Recurrent

Question 1

When required to land without delay at the nearest suitable area where safe approach and landing is reasonably assured, the flight manual will use what phrase

Answer 1

Land as soon as possible

Question 2

The engine out audio signal will be transmitted when the Ng drops below which of the following values?

Answer 2

55%

Question 3

In the event of an engine failure in flight the collective should be adjusted to maintain a rotor RPM not to exceed which speed?

Answer 3

107%

Question 4

What is the airspeed for minimum rate of descent in autorotation

Answer 4

55 KIAS

Question 5

If flameout occurs and automatic relight was unsuccessful, under what conditions may an engine restart be attempted in flight?

Answer 5

Time and altitude permit

Question 6

What is the airspeed and Nr combination that will allow the pilot maximum time to attempt an air restart?

Answer 6

85% Nr at 55 KIAS.

Question 7

In the event of an engine overspeed, which of the following should be accomplished first?

Answer 7

Throttle - Retard

Question 8

Which of the following are indications of an engine compressor stall?

Answer 8

PSI oscillations

Question 9

During the shutdown from an engine hot start, it is noted that the starter remains engaged until the MGT reaches what temperature?

Answer 9

150 degrees C

Question 10

In the event of a Main Driveshaft failure, the engine overspeed system will activate at?

Answer 10

118.5% NP

Question 11

The ENGINE OVSPD caution light will illuminate for which of the following conditions?

Answer 11

Np greater than 102.1% for 2.5 seconds.

Question 12

What is the procedure for a FADEC FAIL message during start?

Answer 12

Close throttle immediately. Ensure starter is motoring engine until MGT stabilizes at normal temperatures.

Question 13

In the event of a FADEC failure in flight, the Nr/Np should be maintained between:

Answer 13

95 to 100%

Question 14

The RPM message will illuminate without audio under which of the following condition?

Answer 14

Nr above 107%

Question 15

If cabin smoke or fumes are experienced in flight, which of the following procedures are to be accomplished?

Answer 15

Side windows - Open

Question 16

In the event of a hydraulic system failure, the airspeed should be established:

Answer 16

70 - 100 KIAS.

Question 17

Which of the following indications are representative of a generator failure?

Answer 17

GEN FAIL message illuminated, AMPS – 0, Volts approx. 24

Question 18

Indications of an excessive electrical load occur and after performing the appropriate procedure smoke/fumes do not decrease. When using Jet B fuel, prior to battery depletion, you should reduce altitude to below:

Answer 18

9000 feet pressure altitude (Hp).

Question 19

Assuming 80% charge, how long will the optional 28-amp hr. battery operate the left fuel boost pump and left fuel transfer pump with the generator and battery OFF?

Answer 19

2.5 hours

Question 20

If the BATTERY HOT message illuminates in conjunction with the BATTERY RLY message, the procedure is to:

Answer 20

Select BATT switch - OFF Select GEN switch - OFF (if conditions permit)

Question 21

Which of the following conditions will cause the illumination of the BATTERY RLY caution message?

Answer 21

Battery relay remains energized when battery switch is OFF. Battery is still connected to DC BUS.

Question 22

The XMSN OIL PRESS message will be displayed when the pressure switch detects a decreasing oil pressure at or below:

Answer 22

30 PSI

Question 23

What is the procedure if any of the following caution messages appear? MGT EXCEED, NG EXCEED, NP EXCEED, or Q EXCEED.

Answer 23

Reduce engine power if possible; maintenance action required prior to the next flight.

Question 24

The FUEL LOW message will illuminate when the fuel remaining in the aft fuel cell is at which of the following?

Answer 24

100 +/- 10 lbs.

Question 25

With both fuel transfer pumps inoperative, the unusable fuel may be as high as ___________, so you should do what?

Answer 25

151 lbs.; land as soon as practical.

Question 26

What are the main components of the FADEC system?

Answer 26

Electronic Engine Control (EEC), Fuel Metering Unit (FMU), and Fuel Pump Power Unit (FPPU).

Question 27

True or False? During flight with the throttle in FLY or Full Open position, the FADEC has complete control over the engine operation.

