Hint | Answer | % Correct |
---|---|---|
Controls roll | ailerons | 100%
|
Controls pitch | elevator | 100%
|
Controls yaw | rudder | 100%
|
At all times above (ft MSL) | 14,000 | 75%
|
All occupants above (ft MSL) | 15,000 | 75%
|
How many minutes for eyes to get "dark adaptation"? | 30 | 75%
|
How many satellites are needed to calculate three-dimensional position? | 4 | 75%
|
weight of gasoline (lb/US gal) | 6 | 75%
|
the speed your lungs can decompress, approximately (s) | 0.5 | 50%
|
for periods longer than 30 minutes above (ft MSL) | 12,500 | 50%
|
lost communications squawk code | 7600 | 50%
|
____ are located at center of vision, and are for color | cones | 50%
|
pressure altitude corrected for non-standard temperature | density altitude | 50%
|
Lack of sufficient oxygen reaching the brain is (four types below) | hypoxia | 50%
|
airspeed read directly off airspeed indicator | indicated airspeed (IAS) | 50%
|
Pitch affects rotation around the | lateral axis | 50%
|
Roll affects rotation around the | longitudinal axis | 50%
|
TH corrected for magnetic variation | magnetic heading (MH) | 50%
|
____ are located around the center of vision and are for night vision | rods | 50%
|
Leading edge of wing flaps | slats | 50%
|
air gap between flap and trailing edge | slotted | 50%
|
High-drag device that will not increase lift | spoilers | 50%
|
Bearings are ___ the VOR | TO | 50%
|
CAS corrected for density altitude | true airspeed (TAS) | 50%
|
course over ground relative to due north | true course (TC) | 50%
|
TC corrected for wind | true heading (TH) | 50%
|
angular difference between true and magnetic north | variation | 50%
|
Yaw affects rotation around the | vertical axis | 50%
|
What are the minimum number of satellites active in the GPS system? | 24 | 25%
|
inform aircraft there may be high volume of pilot training or unusual aerial activity | alert area | 25%
|
IAS corrected for instrument installation error | calibrated airspeed (CAS) | 25%
|
magnetic anomaly that affects the compass | deviation | 25%
|
slides out and down chaning wing shape | Fowler | 25%
|
Radials are ___ the VOR | FROM | 25%
|
separates certain military activities from IFR traffic | MOA | 25%
|
Automatic direciton finder (ADF) receives the signal from a | NDB | 25%
|
altitude shown when altimeter is set to 29.92 | pressure altitude | 25%
|
aircraft flight is prohibited, for security or other reasons | prohibited area | 25%
|
Used to verify whether the signal is usable or corruputed for GPS systems | RAIM | 25%
|
While active, operations may be hazardous to non-participating aircraft | restricted area | 25%
|
improves GPS signals to use for precision approaches (within 25ft 95% of the time) | WAAS | 25%
|
extends from 3 NM outward from the coast of US; warns of potential hazard | warning area | 25%
|
aviator's breathing oxygen has no more than ___ mg of water/liter | 0.005 | 0%
|
aviator's breathing oxygen is ___% pure oxygen | 99.5 | 0%
|
MH corrected for deviation | compass heading (CH) | 0%
|
oxygen is diluted with ambient air in re-breather bag | continuous flow | 0%
|
as altitude increases vision | deteriorates | 0%
|
conserves oxygen at lower altitudes; increasing oxygen at higher altitudes | diluter-demand | 0%
|
change of cabin pressure occurs faster than lungs can decompress | explosive decompression | 0%
|
caused by alcohol or drug use; inability of cells to use oxygen | histotoxic | 0%
|
reduction in oxygen-carrying capacity of the blood | hypemic | 0%
|
a result of decreased oxygen partial pressure in the air | hypoxic | 0%
|
similar to PREVIOUS ANSWER but relies more on ground stations | LAAS | 0%
|
A system of 27 transmitters that emit signals in the LF range | LORAN | 0%
|
hinges down at trailing edge | plain | 0%
|
needed for operations above 40,000 feet, delivers positive pressure oxygen | pressure demand | 0%
|
change of cabin pressure occurs slower than lungs can decompress | rapid decompression | 0%
|
Limitations | Section 2 | 0%
|
Emergency Procedures | Section 3 | 0%
|
Normal Procedures | Section 4 | 0%
|
Performance | Section 5 | 0%
|
Weight and Balance | Section 6 | 0%
|
Airplane Systems | Section 7 | 0%
|
Airplane Maintenance | Section 8 | 0%
|
deflected down at trailing edge | split | 0%
|
poor circulation; experienced during excessive G's | stagnant | 0%
|
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