UCT T-1A Systems 3 & 4 Test-QUESTIONS|VERIFIED
SOLUTIONS (100% CORRECT)!
Does the TCAS in the T-1A provide vertical guidance, horizontal guidance, or both in the event
of traffic? - ✔✔Vertical only.
The radio altimeter provides an indication of AGL height up to ___ ft. - ✔✔2,500.
Will the GPWS alert you to landing with the gear retracted? - ✔✔Yes, passing 200 ft AGL at
approach speeds.
True or false: The standby altimeter is accurate at all altitudes and configurations and no
corrections need to be applied. - ✔✔False.
When are readings from the magnetic compass valid? - ✔✔Only in level, unaccelerated
flight.
Where does the standby airspeed indicator use inputs? - ✔✔From the copilot's pitot static
system.
What setting must the windshield heat be in to ensure accurate magnetic compass readings? -
✔✔LOW.
What would cause the aural alert "don't sink, don't sink"? - ✔✔Excessive altitude loss after
takeoff.
What type of traffic generates a Preventative Resolution Advisory? - ✔✔A traffic conflict that
should be resolved if you do not change present flightpath.
, When and how would you inhibit the "Too Low, Terrain" aural alert from the GPWS? -
✔✔When entering a planned 500' low-level, press the GPWS TAC switch.
The standby attitude indicator is reliable up to ±___° pitch and roll for ____ minutes after
power loss. - ✔✔±6°, 9 mins.
True or false: Pressing either the pilot or copilot EFIS Master Warning Switchlight to extinguish
it, both lights are extinguished. - ✔✔False.
True or false: The flight time on the digital clock in the T-1A automatically zeros when power is
removed from the aircraft. - ✔✔False, you must manually zero it at the start of your flight.
How do you inhibit the Mode 4 GPWS warning when landing with less than 30 degrees of flaps?
- ✔✔Press the GPWS FLP ORIDE switch.
True or false: During cross-side operations, no comparator warnings are available, and the
pilots should crosscheck position, attitude, and altitude with other reliable instruments, such as
the standby instruments. - ✔✔True.
During an RTU failure, how do you communicate via VHF on guard (121.5 MHz)? - ✔✔Pull
and reset the VHF circuit breaker.
Landing gear is _____ controlled, _____ operated. - ✔✔Electrically, hydraulically.
Where are the brake pedals? - ✔✔The upper portion of both the pilot's and copilot's rudder
pedals.
Is nosewheel steering a primary or secondary flight control? - ✔✔Secondary.
SOLUTIONS (100% CORRECT)!
Does the TCAS in the T-1A provide vertical guidance, horizontal guidance, or both in the event
of traffic? - ✔✔Vertical only.
The radio altimeter provides an indication of AGL height up to ___ ft. - ✔✔2,500.
Will the GPWS alert you to landing with the gear retracted? - ✔✔Yes, passing 200 ft AGL at
approach speeds.
True or false: The standby altimeter is accurate at all altitudes and configurations and no
corrections need to be applied. - ✔✔False.
When are readings from the magnetic compass valid? - ✔✔Only in level, unaccelerated
flight.
Where does the standby airspeed indicator use inputs? - ✔✔From the copilot's pitot static
system.
What setting must the windshield heat be in to ensure accurate magnetic compass readings? -
✔✔LOW.
What would cause the aural alert "don't sink, don't sink"? - ✔✔Excessive altitude loss after
takeoff.
What type of traffic generates a Preventative Resolution Advisory? - ✔✔A traffic conflict that
should be resolved if you do not change present flightpath.
, When and how would you inhibit the "Too Low, Terrain" aural alert from the GPWS? -
✔✔When entering a planned 500' low-level, press the GPWS TAC switch.
The standby attitude indicator is reliable up to ±___° pitch and roll for ____ minutes after
power loss. - ✔✔±6°, 9 mins.
True or false: Pressing either the pilot or copilot EFIS Master Warning Switchlight to extinguish
it, both lights are extinguished. - ✔✔False.
True or false: The flight time on the digital clock in the T-1A automatically zeros when power is
removed from the aircraft. - ✔✔False, you must manually zero it at the start of your flight.
How do you inhibit the Mode 4 GPWS warning when landing with less than 30 degrees of flaps?
- ✔✔Press the GPWS FLP ORIDE switch.
True or false: During cross-side operations, no comparator warnings are available, and the
pilots should crosscheck position, attitude, and altitude with other reliable instruments, such as
the standby instruments. - ✔✔True.
During an RTU failure, how do you communicate via VHF on guard (121.5 MHz)? - ✔✔Pull
and reset the VHF circuit breaker.
Landing gear is _____ controlled, _____ operated. - ✔✔Electrically, hydraulically.
Where are the brake pedals? - ✔✔The upper portion of both the pilot's and copilot's rudder
pedals.
Is nosewheel steering a primary or secondary flight control? - ✔✔Secondary.