Answer 27

True. The FADEC maintains the Main Rotor speed (Nr) within limits.

Question 28

At what point will the FADEC EEC select between the 28 VDC bus and the FPPU for its primary power source?

Answer 28

Once the engine reaches minimum run speed and higher.

Question 29

If the FADEC MAINT advisory is displayed during the power-up self-test, this indicates:

Answer 29

The FADEC system requires maintenance.

Question 30

Under which of the following conditions would the FADEC cutoff fuel to abort the start?

Answer 30

Start MGT reaches 912 °C at pressure altitudes greater than 10,000 ft. and residual MGT is greater than 82.2 °C at initiation of start.

Question 31

What happens when all drive power is removed from the stepper motor on the FMU?

Answer 31

The fuel is fixed equal to the last command position.

Question 32

What is the forward tank fuel capacity?

Answer 32

37.6 U.S. gal.

Question 33

What is the total usable fuel capacity without the auxiliary fuel tank installed?

Answer 33

127.8 U.S. gal

Question 34

What is the capacity of the auxiliary fuel tank?

Answer 34

19 US gal

Question 35

In the event the battery switch is selected off during aircraft operation, what circuit allows operation of the left fuel transfer and left fuel boost pumps?

Answer 35

With the FUEL VALVE switch on, battery voltage is supplied by the battery through the alternate circuit.

Question 36

Fuel quantity is measured by:

Answer 36

3 probes in the fuel tanks used by the fuel signal conditioner to calculate fuel weight.

Question 37

In the event the signal conditioner should complete a power up BIT check and detects a failure, or if an error is found in the probe signal, what will be the reading on the Fuel Quantity gauge?

Answer 37

The EIS fuel quantity indication will be blanked.

Question 38

How can the fuel quantity in the forward tank be checked?

Answer 38

By pressing the FUEL QTY FWD TANK button.

Question 39

The hydraulic system provides pressurized fluid to operate which of the following?

Answer 39

Cyclic, collective, and tail rotor flight control servo actuators.

Question 40

The solenoid valve is controlled by a HYD SYS switch which is:

Answer 40

Located on the overhead console.

Question 41

Both hydraulic filters have a filter indicator which activates when the differential pressure across the filter is:

Answer 41

70 +/- 10 PSI.

Question 42

The hydraulic pressure filter bypass valve will open when the differential pressures reach:

Answer 42

None of the answers are correct; the pressure filter does not have a bypass valve.

Question 43

The relief valve is incorporated into the hydraulic system between the pressure filter and the solenoid valve. It is designed to open when the pressure exceeds which of the following value:

Answer 43

1225 +/- 150 PSI

Question 44

To prevent inaccurate indications of the hydraulic filter clogging, the filter indicator will stop working when the hydraulic fluid is below what temperature?

Answer 44

35 °F (2 °C).

Question 45

The HYDRAULIC SYS CAS caution message will be displayed when the hydraulic pressure decreases below:

Answer 45

650 PSI

Question 46

What is the maximum allowable cabin deck loading for cargo?

Answer 46

75 lbs. per sq. ft.

Question 47

With the crew doors removed, how is the indicated altitude affected.

Answer 47

It may be as much as 100 ft. lower than actual altitude.

Question 48

What is the maximum allowable approved GW with jettisonable external load for takeoff and landing?

Answer 48

6000 lbs

Question 49

What is the Vne at takeoff power (93.5 to 100% torque?

Answer 49

100 KIAS

Question 50

What is the maximum operating altitude?

Answer 50

20,000 ft Hd

Question 51

What is the maximum rate of climb authorized?

Answer 51

2,000 ft/min

Question 52

If you are planning a slope landing that will require you to have a nose down attitude, what is the maximum allowable angle permitted?

Answer 52

5 degrees

Question 53

What is the maximum allowable sea level ambient air temperature for operation?

Answer 53

51.7 °C (125 °F).

Question 54

What is the maximum allowable continuous amp meter reading up to 10,000 ft. pressure altitude when starter generator 206-062-200-113 is installed?

