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482 Cards in this Set
- Front
- Back
|
Take off decision speed |
V1
|
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Take off safety speed
|
V2
|
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Climb speed
|
V35
|
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Maneuvering speed
|
Va
|
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Single engine enroute climb speed
|
Venr
|
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Single engine enroute climb speed
|
Venr
|
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Maximum flap extended speed
|
Vfe
|
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Single engine enroute climb speed
|
Venr
|
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Maximum flap extended speed
|
Vfe
|
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Maximum landing gear extended speed
|
Vfe
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Single engine enroute climb speed
|
Venr
|
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Maximum flap extended speed
|
Vfe
|
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Maximum landing gear extended speed
|
Vle
|
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Maximum landing gear operating speed
|
Vlo
|
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Min. airspeed in flight at wich directional control can be maintained
|
Vmc 83kts flaps zero / 76kts flaps 15
|
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Min. airspeed in flight at wich directional control can be maintained |
Vmc 83kts flaps zero / 76kts flaps 15
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Min. Airspeed on gound at wich directional control can be maintained with one eng suddengly INOP using only aerodynamic controls
|
Vmcg 79kts
|
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Maximum Operating Limit Speed
|
Vmo or Mmo
|
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Maximum Operating Limit Speed
|
Vmo or Mmo
|
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Rotation speed
|
Vr
|
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Maximum Operating Limit Speed
|
Vmo or Mmo
|
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Rotation speed
|
Vr
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Airspeed equal to the 50ft point with flaps in landing position and landing gear extended (1.3 Vso)
|
Vref
|
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Maximum Operating Limit Speed
|
Vmo or Mmo
|
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Rotation speed
|
Vr
|
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Airspeed equal to the 50ft point with flaps in landing position and landing gear extended (1.3 Vso)
|
Vref
|
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Stalling speed or minimum flight speed in the landing configuration
|
Vso
|
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Stalling speed or the minimum steady flight speed obtained in a specified configuration
|
Vs1
|
|
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Best Angle of Climb speed
(multiengine, flaps 15) |
Vx 124kts
|
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|
Best Angle of Climb speed
(Multiengine, flaps 15) |
Vy 191kts
|
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Best Angle of Climb speed
(Multiengine, flaps 15) |
Vy 191kts
|
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Maximum ramp weight
|
12,625 lbs
|
|
|
Best Angle of Climb speed
(Multiengine, flaps 15) |
Vy 191kts
|
|
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Maximum ramp weight
|
12,625 lbs
|
|
|
Maximum takeoff weight
|
12,500 lbs
|
|
|
Best Angle of Climb speed
(Multiengine, flaps 15) |
Vy 191kts
|
|
|
Maximum ramp weight
|
12,625 lbs
|
|
|
Maximum takeoff weight
|
12,500 lbs
|
|
|
Maximum Landing Weight
|
11,525 lbs
|
|
|
Best Angle of Climb speed
(Multiengine, flaps 15) |
Vy 191kts
|
|
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Maximum ramp weight
|
12,625 lbs
|
|
|
Maximum takeoff weight
|
12,500 lbs
|
|
|
Maximum Landing Weight
|
11,525 lbs
|
|
|
Maximum Zero Fuel Weight
|
9,700 lbs
|
|
|
Best Angle of Climb speed
(Multiengine, flaps 15) |
Vy 191kts
|
|
|
Maximum ramp weight
|
