PA-34220T - Dgca question bank for pilots

Results

#1. VFE

check answer

115

#2. Feather(coarse) to non feather (fine)

check answer

–oil pressure

#3. Mark the Correct

The one-engine inoperative best rate of climb is 92 KIAS

All of the above are correct.

The one-engine inoperative air minimum control speed is 66 KIAS.

To feather a propeller of an inoperative engine in flight, maintain direction and an airspeed above 85 KIAS.

#4. Lower red radial line signifies:

Answer

: Vmca (one engine inoperative air minimum control speed) = 66 KIAS

#5. Upper red line radial signifies:

Answer

Vne (never exceed speed) = 205 knots.

#6. Nose gear is steerable:

30°

13.5° arc by combination of full rudder and brake on either side, or 27° arc fully.

#7. Total Fuel Tank Capacity:

check answer

98 US Gallons

#8. Is the combustion heater approved above 25,000 feet?

Answer

Operation of the combustion heater above 25,000 feet is not approved.

#9. Engine control consists of:

All of the above

Throttle lever

Propeller control

Mixture control

#10. Power loading:

CHECK ANSWER

10.8 lbs per hp

#11. Usable Fuel:

check answer

93 US Gallons

#12. Propeller over speed:

CHECK ANSWER

(Caused by propeller governor malfunction & allows the propeller to rotate at full low pitch)

Reduce throttle
Move the propeller control to full decrease RPM (do not feather)
Check for control availability
Then reduce airspeed
Adjust throttle to maintain 2600 RPM

#13. Design maneuvering speed

check answer

140 KIAS it decreases with lighter wt of fA/c

#14. Unfeather (Fine) to Feather (Coarse):

check answer

Nitrogen

#15. To recover from an unintentional spin, the immediate actions to be taken are:

check answer

Retard the throttle to idle position, then apply full opposite rudder

#16. In the event of prop overspeed:

check answer

Retard the throttle to full aft and also move the prop control to full decrease RPM.

#17. The landing gear warning horn will sound

check answer

The landing gear warning horn will sound at low throttle settings if the gear is not down and locked.

#18. Engine Prime Time:

check answer

3 seconds (according to ambient temperature)

#19. Oil viscosity

ANSWER

:below 40F:1065 (aviationgrade) 30(SAEno.)

Above40F:1100 (“) 50(“)

#20. Yellow line radial signifies

Answer

: Caution range (in smooth air only) = 166-205 KIAS.

#21. Vyse

check answer

92KIAS

#22. Mark the correct option:

2 fuel tank vents, 1 under each wing

2 fuel drains for fuel tank

One common under fuselage

4 fuel tank vents, 1 under each wing

#23. Vno

check answer

166KIAS

#24. Continuous ground operation limitation above 32” of Hg is:

CHECK ANSWER

Between 2000 and 2200 RPM avoid continuous ground operation (for 2 blade propeller only) above manifold pressure 32” of Hg.

#25. Should an engine fail during flight at an airspeed below 66 KIAS, what action should the pilot take?

As in (b) and the throttle should be retarded to stop the yaw forces produced by the inoperative engine.

As in (a) and lower the nose of the aircraft to accelerate above 66 KIAS.

Apply rudder towards the operative engine to maintain direction control.

Apply rudder towards the inoperative engine to maintain direction control.

#26. Engine fails during Takeoff speed 82 KIAS less R/W to stop ,pilot should

check answer

Close throttle immediately.
Apply maximum brakes.
Turn off battery.
Turn off fuel selector.
Continue stopping straight ahead.

#27. Mag drop is carried out at:

check answer

2000 RPM, max drop 150 RPM, and the max difference in drops shall not exceed 50 RPM.

#28. VNE

check answer

205

#29. Wing loading

ANSWER

:22.8 lbs per sqft

#30. When does stall warning sound?

ANSWER

5 to 10 knots before the actual stall and mild airframe buffeting and gentle pitching may precede the stall.

