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43 Cards in this Set
- Front
- Back
Min for reverse
|
40
|
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VMC
|
86
|
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VA(flaps approach or down)
|
111
|
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Max tire speed (high float)
|
139
|
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Minimum in icing conditions
|
140
|
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Max flaps beyond approach
|
157
|
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Max gear retraction
|
163
|
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recommended turbulence penetration speed
|
170
|
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max gear extension
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181
|
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VA (FLAPS UP)
|
181
|
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Max tire speed standard gear
|
156
|
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Max Flaps Extension
|
200
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Max Windshield de-icing
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226
|
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VMO
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259
|
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Mmo
|
.52
|
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Pneumatic Pressure
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12-20 Normal
20 Max |
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Starter Limitations
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40 sec on 1 min off
40 sec on 1 min off 40 sec on 30 min off |
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Torque limitations
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20% - 100% Normal Operating range
123 Max transient (5 sec) 49 Max props below 1600 81 Max props above 2000 |
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Turbine tachometer (N1) limitations
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61% Min low idle
70% Approx. high idle 88% Max Reverse (1 min) 101.5% Max 102.6 Max transient (10sec) |
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TGT limitations
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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 |
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Engine Malfunction Before V1 (Abort).
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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. |
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Engine Malfunction After V1.
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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 |
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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. |
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SINGLE-ENGINE GO-AROUND.
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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. |
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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. |
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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 |
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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 |
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Propeller RPM Limitations
|
1180 Max low idle
1600 - 2000 Normal 1900 Max reverse (1 min) 2000 Max 2200 Max transient (5 sec) |
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Climb Speeds
|
160 up to 10000 feet
140 10000 -20000 130 20000 -25000 120 25000-35000 |
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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 |
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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 |
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Oil Pressure limitations
|
60 Minimum low idle
60 - 85 Max Torque 49% 85 -135 Normal > 21000ft 100 -135 Normal < 21000ft |
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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) |
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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. |
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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. |