12,625 lbs
|
|
|
Maximum takeoff weight
|
12,500 lbs
|
|
|
Maximum Landing Weight
|
11,525 lbs
|
|
|
Maximum Zero Fuel Weight
|
9,700 lbs
|
|
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Engine type
|
Williams FJ44-3A-24
|
|
|
Best Angle of Climb speed
(Multiengine, flaps 15) |
Vy 191kts
|
|
|
Maximum ramp weight
|
12,625 lbs
|
|
|
Maximum takeoff weight
|
12,500 lbs
|
|
|
Maximum Landing Weight
|
11,525 lbs
|
|
|
Maximum Zero Fuel Weight
|
9,700 lbs
|
|
|
Engine type
|
Williams FJ44-3A-24
|
|
|
Engine start maximum tailwind
|
12kts
|
|
|
Engine start maximum crosswind
|
16 kts
|
|
|
Engine start maximum crosswind
|
16 kts
|
|
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Starting: Maximum time to light-off
|
10 sec
|
|
|
Engine start maximum crosswind
|
16 kts
|
|
|
Starting: Maximum time to light-off
|
10 sec
|
|
|
Minimum engine oil temperature
|
-40C
|
|
|
Engine start maximum crosswind
|
16 kts
|
|
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Starting: Maximum time to light-off
|
10 sec
|
|
|
Minimum engine oil temperature
|
-40C
|
|
|
Maximum airport elevation for ground battery start
|
10,000 ft
|
|
|
Engine start maximum crosswind
|
16 kts
|
|
|
Starting: Maximum time to light-off
|
10 sec
|
|
|
Minimum engine oil temperature
|
-40C
|
|
|
Maximum airport elevation for ground battery start
|
10,000 ft
|
|
|
Maximum airport elevation for ground external power start
|
10,000 ft
|
|
|
Engine start maximum crosswind
|
16 kts
|
|
|
Starting: Maximum time to light-off
|
10 sec
|
|
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Minimum engine oil temperature
|
-40C
|
|
|
Maximum airport elevation for ground battery start
|
10,000 ft
|
|
|
Maximum airport elevation for ground external power start
|
10,000 ft
|
|
|
Minimum voltage for battery start
|
24 volts
|
|
|
Engine start maximum crosswind
|
16 kts
|
|
|
Starting: Maximum time to light-off
|
10 sec
|
|
|
Minimum engine oil temperature
|
-40C
|
|
|
Maximum airport elevation for ground battery start
|
10,000 ft
|
|
|
Maximum airport elevation for ground external power start
|
10,000 ft
|
|
|
Minimum voltage for battery start
|
24 volts
|
|
|
Minimum/ Maximum Power Current Capacity for start
|
800/ 1000 amps
|
|
|
Engine start maximum crosswind
|
16 kts
|
|
|
Starting: Maximum time to light-off
|
10 sec
|
|
|
Minimum engine oil temperature
|
-40C
|
|
|
Maximum airport elevation for ground battery start
|
10,000 ft
|
|
|
Maximum airport elevation for ground external power start
|
10,000 ft
|
|
|
Minimum voltage for battery start
|
24 volts
|
|
|
Minimum/ Maximum Power Current Capacity for start
|
800/ 1000 amps
|
|
|
Start cycle limitations
|
3 engine starts in 30min
3cycles of operation with a 60sec rest between cycles |
|
|
Engine start maximum crosswind
|
16 kts
|
|
|
Starting: Maximum time to light-off
|
10 sec
|
|
|
Minimum engine oil temperature
|
-40C
|
|
|
Maximum airport elevation for ground battery start
|
10,000 ft
|
|
|
Maximum airport elevation for ground external power start
|
10,000 ft
|
|
|
Minimum voltage for battery start
|
24 volts
|
|
|
Minimum/ Maximum Power Current Capacity for start
|
800/ 1000 amps
|
|
|
Start cycle limitations
|
3 engine starts in 30min
3cycles of operation with a 60sec rest between cycles |
|
|
Maximum time for pitot heat on ground
|
2 min
|
|
|
Engine start maximum crosswind
|
16 kts
|
|
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Starting: Maximum time to light-off
|
10 sec
|
|
|
Minimum engine oil temperature
|
-40C
|
|
|
Maximum airport elevation for ground battery start
|
10,000 ft
|
|
|
Maximum airport elevation for ground external power start
|
10,000 ft
|
|
|
Minimum voltage for battery start
|
24 volts
|
|
|
Minimum/ Maximum Power Current Capacity for start
|
800/ 1000 amps
|
|
|
Start cycle limitations
|
3 engine starts in 30min
3cycles of operation with a 60sec rest between cycles |
|
|
Maximum time for pitot heat on ground
|
2 min
|
|
|
Maximum generator current on ground
|
200 amps
|
|
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Engine start maximum crosswind
|
16 kts
|
|
|
Ground operation greater than 75% N2 with engine, wing or windshield anti-ice ON
|
2 min
|
|
|
Starting: Maximum time to light-off
|
10 sec
|
|
|
