BE200 Limitations Flashcards
Maneuvering Speed Va (12,500lbs)
181 KIAS
Max Flap Extension/Extend Speed Vfe
App & Full
App = 200 KIAS
Full = 157 KIAS
Max Landing Gear Operating Speed Vlo
Extension & Retraction
Extension = 181 KIAS
Retraction = 163 KIAS
Minimum Control Air Speed Vmc
86 KIAS
Max Operating Speed
Vmo & Mmo
Vmo = 259 KIAS
Mmo = 0.52 Mach
Wide White Arc
75 - 99 KIAS
Lower limit = Vso
Narrow White Arc
99 - 157 KIAS
Lower limit = Vs1
Power Levers
Do not lift power levers in flight.
Lifting the power levers in flight, or moving the power leverls in flight below the flight idle position, could result in a nose-down pitch and a descent rate leading to aircraft damage and personal injury.
Torque (FT-LBS)
Takeoff and Max Continuous
Transient
Takeoff and Max Continuous = 2230
Transient = 2750 for 5 seconds
Max Observed ITT
Starting
T/O & Max Cont.
Cruise/Normal Climb
Max Reverse
Transient
Starting = 1000°C for 5 seconds
T/O & Max Cont. = 800°C
Cruise/Normal Climb = 770°C
Max Reverse = 750°C
Transient = 850°C for 20 seconds
RPM (% N1)
T/O & Max Cont.
Transient
T/O & Max Cont. = 101.5%
Transient = 102.6% for 10 seconds
Oil Pressure (PSI)
Low Idle
T/O & Max Cont.
Transient
Low Idle = 60 psi (min.)
T/O & Max Cont. = 100-135 psi
Transient = 200 psi
Oil Temperature (°C)
Starting
T/O & Max Cont.
Starting = -40°C (min.)
T/O & Max Cont. = 0°C-99°C (+55°C is recommended)
External Power
Volts
Amps
Volts = 28.0-28.4
Amps = 1000 (momentarily)
300 (continuous)
Generator
Sea Level - 31,000’
>31,000’
>Ground Ops
Sea Level - 31,000’ = 100%
>31,000’ = 88%
Ground Ops = 85%
Starter
40 sec ON
60 sec OFF
40 sec ON
60 sec OFF
40 sec ON
30 min OFF
Approved Fuels
Commercial Grades
Military Grades
Commercial Grades
1. Jet A
2. Jet A-1
3. Jet B
Military Grades
1. JP-4
2. JP-5
3. JP-8
Emergency Fuels/Aviation Gasolines
Commercial Grades
1. 80 Red
2. 91-98
3. 100LL Blue
4. 100 Green
5. 115/145 Purple
Military Grades
1. 80/87 Red
2. 100/130 Green
3. 115/145 Purple
Use of Aviation Gasoline
- Operation is limited to 150 hours between engine overhauls
- Operation is limited to 20,000’ pressure altitude (FL 200) or below if either standby pump is inoperative
- Crossfeed capability is required for climbs above 20,000’ pressure altitude (FL 200)
- Operation above 31,000’ (FL 310) is prohibited
Total Useable Fuel Capacity
Main Tank
Aux Tank
Total = 544 gal./3645 lbs
Main Tank = 193 gal./1293 lbs
Aux Tank = 79 gal./529 lbs
Max Allowable Fuel Imbalance
1000lbs
Fuel Crossfeed
Crossfeeding of fuel is permitted only when one engine is inoperative.
Fuel Gauges in Yellow Arc
Do not take off if fuel quantity gauges indicate in the yellow arc or indicate <265lbs of fuel in each main tank.
Aux Fuel
Do not put any fuel into the aux tanks unless the main tanks are full.
Operating with Low Fuel Pressure
Operation of either engine with its corresponding fuel pressure annunciate (L FUEL PRESS or R FUEL PRESS) illuminated is limited to 10 hours before overhaul or replacement of the engine-driven fuel pump.
Windmilling time does not count
Propeller Rotation Speed Limits
Transient Not Exceeding 5 seconds
Reverse
All Other Conditions
Min Idle Speed:
1. Hartzell Prop
2. McCauley Prop
Transient Not Exceeding 5 seconds = 2200 RPM
Reverse = 1900 RPM
All Other Conditions = 2000 RPM
Min Idle Speed:
1. Hartzell Prop = 1180 RPM
2. McCauley Prop = 1100 RPM
Prop Rotational Overspeed Limits
The maximum propeller overspeed limit is 2200 RPM and is time-limited to 5 seconds.
Sustained propeller overspeeds faster than 2000 RPM indicate failure of the primary governor.
Flight may be continued at propeller overspeeds up to 2120 RPM, provided torque is limited to 1800 ft-lbs.
Sustained propeller overspeeds faster than 2120 RPM indicate failure of both the primary and secondary governor, and such overspeeds are unapproved.
Hartzell Props
Propeller autofeather system must be operable for all flights and must be armed for takeoff, climb, approach, and landing.
Max Ramp Weight
12,590 lbs
Max T/O Weight
12,500 lbs
Max Landing Weight
12,500 lbs
Max Zero Fuel Weight
11,000 lbs
Max Weight in Baggage Compartment
W/ Fold-Up Seats
W/Out Fold-Up Seats
W/ Fold-Up Seats = 510 lbs
W/Out Fold-Up Seats = 550 lbs
Max Operating Pressure-Altitude
Normal Ops
Ops w/ Yaw Damp System Inop
Normal Ops = 35,000’ (FL 350)
Ops w/ Yaw Damp System Inop = 17,000’
Max OAT
S.L. - 25,000’ Pressure Altitude
>25,000’ Pressure Altitude
S.L. - 25,000’ Pressure Altitude = ISA + 37°C
>25,000’ Pressure Altitude = ISA + 31°C
Max Cabin Pressure Differential
6.6 psi
Landing Gear Cycle Limits
Landing gear cycles (1 up-1 down) are limited to one every 5 minutes for a total of 6 cycles, follow by a 15 min. cool-down period.
Aft-Facing Seats
The seat back of each occupied aft-facing seat must be in the upright position and the headrest fully extended for takeoff and landing.
Min. Ambient Temp. for Operation of Deicing Boots
-40°C
Minimum Speed for Sustained Icing Flight
140 KIAS
Flaps Extended in Sustained Icing Conditions
Prohibited except for approach and landings.
Engine Anti-Ice On
Engine Anti-Ice OFF
Engine Anti-Ice, LEFT and RIGHT, shall be ON for operation in ambient temperatures of +5°C or below when flight free of visisble moisture cannot be assured
Engine Anti-Ice, LEFT and RIGHT, shall be OFF for all takeoff and flight operations in ambient temperatures above +15°C
