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OM > OM-B > Flashcards

OM-B Flashcards

1
Q

Manoeuvring speed

A

181

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2
Q

Max flaps approach extension / extended speed

A

200

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3
Q

Max flaps down extension / extended speed

A

146 LTL/157 KVL

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4
Q

Max landing gear extension / extended speed

A

181

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5
Q

Max landing gear retraction speed

A

163

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6
Q

VMCA, flaps up

A

86

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7
Q

Max operating speed

A

259

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8
Q

Max operating speed below flight level 100

A

250

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9
Q

Min speed for sustained icing flight*

A

140 * Min speed for sustained icing flight is not to be used for single engine operaions during climb to safe altitude.

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10
Q

Max airspeed for effective windshield anti-icing

A

226

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11
Q

Turbulent air penetration speed

A

170

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12
Q

Max wind for ground operation

A

45

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13
Q

Max crosswind component (take-off and landing)

A

25

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14
Q

Max tail-wind component

A

10

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15
Q

0.40 or above

A

Good 25/20*

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16
Q

0.35 –0.39

A

Medium-Good 20/16*

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17
Q

0.30 –0.34

A

Medium 14/10*

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18
Q

0.25 –0.29

A

Medium-poor 9/6*

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19
Q

0.20 –0.24

A

Poor 4/4* Limited X-wind applies when the flight operation personnel have less than 100 hours flight time on the Beech 200 in Jonair.

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20
Q

Grass (hard, cut short 5-10 cm) T/O

A

Increase by 10%

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21
Q

Snow (heavy, wet) T/O

A

Increase by 10% per cm. Max 5 cm

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22
Q

Snow (light, dry) T/O

A

Increase by 5%per cm. Max 10 cm

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23
Q

Slush or water T/O

A

Increase by 20% per cm. Max 2,5 cm

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24
Q

Grass, wet, cut short LDG

A

Increase by 20%

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25
Q

Wet, hard packed snow or wet ice LDG

A

Increase by 50%

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26
Q

Dry, hard packed snow or ice LDG

A

Increase by 20%

27
Q

Altimeter setting and checking

A

Deviate not more than 60 ft from true altitude.

28
Q

15 degrees and 121-140 kts to

A

1000 feet above airport elevation

29
Q

10 degrees and 140 kts above

A

1000 feet above airport elevation

30
Q

For one engine climb out?

A

maintain speed between 103-121 kts (actual speed at failure), up to acceleration altitude.If no acceleration altitude is stated on the Performance Manualsheet, 1000feet above airport elevation shall be used as standard.

31
Q

After take-off RA is set to

A

2000ft

32
Q

Indescent, when cleared through the TL, the RA is reset to

A

1000ft

33
Q

On approaches, when established inbound, RA is set to

A

DH/MDH(+ 30 ft if non-precision approach)

34
Q

On visual approach, when cleared for the approach, RA is set to

A

0ft

35
Q

Pilot shall hold hand on yoke and throttles below

A

2500 ft

36
Q

160 KIAS to what altitide?

A

10 000 ft

37
Q

140 KIAS to what altitide?

A

10 000-20 000 ft

38
Q

130 KIAS to what altitide?

A

20 000-25 000 ft

39
Q

120 KIAS to what altitide?

A

25 000-35 000 ft

40
Q

Hot start/hung start

A

Condition lever——Cut off
Ignition/start switch——Starter only
Ignition/start switch——Off at 300 Degress

41
Q

Starter limitations

A

40sec on 60 sec off X2

40sec on 30 minutes off

42
Q

Evacuation

A 
Parking brake----Set
ATC------------------Inform
CL--------------------Cut-off
PL---------------------Feather
Fuel firewall valve-Closed
Fire extinguisher-As required
Master Switch/gangbar-Off
43
Q

Engine fire on ground

A 
Parking brake-Set
CL-(Affected engine)-Cut-off
Fuel firewall valve-Closed
Starter switch-Starter only
Fire extinguisher-Actuate
44
Q

Engine failure

A

Power
Gear
Prop
Flaps

45
Q

Shut down

A

|Power,Gear,Flaps|

L/R Condition lever—- Confirm-Cutoff
L/R Propeller lever—–Confirm-Feather
L/R Fuel firewall valve–Closed
L/R Fire extinguisher—-As required

46
Q

All engine flame out/glide

A

Ignition/start switch–On
Fuel Crossfeed–On

If no relight

Crossfeed -Off
Stand by boost pump-On

47
Q

Decompression/ emergency descent

A

Oxygen mask/ microphone-On
Pass oxygen/man override-Pull on
Smoke goggles-Consider

|Power lever
|Prop lever
|Flaps
|Gear
|Speed
48
Q

Inverter Failure

A

Select other inverter

49
Q

Smoke or fire /electrical or environmental

A

Oxygen masks/mic–On
Mask selector switch-Emergency
Smoke goggles–Consider

50
Q

ASDA

A

TORA+Stopway (if declared available by authority and is capable of bearing the aircraft mass under prevailing condition).

51
Q

LDA

A

Rwy lenght declared available by authority and suitable for landing aircraft ground run.

52
Q

TODA

A

TORA+Clearway

53
Q

TORA

A

Rwy lenght declared available by authority and suitable for departing aircraft ground run.

54
Q

Contaminated Rwy is considered when

A

25% of the rwy is covered by surface water more than 3mm or slush/loose snow equivalent to more than 3mm of water. Compressed snow or ice

55
Q

Fuel start and taxi

A

90 lbs/40 kg

56
Q

Fuel takeoff/ go around

A

150lbs/68 kg

57
Q

Fuel Climb

A

800lbs/362 kg /hr 2000tg 1900rpm

58
Q

Fuel cruise ,descend,hold

A

600lbs/272 kg/hr 2000tq 1700rpm minimum hold alt 5000ft

59
Q

Final reserve fuel

A

30 min holding at 1500ft

60
Q

Oxygen requirements flight crew

A

Entire fligh time over 13000 ft cabin alt and remainder of flighttime between 10-13000 ft after initial 30 minutes. Not less than 30 minutes of oxygen on aircraft certified to 25000 ft. 2hrs above 25000 ft

61
Q

Oxygen requirements 100% passengers

A

Entire flighttime above 15000ft but not less than 10 min supply

62
Q

Oxygen requirements 30% passengers

A

Entire flight time between 14-15000 ft

63
Q

Oxygen requirements 10% passengers

A

remainder of flighttime between 10-14000 ft after initial 30 min

OM (1 decks)

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