TTR

Question 1

The maximum speed not to be exceeded during any operation is:

a. 150 KIAS

b. 175 KIAS

c. 134 KIAS

Answer 1

b. 175 KIAS

Question 2

The maximum weight approved for the start of take off roll is:

a. 8035 Lbs

b. 8000 Lbs

c. 7800 Lbs

Answer 2

b. 8000 Lbs

Question 3

The maximum turbulent air penetration speed recommended is:

a. 134 KIAS

b. 150 KIAS

c. 175 KIAS

Answer 3

b. 150 KIAS

Question 4

The maximum speed at which the flaps may be extended beyond 20 degrees is:

a. 125 KIAS

b. 175 KIAS

c. 150 KIAS

Answer 4

a. 125 KIAS

Question 5

The maximum maneuvering speed is:

a. 150 KIAS

b. 125 KIAS

c. 133 KIAS

Answer 5

a. 150 KIAS

Question 6

The speed which results in the greatest gain in altitude at sea level in a given time is:

a. 125 KIAS

b. 106 KIAS

c. 103 KIAS

Answer 6

b. 106 KIAS

Question 7

Under maximum takeoff power condition at sea level, the maximum permissible engine rotation speed is:

a. 101.6% with temperature adjustment below 30°C

b. 102.6% without temperature adjustment

c. 101.6% without temperature adjustment

Answer 7

a. 101.6% with temperature adjustment below 30°C

Question 8

Under maximum continuous power conditions, the maximum permissible ITT is:

a. 740°C

b. 850°C

c. 805°C

Answer 8

c. 805°C

Question 9

During starting, the maximum permissible ITT is:

a. 685°C for 1 second

b. 1090°C for 1 second

c. 805°C for 1 second

Answer 9

b. 1090°C for 1 second

Question 10

At reverse thrust power settings, the maximum permissible gas generator speed is:

a. 101.6% for 2 seconds

b. 102.6% for 2 minutes

c. 101.6% for 2 minutes

Answer 10

c. 101.6% for 2 minutes

Question 11

The maximum shaft horsepower allowable is:

a. 600 SHP temperature and altitude controlled

b. 600 SHP

c. 600 SHP temperature controlled

Answer 11

a. 600 SHP temperature and altitude controlled

Question 12

The propeller rpm at takeoff is:

a. 1900 rpm

b. 1825 rpm

c. 2090 rpm

Answer 12

a. 1900 rpm

Question 13

The specific power loading is:

a. 28.6 Lbs/Sq.ft

b. 13.3 Lbs/SHP

c. 28.6 Lbs/SHP

Answer 13

b. 13.3 Lbs/SHP

Question 14

The standard empty weight is:

a. 3810 Lbs

b. 4185 Lbs

c. 4190 Lbs

Answer 14

a. 3810 Lbs

Question 15

The maximum take off power under normal operations is limited to:

a. 3 minutes

b. 5 minutes

c. 2 minutes

Answer 15

b. 5 minutes

Question 16

The limitations on the starter operating times using airplane battery is:

a. 30 seconds ON, 60 seconds OFF, with a maximum of 3 attempted starts

b. 30 seconds ON 1 minute OFF, 30 seconds ON 1 minute OFF, 30 seconds ON 30 minutes OFF

c. 30 seconds ON 1 minute OFF, 30 seconds ON 1 minute OFF, 2 minutes OFF

Answer 16

b. 30 seconds ON 1 minute off, 30 seconds ON 1 minute OFF, 30 seconds ON 30 minutes OFF

Question 17

During starting, if ITT approaches the limitation you would:

a. Close and open the throttle to stabilize LTT

b. Select fuel lever OFF, ignition switch NORMAL, and then Motor engine for adequate time

c. Select fuel lever OFF, and then Motor engine for adequate time

Answer 17

b. Select fuel lever OFF, ignition switch NORMAL, and then Motor engine for adequate time

Question 18

To clear an engine of internally trapped fuel and vapor you would:

a. Select fuel lever ON, power lever IDLE, boost pump switches ON, and select start for desired duration, then move to OFF.

b. Allow 5 minutes for self purging with fuel lever OFF before attempting a further start

c. Select fuel lever OFF, power lever IDLE, boost pump switches ON, and select start for desired duration, then move to OFF.

