B200 LIMITATIONS AND MEMORY ITEMS Flashcards
1
Q
VY @ 12,500/13500LBS
A
121/123
2
Q
VX?
A
100
3
Q
Stall speed?
A
91/83-81/71-72
4
Q
Aquaplaning not rotating
A
61
5
Q
Aquaplaning rotating
A
68
6
Q
Emergency decent
A
181
7
Q
max glide range speed
A
135
8
Q
VYSE
A
121/124
9
Q
VXSE
A
115
10
Q
VMCA prop windmilling
A
108
11
Q
VMCA all configs
A
91/88/78
12
Q
VMCG
A
84
13
Q
VA
A
181
14
Q
VFE approach
A
200
15
Q
VFE full flap
A
157
16
Q
VLO extension
A
181
17
Q
VLO retraction
A
163
18
Q
VFE
A
200
19
Q
VMO
A
259/254
20
Q
MMO
A
0.52
21
Q
Max ramp weight
A
12590/13590
22
Q
Max takeoff weight
A
12500/13500
23
Q
Max zero fuel weight
A
11,000
24
Q
Max weight baggage are no seats
A
550lbs
25
Max weight baggage area with seats
510lbs
26
Max fuel imbalance <12500
1000lbs / 300lbs for G600 with autopilot on
27
Max fuel imbalance >12500
300lbs
28
When is fuel crossfeed permitted?
Single engine ops only
29
Gen limit on ground
85percent
30
Gen limit in air up to 31000FT
100percent
31
Gen limit above 31000ft
88percent
32
Starter limits?
40 on 60
40 on 60 off
40 on 30min off
33
Engine torque limit hards
2275-2750 for 5 sec
34
Transient engine torque limits
2230 to 2275 for 7min
35
ITT Start limits
800-850 for 20 sec
850-1000 for 5 sec
36
ITT takeoff limit
800
37
ITT climb and cruise limit
750 (770 to match torque between engines)
38
Prop RPM limit
2040-2200 for 5 sec
39
Transient RPM limit
2000 - 2040 for 7min
40
What will the prop govern to and what are the torque limit if the primary governor fails?
2120rpm and 1800 torque
41
RPM restricted range?
400-1150
42
Feather rpm range
400 allowed
43
Oil temp limit
0-99
44
Transient oil temp limit
99-104 for 10min
45
Oil pressure max
200
46
Transient oil px limit
135 - 200 for 0 sec
47
Oil px range
100-135
85-135 above FL210
48
Max outside tx
SL-25,000ft = ISA plus 37
above 25,000ft Isa plus 31
49
Min outside tx
-45C
50
Landing gears cycle limits
1 every 5min, max of 6 followed by 15min cool down
51
Icing boots temp limit
-40C OAT
52
Min speed icing
140
53
Ice vanes tx limit
ISA plus 27 below 13,650
15C above 13,650
54
Min auto pilot engagement heigh
400ft pl21/ 1000ftG600
55
Min auto pilot height approach
Precision - 79ft for PL21, 200ft for G600
Non precision MDA-50ft
Visual app - 300ft
56
Min auto pilot height in cruise
1000ft
57
Min speed for approach on AP (G600 only)
120kts with flaps approach
58
Max intercept angle for autopilot
PL21 - 90 degrees/ G600 45 Degrees
59
Weather radar safe zone
PL21- outside 2ft/ G600 - outside 11ft
60
Engine failure during takeoff - takeoff continued
1. Power lever - max allowable
2. landing gear - positive rate - up
3.Airspeed - maintain V2 until 400agl min
4. Propeller (inop engine - Feather/check feathered
5. Airspeed (at 400agl min) - VYSE
6.Flaps - up
7. emergency engine shutdown - execute
61
Engine failure in flight below VMCA
1. power levers - Reduce as required to maintain control
2. Nose - lower to accelerate above VMCA
62
Engine failure in flight
Engine fire in flight
Unscheduled engine torque increase in flight
1. Condition lever - Fuel cutoff
2. Prop lever - Feather
3. Firewall shutoff valve - Close
If warning persists
4. Fire extinguisher - actuate
63
Engine fire on ground
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
Emergency engine shutdown on ground
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
Engine failure before takeoff ( takeoff aborted)
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
Hot or hung start
1. Condition lever - Fuel cut off
2. Ignition and engine start - Starter only - max 40sec
3. ignition and engine start switch - off
67
No light start (ITT fails to rise within 10 sec of introducing fuel)
1. Condition lever - Fuel cut off
2. Ignition and engine start switch - Off
68
Engine flameout (2nd engine)
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
Glide
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
Oil pressure low
1. Oil pressure - confirm below 60psi
71
Fuel pressure low
1.Standby pump (failed side) - on
72
Electrical smoke or fire/Environmental smoke or fumes
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
Duel generator failure
1. Generators - Reset, then on
If either comes online:
2. Operating generator load meter - Do not exceed limits
74
Pressurisation loss
1. Oxygen mask - Don
2. MIC switch - Oxy
3.Passenger manual drop out - Pull on (PASS OXY ON light - illuminate)
4. Descend - as required
Note: Highest altitude for passenger masks is 25,000ft
75
High Differential pressure
1.Bleed air valves - ENVIR OFF
2. Oxygen (crew and pax) - as required
3. Descend - As required
76
Bleed air fail
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
Spins
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
Unscheduled electric elevator trim activation
1. airplane attitude - Maintain using elevator control
2. A/P/Trim disconnect - Depress fully and hold ( TRIM illuminated)
79
Unscheduled ruder boost activation
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
Auto pilot mistrim (Red E or A)
1.Flight controls - Hold firmly
2.Autopilot - Disengage
81
Autopilot Trim fail (red TRIM illuminated)
1.Flight controls - hold firmly
2.Autopilot - disengage
82
Autopilot automatic disengagement
1.Airplane control - Maintain
2. AP AND YD - Depress to level 1 to cancel horn
83
Ground proximity warnings ( other than day VMC)
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
5. Gear and flaps - up
84
Tcas 1 warning
1.Controls - Guard flight controls
2. Intruder aircraft - attempt to acquire visually
3. Flight path - Change as required
85
Emergency Descend
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
Airstair door/cargo door unlocked
1. All occupants - seated with seatbelts on
87
Immediate ditching procedure
1. Attitude - for 135 kts
2. Prop levers - feather
2. Ditching heading - select
3. Verbal warning - Prepare to ditch
4. Pilot oxygen mask - DON
5. Distress message - transmit
88
Min battery voltage for start and GPU
23V for start 20V for GPU
89
What is the TQ limit with oil px between 60 and 85
1100ft/lb
90
What does sustained prop RPM faster than 2000rpm indicate, and whats the max you can go to
- Failure of primary governor
- can operate to 2120RPM provided TQ is max 1800FT/LBS
91
Whats green arc for the pneumatics
12-20PSI
92
Whats the suction gauge green arc
SL to 15,000ft = 4.3 to 5.9
15,000ft to 35,000ft = 2.8 to 4.3
93
What are you looking for on the manual feather checks as part of taxi check
props feather to less than 400rpm and increase to more than 1150rpm
94
When should the IGNITION ON annunciator illuminate
approx less than 500 torque
95
When should the auto feather light illuminate
over approx 410 torque
96
At what torque during the autofeather test should both AUTOFEATHER annunciators extinguish?
approx 260 torque
97
Whats the normal charge rate for a generator
25 to 35 percent
98
Can you take off with the BATTERY CHARGE light illuminated
Yes, if the pilot is satisfied that the battery is not being subjected to excessive rates of charge
99
Can you put fuel in the aux tanks if the mains are not full
No
