Weight Limitations / Airspeed Limitations
DC Electrical Limits / Fuel System Limits
VMCA 103 Q 108.5
VREF 111
VSSE 115 Q 120
VYSE
VENR 130
Recommended for
autopilot coupled approaches
Minimum during icing 140
Turbulence Penetration 150
Max for full flaps 151
Landing gear retraction 160
VA 167
VLE 179
Max for approach flaps 197
Max for windshield anti-ice 226
VMO below 11,500’ & Max for 248
autopilot operation
MMO from 11,500’ to FL 350 .472 mach / Max Ramp Weight 16,620 lbs
Max Takeoff 16,500 lbs
Max Landing Weight 15,675 lbs
Max Zero Fuel Weight 13,100 lbs
Airstair Door Limit 300 lbs
Toilet Seat for T/O & 238 lbs
Landing
Max fuel imbalance 300 lbs
Usable Capacity 540 gals
Min for takeoff 265 lbs (mains)
Max time with
FUEL PRESS light on 10 hours
Operating with AVGAS 150 hours
Standby boost pumps on when
Using AVGAS 15,000’
Standby boost pumps on when
Using JP4 30,000’ / Starter Limits
40 seconds ON, 15 minutes OFF
40 seconds ON, 30 minutes OFF
Ground Power Unit
Must be able to supply:
1000 amps for 5 seconds
500 amps for 2 minutes
300 amps continuously
Landing Gear Cycling Limits / Deicing Boot Limits
Brake Deice Limits / Pitot Heat
Engine Ice Vane
Limits
½” Ice build up prior to activating surface deice
¼” Ice build up prior to activating antenna deice
16 psi minimum for deice boot inflation
with one bleed air source inoperative
Below - 40o C operation of deice boots can cause permanent damage / 5 complete cycles (extension and retraction)
in a 20 minute period
10 to 15 minute cooling period between 20
minute time groupings
Cycle rate should not exceed 10 cycles
equally spaced in 1 hour
Use of pitot heat on the ground limited to 15
minutes to prevent damage to the heating elements
Extend the Engine Ice Vanes when operating in visible moisture when temperatures are +5o C and below / Max temp for operation of brake deice is 15o C
Max auto cycle with gear retracted is 10 minutes
Brake deice off for single engine operations
Min 85% N1 for simultaneous use of brake
deice and surface deice
Engine Torque Limits / TGT Limits
N1
(Gas Generator) Limits / N2
(Prop) Limits
Starting - 1000oC (5sec)
Transient - 870oC (20 sec)
Takeoff - 840oC (5 min)
Max Cont - 830oC (Emergency)
Max Cruise/Climb - 810oC
Norm Cruise/Climb - 800oC
Max Reverse - 760oC
Low Idle - 750oC / Transient - 138% (20sec)
Max - 100%
Prop 1700 - 83%
Prop 1500 - 94%
Max reverse - 75%
Prop < 1000 - 54%
Transient - 1870 (20sec)
Max Cont - 1700
Max Reverse - 1650
Minimum - 1000
(unless feathered) /
Max - 104%
Max Reverse - 88%
High Idle - 72%
Low Idle/ Min - 62%
Engine Oil Pressure Limits / Engine Oil Temperature Limits
Miscellaneous Limitations /
Miscellaneous Limitations (cont)
Maximum - 110oC (10 min)
Low Idle/
Transient - -40 - 110oC
Continuous - -40 - 105oC
(actual limits)
Recommended - 75 - 80oC / Max - 200 psi
Continuous - 90 - 135 psi
Low Idle/ Min - 60 psi
Transient - 40 - 200 psi
Pressure less than 90 psi undesirable. 60 - 90 psi permissible
not to exceed 54% TQ
Max G’s flaps up or approach +3.02 to -1.21
Max G’s flaps full +2.00 to 0.00
Pitch limits 30o
Bank limits 60o
Max operating temperature
to FL 250 ISA +37oC
Max operating temperature
above FL 250 ISA +31oC
Windshield heat on Freezing level or
10,000’ AGL /
Min altitude for autopilot 200’ AGL
Max operating altitude FL 350
Max cabin differential 6.5 psi
Max altitude for inop yaw damper 17,000’
Q 12,000’
Max design sink rate 500 fpm
Max demonstrated crosswind 20 kts @ 90o
Engine Malfunction prior to or at V1 (Abort) / Engine Failure after V1
Engine Malfunction During Flight / Engine Malfunction During
Final Approach
1.  Power - Max Allowable
2.  Gear - UP
3.  Propeller - Verify feathered / 1.  Power Levers - GROUND FINE
2.  Braking - As required
1.  Power - As required
2.  Gear - DOWN / 1.  Autopilot/ Yaw Damp - Disengage
2.  Power - As required
3.  Dead Engine - Identify
4.  Power Lever (dead engine) - IDLE
5.  Prop Lever (dead engine) - FEATHER
Single Engine Go Around / Engine Malfunction
(Second Engine)
Loss of Pressurization/ Smoke and Fume Elimination/ Electrical Fire / Propeller Failure
(Over 1802 RPM)
1.  Airspeed - As required
2.  Power Lever - IDLE
3.  Prop Lever - As required / 1. Power - Max Allowable
2. Gear - UP
3. Flaps - UP
4. Airspeed - VYSE
1. Power lever (affected engine) - IDLE
2. Prop Lever - FEATHER / 1. Crew Oxygen Masks - On and 100%
Engine/ Nacelle Fire During Start or Ground Operations / Engine Fire in Flight
(Identified)
Engine Fire in Flight (Fire Pull Handle Illuminated) / Emergency Descent
1.  Power Lever - IDLE
2.  Prop Lever - FEATHER
3.  Condition Lever - FUEL CUT-OFF
4.  Fire Pull Handle - Pull
5.  Fire Extinguisher - Actuate as Required / 1.  Prop Levers - FEATHER
2.  Condition Levers - FUEL CUT-OFF
3.  Fire Pull Handle - Pull
4.  Push to Extinguish Switch - Push
5.  Master Switch - Off
1.  Power Levers - IDLE
2.  Prop Levers - High RPM
3.  Flaps - APPROACH
4.  Gear - DOWN
5.  Airspeed - 179 KIAS Max / 1.  Power Lever (affected engine) - IDLE
2.  If pull handle light extinguishes - Advance Power
3.  If fire pull handle is still illuminated:
Engine Fire in Flight Procedure - Perform