Avionics 2a352g Volume 3
- 1.WHAT FLIGHT ENVIRONMENTAL PRESSURE IS SENSED BY SMALL HOLES LOCATED ON THE SIDES OF THE PITOT AND AIR DATA PROBES?
- A.
PITOT
- B.
STATIC
- C.
IMPACT
- D.
DIFFERNTIAL
- 2.TRUE AOA IS THE ANGLE BETWEEN AN AIRCRAFTS WING CORD LINE AND ITS
- A.
ATTITUDE
- B.
ALTITUDE
- C.
FLIGHT PATH
- D.
GLIDE SLOPE
- 3.HOW MANY SOURCES OF Pt AND Ps ARE ROUTED BY THE PITOT STATIC PROBE PNEUMATIC SYSTEM?
- A.
1
- B.
2
- C.
3
- D.
4
- 4.THE PITOT STATIC PRONE PNEUMATIC SYSTEM SUPPLIES AIR DATA TO THE CADC, AMI, ALTIMETER, AND
- A.
FLCC
- B.
PSA
- C.
ECA
- D.
DFLCC
- 5.THE CADC OUTPUTS ITS DATA USING THREE METHODS. THESE METHODS ARE SERIAL DIGITAL DATA WORDS, DISCRETES, AND
- A.
ANALOG
- B.
DISTINCT
- C.
ISOLATED
- D.
COMBINED
- 6.CADC SERIAL DIGITAL DATA WORDS ARE AVAILABLE ON THE
- A.
A MUX
- B.
B MUX
- C.
C MUX
- D.
D MUX
- 7.HOW ARE CADC ANALOG OUTPUT SIGNALS TRANSFERRED TO THEIR FINAL DESTINATION?
- A.
VIA THE A MUX
- B.
VIA THE D MUX
- C.
VIA AIRCRAFT WING
- D.
VIA FIBER OPTICS
- 8.ONE COMPLETE REVOLUTION OF THE ALTIMETERS ALTITUDE DIAL EQUALS
- A.
100 FEET OF ALTITUDE
- B.
1000 FEET OF ALTITUDE
- C.
5000 FEET OF ALTITUDE
- D.
10000 FEET OF ALTITUDE
- 9.WHATS THE DISPLAY RANGE OF THE ALTIMETERS ALTITUDE DRUM COUNTER?
- A.
0 - 50000
- B.
0 - 80000
- C.
-1000 - 50000
- D.
-1000 - 80000
- 10.WHY WOULD A PILOT ADJUST THE ALTIMETER TO DISPLAY PRESSURE ALTITUDE?
- A.
TO DISPLAY ALTITUDE ABOVE TERRAIN
- B.
TO DISPLAY ALTITUDE BELOW SEA LEVEL
- C.
TO STANDARDIZE AIRCRAFT ALTITUDES FOR LOW ALTITUDE AIR TRAFFIC CONTROL
- D.
TO STANDARDIZE AIRCRAFT ALTITUDES FOR HIGH ALTITUDE AIR TRAFFIC CONTROL
- 11.WHAT COMPONENT DEVELOPS THE VVIs VERTICAL VELOCITY SIGNAL?
- A.
VVI
- B.
FLCC
- C.
PSA
- D.
CADC
- 12.THE AOA INDICATOR IS CONSIDERED A
- A.
BACK UP INDICATOR
- B.
VERTICAL TAPE INDICATOR
- C.
SELF CONTAINED INDICATOR
- D.
HORIZONTAL TAPE INDICATOR
- 13.WHATS THE FUNCTION OF THE AOA INDEXERS LEVER CONTROL SWITCH?
- A.
ON/OFF SWITCH
- B.
SECTOR LIGHT INTENSITY
- C.
ENABLES AOA LOGIC CIRCUITS
- D.
ONLY USED DURING TAKEOFF AND LANDING CONFIGURES
- 14.HOW MANY DEDICATED SENSORS ARE UTILIZED BY THE CSFDR SYSTEM?
- A.
5
- B.
6
- C.
7
- D.
8
- 15.WHATS CSFDR TYPE 1 DATA PRIMARILY USED FOR?
- A.
ENGINE ANALYSIS
- B.
MISHAP INVESTIGATION
- C.
INDIVIDUAL AIRCRAFT TRACKING
- D.
MAINTENANCE TROUBLESHOOTING
- 16.WHAT PREDETERMINES CSFDR SPECIAL EVENT CRITERIA?
- A.
TYPE 1 DATA
- B.
BASELINE DATA
- C.
CMSU CONFIGURATION
- D.
SAU OFP
- 17.WHAT CSFDR TYPE DATA IS DUBBED AS INDIVIDUAL AIRCRAFT TRAKCING DATA?
- A.
1
- B.
2
- C.
3
- D.
4
- 18.WHAT DFLCC BRANCH COMMUNICATES WITH THE SDR?
- A.
A
- B.
B
- C.
C
- D.
D
- 19.WHEN DOES THE SDR CEASE RECORDING OPERATIONS?
- A.
UPON FLCS SHUTDOWN
- B.
UPON A WOW CONDITION
- C.
DURING DIGITAL BACKUP OPERATIONS
- D.
UPON AUTOPILOT ENGAGEMENT
- 20.DANIEL BERNOULLI DEVELOPED A THEORY ON THE RELATIONSHIP OF FLUID SPEED,
- A.
AND PRESSURE
- B.
AIR, AND PRESSURE
- C.
TIME, AND PRESSURE
- D.
AIR PRESSURE, AND VENTURI
- 21.AS FLUID PASSES THROUGH A VENTURI, PRESSURE IS
- A.
EQUAL THROUGHOUT THE VENTURI
- B.
LOWEST WHERE SPEED IS LOWEST
- C.
LOWEST WHERE SPEED IS HIGHEST
- D.
A PRODUCT OF FLUID SPEED, TIME, AND DISTANCE
- 22.AS AIR RUSHES PAST AN AIRFOIL, WHAT FORCE IS CREATED?
- A.
LIFT
- B.
DRAG
- C.
SPEED
- D.
THRUST
- 23.A MORE STREAMLINED AIRFOIL HAS
- A.
LESS DRAG AND LESS LIFT
- B.
MORE DRAG AND LESS LIFT
- C.
LESS DRAG AND MORE LIFT
- D.
MORE DRAG AND MORE LIFT
- 24.WHAT IS THE RELATIONSHIP BETWEEN LIFT AND THE AOA?
- A.
LIFT EQUALS AOA
- B.
LIFT INCREASES WITH AOA
- C.
LIFT DECREASES WITH AOA
- D.
THE TERMS ARE INTERCHANGEABLE
- 25.AT WHAT POINT DO MOST AIRFOILS ENTER A STALL CONDITION?
- A.
10
- B.
20
- C.
30
- D.
40
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