BE200 Limitations

Question 1

Maneuvering Speed Va (12,500lbs)

Answer 1

181 KIAS

Question 2

Max Flap Extension/Extend Speed Vfe

App & Full

Answer 2

App = 200 KIAS
Full = 157 KIAS

Question 3

Max Landing Gear Operating Speed Vlo

Extension & Retraction

Answer 3

Extension = 181 KIAS
Retraction = 163 KIAS

Question 4

Minimum Control Air Speed Vmc

Answer 4

86 KIAS

Question 5

Max Operating Speed

Vmo & Mmo

Answer 5

Vmo = 259 KIAS
Mmo = 0.52 Mach

Question 6

Wide White Arc

Answer 6

75 - 99 KIAS
Lower limit = Vso

Question 7

Narrow White Arc

Answer 7

99 - 157 KIAS
Lower limit = Vs1

Question 8

Power Levers

Answer 8

Do not lift power levers in flight.

Lifting the power levers in flight, or moving the 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 personal injury.

Question 9

Torque (FT-LBS)

Takeoff and Max Continuous
Transient

Answer 9

Takeoff and Max Continuous = 2230
Transient = 2750 for 5 seconds

Question 10

Max Observed ITT

Starting
T/O & Max Cont.
Cruise/Normal Climb
Max Reverse
Transient

Answer 10

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

Question 11

RPM (% N1)

T/O & Max Cont.
Transient

Answer 11

T/O & Max Cont. = 101.5%
Transient = 102.6% for 10 seconds

Question 12

Oil Pressure (PSI)

Low Idle
T/O & Max Cont.
Transient

Answer 12

Low Idle = 60 psi (min.)
T/O & Max Cont. = 100-135 psi
Transient = 200 psi

Question 13

Oil Temperature (°C)

Starting
T/O & Max Cont.

Answer 13

Starting = -40°C (min.)
T/O & Max Cont. = 0°C-99°C (+55°C is recommended)

Question 14

External Power

Volts
Amps

Answer 14

Volts = 28.0-28.4
Amps = 1000 (momentarily)
300 (continuous)

Question 15

Generator

Sea Level - 31,000’
>31,000’
Ground Ops

Answer 15

Sea Level - 31,000’ = 100%
>31,000’ = 88%
Ground Ops = 85%

Question 16

Starter

Answer 16

40 sec ON
60 sec OFF
40 sec ON
60 sec OFF
40 sec ON
30 min OFF

Question 17

Approved Fuels

Commercial Grades
Military Grades

Answer 17

Commercial Grades
1. Jet A
2. Jet A-1
3. Jet B

Military Grades
1. JP-4
2. JP-5
3. JP-8

Question 18

Emergency Fuels/Aviation Gasolines

Answer 18

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

Question 19

Use of Aviation Gasoline

Answer 19

1. Operation is limited to 150 hours between engine overhauls
2. Operation is limited to 20,000’ pressure altitude (FL 200) or below if either standby pump is inoperative
3. Crossfeed capability is required for climbs above 20,000’ pressure altitude (FL 200)
4. Operation above 31,000’ (FL 310) is prohibited

Question 20

Total Useable Fuel Capacity

Main Tank
Aux Tank

Answer 20

Total = 544 gal./3645 lbs
Main Tank = 193 gal./1293 lbs
Aux Tank = 79 gal./529 lbs

Question 21

Max Allowable Fuel Imbalance

Answer 21

1000lbs

Question 22

Fuel Crossfeed

Answer 22

Crossfeeding of fuel is permitted only when one engine is inoperative.

Question 23

Fuel Gauges in Yellow Arc

Answer 23

Do not take off if fuel quantity gauges indicate in the yellow arc or indicate <265lbs of fuel in each main tank.

Question 24

Aux Fuel

Answer 24

Do not put any fuel into the aux tanks unless the main tanks are full.

Question 25

Operating with Low Fuel Pressure

Answer 25

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

Question 26

Propeller Rotation Speed Limits Transient Not Exceeding 5 seconds Reverse All Other Conditions Min Idle Speed: 1. Hartzell Prop 2. McCauley Prop

Answer 26

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

Question 27

Prop Rotational Overspeed Limits

Answer 27

**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.

Question 28

Hartzell Props

Answer 28

Propeller autofeather system must be operable for all flights and must be armed for takeoff, climb, approach, and landing.

Question 29

Max Ramp Weight

Answer 29

12,590 lbs

Question 30

Max T/O Weight

Answer 30

12,500 lbs

Question 31

Max Landing Weight

Answer 31

12,500 lbs

Question 32

Max Zero Fuel Weight

Answer 32

11,000 lbs

Question 33

Max Weight in Baggage Compartment W/ Fold-Up Seats W/Out Fold-Up Seats

Answer 33

W/ Fold-Up Seats = 510 lbs W/Out Fold-Up Seats = 550 lbs

Question 34

Max Operating Pressure-Altitude Normal Ops Ops w/ Yaw Damp System Inop

Answer 34

Normal Ops = 35,000' (FL 350) Ops w/ Yaw Damp System Inop = 17,000'

Question 35

Max OAT S.L. - 25,000' Pressure Altitude >25,000' Pressure Altitude

Answer 35

S.L. - 25,000' Pressure Altitude = ISA + 37°C >25,000' Pressure Altitude = ISA + 31°C

Question 36

Max Cabin Pressure Differential

Answer 36

6.6 psi

Question 37

Landing Gear Cycle Limits

Answer 37

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.

Question 38

Aft-Facing Seats

Answer 38

The seat back of each occupied aft-facing seat must be in the upright position and the headrest fully extended for takeoff and landing.

Question 39

Min. Ambient Temp. for Operation of Deicing Boots

Answer 39

-40°C

Question 40

Minimum Speed for Sustained Icing Flight

Answer 40

140 KIAS

Question 41

Flaps Extended in Sustained Icing Conditions

Answer 41

Prohibited except for approach and landings.

Question 42

Engine Anti-Ice On Engine Anti-Ice OFF

Answer 42

Engine Anti-Ice, LEFT and RIGHT, shall be ON for operation in ambient temperatures of +5°C or below when flight free of visible 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