#31. Blue radial line signifies:-

ANSWER

One engine inoperative best rate of climb speed (VYSE) 92 KIAS

#32. Which is correct with respect to weight & balance?

All are correct

Datum is 78.4”

Basic empty weight is 3212 lbs.

Standard empty weight includes unusable fuel

#33. Blue line radial signifies:

Answer

: Vyse (one engine inoperative best rate of climb speed) = 92 KIAS.

#34. While starting the engine, the starter cranking is limited to a period of:

Answer

30 seconds

#35. The landing gears are held in the retracted position by:

Answer

Hydraulic pressure.

#36. Mark the correct statements:

In the event of combustion heater overheat, the fuel, air, and ignition to the heater is automatically cut off

Takeoff can be attempted with the fuel selector on X-feed

Both are incorrect

Both are correct

#37. Hydraulic Pressure for Landing Gear:

check answer

Electrically powered, reversible hydraulic pump.

#38. CHT Range (Normal):?

answer

240°F
460°F

#39. Alternate air for engine

Answer

: The automatic alternate air door opens if the primary air source is blocked, but the alternate air is unfiltered and should not be used for ground operations.

#40. CGlimits:

Takeoff: 90.6” Forward, 94.6” Rearward

Both are incorrect.

Both are correct.

Landing: 86.7” Forward, 94.6” Rearward

#41. Type of Battery Fitted:

check answer

Type of Battery Fitted:

24 Volts
65 Amps (19 Amp-Hours)

#42. Lower red radial line signifies:-

CHECK ANSWER

One engine inoperative air minimum control speed (VMCA) and it is 66 KIAS

#43. Upper red radial line signifies:-

CHECK ANSWER

Never exceed speed (VNE) 205 KIAS

#44. Braking System:

Answer

: Separate hydraulic reservoir; 2 single discs, double puck brake assemblies.

#45. Max T/o RPM

check answer

2800 for 5minutes

#46. During single-engine operation, fuel selector should be:

CHECK ANSWER

The selector for the operating engine should be on X-feed, and the selector for the inoperative engine should be set to OFF.

#47. VLO

check answer

108KIAS

#48. One engine failure can be identified by:

check answer

Loss of thrust and yawing towards the inoperative engine.

#49. Main gear /nose gear tyre pressure

check answer

55/40

#50. SQUAT Switch in landing gear:

Answer

Prevents gear retraction on the ground and in left gear.

#51. Should the alternate air be used on the ground?

YES

#52. EGT Range (Normal):

answer

1200°F
1525°F

#53. Alternator:

check answer

28Volts, 60amps

#54. Propeller type:

Answer

Three-blade, constant speed, controllable pitch, and feathering McCauley, directly connected to the crankshaft.

#55. Nose landing gear extension & down locking:

Both (a) & (b) are correct

Aerodynamic load

Springs

#56. To execute manual extension of landing gear in flight

check answer

Maintain speed below 85 KIAS, set the landing gear selector switch to gear down, and pull the emergency gear extension knob.

#57. Shimming of Nose Landing Gear:

Answer

: Spring

#58. The stabilator incorporates a

Answer

Anti-servo tab, which moves in the same direction as the stabilator.

#59. Which of the following is incorrect?

One-engine inoperative performance will decrease if the prop of the inoperative engine is not feathered.

When an engine is feathered, the alternator, gyro, air & oil accumulator warning lights will remain illuminated.

The propeller can be feathered only while the engine is retarding above 600 RPM.

a and b

#60. Vmca

check answer

66KIAS

#61. Basic empty weight is:

CHECK ANSWER

The standard empty weight plus optional equipment. In other words the basic empty weight is the aircraft weight plus unusable fuel plus full oil plus unusable fluids

#62. VLE

check answer

130

#63. Air filter for engine intake:

Answer

: Paper element.

#64. Type of engine

check answer

6cylinders ,Direct Drive, Horizontally opposed ,Aircooled

#65. From which drain point is contaminated fuel drained?

Each gascoater provided quick drain

As in (a), fuel quick drain

Crossfeed drains

Both (b) and (c)

Finish