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48 Cards in this Set

  • Front
  • Back
RR 24. What occurs if an EEC and ELC completely fail?
A. Engine shuts down
B. Engine continues to operate via hydro-mechanical controls with no overboost or
overspeed protection
C. Engine ELC channel fails, but overboost protection continues via the EEC channel
B. Engine continues to operate via hydro-mechanical controls with no overboost or
overspeed protection
RR 25. What does the Fuel Control switch RICH position accomplish?
A. Initially schedules additional fuel for start
B. Closes engine and spar fuel valves
C. Terminates ignition
A. Initially schedules additional fuel for start
767 26. When derate climb power (CLB 1 or CLB 2) is used, when does it return to maximum climb
power (CLB)?
A. Gradually, starting at 10,000 ft and returns to maximum climb power at 12,000 ft
B. Gradually, starting at 3000 ft and returns to maximum climb power at 10,000 ft
C. Only when maximum climb power is manually selected
A. Gradually, starting at 10,000 ft and returns to maximum climb power at 12,000 ft
767 27. What does the ENGINE CONTROLS EICAS message indicate on the B767?
A. Faults are detected in the engine control system
B. Thrust lever operation normal
C. HPSOV valve not in commanded position
A. Faults are detected in the engine control system
28. When does the auto relight ignition feature operate?
A. When RICH position is selected on Fuel Control switches
B. When N2 drops below idle speed
C. When N2 is above idle speed
B. When N2 drops below idle speed
767 29. What is the normal starter duty cycle?
A. 5 minutes on, followed by 1/2 minute off per minute on
B. 2 minutes continuous operation, then run down to zero N2
C. 5 minutes on, followed by 10 minutes off per minute on
A. 5 minutes on, followed by 1/2 minute off per minute on
30. What does the APU RUN light indicate?
A. APU generator is running
B. APU selector is ON
C. APU is at operating speed
C. APU is at operating speed
31. What can cause the APU FUEL VAL light to illuminate?
A. One of the two APU fire loops failed
B. APU fuel valve NOT in commanded position
C. Aircraft above 17,000 feet pressure altitude
B. APU fuel valve NOT in commanded position
32. What is the minimum power required to start the APU?
A. APU battery only
B. APU battery and main battery
C. APU battery and ground handling busses
B. APU battery and main battery
33. What is the maximum operating altitude for the APU?
A. 20,000 ft
B. 17,000 ft
C. Service ceiling
C. Service ceiling
34. What occurs when the APU selector is moved to the ON position?
A. Opens the APU fuel valve and inlet door, activates AC or DC fuel pump
B. Initiates automatic start sequence
C. RUN light and EICAS message illuminates to alert crew to select START position
A. Opens the APU fuel valve and inlet door, activates AC or DC fuel pump
35. What occurs when the APU selector is momentarily positioned to START?
A. Automatically opens isolation valve
B. Closes APU fuel valve
C. Initiates automatic start sequence
C. Initiates automatic start sequence
36. What does the APU FAULT light indicate?
A. APU automatic fault shutdown
B. APU shuts down after a 5-minute cool down period
C. APU is running in degraded mode
A. APU automatic fault shutdown
37. Bleed air is available up to 17,000 ft. True or False?
A. True
B. False
A. True
38. If the APU selector is inadvertently moved to OFF and the RUN light is still illuminated,
momentarily moving the APU selector to START cancels the shutdown signal. True or False?
A. True
B. False
A. True
39. What affect does the Battery switch selected to OFF have on the APU if running?
A. None on the ground. In flight, the APU shuts down with a cool down if required
B. In flight, none. On the ground, causes the APU to shut down with a cool down if required
C. None, APU continues to operate on the ground or in flight
B. In flight, none. On the ground, causes the APU to shut down with a cool down if required
40. What are the electrical requirements for starting the APU?
A. APU battery
B. Both the APU battery and the aircraft main battery
C. Power to the left DC bus
B. Both the APU battery and the aircraft main battery
41. When does the APU shut down immediately?
A. When an APU FAULT light illuminates
B. DC fuel pump fails
C. Left FWD fuel boost pump fails
A. When an APU FAULT light illuminates
42. How can the APU shutdown be discontinued if the APU selector was inadvertently moved to
OFF, but the RUN is still illuminated?
A. APU selector OFF, then back ON
B. APU selector to ON
C. Momentarily moving the selector to START cancels the shutdown signal
C. Momentarily moving the selector to START cancels the shutdown signal
43. What occurs if the APU FUEL VAL EICAS message is displayed?
A. APU fuel valve is not in signaled position
B. APU fuel valve is in signaled position
C. APU FUEL VAL EICAS message only occurs in flight
A. APU fuel valve is not in signaled position
44. How many APU start attempts are allowed in a 60-minute period?
A. 1
B. 2
C. 3
C. 3
PW 22. What does the ENG LIMIT PROT light and EICAS message indicate?
A. Overheat
B. Automatic thrust limit protection is not available
C. EGT exceedence
B. Automatic thrust limit protection is not available
PW 23. Which parameters are protected by the EEC?
A. EPR, N1, N2, and EGT
B. EPR, N1, and N2
C. EPR, N1, and EGT
B. EPR, N1, and N2
1. What occurs if EGT exceeds the red line limit?
A. Pointer will change to amber
B. Pointer remains white for takeoff
C. Maximum exceedence value attained will be displayed
C. Maximum exceedence value attained will be displayed
2. What value is represented by the end of the command sector on the EPR (757) or N1 (767)
indicator?
