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This is View Only - You have to be an enrolled Student with AGS to take this exam!!!
1. Takeoff Distance with an engine failure is the distance required to accelerate to V1 with all engines operating normally, experience the loss of an engine, continue to accelerate on the remaining engine(s) to Vr at which time rotation is commenced so as to reach a height of 35 feet above the runway surface at V2.
True
False 2. Vmo/Mmo is:
Very minimum operating speed/Most maximum operating speed.
red line for airspeed (Vmo) or Mach number (Mmo).
Very maximum operating speed (Vmo) and Most minimum operating speed (Mmo). 3. Flights conducted above __________ feet are considered high altitude operations.
25,000
18,000
10,000 4. Aircraft operating above __________ feet MSL must have an operable encoding transponder in the US.
10,000
18,000
25,000 5. At 18,000 MSL, the atmosphere contains only 1/2 the oxygen molecules it has at sea level.
True
False 6. Cirrus and cirriform clouds are:
composed of ice crystals
composed of minute water droplets
middle altitude clouds 7. Cumulonimbus clouds:
are classified as stratus clouds
are an example of vertical development
are always thunderstorms 8. The 700 mb constant pressure chart reflects what altitude?
10,000
18,000
7,000 9. Flights conducted above FL450 are:
military only
direct point to point (RNAV) flights
common for the B727 and B737 aircraft 10. A low altitude VOR has a range of:
40 NM
100 NM
130 NM 11. Ten percent fast on touchdown will increase ground roll by about 21%.
True
False 12. At 30,000 feet in an unpressurized cabin, you have approximately:
1 minute of consciousness if you are not wearing an oxygen mask
15 minutes of consciousness
5 seconds before losing consciousness if you are not wearing an O2 mask 13. The reduced weight of air moving over the control surfaces at high altitude
decreases their effectiveness
makes an autopilot mandatory as per the MEL/CDL
increases drag 14. An airplane's IAS decreases in relation to TAS as the altitude increases
True
False 15. Increasing gross weight (GW) or load factor (G force) will:
increase the low speed buffet and decrease high speed buffet at higher altitudes.
cause low speed and high speed buffet numbers to merge at high altitudes causing jet upset
both are correct 16. Sweeping the wings is a method used by aircraft designers to delay the adverse effect of high Mach flight and create an economical cruise with increase in Critical Mach Number.
True
False 17. Sweeping the wings of an aircraft increases the landing/stall speed which, in turn, means higher touchdown speed, with proportionately longer runway requirements and more tire and brake wear as opposed to a straight-wing design.
True
False 18. The specific fuel consumption of a jet engine decreases as OAT decreases for a constant RPM and TAS
True
False 19. For a given TAS, the Mach number will be significantly higher at high altitude than sea level.
True
False 20. A wet runway doubles the ground roll.
True
False
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Updated: 12/26/2005.
