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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

A

1000 Lbs

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

A

10 Hours

25
Q

Propeller Rotatonal Spped Limits

Minimum idle speed:
Hartzell
McCauley

A

Propeller Rotatonal Spped Limits

Minimum idle speed:
Hartzell……………………………………………………1180 rpm
McCauley………………………………………………..1100 rpm

26
Q

Propeller Autofeather
For airplanes equipped with Hartzell propellers the propellers autofeather system must be operable for …. and must be armed for

A

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
Q

CABIN DIFFERENTIAL PRESSURE GUAUGES

Green Arc (normal Operating Range ).....
Red Arc ( Maximum Operating Limit )......
A

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
Q 
Propeller Deice Ammeter
Green Arc ( Normal Operation Range)
A 
Propeller Deice Ammeter
Green Arc ( Normal Operation Range).......18 to 24 amperes
29
Q 
Weight Limits       
Maximum Ramp Weight         
       Maximum Take-off Weight:
       All Except 14 CFR Part 135 Operation 
Maximum Landing Weight
Maximum Zero Fuel Weight
A

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
Q

Weight Limits
Maximum weight in baggage compartment:
When Equipped with Fold-up Seats
When Not Equipped with Fold-up Seats

A

When Equipped with Fold-up Seats…… 510 pounds

When Not Equipped with Fold-up Seats…..550 pounds

31
Q

What Category is the Beech Super King Air B200/B200c Certified under?

A

Normal Category Aircraft

32
Q

Acrobatic maneuvers, including spins, are

A

PROHIBITED

33
Q

PRESSURE-ALTITUDE LIMITS

Normal Operation………………………………….
Operation with Yaw Damp System Inop……..

A

PRESSURE-ALTITUDE LIMITS

Normal Operation………………………………….35,000 ft
Operation with Yaw Damp System Inop……..17,000 ft

34
Q

Sea Level to 25,000ft pressure altitude

Above 25,000ft pressure altitiude

A

Sea Level to 25,000ft pressure altitude…… ISA + 37’c

Above 25,000ft pressure altitiude……………..ISA +31’c

35
Q

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.

A

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
Q

Minimum Ambient Temp for operation of Deicing Boots……………….
Minimum Airspeed for Sustained Icing Flight…………

A

Minimum Ambient Temp for operation of Deicing Boots…….-40 ‘C
Minimum Airspeed for Sustained Icing Flight…140 Knots

37
Q

Icing Limitations

Engine anti-ice, left and Right, shall be on for

Engine Anti-ice, left and right, shall be off for

A

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
Q

ITT
Green Arc Normal Operation………….
Red Line Maximum Limit………………..

A

ITT
Green Arc Normal Operation………….400’ to 800’C
Red Line Maximum Limit……………….. 800’C

39
Q

Torquemeter

Green Arc Normal Operating………..
Red Line Maximum Limit………………………..

A

Torquemeter

Green Arc Normal Operating………..0-2230ft-lbs
Red Line Maximum Limit………………………..2230ft-lbs

40
Q 
Propeller tachometer (N2)
Red Line Maximum Limit.................
A 
Propeller tachometer (N2)
Red Line Maximum Limit.................2000rpm

King Air 200 Limitations (1 decks)

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