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C310 > C310 > Flashcards

C310 Flashcards

1
Q

NEVER EXCEED SPEED (VNE)

A

223 KIAS

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2
Q

Max structural cruise speed

A

181 KIAS

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3
Q

Max manoeuvre speed

A

148 KIAS

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4
Q

Best angle of climb

A

85 KIAS

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5
Q

Best rate of climb also for SE

A

106 KIAS

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6
Q

Flap extension

A

0-15 - 158 KIAS

15-35 - 139 KIAS

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7
Q

Maximum Cross wind

A

19 KIAS

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8
Q

Landing operation speed (Vlo)

A

138 KIAS

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9
Q

Landing gear extended speed (VLE)

A

138 KIAS

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10
Q

Landing gear operation down (VLO2)

A

138 KIAS

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11
Q

Maximum landing light operation

A

130 KIAS

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12
Q

Load facto flaps up

A

+ 3.8g and - 1.52g

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13
Q

Load factor flaps down

A

+ 2.0

Bill negative

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14
Q

Feather check rpm

A

1200 rpm

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15
Q

Min rpm for feathering

A

1000 rpm

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16
Q

Rpm to test ignition system

A

1700 rpm

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17
Q

Rpm to test govoner system

A

1200 rpm

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18
Q

During ignition test max drop and max diff

A

50 max drop

150 max diff

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19
Q

Climb power settings

A

24.5” at 2700rpm

106 KIAS

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20
Q

MTOW/Ramp

A

2500 kg (5500 lbs)

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21
Q

MAX LANDING WIEGHT

A

2454 kg (5400 lbs)

Must burn 46 kg fuel before able to land. 100lbs

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22
Q

Max ZFW

A

2223 kg (4900 lbs)

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23
Q

Total Fuel

A

Total - 628 lts

Total Useabke - 617 lts

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24
Q

Main tanks fuel

A

Total fuel - 386lts (193 per side)

Useable fuel - 378 lts (189 per side)

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25
Q

Fuel Aux tanks

A

Total fuel - 242lts (121lts per side)

Useable fuel - 239 (119lts per side)

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26
Q

Planned fuel consumption

A

120lts/hr

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27
Q

Min oil capacity per engine

A

9 quarts

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28
Q

Max oil in sump

A

12 quarts

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29
Q

Max weight in nose locker

A

158kg

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30
Q

Max weight in wing locker

A

54kg

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31
Q

Max weight aft baggage area

A

72kg

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32
Q

Min control speed in air (Vmca)

A

80 KIAS

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33
Q

310R empty weight

A

1652kg

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34
Q

Glide speed

A

2494kg - 111 KIAS
2313kg - 107 KIAS
2131kg - 102 KIAS

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35
Q

Engine

A

2 X 285BHP at 2700rpm

6 Cylinder

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36
Q

Take off power/ Max continuous power

A

Full throttle at 2700rpm

37
Q

Propeller Govoner

A

Oil pressure drives blades to High rpm ( low pitch )

Spring and counter weight drives blades to low rpm ( high pitch/feather)

38
Q

Electrical system

A

28v negative ground alternator in each engine.

39
Q

Battery

A

24v DC

Located left wing aft of nacelle fairing

40
Q

Taxi fuel

A

12 lts

41
Q

Variable reserve

A

15% of flight fuel at 120lts/hr

42
Q

Fixed reserves

A

45 min 90 lts

43
Q

Holding fuel

A

75 lts

44
Q

Climb power

A

24.5” at 2500 rpm

45
Q

Cruise power

A

Below full throttle height
23” 2450rpm

About full throttle height
22” 2400rpm
21” 2450rpm

46
Q

Fuel flow in cruise and leaning process

A

90lbs/hr

Lean to peak EGT the. Riches 3 divisions (75 c)

47
Q

Descent procedure

A

Descent at 500f/min.

Reduce MAP to 20” and 1” per
Min.

Not below 17”-18”

Increase mix on descent to aid cooling.

48
Q

Circuit configuration

A

Down wind - 18-20”, 2300rpm, 15 degree flap

Abeam threshold - time 20 sec then gear down.

Final - Max RPM, flaps 35 degree

Assymetric circuit

15 degree flaps base and 35 only when sure of making RWY.

49
Q

Committed to land when

A

Below 400ft AGL or

More than 15 degree flaps selected

50
Q

Aircraft configuration holding

A

21.5” 2100rpm, flap 15, gear up.

51
Q

Aircraft configuration IAF

A

20”, 2300rpm, 15 flap, gear up

52
Q

Descent after IAF

A

15-18”, 2300rpm, 15 flaps, gear down

53
Q

Aircraft configuration FAF

A

15-18” max rpm, 15 flap, gear down

54
Q

Aircraft configuration circling

A

18-22”, max rpm, 15 flap, gear down

55
Q

Aircraft configuration missed approach

A

18-22”, max rpm, retract to 0 flap

56
Q

On approaching fix include 5nm level segment to?

