B200 LIMITATIONS AND MEMORY ITEMS Flashcards

1
Q

VY @ 12,500/13500LBS

A

121/123

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2
Q

VX?

A

100

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3
Q

Stall speed?

A

91/83-81/71-72

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4
Q

Aquaplaning not rotating

A

61

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5
Q

Aquaplaning rotating

A

68

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6
Q

Emergency decent

A

181

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7
Q

max glide range speed

A

135

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8
Q

VYSE

A

121/124

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9
Q

VXSE

A

115

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10
Q

VMCA prop windmilling

A

108

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11
Q

VMCA all configs

A

91/88/78

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12
Q

VMCG

A

84

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13
Q

VA

A

181

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14
Q

VFE approach

A

200

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15
Q

VFE full flap

A

157

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16
Q

VLO extension

A

181

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17
Q

VLO retraction

A

163

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18
Q

VFE

A

200

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19
Q

VMO

A

259/254

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20
Q

MMO

A

0.52

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21
Q

Max ramp weight

A

12590/13590

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22
Q

Max takeoff weight

A

12500/13500

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23
Q

Max zero fuel weight

A

11,000

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24
Q

Max weight baggage are no seats

A

550lbs

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25
Q

Max weight baggage area with seats

A

510lbs

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26
Q

Max fuel imbalance <12500

A

1000lbs / 300lbs for G600 with autopilot on

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27
Q

Max fuel imbalance >12500

A

300lbs

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28
Q

When is fuel crossfeed permitted?

A

Single engine ops only

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29
Q

Gen limit on ground

A

85percent

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30
Q

Gen limit in air up to 31000FT

A

100percent

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31
Q

Gen limit above 31000ft

A

88percent

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32
Q

Starter limits?

A

40 on 60
40 on 60 off
40 on 30min off

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33
Q

Engine torque limit hards

A

2275-2750 for 5 sec

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34
Q

Transient engine torque limits

A

2230 to 2275 for 7min

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35
Q

ITT Start limits

A

800-850 for 20 sec
850-1000 for 5 sec

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36
Q

ITT takeoff limit

A

800

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37
Q

ITT climb and cruise limit

A

750 (770 to match torque between engines)

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38
Q

Prop RPM limit

A

2040-2200 for 5 sec

39
Q

Transient RPM limit

A

2000 - 2040 for 7min

40
Q

What will the prop govern to and what are the torque limit if the primary governor fails?

A

2120rpm and 1800 torque

41
Q

RPM restricted range?

A

400-1150

42
Q

Feather rpm range

A

400 allowed

43
Q

Oil temp limit

A

0-99

44
Q

Transient oil temp limit

A

99-104 for 10min

45
Q

Oil pressure max

A

200

46
Q

Transient oil px limit

A

135 - 200 for 0 sec

47
Q

Oil px range

A

100-135
85-135 above FL210

48
Q

Max outside tx

A

SL-25,000ft = ISA plus 37
above 25,000ft Isa plus 31

49
Q

Min outside tx

A

-45C

50
Q

Landing gears cycle limits

A

1 every 5min, max of 6 followed by 15min cool down

51
Q

Icing boots temp limit

A

-40C OAT

52
Q

Min speed icing

A

140

53
Q

Ice vanes tx limit

A

ISA plus 27 below 13,650
15C above 13,650

54
Q

Min auto pilot engagement heigh

A

400ft pl21/ 1000ftG600

55
Q

Min auto pilot height approach

A

Precision - 79ft for PL21, 200ft for G600
Non precision MDA-50ft

56
Q

Min auto pilot height in cruise

A

1000ft

57
Q

Min speed for approach on AP (G600 only)

A

120kts with flaps approach

58
Q

Max intercept angle for autopilot

A

PL21 - 90 degrees/ G600 45 Degrees

59
Q

Weather radar safe zone

A

PL21- outside 2ft/ G600 - outside 11ft

60
Q

Engine failure during takeoff - takeoff continued

A
  1. Power lever - max allowable
  2. landing gear - positive rate - up
    3.Airspeed - maintain V2 until 400agl min
  3. Propeller (inop engine - Feather/check feathered
  4. Airspeed (at 400agl min) - VYSE
    6.Flaps - up
  5. emergency engine shutdown - execute
61
Q

Engine failure in flight below VMCA

A
  1. power levers - Reduce as required to maintain control
  2. Nose - lower to accelerate above VMCA
62
Q

Engine failure in flight
Engine fire in flight
Unscheduled engine torque increase in flight

A
  1. Condition lever - Fuel cutoff
  2. Prop lever - Feather
  3. Firewall shutoff valve - Close

If warning persists
4. Fire extinguisher - actuate

63
Q

Engine fire on ground

A
  1. Condition lever - fuel cut off
  2. Firewall shutoff valve - close
  3. Ignition and engine start - starter only
    IF WARNING PERSISTS
  4. Fire extinguisher - actuate
64
Q

Emergency engine shutdown on ground

A
  1. Condition lever(s) - fuel cut off
  2. Prop lever(s) - feather
  3. Firewall fuel shutoff valve(s) - close
  4. Master switch gang bar - off
  5. Esis power - off
  6. Medical power - off
65
Q

Engine failure before takeoff ( takeoff aborted)

A
  1. Power lever - Ground fine
  2. Brakes - maximum or as required to achieve stopping distance
  3. Power levers - Max reverse

