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King Air 200 Limitations > King Air 200 Limitation. > Flashcards

King Air 200 Limitation. Flashcards

1
Q

MANEUVERING SPeed Va

A

181 KIAS

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2
Q

MAXIMUM fLAP EXTENSION/extended SPEED Vfe Approach Position 40% (White Triangle)
FULL Down Position 100%

A

Approach Flaps 40%

Full Flaps 100%

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3
Q

Vlo Extension……………………………………….

Vlo Retraction………………………………………

A

…………………………………………181 KIAS

………………………………………….163KIAS

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4
Q

Maximum Landing Gear Extended Speed

A

Vle…………………181 KIAS

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5
Q

Air Minimum Controls Speed Vmca ( Red Line)

A

Vmca 86 Kias

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6
Q

Maximum Operating Speed

A

Vmo……………………………………..259 KIAS

Mmo…………………………………….0.52 Mach

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7
Q

White Arc (Full Flap Operating Range )

A

75 To 157 KIAS

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8
Q

Wide White Arc………………………………….
Narrow White Arc…………………………………
Upper Limit…………………………………………
Lower Limit………………………………………..

A

……………………75 TO 99 KIAS

…………………….157 KIAS
……………………..99 KIAS

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9
Q

Vyse (blue Line )…………………………………

 Vxse............................................................
A

…………………………………….121 KIAS

……………………………………..115KIAS

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10
Q

SHP

Takeoff & MAX Cont………………………………

A

………………………………………850SHP

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11
Q

Takeoff & Max Cont………………………………

Transient………………………………………………..

A

Takeoff & Max Cont……….2230 Ft-Lbs

Transient…………….. 2750 Ft-LBS for 5 Seconds

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12
Q

Maximum Observed ITT ‘C
Starting………………………………………………………………
Low Idle………………………………………………………………
Takeoff & Max Cont & Max Cruise…………………….
Max Reverse………………………………………………………
Transient………………………………………………………….

A

Maximum Observed ITT ‘C
Starting……………………………..1000’C Limited to 5 seconds
Low Idle………………………………………………….750’C
Takeoff & Max Cont & Max Cruise………..800’C
Max Reverse…………………………………………..750’C
Transient……………………………….850’C for 20 Seconds

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13
Q 
Prop RPM N2
Takeoff & Max Cont & Max Cruise
Max Reverse
Transient
Overspeed Governor up to 2120 RPM
A

Prop RPM N2
Takeoff & Max Cont & Max Cruise………………….2000RPM
Max Reverse…………………………………………………….1900 RPM
Transient……………………………………2200 rpm for 5 second
Overspeed Governor up to 2120 RPM…1800ft-lb torque

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14
Q

Oil Press PSI
Minimum………………………..
Maximum………………………..
Transient…………………….

A

Oil Press PSI
Minimum………………………..60 psi
Maximum………………………..135 psi
Transient…………………….200psi

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15
Q

Oil Temp ‘C
Starting……………………………………
Takeoff & Max Cont……………….
Transient………………………………….

A

Oil Temp ‘C
Starting……………………………………-40’C( min )
Takeoff & Max Cont……………….0’C to +99’C
Transient…………………………………. 0’C to + 104’C

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16
Q

EXTERNAL POWER LIMITS
Set to…………volts, Minimum of ……. amps momentarily
and……..amps continuously

A

EXTERNAL POWER LIMITS
Set to.28.0-28.4.volts, Minimum of 1.000 amps momentarily
and 300 amps continuously

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17
Q

GENERATOR LIMITS
SEA LEVER TO 31,000 FEET ALTITUDE…..
ABOVE 31,000 FEET ALTITUDE………..
GROUND OPERATION………………………

A

GENERATOR LIMITS
SEA LEVER TO 31,000 FEET ALTITUDE…..100%
ABOVE 31,000 FEET ALTITUDE………..88%
GROUND OPERATION………………………85%

18
Q

STARTER LIIMITS

…………..ON,……………………..OFF
…………..ON,……………………..OFF
…………..ON,……………………..OFF

A

STARTER LIIMITS

….40 SEC……….ON,…….60..SEC….OFF
….40 SEC……….ON,…….60..SEC….OFF
….40 SEC……….ON,…….30..MIN….OFF

19
Q

FUEL MANAGEMENT
TOTAL USABLE FUEL……………………….
EACH MAIN TANK FUEL SYSTEM…….
EACH AUXILIARY FUEL TANK……………

A

FUEL MANAGEMENT(usable fuel Gallons x 6.7= pound
TOTAL USABLE FUEL………………544 G 3645 lbs
EACH MAIN TANK FUEL SYSTEM…….193G 1293 lbs
EACH AUXILIARY FUEL TANK……………79 G 529 lbs