Answer 18

c. Select fuel lever OFF, power lever IDLE, boost pump switches ON, and select start for desired duration, then move to OFF.

Question 19

During engine starting the minimum engine speed to obtain a satisfactory light up is:

a. 15% Ng

b. 12% Ng

c. 10% Ng

Answer 19

b. 12% Ng

Question 20

After starting an engine the minimum oil temperature for acceleration is:

a. 0°C

b. Minus 40°C

c. 10°C

Answer 20

b. Minus 40°C

Question 21

To carry out an overspeed governor check, you would set power lever to give a certain propeller speed and then select PROP. O./SPEED TEST switch as appropriate. The propeller speed selected is:

a. 1850 rpm

b. 1750 +/- 60 rpm

c. 1850 +/- 60 rpm

Answer 21

b. 1750 +/- 60 rpm

Question 21

If the engine oil pressure falls below 65 psi at 72% gas generator rpm or above you would:

a. Continue the flight with power on the engine below 72% rpm

b. Not be concerned

c. Continue the flight with power on the affected engine 72% - 85% rpm

Answer 21

c. Continue the flight with power on the affected engine 72% - 85% rpm

Question 22

If a gas generator speed in excess of 101.6% occur you would:

a. Reduce the gas generator speed to a safer figure

b. Shut down the engine, noting maximum rpm and duration of this rpm and record in technical log

c. Reduce speed to a safe figure, note maximum rpm and duration of this rpm and record

Answer 22

c. Reduce speed to a safe figure, note maximum rpm and duration of this rpm and record

Question 23

In order to achieve reverse pitch on the propellers you would:

a. Select reverse pitch on the propeller controls

b. Operate the propeller controls by pushing upward through the gate and continuing rearward

c. Operate the power lever rearward into BETA range

Answer 23

c. Operate the power lever rearward into BETA range

Question 24

The selection of ignition switch to NORMAL should be limited to: a. 5 minutes b. 46% Ng max c. Does not have limitations

Answer 24

b. 46% Ng max

Question 25

Engine intake inertial separator is provided in order to: a. Give the pilot some measure of control over power plant and oil temperature b. Cater for tropical and subtropical climates c. Prevent the entry of snow, rain and dust into the compressor inlet duct by diverting the particles

Answer 25

c. Prevent the entry of snow, rain and dust into the compressor inlet duct by diverting the particles

Question 26

If starting on the ground you are unable to clear an engine by purging and fire is apparent, you would select: a. Booster pumps OFF, Fuel shut off valves CLOSED, and apply fire extinguisher b. Items from the FIRE EMERGENCY PANEL and carry them out in that order c. Booster pumps OFF, Fuel shut off valves CLOSED, and pull Fire handle

Answer 26

a. Booster pumps OFF, Fuel shut off valves CLOSED, and apply fire extinguisher

Question 27

The correct order for the actions in the event of engine fire in the air is: a. Power lever OFF, propeller lever FEATHER, fuel lever OFF, fuel shut off valves OFF, heat shut off control PULL, forced landing EXECUTED. b. Fuel lever OFF, power lever IDLE, propeller lever FEATHER, fuel shut off valves OFF, fire pull handle PULL, booster pumps OFF. c. Fuel lever OFF, fuel shut off valves OFF, booster pumps OFF, power lever IDLE, propeller lever FEATHER, heat shut off control PULL, forced landings EXECUTED.

Answer 27

a. Power lever OFF, propeller lever FEATHER, fuel lever OFF, fuel shut off valves OFF, heat shut off control PULL, forced landing EXECUTED.

Question 27

Fuel selectors are located at: a. The fuel control panel b. The overhead panel c. The emergency panel

Answer 27

b. The overhead panel

Question 28

During a normal engine start, the emergency power lever must be in: a. IDLE position b. manual position c. full aft position

Answer 28

c. full aft position

Question 29

The fuel condition lever cut-off position: a. Will provide an rpm of 65% Ng b. Will provide an rpm of 52% Ng c. Shuts off all fuel to the engine fuel nozzles

Answer 29

c. Shuts off all fuel to the engine fuel nozzles

Question 30

The fuel vent outlets are located at the: a. Wing tips leading edge reservoir vented to starboard tank b. Wing tips leading edge reservoir to port wing tank c. Wing tips leading edge reservoir vented to both wing tanks