Minimum engine oil temperature
|
-40C
|
|
|
Maximum airport elevation for ground battery start
|
10,000 ft
|
|
|
Maximum airport elevation for ground external power start
|
10,000 ft
|
|
|
Minimum voltage for battery start
|
24 volts
|
|
|
Minimum/ Maximum Power Current Capacity for start
|
800/ 1000 amps
|
|
|
Start cycle limitations
|
3 engine starts in 30min
3cycles of operation with a 60sec rest between cycles |
|
|
Maximum time for pitot heat on ground
|
2 min
|
|
|
Maximum generator current on ground
|
200 amps
|
|
|
Engine start maximum crosswind
|
16 kts
|
|
|
Ground operation greater than 75% N2 with engine, wing or windshield anti-ice ON
|
2 min
|
|
|
Windshield Ice Protection Fluid
|
Isopropyl alcohol
|
|
|
Starting: Maximum time to light-off
|
10 sec
|
|
|
Minimum engine oil temperature
|
-40C
|
|
|
Maximum airport elevation for ground battery start
|
10,000 ft
|
|
|
Maximum airport elevation for ground external power start
|
10,000 ft
|
|
|
Minimum voltage for battery start
|
24 volts
|
|
|
Minimum/ Maximum Power Current Capacity for start
|
800/ 1000 amps
|
|
|
Start cycle limitations
|
3 engine starts in 30min
3cycles of operation with a 60sec rest between cycles |
|
|
Maximum time for pitot heat on ground
|
2 min
|
|
|
Maximum generator current on ground
|
200 amps
|
|
|
Engine start maximum crosswind
|
16 kts
|
|
|
Ground operation greater than 75% N2 with engine, wing or windshield anti-ice ON
|
2 min
|
|
|
Windshield Ice Protection Fluid
|
Isopropyl alcohol
|
|
|
Hydraulic Fluid
|
MIL-PRF-83282
|
|
|
Starting: Maximum time to light-off
|
10 sec
|
|
|
Minimum engine oil temperature
|
-40C
|
|
|
Maximum airport elevation for ground battery start
|
10,000 ft
|
|
|
Maximum airport elevation for ground external power start
|
10,000 ft
|
|
|
Minimum voltage for battery start
|
24 volts
|
|
|
Minimum/ Maximum Power Current Capacity for start
|
800/ 1000 amps
|
|
|
Start cycle limitations
|
3 engine starts in 30min
3cycles of operation with a 60sec rest between cycles |
|
|
Maximum time for pitot heat on ground
|
2 min
|
|
|
Maximum generator current on ground
|
200 amps
|
|
|
Engine start maximum crosswind
|
16 kts
|
|
|
Ground operation greater than 75% N2 with engine, wing or windshield anti-ice ON
|
2 min
|
|
|
Windshield Ice Protection Fluid
|
Isopropyl alcohol
|
|
|
Hydraulic Fluid
|
MIL-PRF-83282
|
|
|
Fuel boost pumps on when...
|
Fuel Low Level lights illuminate
(Approx. 220 lbs or less) |
|
|
Starting: Maximum time to light-off
|
10 sec
|
|
|
Minimum engine oil temperature
|
-40C
|
|
|
Maximum airport elevation for ground battery start
|
10,000 ft
|
|
|
Maximum airport elevation for ground external power start
|
10,000 ft
|
|
|
Minimum voltage for battery start
|
24 volts
|
|
|
Minimum/ Maximum Power Current Capacity for start
|
800/ 1000 amps
|
|
|
Start cycle limitations
|
3 engine starts in 30min
3cycles of operation with a 60sec rest between cycles |
|
|
Maximum time for pitot heat on ground
|
2 min
|
|
|
Maximum generator current on ground
|
200 amps
|
|
|
Engine start maximum crosswind
|
16 kts
|
|
|
Ground operation greater than 75% N2 with engine, wing or windshield anti-ice ON
|
2 min
|
|
|
Windshield Ice Protection Fluid
|
Isopropyl alcohol
|
|
|
Hydraulic Fluid
|
MIL-PRF-83282
|
|
|
Fuel boost pumps on when...
|
Fuel Low Level lights illuminate
(Approx. 220 lbs or less) |
|
|
Approved oils
|
Mobile Jet II Mbil 254
|
|
|
Starting: Maximum time to light-off
|
10 sec
|
|
|
Minimum engine oil temperature
|
-40C
|
|
|
Maximum airport elevation for ground battery start
|
10,000 ft
|
|
|
Maximum airport elevation for ground external power start
|
10,000 ft
|
|
|
Minimum voltage for battery start
|
24 volts
|
|
|
Minimum/ Maximum Power Current Capacity for start
|
800/ 1000 amps
|
|
|
Start cycle limitations
|
3 engine starts in 30min
3cycles of operation with a 60sec rest between cycles |
|
|
Maximum time for pitot heat on ground
|
2 min
|
|
|
Maximum generator current on ground
|
200 amps
|
|
|
Engine start maximum crosswind
|
16 kts
|
|
|
Ground operation greater than 75% N2 with engine, wing or windshield anti-ice ON
|
2 min
|
|
|
Windshield Ice Protection Fluid
|
Isopropyl alcohol
|
|
|
Hydraulic Fluid
|
MIL-PRF-83282
|
|
|
Fuel boost pumps on when...
