-
Maneuvering Speed (VA) (300)
184 KIAS
-
Maneuvering Speed (VA) (ER)
182 KIAS
-
Max Flap Extension / Extended (VFE) (ER & 300)
- Approach: 202 KIAS
- Full Down: 158 KIAS
-
Max Landing Gear Operating Speed (VLO) (300)
- Extension: 184 KIAS
- Retraction: 166 KIAS
-
Max Landing Gear Operating Speed (VLO) (ER)
- Extension: 182 KIAS
- Retraction: 164 KIAS
-
Air Min Control Speed (VMCA) (300)
- Flaps Up: 94 KIAS
- Flaps Down: 93 KIAS
-
Air Min Control Speed (VMCA) (ER)
- Flaps Up: 101 KIAS
- Flaps Down: 98 KIAS
-
Max Operating Speed (VMO) (300)
- To 21,000': 263 KIAS
- Above 21,000': .58 Mach
-
Max Operating Speed (VMO) (ER)
- To 24,000': 245 KIAS
- Above 24,000': .58 Mach
-
Two Engine Best Rate of Climb (VY) (300)
140 KIAS
-
Two Engine Best Rate of Climb (VY) (ER)
135 KIAS
-
Turbulent Air Penetration
170 KIAS
-
Max Airspeed for Effective Windshield Anti-Icing
226 KIAS
-
Min Airspeed for Sustained Flight in Icing
140 KIAS
-
Intentional One-Engine Inop Speed (VSSE) (300)
110 KIAS
-
Intentional One-Engine Inop Speed (VSSE) (ER)
135 KIAS
-
One-Engine Inop Best Angle of Climb (VXSE) (300)
125 KIAS
-
One-Engine Inop Best Rate of Climb (VYSE) (300)
125 KIAS
-
One-Engine Inop Best Angle of Climb (VXSE) (ER)
135 KIAS
-
One-Engine Inop Best Rate of Climb (VYSE) (ER)
135 KIAS
-
Emergency Descent (300)
184 KIAS
-
Emergency Descent (ER)
182 KIAS
-
-
Torque Limits: Takeoff
100%
-
Torque Limits: Max Continuous
100%
-
Torque Limits: Transient
156% for 20sec
-
Inadvertent torque excursions up to ___% are limited to ___.
102% ; 7minutes
-
ITT Limits: Starting
1000oC for 5sec
-
-
ITT Limits: Takeoff
820oC
-
ITT Limits: Max Continuous
820oC
-
ITT Limits: Transient
850oC for 20sec
-
ITT Limits: Cruise / Climb
785oC
-
ITT Limits: Max Reverse
760oC
-
N1% Limits: Takeoff
104% N1
-
N1% Limits: Max Continuous
104% N1
-
N1% Limits: Cruise / Climb
104% N1
-
N1% Limits: Max Cruise
104% N1
-
N1% Limits: Transient
104% N1
-
N1% Limits: Idle
62% N1 (min)
-
N2 Limits: Idle
1050 min RPM
-
N2 Limits: Takeoff
1700 RPM
-
N2 Limits: Max Continuous
1700 RPM
-
N2 Limits: Cruise / Climb
1700 RPM
-
N2 Limits: Max Cruise
1700 RPM
-
N2 Limits: Max Reverse
1650 RPM
-
N2 Limits: Transient
1870 RPM for 20sec
-
Inadvertent propeller excursions up to ____ are time limited to ___.
1735 RPM ; 7 minutes
-
Sustained prop overspeeds faster than ____ indicate failure of the primary governor. Flight may be continued at propeller overspeeds up to ___, provided torque is limited to ___. Sustained propeller overspeeds faster than ___ indicate failure of both the primary governor and the secondary governor and such overspeeds are not approved.
1700 RPM ; 1768 RPM ; 96% ; 1768 RPM
-
Autofeather must be operable for:
All Flights
-
Autofeather must be armed for:
Takeoff - Climb - Approach - Landing
-
Oil Px Limits: Starting
0-200 psi
-
Oil Px Limits: Idle
60 psi (min)
-
Oil Px Limits: Normal (T/O, Max Cont, Cruise/Climb, Max Cruise, Max Reverse)
90-135 PSI
-
Oil Px Limits: Transient
200 psi
-
Undesireable Oil Px Limits
<90 PSI
-
Under emergency conditions oil px permitted:
60 PSI with reduced power of 62% Torque
-
Unsafe oil px requiring shutdown or min power to land:
<60 PSI
-
Acceptable oil fluctuations:
+/- 10 PSI
-
Oil Temp Limits: Normal (& Idle)
-40 thru 110oC
-
Oil Temp Limits: Starting
-40oC (min)
-
Oil Temp Limits: T/O, Max Cont, Cruise/Climb, Max Cruise, Transient
0 thru 110oC
-
Oil Temp Limits: Max Reverse
0 thru 99oC
-
External Power Carts: ____ v
Sustained: ____ amps
Momentary: ____ amps
- 28-28.4 Volts
- 300 Amps
- 1000 Amps
-
Starter Limits:
- 30 sec On 5 min Off
- 30 sec On 5 min Off
- 30 sec On 30 min Off
-
Total Useable Fuel
3611 lbs
-
Total Useable Fuel (ER)
5192 lbs
-
Max Allowable Fuel Imabalance
300 lbs
-
Don't take off if fuel gages each read less than:
265 lbs
-
Don't put any fuel into the ___ unless both the auxiliary and main tanks are full (ER).
extended range tanks
-
Max Ramp Weight (300)
15,100 lbs
-
Max Ramp Weight (ER)
16,600 lbs
-
Max Takeoff Weight (ER)
16,500 lbs
-
Max Landing Weight (ER)
15,675 lbs
-
Max Zero Fuel Weight (ER)
13,000 lbs
-
Load Factor
- Flaps Up: -1.24 thru 3.1 Gs
- Flaps Down: 0 thru 2.0 Gs
-
Landing Gear Cycles (1 up & 1 down = 1 cycle)
- 1 every 5 minutes
- Followed by: a 15 min cool down
-
Max Cabin Px Differential
6.6 PSI
-
Rudder boost must be ____ for ___.
operational ; all flights
-
Sustained flight in icing conditions with flaps extended is ___ except for ___ and ___.
prohibited ; approach ; landing
-
Engine anti-ice ON
< 5oC + Visible moisture
-
Engine anti-ice OFF
for takeoff operations in temps > 10oC
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