Answer 30

c. Wing tips leading edge reservoir vented to both wing tanks

Question 30

The total drain valves on the aircraft are: a. 5 valves b. 9 valves c. 6 valves

Answer 30

b. 9 valves

Question 31

The firewall shut off valve push-pull knob is located on: a. Centre of pedestal b. Right side of pedestal c. Overhead console

Answer 31

b. Right side of pedestal

Question 32

Normal fuel management is with: a. Either fuel tank selector in the ON position b. Either fuel tank selector or both fuel tank selector in the ON position c. Both fuel tank selectors in the ON position

Answer 32

c. Both fuel tank selectors in the ON position

Question 32

Fuel system management control position for normal operation is: a. Selection of fuel selector to BOTH RIGHT b. Selection of fuel selector to BOTH LEFT c. Selection of fuel selector to BOTH ON

Answer 32

Selection of fuel selector to BOTH ON

Question 33

The fuel contents gauges are located: a. On the instrument panel left hand side b. On the upper portion of the instrument panel c. On the fuel control panel situated in the L-H flight instrument panel

Answer 33

b. On the upper portion of the instrument panel

Question 34

The oil tank access panel is located: a. On the rear of the engine left side b. On the portside of the air intake casing c. On the top rear engine cowling

Answer 34

a. On the rear of the engine left side

Question 34

The oil approved for engine lubrication is: a. Mil-J-5642E or MIL-G5572C b. Mobil Jet oil 11 or 254, Aero Shell Turbine oil 500 or 555, Royco Turbine oil 500 or 555 c. D.T-D585

Answer 34

b. Mobil Jet oil 11 or 254, Aero Shell Turbine oil 500 or 555, Royco Turbine oil 500 or 555

Question 35

The oil tank capacity is: a. 9.5 D.S Quarts b. 14 D.S Quarts c. 12 D.S Quarts

Answer 35

a. 9.5 D.S Quarts

Question 35

Wing tank fuel low warning annunciations will illuminate if: a. Fuel in the respective tank is 25 gallons or less b. Fuel in the respective tank is approximately one-half full c. Fuel pressure in the respective tank is below 4.75 psi

Answer 35

a. Fuel in the respective tank is 25 gallons or less

Question 36

To obtain an accurate oil level reading after a flight: a. Check oil level 10 minutes after engine shutdown b. Check oil level immediately after engine shutdown c. Check oil level after more than 10 minutes has elapsed since engine shutdown

Answer 36

a. Check oil level 10 minutes after engine shutdown

Question 37

Total unusable fuel with both tanks ON is: a. 3 US Gallons b. 5 US Gallons c. 2.5 US Gallons

Answer 37

a. 3 US Gallons

Question 38

The rudder trimming is accomplished through: a. A trim control wheel and nose wheel steering bungee b. A geared tab and a trim tab c. A trim tab and a spring servo tab

Answer 38

a. A trim control wheel and nose wheel steering bungee

Question 39

The elevators are fitted with: a. A right and left trim tab manually or electrically operated b. A trim tab on the left elevator c. A trim/spring servo tab on the right elevator

Answer 39

a. A right and left trim tab manually or electrically operated

Question 40

The aileron trimming is achieved by: a. A geared tab on the left and right aileron and a trim tab on the left aileron only b. Manually operated servo tab on the right aileron only c. A geared tab on the right aileron and a trim tab on the left aileron only

Answer 40

b. Manually operated servo tab on the right aileron only

Question 41

In order to engage the control locks you would: a. Install external gust locks on the control surface b. Install portable aileron/elevator locks which are in turn connected to a permanently installed rudder lock mechanism c. Install control lock rods with holes on control wheel shafts aligned and pull out the rudder lock to lock the rudder

Answer 41

c. Install control lock rods with holes on control wheel shafts aligned and pull out the rudder lock to lock the rudder

Question 42

The elevator trim tab is operated by: a. An electric actuator b. Vertically mounted trim control wheel on the top left side of control pedestal c. A trim tab hand wheel mounted on the trim console

Answer 42

b. Vertically mounted trim control wheel on the top left side of control pedestal

Question 43

The aileron trim tab is operated by: a. Mechanical hand operated wheel on the trim console b. A mechanical knob on the control pedestal c. The movement of aileron

