Ae2100D3 Engine Run

Front 1

What is the minimum number of personnel required for an engine runup?

Back 1

3

Front 2

What kind of continual contact will all crew members maintain during engine runup?

Back 2

Voice (audio)

Front 3

True or False: OMP must be loaded in order to run up engines?

Back 3

False

Front 4

What is the maximum MGT at which engine start is allowed?

Back 4

175 degrees C

Front 5

Any time another aircraft (vehicle) passes or stops in front of an aircraft with engines running, what must the engine power levers be reduced to?

Back 5

Ground Idle

Front 6

How long (in seconds) must engine oil pressure indicate after Ng rotation?

Back 6

15

Front 7

What is the maximum weight difference between main fuel tanks allowed for engine operation?

Back 7

1000 lbs

Front 8

What is the engine starter duty cycle?

Back 8

70 seconds, 60 seconds off, for a total of 5 cycles. Then a 20 minute cooldown

Front 9

True or False: The prop must be in the feather position prior to engine start?

Back 9

False

Front 10

Engine power is limited to ground idle when the oil temp is less than ________ degrees C?

Back 10

0

Front 11

Abort the start if the prop does not begin to rotate within ____ minute(s) after Ng speed reaches 72%

Back 11

2

Front 12

During engine start, if bleed air pressure drops below _____ psi, discontinue start.

Back 12

22

Front 13

Avoid stabilized operations between _____% and ____% Np RPM

Back 13

52-68 and 75-85

Front 14

What horsepower setting must be maintained when operating a single engine?

Back 14

50 HP

Front 15

How long should the engine start switch be held in the start position?

Back 15

until the start box appears on the HDD

Front 16

limit horsepower to ____HP when oil temps are below 45 degrees C

Back 16

1000

Front 17

Maximum MGT during engine start is ____ degrees C for ____ seconds

Back 17

807, 3

Front 18

Flaps must be set to ____% if engines will be operated above ground idle

Back 18

50

Front 19

Each engine should be run a minimum of ____ minutes at _____ before engine shutdown

Back 19

2, Low speed ground idle

Front 20

True or False: Props are required to be in feather after engine shutdown?

Back 20

True

Front 21

True or False: Do not motor an engine when a tailpipe fire exists on engine shutdown?

Back 21

True

Front 22

True or False: Do not operate any engine above flight idle without operating opposite engine at ground idle?

Back 22

False

Front 23

During engine start, if there is no positive indication of hydraulic pressure within ____ seconds after prop rotation, discontinue start

Back 23

25 seconds

Front 24

Pressurization mode select switch should be in the ____ position for an engine run

Back 24

No Press

Front 25

Who can call a "Stop Start" during an engine start?

Back 25

Both A and B mechanics

Front 26

The auxiliary hydraulic system pressure should indicate ____ psi prior to engine start

Back 26

3000

Front 27

During engine operation, normal generator voltage is ____ volts

Back 27

108-117

Front 28

To ensure brakes are set, ____________________?

Back 28

lightly depress the tops of the rudder pedals

Front 29

With the engine operating, normal oil temp is ____ Degrees C

Back 29

60-85

Front 30

With the engine operating, normal PGB oil pressure is ____ psi

Back 30

170-210

Front 31

With the engine operating at Low speed ground idle (feathered), minimum PGB oil pressure is ____ PSI

Back 31

15

Front 32

Engine starter sequence lights turn of at approx. ____ % Ng

Back 32

65

Front 33

Max continuous HP is ____+ or -____

Back 33

4691, 74

Front 34

While operating the engine at low speed ground idle, Ng RPM will be a minimum of ____ %

Back 34

72

Front 35

When operating an engine at max reverse, Np RPM should maintain ____ %

Back 35

99-101

Front 36

While operating an engine at max continuous or take off, Np RPM is ____ %

Back 36

99-101

Front 37

An engine operating at low speed ground idle (feathered or "hotel" mode), Np RPM is ____ %

Back 37

20-30

Front 38

Normal utility hydraulic pressure with engines operating for # 1 and 2 is ____ PSI

Back 38

2900-3200

Front 39

Utility and Booster accumulator preloaded pressure is ____ PSI

Back 39

1500 (+ or - 100)

Front 40

Normal brake accumulator preloaded pressure is _____ PSI

Back 40

1500 (+ or - 100)

Front 41

Emergency brake accumulator preloaded pressure is ____ PSI

Back 41

1000 (+ or - 100)

Front 42

True or False: Turn off the engine hydraulic pump switches after final engine shutdown?

