• Shuffle
    Toggle On
    Toggle Off
  • Alphabetize
    Toggle On
    Toggle Off
  • Front First
    Toggle On
    Toggle Off
  • Both Sides
    Toggle On
    Toggle Off
  • Read
    Toggle On
    Toggle Off
Reading...
Front

Card Range To Study

through

image

Play button

image

Play button

image

Progress

1/21

Click to flip

Use LEFT and RIGHT arrow keys to navigate between flashcards;

Use UP and DOWN arrow keys to flip the card;

H to show hint;

A reads text to speech;

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%



8%

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