20
Q

Maximum fuel imbalance between wing fuel systems

21
Q

Crossfeeding of fuel is permitted only when

A

One engine is inoperative

22
Q

Do not takeoff if fuel quantity gauges indicate

A

in the yellow arc or les that 265 lbs

23
Q

When can you put fuel in the Aux tank

A

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

24
Q

Operation with the L/R fuel pressure annunciator illuminated is limited to

25
Propeller Rotatonal Spped Limits Minimum idle speed: Hartzell McCauley
Propeller Rotatonal Spped Limits Minimum idle speed: Hartzell............................................................1180 rpm McCauley........................................................1100 rpm
26
Propeller Autofeather For airplanes equipped with Hartzell propellers the propellers autofeather system must be operable for .... and must be armed for
Propeller Autofeather For airplanes equipped with Hartzell propellers the propellers autofeather system must be operable for .ALL FLIGHT and must be armed for TAKEOFF, CLIMB, APPROACH AND LANDING.
27
CABIN DIFFERENTIAL PRESSURE GUAUGES ``` Green Arc (normal Operating Range )..... Red Arc ( Maximum Operating Limit )...... ```
CABIN DIFFERENTIAL PRESSURE GUAUGES ``` Green Arc (normal Operating Range ).....0 to 6.6 psa Red Arc ( Maximum Operating Limit )...... 6.6 psi to end scale. ```
28
``` Propeller Deice Ammeter Green Arc ( Normal Operation Range) ```
``` Propeller Deice Ammeter Green Arc ( Normal Operation Range).......18 to 24 amperes ```
29
``` Weight Limits Maximum Ramp Weight Maximum Take-off Weight: All Except 14 CFR Part 135 Operation Maximum Landing Weight Maximum Zero Fuel Weight ```
Weight Limits Maximum Ramp Weight .....................12,590 Pounds Maximum Take-off Weight:.....12,500 pounds All Except 14 CFR Part 135 Operation ....12,500 pounds Maximum Landing Weight..........................12,500 pounds Maximum Zero Fuel Weight...................11,000 pounds
30
Weight Limits Maximum weight in baggage compartment: When Equipped with Fold-up Seats When Not Equipped with Fold-up Seats
When Equipped with Fold-up Seats...... 510 pounds | When Not Equipped with Fold-up Seats.....550 pounds
31
What Category is the Beech Super King Air B200/B200c Certified under?
Normal Category Aircraft
32
Acrobatic maneuvers, including spins, are
PROHIBITED
33
PRESSURE-ALTITUDE LIMITS Normal Operation........................................ Operation with Yaw Damp System Inop........
PRESSURE-ALTITUDE LIMITS Normal Operation........................................35,000 ft Operation with Yaw Damp System Inop........17,000 ft
34
Sea Level to 25,000ft pressure altitude | Above 25,000ft pressure altitiude
Sea Level to 25,000ft pressure altitude...... ISA + 37'c | Above 25,000ft pressure altitiude.................ISA +31'c
35
LANDING GEAR CYCLE LIMITS HYDRAULIC LANDING gear 1 Up 1 down are limited to........every........for a total of .......followed by a ..............cool down period.
LANDING GEAR CYCLE LIMITS HYDRAULIC LANDING gear 1 Up 1 down are limited to...1.....every....5min....for a total of ...6 cycles..followed by a ...15 min.....cool down period.
36
Minimum Ambient Temp for operation of Deicing Boots................... Minimum Airspeed for Sustained Icing Flight............
Minimum Ambient Temp for operation of Deicing Boots.......-40 'C Minimum Airspeed for Sustained Icing Flight...140 Knots
37
Icing Limitations Engine anti-ice, left and Right, shall be on for Engine Anti-ice, left and right, shall be off for
Icing Limitations Engine anti-ice, left and Right, shall be on for. Operation in ambient temperature of +5'C or below when flight free of visible moisture cannot be assured. Engine Anti-ice, left and right, shall be off for. takeoff and flight operations in ambient temperatures of above+15'C.
38
ITT Green Arc Normal Operation............. Red Line Maximum Limit....................
ITT Green Arc Normal Operation.............400' to 800'C Red Line Maximum Limit.................... 800'C
39
Torquemeter Green Arc Normal Operating........... Red Line Maximum Limit.............................
Torquemeter Green Arc Normal Operating...........0-2230ft-lbs Red Line Maximum Limit.............................2230ft-lbs
40
``` Propeller tachometer (N2) Red Line Maximum Limit................. ```
``` Propeller tachometer (N2) Red Line Maximum Limit.................2000rpm ```

King Air 200 Limitations (1 decks)

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