Answer 54

180 amps

Question 55

What is the maximum allowable starter activation time when using a GPU?

Answer 55

40 seconds.

Question 56

What is the maximum continuous allowable operation for the gas producer (Ng)?

Answer 56

105%

Question 57

What is the maximum continuous Power Turbine (Np) limitation?

Answer 57

100%

Question 58

What is the maximum continuous MGT limitation?

Answer 58

727 degrees C

Question 59

What is the maximum continuous torque limitation?

Answer 59

93.5%

Question 60

What is the minimum allowable fuel pressure limitation?

Answer 60

8 PSI

Question 61

What is the minimum allowable engine oil pressure below 79% Ng

Answer 61

50 PSI

Question 62

What is the maximum allowable transmission oil pressure?

Answer 62

50 PSI

Question 63

What is the maximum allowable transmission oil temperature for continuous operation?

Answer 63

110 °C

Question 64

For cold weather operations where the helicopter and battery have been cold soaked, battery starts have been demonstrated with the standard 17 amp-hour battery to temperatures of:

Answer 64

-22 °F (-30 °C)

Question 65

Engine oil temperature should be closely monitored when hovering with a tailwind greater than 10 knots at what OAT?

Answer 65

37.8 °C (100 °F)

Question 66

Failure to remove the rotor tie-downs before engine starting may result in:

Answer 66

Severe damage and possible injury.

Question 67

When draining the fuel sump, contaminants may not be properly drained under which of the following conditions?

Answer 67

The helicopter is not parked on a level surface.

Question 68

What is the minimum voltage for engine start?

Answer 68

24

Question 69

Starter latching is disabled if the throttle is positioned to IDLE for more than:

Answer 69

60 seconds

Question 70

When below 10,000 ft. pressure altitude it is recommended that the MGT be below which of the following values before attempting an engine start?

Answer 70

150 °C.

Question 71

After the START switch is momentarily activated, which lights should be illuminated?

Answer 71

The START and AUTO RELIGHT CAS message.

Question 72

The start must be aborted if the main rotor is not turning by:

Answer 72

25% Ng.

Question 73

The normal idle speed is which of the following?

Answer 73

63% +/- 1%.

Question 74

To conduct a dry motoring run, close the throttle and engage the start switch for:

Answer 74

15 seconds.

Question 75

During engine run-up the throttle is increased smoothly to the FLY detent position while maintaining torque less than:

Answer 75

40%.

Question 76

RPM warning light and audio should be extinguished at:

Answer 76

95% Nr

Question 77

The hydraulic check is accomplished when Nr/Np reaches ______ RPM?

Answer 77

100.

Question 78

The recommended torque setting for takeoff is:

Answer 78

5% above hover power.

Question 79

At high power and high airspeed, cyclic only accelerations and maneuvering may:

Answer 79

Increase MGT and torque without collective input.

Question 80

When the ENG ANTI-ICE switch is selected ON the:

Answer 80

MGT will increase.

Question 81

During descent and landing, an independent increase of Nr may occur:

Answer 81

When large collective reductions are made at heavy GW

Question 82

Positioning the throttle out of CUT-OFF during Ng spool down may:

Answer 82

Cause a post engine shutdown fire.

Question 83

How are the rotors slowed down during coastdown?

Answer 83

The rotor brake.

Question 84

Certain actions, such as installing main rotor blade tiedowns, are required if:

Answer 84

Thunderstorms are forecasted.

Question 85

True or False? Power assurance check may not be performed in a hover prior to takeoff.

Answer 85

False, it may, depending on ambient conditions and gross weight.

Question 86

Which of the following switches should be selected off in order to properly perform the power assurance check?

Answer 86

Engine anti-icing.

Question 87

If the helicopter configuration is invalid, what error message is displayed when performing an automatic power assurance check with the G1000H?

Answer 87

CHK LIMITS.

Question 88

As temperature increases above standard for an altitude, Hd will also.

Answer 88

Increase to values higher than Hp.

Question 89

The Height-Velocity Envelope diagrams:

Answer 89

Are valid only if gross weight does not exceed the limits of the Altitude vs. Gross Weight for Height Velocity Chart.

