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21 Cards in this Set
- Front
- Back
Max t/o weight ISA PA 4000FT Weight 2640lbs H wind 5kt Runway 2000 ft tarred and dry Obstacle height 50ft >3500lbs 2860 2400 3240 |
2860 |
|
Ground distance to Height 2000ft Oat 25 PA 1000 3600lbs 100kias 15kt headwind 18347ft 24637ft 21505ft 18832ft |
18347 |
|
Ground distance to reach height of 1500 ft Oat isa Pa 5000 3300lbs 100kias 5kts tail w 16665 18073 18909 20109 |
16665 |
|
Power setting table Oat 13 Pa 8000 Rpm 2300 159kt and 71.7 lbs/hr 160 71.1 158 74.4 160 69.3 |
160kts and 693lbs/hr |
|
Power setting table Oat 13 Pa 8000 2300 23inhg and 69lbs/hr 22.4 69.3 22.4 71.1 22.4 73.8 |
22.4 inhg and 69.3lbs/hr |
|
Given Rwy 17 touchdown elevation 146ft Tora 1400m Asda 1600 Toda 1800 Rwy 35 touchdown elevation 34ft Tora 1500 Asda 1700 Toda 1900 Slope of rwy 35 is 2.28% up 2.28 down 2.44 up 2.44 down |
2.28% up |
|
Following a take off determined by the 50ft screen height a light twin climbs on a 10% over the ground climb gradient. It Will clear a 900m high Obstacle in relation to the Runway horizontally, situated at 10 000m from the 50 ft clearing Point with an Obstacle clearance of 85m 100m 115m It will not clear the obstacle |
115m |
|
3.3 % gradient at 100kts 330ft/min 3300ft/min 3.30m/s 33m/s |
330ft/min |
|
True airspeed of 194kt and a vertical speed of 1000ft/min the gradient is 3° 3% 5° 8% |
3° |
|
If airworthiness documents do not specify a correction for landing on a wet runway; the landing distance must be increased by 20% 5% 10% 15% |
15% |
|
Deployment for flaps ......CL/CD Increases Reduces Only slightly increases Does not affect |
Reduces |
|
110 000kg gradient of 2.6%, what mass would it be able to achieve a gradient of 2.4 119 167 kg 101 530 kg 110 000 kg 121 167 kg |
119 167 kg |
|
Roc 1000 ft/min tas 198kts What is the climb gradient 5.08% 3 % 4 % 4.98% |
4.98% |
|
Thrust to weight ration 1:4 , lift to drag 12:1 What will climb gradient be 3.0% 8.3 % 16.7% 3.3% |
16.7% |
|
VMD for a jet aeroplane is approximately equal to 1.3 vs 1.7 vs 1.6 vs 2.1 vs |
1.6 vs |
|
Best EAS / drag ratio IS approximately 1.3 VMD 1.32 VMD 1.6 VMD 1.8 VMD |
1.32 VMD |
|
Climb gradient 3.8% tas 100kts G's 130kts The wind effective climb gradient is 4.9% 4.2% 3.8% 2.9% |
2.9% |
|
An Obstacle is 5000m from end of TODR IS 160M high thecscreen height is 50ft and the climb gradient is 5% which statement is correct Cleared by 710ft Cleared by 345ft Cleared by 295ft Not Cleared |
Cleared by 345ft |
|
Max take off weight Flap 5 / 10 / 15 Field length limited mass 49650kg / 52600kg / 56950 kg WAT limited Mass 51250 kg / 49100 kg / 45500kg 49650 kg 49100 kg 45500 kg 56950 kg |
49650 kg |
|
The speed V2 of a jet aeroplane must be greater than 1.3v1 1.2vmcg 1.05vlof 1.2vs |
1.2vs |
|
V2 min for turbo prop with more than three engines 1.2vs 1.3vs 1.15vs 1.2vs1 |
1.15vs |