Course Hero Logo

C 490 feet 3694 refer to figure 39 determine the

Course Hero uses AI to attempt to automatically extract content from documents to surface to you and others so you can study better, e.g., in search results, to enrich docs, and more. This preview shows page 5 - 6 out of 6 pages.

C) 490 feet.3694.
(Refer to figure 39.) Determine the total distancerequired to land over a 50-foot obstacle.Temperature 32°F
Runway Hard surface
B)1,004 feet.C) 1,506 feet.
3695.(Refer to figure 39.) Determine the total distancerequired to land over a 50-foot obstacle.Pressure altitude 5,000 ft.Headwind 8 kts.Temperature 41°F
Runway Hard surface
C) 1,076 feet.3696.
(Refer to figure 39.) Determine the approximatelanding ground roll distance.Pressure altitude 5,000 ft.Headwind Calm.Temperature 101°F
Performance- Page 72Aviation Seminars3697. H317(Refer to figure 39.) Determine the total distancerequired to land over a 50-foot obstacle.Pressure altitude 3,750 ftHeadwind 12 ktsTemperature StdA) 794 feet.B)816 feet.C) 836 feet.3698.(Refer to figure 39.) Determine the approximatelanding ground roll distance.Pressure altitude 1,250 ftHeadwind 8 ktsTemperature StdA) 275 feet.B)366 feet.C) 470 feet.(Refer to figure 41.) Determine the approximateground roll distance required for takeoff.OAT 100Pressure altitude 2,000 ftTakeoff weight 2,750 lbHeadwind component Calm3705. H946(Refer to figure 41.) Determine the total distancerequired for takeoff to clear a 50-foot obstacle.OAT StdPressure altitude 4,000 ftTakeoff weight 2,800 lbHeadwind component CalmA) 1,500 feet.(Refer to figure 41.) Determine the approximateground roll distance required for takeoff.OAT 90°FPressure altitude 2,000 ftTakeoff weight 2,500 lbHeadwind component 20 kts3706.(Refer to figure 41.) Determine the total distancerequired for takeoff to clear a 50-foot obstacle.OAT StdPressure altitude Sea levelTakeoff weight 2,700 lbHeadwind component Calm3707.(Refer to figure 41.) Determine the approximateground roll distance required for takeoff.OAT 100Pressure altitude 2,000 ftTakeoff weight 2,750 lbHeadwind component CalmA)1,150 feet.B) 1,300 feet.C) 1,800 feet.3708.(Refer to figure 41.) Determine the approximateground roll distance required for takeoff.OAT 90°FPressure altitude 2,000 ftTakeoff weight 2,500 lbHeadwind component 20 kts
End of preview. Want to read all 6 pages?

Upload your study docs or become a

Course Hero member to access this document

Term
Fall
Professor
N/A
Tags
Atmosphere, Standard conditions for temperature and pressure, Altimeter, Pressure altitude Sea

Newly uploaded documents

Show More

Newly uploaded documents

Show More

  • Left Quote Icon

    Student Picture

  • Left Quote Icon

    Student Picture

  • Left Quote Icon

    Student Picture