Back 42

False

Front 43

The engine starter must be allowed to cool for ____ if the starter duty cycle is reached?

Back 43

20 minutes

Front 44

ACAWS warnings and digital readout warnings appear on the HDD screens in what color?

Back 44

Red

Front 45

ACAWS cautions and digital readout cautions appear on the HDD screens in what color?

Back 45

Yellow

Front 46

ACAWS advisories appear on the HDD screens in what color?

Back 46

White

Front 47

ACAWS messages appearing on the HDD screens that require immediate corrective or compensatory actions are _______ and display in ____ (color)

Back 47

Warnings, RED

Front 48

ACAWS messages appearing on the HDD screens that require corrective or compensatory actions are _______ and display in ____ (color)

Back 48

Cautions, Yellow

Front 49

Maximum MGT with the power levers at Takeoff is less than ____ degrees C

Back 49

852

Front 50

True or False: When operating the aircraft on slippery surfaces, deviations must be made for engine and prop check procedures?

Back 50

True

Front 51

True or False: Wind speed and direction are required to be checked only before engine start?

Back 51

False

Front 52

Max MGT with power levers at low speed ground idle or ground idle is less than ____ degrees C

Back 52

600

Front 53

Np RPM with an engine operating at low speed ground idle is ____ %

Back 53

71-75

Front 54

After engine start and at any power lever setting, P/S E PSI will be between ____.

Back 54

40-90

Front 55

With PLA at max reverse or at flight idle and above, Ng RPM will be below ___ %

Back 55

102

Front 56

The maximum amount of time allowed for an engine to run with PLA at takeoff is ____

Back 56

5 minutes

Front 57

True or False: With a wind speed of 15 knots and a direction of somewhere between 0-45 degrees relative to the nose of the aircraft, engine operation is not allowed?

Back 57

False

Front 58

True or False: During engine run operations, the person in charge (Mech A), is the only person that needs to understand the checklist and referenced publications?

Back 58

False

Front 59

True or False: If voice contact is lost between the ground observer and the other runup crew members, the engine run may continue as long as visual contact is maintained

Back 59

False

Front 60

True or False: The inlet, visible compressor stages, and exhaust area must be checked for foreign objects and damage prior to engine start

Back 60

True

Front 61

True or False: As long as there are no indications of any problems with the aircraft's fire extinguishing systems, an external fire extinguisher is optional?

Back 61

False

Front 62

Minimum battery voltage is ____ voltage

Back 62

22

Front 63

On the Pressurization panel, LDG/CONST ALT will be _________.

Back 63

Set to field elevation + 1000 ft

Front 64

Normal engine start sequence is ____.

Back 64

3,4,2,1

Front 65

True or False: Unless a specific emergency procedure dictates other action, any person in the flight deck may place the engine start switch to STOP if " STOP START" is called?

Back 65

False

Front 66

True or False: At all times during an engine run, Mech A will be prepared to steer the aircraft and Mech B will be prepared to set the power levers?

Back 66

False

Front 67

What systems must be operational prior to engine start?

Back 67

electrical, hydraulic, fuel, fire extinguisher, bleed air, ACAWS

Front 68

True or False: The area around the aircraft needs to be checked for potential FOD hazards prior to engine start?

Back 68

True

Front 69

True or False: Before an aircraft exit door is opened during or following an engine run, a window in the flight station should be opened to confirm the aircraft isn't pressurized?

Back 69

True

Front 70

What is the correct procedure immediately following an automatic engine shutdown for no light off, stagnant start, or flameout?

Back 70

Place the engine start switch to stop and motor the engine for 30 seconds after Ng decreases to 0%

Front 71

True or False: Do not start an engine with an inoperative suction boost pump?

Back 71

True

Front 72

When should the fuel panel be monitored?

Back 72

Throughout engine operation

Front 73

What indicates a start sequence has been initiated by the FADEC?

Back 73

A white box appears around the engine display

Front 74

When are the suction boost pump switches turned off?

Back 74

After the last engine is shutdown and Np has stopped

Front 75

True or False: Radio ground control frequency shall be monitored at all timed during an engine run?

Back 75

True

Front 76

After the crew briefing, personnel are not allowed to enter or exit the aircraft without ______.

Back 76

permission from the engine run supervisor

Front 77

True or False: The parking brake is not required to be set if only one engine is being run and it does not go above ground idle?

Back 77

False

Front 78

True or False: Aircraft forms must be checked prior to engine start?

Back 78

True