1.
What flight environment pressure is sensed by small holes located on the sides of the pilot and air data probes
A. 
B. 
C. 
D. 
2.
True angle-of-attack (AOA) is the angle between an aircraft's wing cord line and its
A. 
B. 
C. 
D. 
3.
How many sources of pitot pressure (Pt) and static pressure (Ps) are routed by the pitot-static probe pneumatic system?
A. 
B. 
C. 
D. 
4.
The pitot-static probe pneumatic system supplies air data to the central air data computer (CADC), airspeed mach indicator (AMI), altimeter, and
A. 
Flight control computer (FLCC)
B. 
Pneumatic sensor assembly (PSA)
C. 
Electronic component assembly (ECA)
D. 
Digital flight control computer (DFLCC)
5.
What component(s) receive air data inputs from the air data probe pneumatic system?
A. 
B. 
Airspeed mach indicator (AMI)
C. 
Pneumatic sensor assembly (PSA)
D. 
PSA and central air data computer (CADC)
6.
The angle of sideslip pneumatic system routes air data pressures to the
A. 
Differential pressure sensor (DPS)
B. 
Pneumatic sensor assembly (PSA)
C. 
Electronic component assembly (ECA)
D. 
Digital flight control computer (DFLCC)
7.
How are central air data computer (CADC) analog output signals transferred to their final destination?
A. 
Via the A-multiplex (MUX) bus
B. 
C. 
D. 
8.
The pitot-static probe pneumatic system supplies the airspeed mach indicator (AMI) with
A. 
B. 
C. 
D. 
Pt and static pressure (Ps)
9.
One complete revolution of the altimeter's altitude dial equals
A. 
B. 
C. 
D. 
10.
What's the display range of the altimeter's altitude drum counter?
A. 
B. 
C. 
D. 
11.
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
12.
Which component develops the vertical velocity indicator's (VVI) vertical velocity signal?
A. 
B. 
Flight control computer (FLCC)
C. 
Pneumatic sensor assembly (PSA)
D. 
Central air data computer (CADC)
13.
The angle-of-attack (AOA) indicator is considered a
A. 
B. 
C. 
D. 
Horizontal tape indicator
14.
What's the function of the angle-of-attack (AOA) indexer's lever control switch?
A. 
B. 
C. 
Enables AOA logic circuits
D. 
Only used during takeoff and landing configurations
15.
What's the crash survivable flight data recorder (CSFDR) system's prime component?
A. 
B. 
Signal acquisition unit (SAU)
C. 
Crash survivable memory unit (CSMU)
D. 
Linear variable differential transformer (LVDT)
16.
What data is only stored in the crash survivable flight data recorder (CSFDR)?
A. 
B. 
C. 
D. 
17.
How many dedicated sensors are utilized by the crash survivable flight data recorder (CSFDR) system?
A. 
B. 
C. 
D. 
18.
Which crash survivable flight data recorder (CSFDR) system component utilizes a pendulous device?
A. 
Crash survivable memory unit (CSMU)
B. 
Axial accelerometer transmitter
C. 
Control surface position transducer
D. 
Engine power lever angle potentiometer
19.
Which crash survivable flight data recorder (CSFDR) system control surface position transducer is not connected to an integrated servo-actuator (ISA)?
A. 
B. 
C. 
D. 
20.
What's crash survivable flight data recorder (CSFDR) type 1 data primarily used for?
A. 
B. 
C. 
Individual aircraft tracking
D. 
Maintenance troubleshooting
21.
What predetermines the crash survivable flight data recorder (CSFDR) special event criteria?
A. 
B. 
C. 
Crash survivable memory unit (CMSU) configuration
D. 
Signal acquisition unit operational flight program (SAU OFP)
22.
Which crash survivable flight data recorder (CSFDR) type data is dubbed as individual aircraft tracking data?
A. 
B. 
C. 
D. 
23.
Which crash survivable flight data recorder (CSFDR) type data is known as structural loads environmental data
A. 
B. 
C. 
D. 
24.
Which crash survivable flight data recorder (CSFDR) type data is used for engine analysis?
A. 
B. 
C. 
D. 
25.
When does the seat data recorder (SDR) cease recording operations?
A. 
Upon flight control system (FLCS) shutdown
B. 
Upon a weight-on-wheels (WOW) condition
C. 
During digital backup operations
D. 
Upon autopilot engagement