Answer 43

b. A mechanical knob on the control pedestal

Question 44

The wing flap position indicator is: a. On the left side of the selector lever indicating flap travel by a sliding white tipped pointer b. On the flight instrument panel indicating electrically the flap travel c. On the windshield center post indicating flap travel by a mechanical sliding pointer

Answer 44

a. On the left side of the selector lever indicating flap travel by a sliding white tipped pointer

Question 45

With flaps in the lowered position: a. The aileron range of movement is increased but without differential action b. The aileron range of movement is increased and differential aileron movement is maintained c. The aileron range of movement is unchanged and differential aileron movement is maintained

Answer 45

c. The aileron range of movement is unchanged and differential aileron movement is maintained

Question 46

Hydraulic power is used for the operation of: a. Flaps, wheel brakes and the air intake deflector b. Flaps, wheel brakes, nose wheel steering and the air intake deflector c. Wheel brakes only

Answer 46

c. Wheel brakes only

Question 47

The hydraulic fluid reservoir should be refilled when: a. The level drops to 1/4 full b. The level drops to 1/2 full c. The level drops to 3/4 full

Answer 47

b. The level drops to 1/2 full

Question 48

The pneumatic system provides air suction for operation: a. Of airframe de-icing only b. Of the gyroscopic instruments and autopilot c. Of gyroscopic instruments and if applicable, airframe de-icing and autopilot

Answer 48

a. Of airframe de-icing only

Question 48

For effective braking: a. A brake reservoir is provided in addition to brake master cylinders b. A brake reservoir is provided only to meet the braking requirement c. The brake master cylinders will provide the braking requirement

Answer 48

a. A brake reservoir is provided in addition to brake master cylinders

Question 49

Propeller blade de-icing is provided by: a. Electrically heated elements in boots cycling 1 1/2 minutes ON and 1 1/2 minutes OFF b. Slinger rings at the blade roots ejecting isopropyl alcohol c. Electrically heated boots cycling FAST and SLOW with air intake lower cowling boots

Answer 49

a. Electrically heated elements in boots cycling 1 1/2 minutes ON and 1 1/2 minutes OFF

Question 50

Engine anti icing is provided to: a. The lower intake cowling, alternating with the propeller blades b. Leading edge of the air intake cowling c. The propeller blades only

Answer 50

c. The propeller blades only

Question 51

Wing and horizontal tail de-icing is provided by: a. Pressure from engine bleed air system and vacuum created by dumping in a cycle of about 18 seconds b. Ejection of isopropyl alcohol through a porous element installed in the leading edges c. Electrically heated boots, thermostatically controlled MANUAL or AUTO; FAST or SLOW cycle

Answer 51

a. Pressure from engine bleed air system and vacuum created by dumping in a cycle of about 18 seconds

Question 52

With PROP DE-ICE selected the system will be operative: a. Only when the oil pressure switch is made and the propeller is in the unfeathered position b. As soon as the propeller is out of the feather position regardless of oil pressure c. As soon as the oil pressure switch is made regardless of propeller position

Answer 52

c. As soon as the oil pressure switch is made regardless of propeller position

Question 53

The failure of oil operated pressure switch in propeller anti ice system is: a. Detected by continuously monitoring the ammeter b. Cannot be detected c. Easily detected by amber light near the switch

Answer 53

a. Detected by continuously monitoring the ammeter

Question 54

In the event of the propeller anti-ice system timer malfunction: a. The 3 position toggle switch in AUTO position will achieve the emergency propeller anti-icing b. The switch should be placed to OFF position and carry out emergency landing form icing condition c. The 3 position toggle switch can be held in the momentary MANUAL position to achieve emergency propeller anti-icing

Answer 54

c. The 3 position toggle switch can be held in the momentary MANUAL position to achieve emergency propeller anti-icing

Question 55

The windshield anti-icing panel: a. Is a segment of the windshield electrically heated b. Is a detachable electrically heated glass panel on the windshield c. Is the permanently installed electrically heated glass panel on the windshield

Answer 55

b. Is a detachable electrically heated glass panel on the windshield

Question 56

To keep the ice detector light illuminating: a. The two position toggle switch should be either in ON or AUTO position b. The two position toggle switch should be held in ON position c. The two position toggle switch should be in AUTO position