Question 90

What is important to note when referring to the Hover Ceiling chart?

Answer 90

Hover performance charts are based on 100% rotor RPM.

Question 91

Using the Rate of climb charts, the recommended best rate of climb airspeed is:

Answer 91

60 KIAS

Question 92

With any combination of the doors removed, the rate of climb data presented in the rate of climb charts should be reduced:

Answer 92

100 FPM.

Question 93

Given the following conditions, use the provided Power Assurance Chart to find the maximum allowable MGT. (6000 feet pressure altitude, 75% torque, OAT 15 °

Answer 93

712 °C

Question 94

Using the provided Density Altitude Chart, find the Density Altitude and True Airspeed for the following conditions. (OAT 10 °C, Pressure Altitude 9000 feet, 100 KCAS

Answer 94

10,500 feet Hp; 117 KTAS.

Question 95

For the following values, find the appropriate limiting envelope for an aircraft to landing safely following an engine failure. (OAT 20 °C, 4,000 feet pressure altitude, gross weight of 4,200 pound

Answer 95

Region B.

Question 96

Using the provided chart, determine the allowable gross weight for a Hover In Ground Effect. (Takeoff power, heater ON, anti-ice OFF, OAT 0 °C, pressure altitude of 6,000 feet

Answer 96

5,600 lbs.

Question 97

For the following conditions, use the rate of climb chart to the maximum rate of climb. (Maximum continuous power, Heater OFF, Anti-ice OFF, 4,000 lbs. gross weight, OAT 20 °C, pressure altitude 8,000)

Answer 97

1250 ft./min.

Question 98

During takeoff, how much horsepower will the Rolls-Royce 250-C47E/4 powerplant provide?

Answer 98

674

Question 99

The ENG ANTI-ICE switch, located on the overhead console, controls the engine anti-ice bleed air solenoid valve. In the event of a total electrical failure the system will:

Answer 99

Fail safe to ON.

Question 100

When the EEC has recorded an Np exceedence, the ENGINE OVSPD CAS message illuminates when Ng speeds reach ______ upon engine shutdown.

Answer 100

9.5%.

Question 101

What percent of air delivered to the first stage gas producer is required to burn fuel

Answer 101

20 to 25%.

Question 102

Which of the following is true regarding the Engine Oil gauge?

Answer 102

The engine oil pressure signal is provided by a transducer mounted on the forward right side of the engine gearbox.

Question 103

The engine oil system pressure must always be greater than torquemeter oil pressure and is regulated to a value of:

Answer 103

115-130 PSI.

Question 104

What is the approximate capacity of the engine oil tank?

Answer 104

6 qt

Question 105

How many engine chip detectors are associated with the ENGINE CHIP caution message?

Answer 105

2

Question 106

Transmission oil level may be determined by:

Answer 106

An oil level sight glass located on the right side of the transmission lower case.

Question 107

What is the transmission oil pump output per minute?

Answer 107

6.0 to 6.7 gal.

Question 108

What is the approximate pressure of the transmission oil regulator valve?

Answer 108

52 PSI.

Question 109

When is the impending bypass indicator on the end of the filter housing in the transmission oil system designed to extend? At:

Answer 109

14 +/- 2 PSI.

Question 110

At what temperature does the thermostatic valve begin to direct flow to the oil cooler?

Answer 110

Above 66 °C (150 °F).

Question 111

The XMSN OIL TEMP CAS warning message will be displayed when the transmission oil temperature is at or above:

Answer 111

110 °C.

Question 112

Which of the following are included in the empty weight of the helicopter?

Answer 112

Optional equipment kits.

Question 113

Under which of the following conditions is the helicopter empty weight center of gravity chart not valid?

Answer 113

If the aircraft is configured with a non-standard seating arrangement.

Question 114

Which of the following describes the structural design limit for Cabin floor loading?

Answer 114

75 lbs. per sq. ft.

Question 115

Which of the following are true regarding baggage compartment loading requirements?

Answer 115

If the load is not secured, the center of gravity must be computed with load in most adverse position