ATPL Graphs part 2, Long range cruise, buffet boundary - QUIZ



Question 1

Tries remaining: 1
Marked out of 1.0
Flag question

Question text

Take-off Performance Chart




Using the given performance chart calculate the take-off distance under the following conditions:

  • Temperature = 25º F
  • Pressure Altitude = 6000'
  • Gross Weight = 15,000 lbs
  • Headwind Component = 10 knots
  • Runway Gradient = 0
  • Anti-skid is on
Select one:

Question 2

Tries remaining: 1
Marked out of 1.0
Flag question

Question text

Take-off Performance Chart



Using the given performance chart calculate the take-off distance under the following conditions:

  • Temperature = 0º F
  • Pressure Altitude = Sea Level
  • Gross Weight = 14,500 lbs
  • Headwind Component = 30 knots
  • Runway Gradient = 0
  • Anti-skid is off
Select one:

Question 3

Tries remaining: 1
Marked out of 1.0
Flag question

Question text

Take-off Speed Chart

Using the given performance chart calculate the V1, Vr, and V2 under the following conditions:

  • Temperature = -20º C
  • Pressure Altitude = 5000'
  • Gross Weight = 15,000 lbs
  • Anti-ice is on
  • Headwind Component = 20 knots
  • Runway Gradient = 0
Select one:

Question 4

Tries remaining: 1
Marked out of 1.0
Flag question

Question text

Take-off Speed Chart

Using the given performance chart calculate the V1, Vr, and V2 under the following conditions:

  • Temperature = 0º C
  • Pressure Altitude = Sea Level'
  • Gross Weight = 16,500 lbs
  • Anti-ice is off
  • Headwind Component = 15 knots
  • Runway Gradient = +2
Select one:

Question 5

Tries remaining: 1
Marked out of 1.0
Flag question

Question text

Accelerate-Go Chart



Using the given performance chart calculate the field length required (accelerate-go) under the following conditions:

  • Temperature = 20º C
  • Pressure Altitude = 2,500'
  • Gross Weight = 11,000 lbs
  • Headwind Component = 15 knots
Select one:

Question 6

Tries remaining: 1
Marked out of 1.0
Flag question

Question text

Accelerate-Go Chart

Using the given performance chart calculate the field length required (accelerate-go) under the following conditions:

  • Temperature = -10º C
  • Pressure Altitude = 4,500'
  • Gross Weight = 9,100 lbs
  • Headwind Component = 0 knots
Select one:

Question 7

Tries remaining: 1
Marked out of 1.0
Flag question

Question text

Long Range Cruise Chart



Using the given performance chart calculate the distance the aircraft can travel at 35,000' (ISA = -54.3) under the following conditions:

  • Gross Weight = 15,000 lbs
  • Landing Weight = 10,000 lbs
  • Temperature at altitude = -54.3º C
  • Headwind Component = 50 knots
Select one:

Question 8

Tries remaining: 1
Marked out of 1.0
Flag question

Question text

Long Range Cruise Chart

Using the given performance chart calculate the distance the aircraft can travel at 35,000' (ISA = -54.3) under the following conditions:

  • Gross Weight = 13,000 lbs
  • Landing Weight = 12,000 lbs
  • Temperature at altitude = -54.3º C
  • Headwind Component = 0 knots
Select one:

Question 9

Tries remaining: 1
Marked out of 1.0
Flag question

Question text

Long Range Cruise Chart



Using the given performance chart calculate the fuel required and the trip time for a 1500 NM trip under the following conditions:

  • Cruising Altitude = FL390
  • Landing Weight = 550,000 lbs
  • Temperature at altitude = ISA
  • Headwind Component = 75 knots
Select one:

Question 10

Tries remaining: 1
Marked out of 1.0
Flag question

Question text

Long Range Cruise Chart

Using the given performance chart calculate the fuel required and the trip time for a 3500 NM trip under the following conditions?

  • Cruising Altitude = FL390
  • Landing Weight = 625,000 lbs
  • Temperature at altitude = ISA + 20
  • Headwind Component = 50 knots
Select one:



 

Comments

Post a Comment

Popular posts from this blog

VNC / VTA, Lambert and Mercator, Arc of great circle, Rhumb Lines

Image
 VNC and VTA maps are owned by nav canada.  This pdf shows current version and next planned update: https://www.navcanada.ca/en/vfrchartlist.pdf For general VFR dead reckoning airspace navigation: VNC - 1 : 500,000 This is a Lambert conformal conic projection. A line on this map is an arc of a great circle and will match your compass heading after you add variation (on the map as isogonal / agonic lines) and deviation (your airplanes specific compass' error card), though it will not stay the same if you want to follow the great circle. This is impossible to navigate without computerized navigation.  For busier areas (eg Toronto airspace): VTA - 1 : 250,000 This is a Transverse Mercator Projection .  A line on this map is a direct route to your destination, or a Rhumb line.  Rumb lines are easier to navigate because you use a constant bearing. A Rhumb line is a curved line that meets all meridians at the same angle. Is a straight line on a Transverse Mercator P...
Read more

VFR Day & Night required equipment, required equipment MOOFACTAR & FATDAPPILOV

  Requirements for power driven aircraft MOOFACTAR (DAYVFR)  605.14 PG 24 of flight test notes Manifold pressure gauge for each variable pitched prop, or helicopter, or turbocharged, or supercharged engine Oil pressure Oil temperature (Coolant temp gauge if liquid cooled) Fuel gauge Altimeter Compass Tachometer (either this or manifold) Airspeed Radio (two way if in controlled airspace) FATDAPPILOV (Night extra, add day) 605.16  PG 24 of flight test notes Fuses (50% of total fuses equipped) Attitude Turn and slip Coordinator Directional Gyro (heading indicator) if beyond visual aerodrome Altimeter (sensitive pressure version) Pitot heat Position lights and anti-collision lights Instrument lights Landing lights (when carrying passengers) Oat gauge VSI As well as Current VFR Charts and CFS if departing aerodrome 602.60: a flashlight that is readily available to each crew member Requirements for power driven aircraft for IFR flight include: A checklist Current charts and ...
Read more