A

Allow slowing to first stage flap 15 - 158 KIAS

And gear extension speed 139 KIAS

57
Q

Landing light

A

Used for all night landings

Exemption speed 130 KIAS

58
Q

Vortex Generators (Vg)

A

88 VG ON WINGS AND FIN with strakes mounted outboard of each engine nacelle.

Up to 4 missing No change
5 or more missing revert of non Vg limitations

59
Q

Oil checks

A

Prior to first flight and not more than 3 hours flight time after

60
Q

Cold Start procedure

A 
Mixture.    Rich
Pitch.        Full fine
Throttles.  Full
Mags.        On
Alternators on
Battery        On
Primer.       Till positive fuel flow
Throttle       Open 1 to 2”
Starter.       Engage left engine and repeat for right.
61
Q

Cranking starter care

A

Longer than 50 seconds allow 5 min cool down. As excessive heat can damage a mature windings

62
Q

Hot start procedures

A 
Mixture ICO
Throttle full open
Aux pump low for 20 seconds
Aux pump off
Throttle closed
Start normally
63
Q

After start procedures

A

Manifold pressure. Stable
Rpm less than 1000
Oil pressure green working 30 seconds
Suction. Check after each start

64
Q

TKOF safety Breif decision point?

A

Will be gear up selection when landing ahead option disappears or Vyse reached 106KIAS

65
Q

TKOF safety breif with examining runway

A

If engine fails prior to decision point. I will close throttles, control aircraft and stop on remaining runway.

66
Q

TKOF safety breif gear up or 106KIAS

A 
If engine fails past gear up or 106KIAS I will 
lower the nose, 
maintain controls at 106KIAS (vyse), 
check mixture up
Pitch up
Power up
Identify dead engine
Feather dead engine
Make a circuit and land informing TWR or ATC
67
Q

TKOF procedure

A 
Power full
Check P and Ts
Fuel flows 130-150 lbs/hr
Vmca 80KIAS
Climb to 50ft at 92KIAS
Gear up nil RWY remaining
Increase speed Vy - 106KIAS
68
Q

Climb Procedure

A

Power 24” 2500rpm
Mixtures lean to 110/lbs per engine
Cowl flaps as required

69
Q

Cruise procedures below full throttle height (65% power)

A

23” 2300 rpm

70
Q

Cruise procedures about full throttle height

A

For 22”, 2400rpm
For 21”, 2450

If max MAP achievable is below 21” leave rpm at 2450.

71
Q

Learning procedure in cruise

A

Lean to peak EGT
en riches 3 divisions (75 f)
Fuel flow should stabilise at 90lbs/hr

72
Q

Short sector power setting ( less then 15min)

A

22”, 2300rpm

73
Q

Descent Procedure

A

Calculated at 500fpm

Reduce power to 20” making sure to recursive at 1” per minute.

Set not below 17-18”

En rich mixtures in descent to dec EGT steadily.

74
Q

Asymmetric circuit procedure

A

Down wind 18-20”, 2300rpm
Abeam threshold 20 sec, turn base, set 15 flap if needed
Final Max rpm
Gear down and flaps 35 once sure of making the landing environment

75
Q

Committed to land when?

A

Below 400ft AGL OR

more than 15 flap selected

76
Q

Final approach to land

A 
Fuel mains
Aux pumps on
Gear down three greens
Flaps 35 
Pitch full fine
Approach speed 93 KIAS
VMCA 80KIAS
77
Q

Baulked landing

A 
Mixture up
Pitch up
Throttle up
Flaps 15
Gear up positive rate 
Flaps 0
78
Q

When does the stall warning sound?

A

4 to 9 kts about stall speed

76kts flap down, 70kt flaps up

79
Q

Wing flap system

A

Split flap design
Actuated my electrical motor
when flap position equals selected position on switch a micro switch de energises flap motor.

80
Q

Landing gear system

A

Retractable, tricycle type
Gear doors mechanically linked with gear.
Moving selector allows electrical power to energise gear motor.
Motor continues to run till up or down limits reached. Then gear box disconnects electrical power from motor.

81
Q

Landing gear squat switch

A

Prevents gear retraction on ground
Safety switch on left shock strut.
When compressed switch is open, preventing power reaching gear motor.

82
Q

Landing gear position lights

A

Three green when locked.

Red light illuminates when any or all gears are in locked.

No light illumination gear is up and locked.

83
Q

Landing gear warning horn

A

Controlled by throttle and flap position

If throttles retard below 15” with gear up horn will sound

If 35 flaps selected horn will sound

When gear selected up on the ground

84
Q

Landing gear hand crank

A

Below right front seat edge

About 52 cranks till gear locks.

Clock wise rotation.

85
Q

Fuel low level warning light

A

When main tanks contain approx 60lbs of fuel each

Provided by two warning lights

Actuated by float switch.

86
Q

Stall warning system

A

Left wing lead edge

Electrical Heater selected by turning on pitot heat

87
Q

How do vortex generators improve MTOW?

A 
By delaying flow separation of airflow. 
Improves STOL performance
Reduces stall speed
Reduces Vmca
Improves aileron effectiveness
Improves SE climb performance
88
Q

Low system voltage warning

A

Low system voltage warning lights illuminate when voltage decreases below approx 25v

89
Q

Emergency alternate field switch

A

Used when alternators won’t self excited. Provides excitation from battery.

C310 (1 decks)

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