setting
Runway: Tarred and Dry
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O.A.T: 38°C
Pressure Altitude: 4000 ft
Aeroplane Mass: 3400 lbs
Tailwind component: 5 kt
Flaps: Approach setting
Runway: Dry Grass
Correction factor: 1.2
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OAT: +18 C
Aerodrome Pressure Altitude: 1500ft
Aeroplane Mass: 1270kg
Wind Component: 4kt tailwind
Runway Surface: Hard, Dry Runway Slope: 0%
The approximate take-off distance to 50ft is:
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