MANEUVERING SPeed Va
181 KIAS
MAXIMUM fLAP EXTENSION/extended SPEED Vfe Approach Position 40% (White Triangle)
FULL Down Position 100%
Approach Flaps 40%
Full Flaps 100%
Vlo Extension……………………………………….
Vlo Retraction………………………………………
…………………………………………181 KIAS
………………………………………….163KIAS
Maximum Landing Gear Extended Speed
Vle…………………181 KIAS
Air Minimum Controls Speed Vmca ( Red Line)
Vmca 86 Kias
Maximum Operating Speed
Vmo……………………………………..259 KIAS
Mmo…………………………………….0.52 Mach
White Arc (Full Flap Operating Range )
75 To 157 KIAS
Wide White Arc………………………………….
Narrow White Arc…………………………………
Upper Limit…………………………………………
Lower Limit………………………………………..
……………………75 TO 99 KIAS
…………………….157 KIAS
……………………..99 KIAS
Vyse (blue Line )…………………………………
Vxse............................................................
…………………………………….121 KIAS
……………………………………..115KIAS
SHP
Takeoff & MAX Cont………………………………
………………………………………850SHP
Takeoff & Max Cont………………………………
Transient………………………………………………..
Takeoff & Max Cont……….2230 Ft-Lbs
Transient…………….. 2750 Ft-LBS for 5 Seconds
Maximum Observed ITT ‘C
Starting………………………………………………………………
Low Idle………………………………………………………………
Takeoff & Max Cont & Max Cruise…………………….
Max Reverse………………………………………………………
Transient………………………………………………………….
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
Prop RPM N2 Takeoff & Max Cont & Max Cruise Max Reverse Transient Overspeed Governor up to 2120 RPM
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
Oil Press PSI
Minimum………………………..
Maximum………………………..
Transient…………………….
Oil Press PSI
Minimum………………………..60 psi
Maximum………………………..135 psi
Transient…………………….200psi
Oil Temp ‘C
Starting……………………………………
Takeoff & Max Cont……………….
Transient………………………………….
Oil Temp ‘C
Starting……………………………………-40’C( min )
Takeoff & Max Cont……………….0’C to +99’C
Transient…………………………………. 0’C to + 104’C
EXTERNAL POWER LIMITS
Set to…………volts, Minimum of ……. amps momentarily
and……..amps continuously
EXTERNAL POWER LIMITS
Set to.28.0-28.4.volts, Minimum of 1.000 amps momentarily
and 300 amps continuously
GENERATOR LIMITS
SEA LEVER TO 31,000 FEET ALTITUDE…..
ABOVE 31,000 FEET ALTITUDE………..
GROUND OPERATION………………………
GENERATOR LIMITS
SEA LEVER TO 31,000 FEET ALTITUDE…..100%
ABOVE 31,000 FEET ALTITUDE………..88%
GROUND OPERATION………………………85%
STARTER LIIMITS
…………..ON,……………………..OFF
…………..ON,……………………..OFF
…………..ON,……………………..OFF
STARTER LIIMITS
….40 SEC……….ON,…….60..SEC….OFF
….40 SEC……….ON,…….60..SEC….OFF
….40 SEC……….ON,…….30..MIN….OFF
FUEL MANAGEMENT
TOTAL USABLE FUEL……………………….
EACH MAIN TANK FUEL SYSTEM…….
EACH AUXILIARY FUEL TANK……………
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
Maximum fuel imbalance between wing fuel systems
1000 Lbs
Crossfeeding of fuel is permitted only when
One engine is inoperative
Do not takeoff if fuel quantity gauges indicate
in the yellow arc or les that 265 lbs
When can you put fuel in the Aux tank
Do not put any fuel into aux tank unless main tanks are full
Operation with the L/R fuel pressure annunciator illuminated is limited to
10 Hours
Propeller Rotatonal Spped Limits
Minimum idle speed:
Hartzell
McCauley
Propeller Rotatonal Spped Limits
Minimum idle speed:
Hartzell……………………………………………………1180 rpm
McCauley………………………………………………..1100 rpm
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.
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.
Propeller Deice Ammeter Green Arc ( Normal Operation Range)
Propeller Deice Ammeter Green Arc ( Normal Operation Range).......18 to 24 amperes
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
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
What Category is the Beech Super King Air B200/B200c Certified under?
Normal Category Aircraft
Acrobatic maneuvers, including spins, are
PROHIBITED
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
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
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.
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
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.
ITT
Green Arc Normal Operation………….
Red Line Maximum Limit………………..
ITT
Green Arc Normal Operation………….400’ to 800’C
Red Line Maximum Limit……………….. 800’C
Torquemeter
Green Arc Normal Operating………..
Red Line Maximum Limit………………………..
Torquemeter
Green Arc Normal Operating………..0-2230ft-lbs
Red Line Maximum Limit………………………..2230ft-lbs
Propeller tachometer (N2) Red Line Maximum Limit.................
Propeller tachometer (N2) Red Line Maximum Limit.................2000rpm