310 QUIZ Flashcards

1
Q

What model, type and horsepower are the engines on the 310?

A

Model–IO520MB
Type–Fuel injected, direct drive, aircooled, horizontally opposed, 6 cylinder, 520 cubic inch
Horsepower–285 hp @ 2700 rpm

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2
Q

What is the height, width, and length of 310?

A

H - 11 feet / W - 37 feet / L - 32 feet

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3
Q

What is the normal prop tip ground clearance?

A

Less than 1 foot

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4
Q

What type of props are on the 310?

A

Constant speed, full feathering, non reversing, hydraulically actuated.

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5
Q

What type of fuel does our 310 use?

A
100 AV FUEL (green)
100 LowLead (blue)
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6
Q

Max weight capacity of nose baggage compartment?

A

350 pounds

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7
Q

Max ramp weight?

A

5725 pounds

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8
Q

Max Take off weight?

A

5680 pounds

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9
Q

Max landing weight?

A

5400 pounds

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10
Q

What is the max luggage weight for the aft baggage (station 126)?

A

160 pounds

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11
Q

What is the total fuel capacity of our 310, how many tanks and their respective quantities?

A

183 gallons total

5 tanks – (2) Main/Tip tanks=50 gallons each, (2) Aux tanks=31.5 gallons each, (1) Nacel tank=20 gallons

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12
Q

What is the total Oil Capacity of each engine?

A

13 quarts (1 quart for the oil fliter)

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13
Q

What is the minimum oil capacity to operate?

A

9 quarts

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14
Q

What is the Vmc airspeed for the 310?

A

Vmc-80

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15
Q

What is Vy (blueline) airspeed for the 310?

A

Vy 106 kts

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16
Q

What is the Vne (never exceed) airspeed for the 310?

A

Vne - 223 kts

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17
Q

What is the Vr (rotate) airspeed for the 310?

A

Vr - 92 kts

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18
Q

What is Vbg (best glide-dual engine failure) airspeed for the 310?

A

Vbg - 111 kts

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19
Q

What is the normal operating range for the Tachometer?

A

2100 -2500 (green arc)

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20
Q

What is the normal operating range for the manifold pressure gauge?

A

15.0 - 24.5 inches of Hg (green arc)

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21
Q

What is the Max Oil Pressure?

A

100 PSI

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22
Q

What is the Max Oil Temp?

A

240 Degrees (red line)

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23
Q

What is the Max Cylinder Head Temp?

A

460 Degrees F (red line)

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24
Q

What is the minimum Fuel Flow?

A

2.5 PSI

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25
Q

How many emergency exits, and where are they located?

A

2 - Entry door and left pilot side window

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26
Q

What is the fuel capacity of the left AUX tank?

A

31.5 gallons

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27
Q

Which tanks MUST be selected during take off and landing?

A

MAINS/TIPS

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28
Q

What are the emergency procedures for Engine Failure before takeoff?

A

A) Throttles – Close immediately

B) Brakes or Land and brakes

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29
Q

What are the Emergency Procedures for Engine Failure after takeoff?

A

A) Mixture, Props, Throttles - full forward
B) Gear up
C) identify INOP Engine
D) For Inop Engine (throttles/mixture closed, prop feather)

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30
Q

What is an important flight consideration when flying on 1 engine?

A

Establish 5 degree bank into OP engine, no more than 10 degrees bank into INOP engine during any turn

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31
Q

What are the Emergency Procedures for both engines failing in cruise?

A

Wings flaps up, landing gear up, Props to feather…minimum airspeed…111 kts

32
Q

What are the emergency procedures for ground fire on the ground?

A

If possible move aircraft off the fire, brake, both throttles closed, both mixtures idle cutoff, batteries off, mags off, GET OUT.

33
Q

What are the emergency procedures for engine fire inflight?

A
1) AUX fuel pumps off
B) Secure Engine with fire
   I. THROTTLES CLOSED
   II. MIXTURE CUT OFF
   III. PROP FEATHER
   IV. FUEL SELECTOR OFF
34
Q

What are the emergency procedures for inflight cabin fire?

A

A) Electrical load reduced/minimized
B) Attempt to isolate the source of fire/smoke
C) Wemacs open
D) cabin Air Controls Open all vents (close if increased air flow make smoke worse)

35
Q

What are emergency procedures for emergency descent?

A

A) Throttles - idle, Props - Full Forward, Mixtures - adjust as needed
B) Wing flaps UP
C) Landing gear UP
D) Moderate bank initiated

36
Q

What are the emergency procedures for a Spin?

