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43 Cards in this Set

  • Front
  • Back
Min for reverse
40
VMC
86
VA(flaps approach or down)
111
Max tire speed (high float)
139
Minimum in icing conditions
140
Max flaps beyond approach
157
Max gear retraction
163
recommended turbulence penetration speed
170
max gear extension
181
VA (FLAPS UP)
181
Max tire speed standard gear
156
Max Flaps Extension
200
Max Windshield de-icing
226
VMO
259
Mmo
.52
Pneumatic Pressure
12-20 Normal
20 Max
Starter Limitations
40 sec on 1 min off
40 sec on 1 min off
40 sec on 30 min off
Torque limitations
20% - 100% Normal Operating range
123 Max transient (5 sec)
49 Max props below 1600
81 Max props above 2000
Turbine tachometer (N1) limitations
61% Min low idle
70% Approx. high idle
88% Max Reverse (1 min)
101.5% Max
102.6 Max transient (10sec)
TGT limitations
750*C Max low idle
750* C Max Reverse
770* C Recom. Cruise/Max Cruise Climb
800* C Max continuous/takeoff/cruise
850*C Max transient
1000*C Max during engine start
Engine Malfunction Before V1 (Abort).
If
an engine fails and the aircraft has not accelerated to
recommended decision speed (V1), retard POWER
levers to IDLE and stop the aircraft.
1. POWER – IDLE.
2. Braking – As required.
Engine Malfunction After V1.
1. GEAR (positive climb) – UP.
2. POWER – As required.
3. FLAPS (105 KIAS) – UP.
IF THE PROP DID NOT FEATHER, PERFORM
STEP 4.
4. PROP lever (dead engine) – FEATHER.
ONCE THE PROP IS FEATHERED, PERFORM
STEPS 5 THROUGH 8.
O 5. TCAS – Set TA.
6. LANDING/TAXI LIGHTS – OFF.
7. BRAKE DEICE – OFF.
8. Engine cleanup – Perform.
NOTE
Holding 3° to 5° bank (1/4 to 1/2 ball width)
toward the operating engine will assist in
maintaining directional control and
improving aircraft performanc
Engine Malfunction During Flight.
1. Autopilot/yaw damper – Disengage.
2. POWER – As required.
3. Dead engine – Identify.
4. PROP lever (dead engine) – FEATHER.
5. GEAR – As required.
6. FLAPS – As required.
O 7. TCAS – Set TA.
8. POWER – Set for single-engine cruise.
SINGLE-ENGINE GO-AROUND.
1. POWER – As required.
2. FLAPS – APPROACH.
3. GEAR (Positive climb)- UP
4. FLAPS (105 KIAS) – UP.
5. LANDING/TAXI LIGHTS – OFF.
6. POWER – As required.
7. YD– As required.
Engine Fire in Flight (Identified).
1. POWER lever – IDLE.
2. PROP lever – FEATHER.
3. CONDITION lever – FUEL CUT –
OFF.
4. Fuel FIREWALL SHUTOFF VALVE –
CLOSED.
5. PUSH TO EXTINGUISH switch –
Push as required.
6. Engine cleanup – Perform.
7. Land as soon as practicable.
G load limitations
-1.27 to 3.17 Flaps up( 12,500)
-1.24 to 3.10 Flaps up ( 14,000lbs)
0 to to 2.0 flaps approach or down
AC/DC power limitations
380-420 normal HZ
105 -120 Normal Volts AC
27.5 - 29 Normal Voltz DC
85% Max load on the ground
100% Max load < 31000ft
88% Max > 3100f0t
Propeller RPM Limitations
1180 Max low idle
1600 - 2000 Normal
1900 Max reverse (1 min)
2000 Max
2200 Max transient (5 sec)
Climb Speeds
160 up to 10000 feet
140 10000 -20000
130 20000 -25000
120 25000-35000
Weight limitations
14000 Max T/O weight
14090 Max ramp weight
12500 Max landing weight
11000 Max zero fuel weight
550 Max baggage compartment weight
300 Max airstair door weight
1 Hour Min Flt duration > 12500
10000 Min Altitude > 12500
Autopilot Limitations
1.Satisfactory preflight
2. Must have pilot at the controls
3. Don't use below 200 AGL/ TO& landing
4. 120 min coupled approaches
5. 259 KIAS/.52 Mach
6. VOR NAV or APP- DME and
NAV same source
Oil Pressure limitations
60 Minimum low idle
60 - 85 Max Torque 49%
85 -135 Normal > 21000ft
100 -135 Normal < 21000ft
Oil temperature limatations
-40 to 99 Start/Low idle/ High idle
0-99 Max Reverse ( 1 min)
0 to 99 Takeoff/ Max Cont./ Cruise Climb
0 to 104 Max transient ( 5min)
Battery Note from chapter 8
If the battery is partially discharged, the
BATTERY CHG annunciator will illuminate
approximately 6 seconds after external
power is on line. If the annunciator does
not extinguish within 5 minutes, refer to
the Battery Chg Annunciator Illuminated
procedure in Chapter 9.
