T-6 Systems 1, intro, Systems tour, propulsion 1+2 Flashcards
The Trim Aid Device (TAD) assists trimming for which control surface during airspeed and power changes?
The TAD senses torque, altitude, airspeed, and pitch rate and computes a desired rudder trim tab position
Tuning for each of the communications and navigation radios and the transponder is provided by which component?
RMU (Radio Management Unit)
True or False? Engine exhaust augments the thrust of the propeller.
True. Exhaust gases are ejected rearward providing thrust which augments that produced by the propeller.
Which control surface controls aircraft movement around the pitch axis?
Elevator
True or False? The VHF navigation system provides VOR, ILS, localizer and GPS capability.
False. The VHF system provides VOR, ILS, localizer, and DME capability.
Primary navigation display is provided by which component of the Electronic Flight Instrument System (EFIS)?
Electronic Horizontal Situation Indicator (EHSI)
Which standby flight instruments will operate without electrical power?
The standby altimeter, airspeed indicator, the ball in the turn and bank indicator, and the magnetic compass
True or False? The entire canopy structure is engineered to be protected from birdstrikes.
False. Only the windscreen and front canopy transparency are protected.
Primary aircraft electrical power is provided by which component of the electrical system?
The generator function of the starter/generator.
Landing gear extension and retraction is operated by which aircraft system?
Hydraulic
Movement around the roll axis is controlled by which primary control surface(s)?
Ailerons
What component of the ejection seat provides sufficient altitude for parachute deployment?
Rocket motor
True or False? The magnetic compass is one of the primary flight instruments.
False. The magnetic compass is a standby flight instrument.
Secondary aircraft electrical power is provided by what component?
Aerobatic 24 volt battery
Which aircraft system provides automatic temperature and pressure control?
Environment control system
Control of the transponder is provided by which component?
Radio Management Unit (RMU)
True or False? The canopy is hinged at the rear and opens up.
False. The canopy is hinged along the right side and opens to that side.
Which primary instrument provides primary attitude display?
Electronic Attitude Director Indicator (EADI)
In the event of inadvertent aircraft contact with the ground, which component will be activated and generate a radio signal?
The Emergency Locator Transmitter (ELT) senses impact loads and generates a signal on 121.5 and 406.0 MHz.
The engine cowling does all of the following except __________. (B/1/1)
a. protect the engine components
b. decrease drag
c. include an air inlet to the engine
d. secure the engine to the frame
d
The purpose of the inertial separator is to __________. (B/1/2)
a. separate cool incoming air and hot exhaust gases
b. remove water that may get in the fuel tanks
c. keep debris away from the engine
d. distribute air evenly over the wings
c
The compressor and power turbines are physically connected. (B/2/1)
a. True
b. False
False
What three elements are necessary for engine operation? (B/2/2)
a. Heat, smoke, and fire
b. Air, oil, and fuel
c. Gas, oil, and heat
d. Air, fuel, and heat
d
As exhaust is released, additional thrust is provided. (B/3/1)
a. True
b. False
True
Once the engine is started, and the ignition switch is in the ON position, igniters are automatically energized and de-energized by the PMU. (B/4/1)
a. True
b. False
False
The primary purpose of the ignition system is to __________. (B/4/2)
a. mix fuel and compressed air in the combustion chamber
b. turn the compressor turbine until engine start
c. ignite the air and fuel mixture in the combustion chamber
d. turn the starter motor until combustion
c
Friction control settings made to the front PCL affect the rear PCL. (B/5/1)
a. True
b. False
True
When starting the T-6A, the PCL should be __________. (B/5/2)
a. in the START/IDLE detent position
b. in the IDLE position
c. pushed forward until a green ST READY annunciator is illuminated
d. pushed forward until a green IGN SEL annunciator is illuminated
c
The PMU is located __________. (B/6/1)
a. underneath the engine, in the accessory compartment
b. on the reduction gearbox, next to the propeller interface unit
c. in the left avionics bay
d. in the front cockpit
a
- The PMU performs the following functions, except __________. (B/6/2)
a. maintain operating limits
b. process power requests
c. determine available power
d. release the correct amount of fuel
d
The PMU STATUS annunciator illuminates after landing when the PMU __________. (B/6/3)
a. is regulating normal fuel flow
b. is ready for operation
c. needs maintenance
d. is monitoring engine operation
c
After engine start, the starter becomes a generator.
a. True
b. False
True
The MANUAL starter switch position will be used under normal circumstances.
a. True
b. False
False
If oil pressure is __________ psi or below at IDLE power, the red OIL PX annunciator will illuminate.
a. 15
b. 20
c. 40
d. 90
a
If oil pressure remains between 15 and 40 psi at IDLE power for more than 5 seconds, __________ will be illuminated.
a. the amber OIL PX annunciator
b. the red OIL PX annunciator
c. both the amber and red OIL PX annunciators
d. neither OIL PX annunciator
c
The chip detector sensor is located in the __________. (C/2/3)
a. oil tank
b. cool oil return line
c. cooling assembly
d. reduction gearbox
d
The oil system provides filtered oil to all of the following systems, except the __________. (C/2/4)
a. propeller
b. reduction gears
c. engine
d. wheel brakes
d