When is the half-bank mode inhibited? - ANSWER Takeoff Mode
GA Mode
Onside approach mode capture
Any onside localizer capture.
In the pitch mode, rotating the pitch wheel one click will provide how much pitch change?
- ANSWER 1/2 degree.
In the vertical speed mode, rotating the pitch wheel one click provides how much VVI change? -
ANSWER 100 feet/min.
To fly a full ILS approach with glideslope, you should select the NAV mode of the FCP. - ANSWER
False.
When conducting a go-around from autopilot coupled approach, you must press the TOGA
button AND the A/P disc button on the yoke to disconnect the autopilot. - ANSWER False.
Prior to using SPEED, V/S or Pitch mode to change altitude, what must first be done? -
ANSWER Selection of a new altitude with the ALT knob.
Pressing the ALT button on the FCP will: - ANSWER Provide instantaneous capture of
the pressure altitude existing in the FCC at the time of engagement.
What will happen if the primary trim switches on the yoke are activated when the A/P
is engaged? - ANSWER The A/P will disconnect.
,When the A/P transfer switch is selected to the copilot's side, _______________________. -
ANSWER The copilot's flight computer commands both flight directors.
What is the range where the APU starter cut-out will occur? - ANSWER 46% on the ground and
46-60% in flight.
What are the APU starter limits? - ANSWER Three attempts in a one hour period, with a
two minute waiting period between each attempt.
What will the APU automatic fire protection provide in flight? - ANSWER Automatic
shutdown of the APU, but not automatic discharge of the fire bottle.
Prior to APU start the minimum battery voltage should be_______________. - ANSWER 22 volts
on both batteries.
If the APU is rotating above ___% in flight or ____% on the ground the APU Electronic Control
Unit will inhibit start. - ANSWER 12/5.
Where does fuel to operate the APU come from? - ANSWER The left collector tank via a
dedicated APU fuel pump.
The maximum altitude for starting the APU is ________. It can be operated up to _________. -
ANSWER 37,000 feet/41,000 feet.
APU bleed air can be used in flight up to what altitude? - ANSWER 25,000 feet.
The APU can be used as a source of bleed air for the aircraft ice protection systems. -
ANSWER False.
, If the APU door is stuck open or its position is uncertain, what must be done? - ANSWER
Maintain a max airspeed of 220 knots or run the APU continuously.
The APU control system ensures that priority is given to ____________. - ANSWER Electrical
power.
APU bleed air is controlled by modulating the ____________. - ANSWER APU LCV.
When the Captain's NORM/EMER switch on the ACP is set to EMER, what happens? -
ANSWER Connects the Captain's headset to VHF COMM 1 and VHF NAV 1.
To make a cabin announcement on the PA system, what should you do? - ANSWER Press the PA
switchlight on the Interphone Control Unit after selecting the transmit switch on the ACP to the
PA position.
With a failure of the pilot's RTU, how can the VHF COMM and NAV frequencies be changed? -
ANSWER Either use the Backup Tuning Unit, or press the RTU inhibit switchlight for the pilot
RTU and use the 1/2 switch on the F/O RTU to change the frequency.
Which radio(s) are tuned with the Backup Tuning Unit? - ANSWER VHF Comm 1 and VHF Nav 1.
Depressing the RTU Inhibit switchlight _______________________. - ANSWER Enables
alternate cross side tuning of the radios of the failed RTU.
What does the AC ESS XFER switchlight do when selected? - ANSWER Transfers the AC
Essential Bus to AC BUS 2.
How can the DC Service bus be powered? - ANSWER From DC BUS 2 during normal DC
operation, or from the APU BAT DIR BUS through use of the DC service switch.
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