A. Actual thrust value
B. EPR (757) or N1 (767) commanded by thrust lever position
C. Maximum rated thrust for takeoff
B. EPR (757) or N1 (767) commanded by thrust lever position
3. What system is controlled by the thrust management computer?

A. Auto throttles
B. Actual N1 indication
C. Actual N3 indication
A. Auto throttles
4. What is calculated by the thrust management computer?
A. Maximum EPR (757) or N1 (767) reference
B. Fuel on command bug
C. In flight start envelope
A. Maximum EPR (757) or N1 (767) reference
5. What occurs if one EICAS CRT fails?
A. Engine parameters are displayed in Compacted Mode
B. Status messages are viewable in flight
C. Only EPR/N1 (757) or N1 (767) and EGT indications are available for the duration of
the flight
A. Engine parameters are displayed in Compacted Mode
6. Do autothrottles respond to manually set EPR (757) or N1 (767) reference values by pulling
the Manual Thrust Reference selectors?
A. Yes
B. No
B. No
7. What does D-TO indicate on EICAS?
A. Assumed temperature derated takeoff thrust
B. Derate 1
C. Max
A. Assumed temperature derated takeoff thrust
8. What is the maximum Assumed Thrust reduction to takeoff thrust allowed by the thrust
management computer?
A. 25% reduction from Max, Derate 1, and Derate 2, and cruise thrust, whichever is the
greater thrust value
B. 25% reduction from maximum takeoff thrust or selected climb thrust, whichever is the
greater thrust value
C. 12% reduction from maximum takeoff thrust or selected continuous thrust, whichever is
the greater thrust value
B. 25% reduction from maximum takeoff thrust or selected climb thrust, whichever is the
greater thrust value
9. What does TO 1 indicate on EICAS?
A. Max
B. Takeoff thrust one, climb one preselected
C. Assumed off Derate 1
B. Takeoff thrust one, climb one preselected
10. What does TO 2 indicate on EICAS?
A. Max
B. Assumed off Derate 2
C. Takeoff thrust two, climb two preselected
C. Takeoff thrust two, climb two preselected
11. What does D-TO 2 indicate on EICAS?
A. Derate 2
B. Assumed temperature derated takeoff thrust two, climb two preselected
C. Climb 2
B. Assumed temperature derated takeoff thrust two, climb two preselected
12. What does the L or R ENG STARTER EICAS message indicate?
A. Engine starter overheat
B. Engine starter valve is not in the commanded position
C. Engine starter low oil pressure and high oil temperature
B. Engine starter valve is not in the commanded position
13. What does the L or R STARTER CUTOUT EICAS message indicate?
A. Indicates start valve operates normally by automatically moving to AUTO at 50% N2 or
N3 (RR)
B. No ignition during start
C. Engine starter valve is not in the commanded position
C. Engine starter valve is not in the commanded position
14. During engine start, the red Maximum Start EGT limit radial remains in view _____________.,
A. during and after engine start
B. until the EGT reaches 900 degrees kelvin
C. until the engine start is completed
C. until the engine start is completed
15. The assumed temperature can be entered manually on the ___________.
A. TAKEOFF REF page on the FMC only
B. TAKEOFF REF page on the FMC or selected with the Assumed Temperature selector
on the TMSP
C. ACARS ASSUMED THRUST page
B. TAKEOFF REF page on the FMC or selected with the Assumed Temperature selector
on the TMSP
16. What color is the REV annunciation on EICAS when the thrust reverser is unlocked and
in transit?
A. Green
B. Amber
C. Magenta
B. Amber
17. What malfunction has occurred if the R ENG OIL PRESS light is illuminated, the R ENG OIL
PRESS EICAS message is displayed, and oil pressure indicates normal for the right engine?
A. Low oil pressure
B. High oil pressure
C. Oil pressure switch fault
C. Oil pressure switch fault
18. Prior to engine start, the SPAR VALVE light for the left engine is illuminated. What is the
system condition?
A. Fuel spar valve is not in commanded position
B. Engine fuel valve is not in commanded position
C. Fuel spar valve is in the commanded position
A. Fuel spar valve is not in commanded position
PW 19. What does the green TAI bug on the N1 parameter indicate?
A. Wing anti-ice on
B. TAT probe heat inoperative
C. Engine anti-ice is on and only one engine bleed source is available
C. Engine anti-ice is on and only one engine bleed source is available
PW 20. With only one engine bleed source available, what does the amber TAI above the N1
parameter indicate?
A. N1 is below the reference level
B. N1 is above the reference level
C. N2 is below the reference level
A. N1 is below the reference level
PW 20. With only one engine bleed source available, what does the amber TAI above the N1
parameter indicate?
A. N1 is below the reference level
B. N1 is above the reference level
C. N2 is below the reference level
B. N1 is above the reference level
PW 21. What does the ENG LIMIT PROT light and EICAS message indicate?
A. Overheat
B. EGT exceedence
C. EEC using N2 as control parameter
C. EEC using N2 as control parameter
45. Which of the following describes the START position of the APU selector?
A. Momentary, spring-loaded to ON
B. Latched, remains in START until moved
C. Magnetically held until starter cutout
A. Momentary, spring-loaded to ON
PW 22. What does the ENG LIMIT PROT light and EICAS message indicate?
A. Overheat
B. Automatic thrust limit protection is not available
C. EGT exceedence
B. Automatic thrust limit protection is not available
PW 23. Which parameters are protected by the EEC?
A. EPR, N1, N2, and EGT
B. EPR, N1, and N2
C. EPR, N1, and EGT
B. EPR, N1, and N2