Note : If circumstances permit,and required to execute shutdown checklist. Transmit abort call prior to selection of gang bar OFF

66
Q

Hot or hung start

A
  1. Condition lever - Fuel cut off
  2. Ignition and engine start - Starter only - max 40sec
  3. ignition and engine start switch - off
67
Q

No light start (ITT fails to rise within 10 sec of introducing fuel)

A
  1. Condition lever - Fuel cut off
  2. Ignition and engine start switch - Off
68
Q

Engine flameout (2nd engine)

A
  1. Power lever - Idle
  2. Prop lever - DO NOT feather
  3. Condition lever - fuel cut off
    If time permits:
  4. Airstart procedure (abnormal tab1) - execute

Note: Consider the glide checklist before attempting air start

69
Q

Glide

A

WARNING: Determine that procedures for restarting first and second failed engines are ineffective before feathering the second engine propeller.

1.Landing gear - up
2.Flaps - up
3. Propeller lever - Feather
4. Airspeed - 135kts
5. ELT - on

Note: Glide range = 2nm for 1000ft (-0.2nm/10kts)

70
Q

Oil pressure low

A
  1. Oil pressure - confirm below 60psi
71
Q

Fuel pressure low

A

1.Standby pump (failed side) - on

72
Q

Electrical smoke or fire/Environmental smoke or fumes

A
  1. Oxygen mask - Don
  2. Mask selector switch - EMERG position
    3.Mic switch - Oxy

Note: Electrical smoke tends to be grey and irritating to nose and eyes. Environmental smoke and fumes tend to be white and much less irritating.

If smoke is prevalent in cabin, passengers should not use overhead oxygen masks

73
Q

Duel generator failure

A
  1. Generators - Reset, then on
    If either comes online:
  2. Operating generator load meter - Do not exceed limits
74
Q

Pressurisation loss

A
  1. Oxygen mask - Don
  2. MIC switch - Oxy
    3.Passenger manual drop out - Pull on (PASS OXY ON light - illuminate)
  3. Descend - as required

Note: Highest altitude for passenger masks is 25,000ft

75
Q

High Differential pressure

A

1.Bleed air valves - ENVIR OFF
2. Oxygen (crew and pax) - as required
3. Descend - As required

76
Q

Bleed air fail

A

Bleed air fail ( affected engine) - INST & ENVIR OFF
L BL AIR OFF or R BL AIR OFF illuminated

Note: Bleed air warning will not extinguish after closing bleed air valve

77
Q

Spins

A
  1. Control column - Full forwards, ailerons neutral
  2. Full rudder - Opposite direction of spin
  3. Power lever - Idle
  4. Rudder - Neutralize when rotation stops
  5. Execute smooth recovery
78
Q

Unscheduled electric elevator trim activation

A
  1. airplane attitude - Maintain using elevator control
  2. A/P/Trim disconnect - Depress fully and hold ( TRIM illuminated)
79
Q

Unscheduled ruder boost activation

A
  1. Directional control - Maintain using rudder pedals
  2. Rudder boost - Off
    If condition persists:
  3. Rudder boost circuit breaker (R down 6 across 7 ) - Pull
80
Q

Auto pilot mistrim (Red E or A)

A

1.Flight controls - Hold firmly
2.Autopilot - Disengage

81
Q

Autopilot Trim fail (red TRIM illuminated)

A

1.Flight controls - hold firmly
2.Autopilot - disengage

82
Q

Autopilot automatic disengagement

A

1.Airplane control - Maintain
2. AP AND YD - Depress to level 1 to cancel horn

83
Q

Ground proximity warnings ( other than day VMC)

A
  1. Wings - level
    2.Power - max available
    3.Pitch - Increase
    Promptly and smoothly increase pitch towards initial attitude of 20 - 25 degrees.
    Adjust pitch to avoid continuous buffeting and/or stall warning
    4.Airspeed - maintain 100 kts
  2. Gear and flaps - up
84
Q

Tcas 1 warning

A

1.Controls - Guard flight controls
2. Intruder aircraft - attempt to acquire visually
3. Flight path - Change as required

85
Q

Emergency Descend

A
  1. Power levers - idle
  2. Prop levers - full forward
  3. Flaps - approach
  4. Gear - down
    5.Airspeed - 181kts max

Note: Attitude should be set at approx 13 degrees down

86
Q

Airstair door/cargo door unlocked

A
  1. All occupants - seated with seatbelts on
87
Q

Immediate ditching procedure

A
  1. Attitude - for 135 kts
  2. Prop levers - feather
  3. Ditching heading - select
  4. Verbal warning - Prepare to ditch
  5. Pilot oxygen mask - DON
  6. Distress message - transmit
88
Q

Min battery voltage for start and GPU

A

23V for start 20V for GPU

89
Q

What is the TQ limit with oil px between 60 and 85

A

1100ft/lb

90
Q

What does sustained prop RPM faster than 2000rpm indicate, and whats the max you can go to

A
  • Failure of primary governor
  • can operate to 2120RPM provided TQ is max 1800FT/LBS
91
Q

Whats green arc for the pneumatics

A

12-20PSI

92
Q

Whats the suction gauge green arc

A

SL to 15,000ft = 4.3 to 5.9
15,000ft to 35,000ft = 2.8 to 4.3

93
Q
A