 3. AUTOFEATHER/AUTO IGNITION – Check
as required.
a. AUTO IGNITION switches – ARM.
b. POWER levers – 22% torque. Auto
ignition annunciators extinguish.
c. AUTOFEATHER switch – Hold to TEST.
Both AUTOFEATHER annunciators
illuminated.
d. POWER levers – Retard individually.
AUTOFEATHER annunciators will
illuminate and extinguish with each
fluctuation of torque as the propeller
feathers.
(1) Approximately 16 to 21% torque,
opposite AUTOFEATHER
annunciator extinguishes, IGN ON
annunciator illuminated.
(2) Approximately 9 to 14% torque, both
AUTOFEATHER annunciators
extinguished (prop begins to feather).
(3) Return POWER levers to
approximately 22% torque.
e. Repeat procedure with other engine.
f. POWER levers – IDLE.
g. AUTOFEATHER switch – ARM.
h. AUTO IGNITION switches – OFF.
5-32. TEMPERATURE LIMITS.
a. The aircraft shall not be operated when the
ambient temperatures are warmer than ISA +37 °C at
sea level to 25,000 feet, or ISA +31 °C above 25,000
feet.
b. The ice vanes shall be extended for
operations in ambient temperatures of 5 °C or below
when flight free of visible moisture cannot be assured.
c. Minimum free air temperature for operation of
deicing boots shall be –40 °C
f. Engine Malfunction During Final
Approach. If an engine malfunctions during final
approach, after Landing Check, the propeller should
not be manually feathered unless time and altitude
permit or conditions require it. Continue approach
using the following procedure:
1. POWER – As required.
2. GEAR – DN.
g. Engine Malfunction (Second Engine). If
the second engine fails, do not feather the propeller if
an engine restart is to be attempted. Engine restart
without starter assist cannot be accomplished with a
feathered propeller, and the propeller will not unfeather
without the engine operating. The airspeed to fly will
depend upon whether or not a restart will be
attempted, and whether or not the restart attempt will
be accomplished with or without starter assist. If no
restart is to be attempted, use maximum glide speed
from Figure 9-2. Perform the following procedure if the
second engine fails during cruise flight.
1. Airspeed – As required.
2. PROP lever – As required.
e. Smoke and Fume Elimination. To eliminate
smoke and fumes from the aircraft, perform the
following:
1. Crew oxygen masks – 100% and on.
2. Passenger oxygen – ON.
9-29. EMERGENCY DESCENT.
1. POWER levers – IDLE.
2. PROP levers – HIGH RPM.
3. FLAPS – APPROACH.
4. GEAR – DN.
5. Airspeed – 181 KIAS maximum.
d. Electrical Fire. Upon noting the existence or
indications of an electrical fire, turn off all affected
electrical circuits, if known. If electrical fire source is
unknown, perform the following:
1. Crew oxygen masks – As required.
2. Passenger oxygen – As required.
3. MASTER SWITCH – OFF (visual
conditions only).
4. All nonessential electrical equipment – Off.
(1) Engine/Nacelle Fire During Start or
Ground Operations. If engine/nacelle fire is identified
during start or ground operation, perform the following:
(1) Engine/Nacelle Fire During Start or
Ground Operations. If engine/nacelle fire is identified
during start or ground operation, perform the following:
1. PROP levers – FEATHER.
2. CONDITION levers – FUEL CUTOFF.
3. Fuel FIREWALL SHUTOFF VALVES
– CLOSED.
CAUTION
If fire extinguisher has been used to
extinguish an engine fire, do not attempt to
restart until maintenance personnel have
inspected the aircraft and released it for
flight.
4. PUSH TO EXTINGUISH switch –
Push.
5. MASTER SWITCH – OFF.
9-25. PROPELLER FAILURE, OVER 2120 RPM.
If an overspeed condition occurs that cannot be
controlled with the PROP lever or by reducing power,
perform the following:
1. POWER lever (affected engine) – IDLE.
2. PROP lever (Affected Engine) –
FEATHER.
3. CONDITION lever – As required.
4. Engine cleanup – As required.