1
Q
One Engine Inop Best Angle of Climb Airspeed Vxse
A
115 KIAS
2
Q
One Engine Inop Best Angle of Climb Airspeed Vxse
A
115 KIAS
3
Q
One Engine Inop Best Angle of Climb Airspeed Vyse
A
121 KIAS
4
Q
One Engine Inop Enroute Climb Speed
A
121 KIAS
5
Q
Air Minimum Control Speed Vmca
A
86 KIAS
6
Q
Emergency Descent Airspeed
A
181 KIAS
7
Q
Emergency Engine Shutdown
A
Affected Engine:
- Condition Lever — Fuel Cutoff
- Prop Lever — Feather
- Firewall Shutoff Valve — Close
- Fire Extinguisher (if installed) (if fire persists) — Activate
8
Q
Engine Fire on Ground
[L ENG FIRE] or [R ENG FIRE]
A
Affected Engine:
1. Condition Lever - FUEL CUTOFF
2. Firewall Shutoff Valve - CLOSE
3. Ignition and Engine Start - STARTER ONLY
If Fire Warning Persists:
4. Fire Extinguisher (if installed ) - ACTUATE
9
Q
Emergency Engine Shutdown on the Ground
A
- Condition Levers — Fuel Cutoff
- Prop Levers - FEATHER
- Firewall Shutoff Valves - CLOSE
- Master Switch (gang bar) - OFF
10
Q
Engine Failure During Takeoff (at or below V1) - Takeoff Aborted
A
- Power Levers — Ground Fine
- Brakes — As required
- Operative Engine — Max reverse
11
Q
Engine Failure During Takeoff (At or Above V1) - Takeoff Continued
A
- Power — Max Allowable
- Airspeed — Maintain
- Landing Gear — Up
- Prop Lever (inop engine) — Feather
- Airspeed (after obstacle clearance altitude — Vyse
12
Q
Engine Failure in Flight Below Air Minimum Control Airspeed (Vmca)
A
- Power — Reduce as required to maintain control
2. Nose — Lower to accelerate above Vmca
13
Q
Engine Flameout (2nd Engine)
A
- Power Lever — Idle
- Prop lever — Do not feather
- Condition Lever — Fuel Cutoff
- Conduct Air Start Procedure in Section IIIA, Abnormal Procedures
14
Q
Fuel Pressure Low
A
- Standby Pump (failed side) — On
15
Q
Electrical Smoke or Fire
A
- Oxygen Masks — Don
- Mask Selector Switch — EMERG
- Headset — Don, or Audio Speakers - ON
- Mic Switches — Oxygen Mask
16
Q
Environmental System Smoke or Fumes
A
- Oxygen Masks — Don
- Mask Selector Switch — EMERG
- Headset — Don, or Audio Speakers - ON
- Mic Switches — Oxygen Mask
17
Q
Airstair Door/Cargo Door Unlocked
A
If the DOOR UNLOCKED light illuminates, or if it is suspected:
1. All Occupants — Seated with Seat Belts Securely Fastened
18
Q
Emergency Descent
A
- Power Levers — Idle
- Prop Levers — Full Forward
- Flaps (200 KIAS Max) — APPROACH
- Landing Gear (181 KIAS Max) - DN
- Airspeed — 181 KIAS Max
19
Q
Glide
A
- Landing Gear — Up
- Flaps — Up
- Props — Feathered
- Airspeed — 135 KIAS
20
Q
Dual Generator Failure
[L DC GEN] and [R DC GEN]
A
- Generators — Reset, then On
If either generator will reset: - Operating Generator Loadmeter — Do not exceed 100%
21
Q
Flight Controls - Unscheduled Electrical Elevator Trim
A
- Airplane Attitude — Maintain using elevator control
2. A/P Trim Disconnect Switch — Depress fully
22
Q
Unscheduled Rudder Boost Activation
A
- Directional control — Maintain using rudder pedals
- Rudder Boost — Off
If condition persists: - Rudder Boost CB — Pull
23
Q
Use of Oxygen
A
Crew
24
Q
[ALT WARN]
A
- Oxygen Masks — Don
25
High Differential Pressure (Cabin Differential Pressure Exceeds 6.6 PSI)
1. Bleed-Air Valves --- ENVIR OFF
26
[ALT WARN] illuminated and [PASS OXY ON] extinguished
1. Passenger Manual Drop-Out --- Pull On
27
[L BL AIR FAIL] or [R BL AIR FAIL]
1. Bleed-Air Valve (affected engine) --- INSTR & ENVIR OFF
28
Spins
1. Control Column --- Full Forward, Ailerons Neutral
29
Maneuvering Speed Va (12,500 lbs)
181 KIAS
30
Vfe (approach position - 40%)
200 KIAS
31
Vfe (full down position - 100%)
157 KIAS
32
Vlo (extension)
181 KIAS
33
Vle (retraction)
163 KIAS
34
Vmca (hartzell propellers)
86 KIAS
35
Vmo
259 KIAS
36
Mmo
0.52 Mach
37
Wide white arc
75 KIAS
38
Narrow white arc
99 KIAS
39
Power Levers
Do not lift power levers in flight. Lifting power levers in flight, or moving power levers in flight below the flight idle position could result in a nose-down pitch and a descent rate leading to aircraft damage and injury to personnel.