A

A) Throttles closed
B) Ailerons neutralized
C) Rudder full opposite direction of spin
D) Yoke push forward until spin stops - neutralize rudder once soin stops
E) Yoke pull back to recover from the dive

37
Q

A Main tire blows out during takeoff (above Vr), on climb out, what should a pilot NOT DO?

A

Retract the gear

38
Q

What memorization items are there on the Landing Gear will not extend?

A

NONE - refer to the AFM - Chapter 3-29 and follow check list
FYI–Announce PAN-PAN-PAN to controlers to troubleshoot. If gear extension continues to fail without solution, declare an emergency before landing

39
Q

What is the Max Demo Crosswind Velocity

A

19 kts

40
Q

When using external power source (EPU), DO NOT turn on these switches until EDU is removed to avoid damage?

A

The batteries and alternators

41
Q

During prop feathering checks at run up, do not allow the RPMs to fall below ______ RPMs?

A

1000 RPMs

42
Q

What are the max and min allowable suction ranges on the instrument?

A

4.75 - 5.25 inches Hg

43
Q

What is lift off speed?

A

92 kts

44
Q

What is the cruise climb settings for the 310?

A

2500 RPM and 24.5 inches Hg

45
Q

With an obstacle ahead requiring steep climb angle, what speed with flaps up gear up should the aircraft be flown?

A

Vx - 85 kts sea level

89 kts at 15000 feel

46
Q

Make sure the aircraft does not exceed _______ pounds before attempting to land?

A

5400 pounds

47
Q

The Pitot Heat switch should be turned “ON” at least ______ minutes before entering potential icing conditions?

A

5 minutes inflight

2 minutes on the ground

48
Q

What is the empty weight of the 310?

A

3876 pounds

49
Q

How often must our 310 be weighed?

A

Every 3 years or after addition or removal of equipment

50
Q

What is the zero-fuel weight of the 310?

A

4900 pounds

51
Q

What are described as the flight controls on the 310?

A

Ailerons, elevator, rudder, and trim systems

52
Q

The ailerons trim is located on which side?

A

Left

53
Q

What type of system are the ailerons and elevator?

A

Push pull rod attached to bell crank

54
Q

How are the wing flaps powered?

A

Electric

55
Q

Can the landing gear be retracted on the ground?

A

No - a squat switch is located on the left landing gear shock strut…when aircraft weight is on switch it cuts power to landing gear retraction

56
Q

If the landing gear emergency hand-crank is not stowed in its clip, what condition will prevail?

A

The gear will not operate normally electrically.

57
Q

How many detents (selections) can the 310 fuel selectors provide, and what are they?

A

4 – main, aux, cross feed, no fuel (off)

58
Q

How are the brakes powered?

A

Hydraulics

59
Q

What type of electrical system does the 310 have?

A

28 volt, negative ground, DC system. a 24 volt battery, (2) 100 amp alternators

60
Q

“Low Voltage”light illuminates when the airplane bus voltage falls below ______ volts?

A

25 volts

61
Q

What setting should be selected on an external power source (EDU) before using it on the 310?

A

28 volts

62
Q

When the Pitot Heat Switch is turned “ON”, what items are heated?

A

Pitot tube, Stall warning vane, & optional wing locker fuel vents

63
Q

How will a failed vacuum pump be alarmed/signaled to the pilot?

A

A red button will pop out on the suction gauge

64
Q

At what point will a stall warning horn sound?

A

5 to 10 kts above the stall

65
Q

Where is the gas fired heater located in the 310?

A

Nose compartment

66
Q

What type of props are on the 310?

A

All-metal, 3 bladed, constant speed, full feathering, single acting, governor regulated

67
Q

What inspections are required on our 310?

A

100 hour and annual

68
Q

What items are to be displayed in the aircraft at all times?

A

Airworthiness Cert, Aircraft Registeration, Radio License

69
Q

What items are to he carried at all times?

A

W&B, Equipment List, POH/AFM, Pilot check list

70
Q

How and in what order do the de-ice boots system work?

A

Manual switch activated, tail boots activated for 6 seconds first, then the wing boots activated for 6 seconds, then the switch springs back to off

71
Q

When should Deice Boots be activated?

A

When ice accumulates between 1/4 to 1/2 inch

72
Q

When should the heated windshield be activated?

A

On the ground–for brief electrical test

Inflight–before entering visible moisture with O.A.T. below 40F

73
Q

Is our 310 Certified for Flight into Known Icing?

A

Yes

74
Q

What equipment is required to be Certified for Known Ice?

A

Wing boots (inboard and outboard) and Rudder/Elevator Deice Boots, Windshield Heat, Dual 100 amp alternator, Heated Pitot Tube, Stall Warning Heat, Prop Heat

75
Q

Read chapter 7 of POH before

TEST DAY.

A

310 and 414