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ATP Seneca|Accessible Aviation Seneca Student Guide Qs & As

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ATP Seneca|Accessible Aviation Seneca Student Guide Qs & As

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Institution
ATP
Course
ATP

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Uploaded on
October 14, 2024
Number of pages
17
Written in
2024/2025
Type
Exam (elaborations)
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Questions & answers

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ATP Seneca| Accessible Aviation Seneca Student Guide
Qs & As

Flap Speed Limits Correct Ans-10 degrees/1st notch - 160 mph max


25 degrees/2nd notch - 140 mph max


40 degrees/ 3rd notch - 125 mph max




VR Rotation Speed Correct Ans-80 - 85 mph


70 on max effort short field w/ 25 flap




Vso Stall Speed in Landing Configuration Correct Ans-69 mph (bottom of white arc)




Vs Stall Speed Clean Correct Ans-76 mph (bottom of green arc)




VMC Min controllable speed Correct Ans-80 mph (Red Radial Line)




Vx Best angle of climb Correct Ans-90 mph




Vsse Safe Speed for Intentional Engine Failure Correct Ans-90 mph

, ATP Seneca| Accessible Aviation Seneca Student Guide
Qs & As

Vyse Best rate of climb single engine Correct Ans-105 mph (Blue radial line)




Vy Best rate of climb Correct Ans-105 mph




VFe Max full flap extension speed


Vlo (up) Correct Ans-125 mph (top of white arc)




Va Maneuvering Speed Correct Ans-146 mph @ 4200 pounds


133 mph @ 2743 pounds




Vlo (down) Max gear extension speed Correct Ans-150 mph




Max speed for storm window Correct Ans-150 mph




Drag Factors Correct Ans-Full Flaps: -400 fpm


Windmilling Prop: -400 fpm

, ATP Seneca| Accessible Aviation Seneca Student Guide
Qs & As
Gear Extended: -150 fpm




SINGLE ENGINE SERVICE CEILING Correct Ans-The maximum density altitude at which best

rate of climb airspeed (Vyse) will produce a 50 fpm rate of climb with the critical engine

inoperative and propellor feathered.




SINGLE ENGINE ABSOLUTE CEILING Correct Ans-The maximum density altitude that an

aircraft can attain or maintain with the critical engine inoperative. Vyse and Vxse are equal at

this altitude.




What determines Vmc (scam5ff) Correct Ans-Standard Day Conditions at S


Maximum Power on the operating engine


Critical engine windmilling


Flaps in takeoff position


Aft legal cg


5 degrees max bank


Max takeoff weight


full rudder into operating engine

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