40
Takeoff and Max Continuous
2,330 lbs
41
Transient
2,750 lbs for 5 seconds
42
Max starting ITT
1,000 C for 5 seconds
43
Max Takeoff and Max Continuous ITT
800 C
44
Max Cruise Climb and REC (Normal) Cruise ITT
770 C
45
Max Reverse ITT
750 C
46
Max Transient ITT
850 C for 20 seconds
47
Max Takeoff and Max Continuous RPM (%N1)
101.50%
48
Max Transient RPM (%N1)
102.6% for 10 seconds
49
Low Idle Min Oil Pressure
60 PSI
50
Takeoff and Max Continuous Oil Pressure
100-135 PSI
51
Transient Oil Pressure
200 PSI
52
Min Starting Oil Temp
-40 C
53
Takeoff and Max Continuous Oil Temp
0 C - 99 C (55 C recommended)
54
External Power Voltage Limit
28.0 -28.4 V
55
External Power Amps Limit
1000 amps (momentary) / 300 amps (continuous)
56
Sea Level to 31,000 ft
100%
57
Above 31,000 ft
88%
58
Ground Operation
85%
59
Starter Limits
40 secs On/60 secs Off
60
Approved Engine Grades
Commercial: Jet A, Jet A-1, Jet B
61
Emergency Engine Fuels
Commercial: 80 Red, 91/98, 100LL Blue, 100 Green, 115/145 Purple
62
Emergency Engine Fuel Limits
1. Limited to 150 hrs between engine overhauls
63
Total Useable Fuel Quantity
544 GAL (3,645 lbs)
64
Each Main Tank Fuel Quantity
193 GAL (1,293 lbs)
65
Each Aux Tank Fuel Quantity
79 GAL (529 lbs)
66
Max Allowable Fuel Imbalance Between Wing Fuel Systems
1,000 lbs
67
Fuel Crossfeed
Crossfeed is only permitted when one engine INOP
68
Fuel Gauges in Yellow Arc
Do not takeoff if fuel quantity gauges in the yellow arc or indicate less than 265 lbs of fuel in each main tank.
69
Aux Tank Fuel Management
Do not fuel Aux tanks unless the main tanks are full.
70
Operating with Low Fuel Pressure
Operation of either engine with corresponding FUEL PRES light illuminated is limited to 10 hrs before overhaul or replacement of engine-driven fuel pump. Windmilling time need not be charged against this time limit.
71
Max Transient Prop Speed
2,200 RPM
72
Max Reverse Prop Speed
1,900 RPM
73
Max 'All Other Conditions' Prop Speed
2,000 RPM
74
Min Prop Idle Speed
Hartzell 1,180 RPM
75
Prop Overspeed Limits
Max prop overspeed limit is 2,200 RPM/5 secs. Sustained prop overspeeds faster than 2,000RPM indicate primary governor failure. Flight may be continued at prop overspeeds up to 2,120 RPM with torque limited to 1,800 ft/lbs. Sustained prop overspeeds faster than 2,120 RPM indicate failure of primary governor and secondary governor, and such overspeeds are unapproved.
76
Prop Autofeather
For aircraft with Hartzell props, auto feather must be operable for all flights and must be armed for takeoff, climb, approach and landing.
77
Max Ramp Weight
12,590 lbs
78
Max Takeoff Weight
12,500 lbs
79
Max Landing Weight
12,500 lbs
80
Max Zero Fuel Weight
11,000 lbs
81
Max Weight in Baggage Compartment
With Fold-Up Seats - 510 lbs
82
(Normal and With Yaw Damp Inop)
Normal Operation - 35,000ft
83
Max OAT Limits
SL to FL250 - ISA +37 C
84
Cabin Pressure Differential Limit
6.6 PSI
85
Landing Gear Cycle Limit
1 cycle every 5 mins for up to 6 cycles, then 15-minute cool-down period
86
Aft-Facing Seats
Seat back upright and headrest fully extended for takeoff and landing.
87
Min Ambient Temp for Operation of Deicing Boots
-40C
88
Min Airspeed for Sustained Icing Flights
140 KIAS
89
When Must Engine Anti-Ice be ON?
For operation in ambient temps of 5 C or below when flight free of visible moisture cannot be assured.
90
When Must Engine Anti Ice be Off?
For all takeoffs and flight operations in ambient temps above 15 C
91
One Engine Inop Best Angle of Climb Airspeed Vyse
121 KIAS
92
One Engine Inop Enroute Climb Speed
121 KIAS
93
Air Minimum Control Speed Vmca
86 KIAS
94
Emergency Descent Airspeed
181 KIAS
95
Maximum Range Glide
135 KIAS
96
Engine Failure During Ground Roll
1. Power Levers - IDLE
2. Brakes - As Req'd
3. Operative Engine - MAX REVERSE
4. Condition Levers - Fuel Cut Off
5. Firewall shutoff valves - CLOSED
6. Master Switch - OFF (Gand bar down)
King Air B200
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