ATP Electronics Piper Archer Training Supplement page 55

21. What is the fuel capacity? How many gallons are unusable?
22. What grade fuel is to be used in the PA-28?
23. How many fuel pumps are on the aircraft?
24. When is the electric fuel pump to be used?
25. What are the various positions on the fuel selector control?
26. In the event of an electrical failure, what pilot actions are necessary to
ensure continued operation of the standby attitude indicator?
27. If the standby power button on the attitude indicator is not pressed
within one minute of electrical failure, what will happen?
28. How do you determine a standard rate turn on an aircraft with a G500
system?
29. In the event of an AHRS failure, which indications will no longer be
displayed on the PFD? Which indications will still be visible on the PFD?
30. Which approaches can be accomplished with an AHRS failure?
31. What instrument approaches are available with the PFD inoperative?
With the MFD inoperative? With a total PFD/MFD failure?
32. How long does the internal battery last when providing power to
the standby attitude indicator? With the loss of the ADC, which
lost instrument does not have a backup? What should you do to
compensate for the lack of information?
Oral Review • 51