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