Answer 56

b. The two position toggle switch should be held in ON position

Question 57

Power can be fed to the two general busses from: a. A 200 amp engine driven starter generator, 24 volt nickel cadmium or lead battery and an external power supply b. A 200 amp engine driven starter generator and a 24 volt lead acid battery or Ni-cad battery c. Two 200 amp engine driven generators, two 24 volt nickel cadmium batteries and external power supply

Answer 57

a. A 200 amp engine driven starter generator, 24 volt nickel cadmium or lead battery and an external power supply

Question 57

Generator failure is indicated by: a. The illumination of red light on the annunciator panel b. The illumination of red light and generator going off c. The illumination of generator amber caution light

Answer 57

b. The illumination of red light and generator going off

Question 58

When erratic operation of the generating system is observed: a. Shut off the system momentarily with the generator switch to TRIP position and then recycle by placing the switch back to ON position b. Shut off the system momentarily with the generator switch to TRIP position and then recycle by placing the switch to RESET momentarily before putting it back to ON position c. Shut off the system momentarily with the generator switch to TRIP position and then recycle by placing the switch RESET

Answer 58

b. Shut off the system momentarily with the generator switch to TRIP position and then recycle by placing the switch to RESET momentarily before putting it back to ON position

Question 59

When external power switch is in the STARTER position: a. External power is applied to the battery and starter generator b. External power is applied to starter only c. External power is applied to starter generator

Answer 59

b. External power is applied to starter only

Question 60

When external power is in the Bus position: a. External power is applied to the starter generator and battery busses b. External power is applied to the starter generator only c. External power is applied to the main Bus with no power to starter

Answer 60

c. External power is applied to the main Bus with no power to starter

Question 61

With the battery switch in the OFF position: a. Power is supplied to the two general busses b. Power is supplied to the battery Bus only c. Power is cut off to all busses

Answer 61

b. Power is supplied to the battery Bus only

Question 62

The battery HOT annunciator indicates: a. Battery temperature exceeds 160°F. Terminate the flight as soon as practicable. b. Battery is not charging c. Battery temperature is higher than 140°F. Monitor the temperature during flight

Answer 62

c. Battery temperature is higher than 140°F. Monitor the temperature during flight

Question 63

The sequence in event of electrical fire is: a. Battery switch ON, generator switch OFF, standby switch OFF, and activate fire extinguisher b. Battery switch ON, generator switch TRIP and release, standby power switch OFF, and fire extinguisher ACTIVATE. c. Battery switch OFF, generator switch TRIP and release, standby power switch OFF, and fire extinguisher ACTIVATE.

Answer 63

c. Battery switch OFF, generator switch TRIP and release, standby power switch OFF, and fire extinguisher ACTIVATE.

Question 64

The stall warning electrical circuit is operated by: a. A lift detecting vane mounted in the port main plane operating throughout full flap travel b. A sensor situated in the port main plane operated pneumatically c. Lift detecting vanes upper and lower, mounted in the leading edge of the port main plane

Answer 64

b. A sensor situated in the port main plane operated pneumatically

Question 65

Standby electrical system is supplied to: a. Provide additional power during starting b. Provide additional power for non essential electrical services c. Supplement power in the event of voltage drop during flight

Answer 65

Supplement power in the event of voltage drop during flight

Question 66

Visual engine fire warning is given by: a. Illumination of red lights in fire pull handle on the fire emergency panel b. Illumination of red engine fire annunciator c. Illumination of red caution lights in the caution panel

Answer 66

b. Illumination of red engine fire annunciator

Question 66

The oxygen cylinder for crew use is located: a. Under the pilot's seat b. In the fuselage tail-cone c. Under the co-pilot's seat

Answer 66

b. In the fuselage tail-cone

Question 67

Nominal charged pressure of the oxygen system is: a. 1850 +/- 50 psi b. 2100 +/- 50 psi c. 1500 +/- 50 psi

Answer 67

b. 2100 +/- 50 psi

Question 68

Indication that oxygen is flowing on demand to the users mask is by: a. A blinker indicator marked FLOW b. Indicator being forced away from the mask c. Indicator being forced toward mask

Answer 68

c. Indicator being forced toward mask