|
Fuel Low Level lights illuminate
(Approx. 220 lbs or less) |
|
|
Approved oils
|
Mobile Jet II Mbil 254
|
|
|
Maximum speeds
|
Mmo .737
|
|
|
Starting: Maximum time to light-off
|
10 sec
|
|
|
Minimum engine oil temperature
|
-40C
|
|
|
Maximum airport elevation for ground battery start
|
10,000 ft
|
|
|
Maximum airport elevation for ground external power start
|
10,000 ft
|
|
|
Minimum voltage for battery start
|
24 volts
|
|
|
Minimum/ Maximum Power Current Capacity for start
|
800/ 1000 amps
|
|
|
Start cycle limitations
|
3 engine starts in 30min
3cycles of operation with a 60sec rest between cycles |
|
|
Maximum time for pitot heat on ground
|
2 min
|
|
|
Maximum speeds
|
Mmo .737 (above FL290) Vmo 278KIAS (between 8,000 and 29,000). Vmo 260 KIAS (below 8,000)
|
|
|
Maximum Turbulent Air Penetration Speed
|
180 KIAS
|
|
|
Maximum Turbulent Air Penetration Speed
|
180 KIAS
|
|
|
Vfe flaps 15
|
200 KIAS
|
|
|
Maximum Turbulent Air Penetration Speed
|
180 KIAS
|
|
|
Vfe flaps 15
|
200 KIAS
|
|
|
Vfe flaps 35
|
161 KIAS
|
|
|
Maximum Turbulent Air Penetration Speed
|
180 KIAS
|
|
|
Vfe flaps 15
|
200 KIAS
|
|
|
Vfe flaps 35
|
161 KIAS
|
|
|
Vfe ground flaps 60
|
140 KIAS Intentional selection of ground flaps in flight is prohibited
|
|
|
Maximum Turbulent Air Penetration Speed
|
180 KIAS
|
|
|
Vfe flaps 15
|
200 KIAS
|
|
|
Vfe flaps 35
|
161 KIAS
|
|
|
Vfe ground flaps 60
|
140 KIAS Intentional selection of ground flaps in flight is prohibited
|
|
|
Vle
|
200 KIAS
|
|
|
Maximum Turbulent Air Penetration Speed
|
180 KIAS
|
|
|
Vfe flaps 15
|
200 KIAS
|
|
|
Vfe flaps 35
|
161 KIAS
|
|
|
Vfe ground flaps 60
|
140 KIAS Intentional selection of ground flaps in flight is prohibited
|
|
|
Vle
|
200 KIAS
|
|
|
Vlo extending
|
200 KIAS
|
|
|
Maximum Turbulent Air Penetration Speed
|
180 KIAS
|
|
|
Vfe flaps 15
|
200 KIAS
|
|
|
Vfe flaps 35
|
161 KIAS
|
|
|
Vfe ground flaps 60
|
140 KIAS Intentional selection of ground flaps in flight is prohibited
|
|
|
Vle
|
200 KIAS
|
|
|
Vlo extending
|
200 KIAS
|
|
|
Vlo retracting
|
200 KIAS
|
|
|
Maximum Turbulent Air Penetration Speed
|
180 KIAS
|
|
|
Vfe flaps 15
|
200 KIAS
|
|
|
Vfe flaps 35
|
161 KIAS
|
|
|
Vfe ground flaps 60
|
140 KIAS Intentional selection of ground flaps in flight is prohibited
|
|
|
Vle
|
200 KIAS
|
|
|
Vlo extending
|
200 KIAS
|
|
|
Vlo retracting
|
200 KIAS
|
|
|
Vsb (maximum speed speed break operation)
|
No limit
|
|
|
Maximum Turbulent Air Penetration Speed
|
180 KIAS
|
|
|
Vfe flaps 15
|
200 KIAS
|
|
|
Vfe flaps 35
|
161 KIAS
|
|
|
Vfe ground flaps 60
|
140 KIAS Intentional selection of ground flaps in flight is prohibited
|
|
|
Vle
|
200 KIAS
|
|
|
Vlo extending
|
200 KIAS
|
|
|
Vlo retracting
|
200 KIAS
|
|
|
Vsb (maximum speed speed break operation)
|
No limit
|
|
|
Maximum Autopilot Speed
|
278 KIAS or .737 Mach
|
|
|
Maximum Turbulent Air Penetration Speed
|
180 KIAS
|
|
|
Vfe flaps 15
|
200 KIAS
|
|
|
Vfe flaps 35
|
161 KIAS
|
|
|
Vfe ground flaps 60
|
140 KIAS Intentional selection of ground flaps in flight is prohibited
|
|
|
Vle
|
200 KIAS
|
|
|
Vlo extending
|
200 KIAS
|
|
|
Vlo retracting
|
200 KIAS
|
|
|
Vsb (maximum speed speed break operation)
|
No limit
|
|
|
Maximum Autopilot Speed
|
278 KIAS or .737 Mach
|
|
|
Maximum Altitude for Takeoff
|
10,000 ft
|
|
|
Maximum Turbulent Air Penetration Speed
|
180 KIAS
|
|
|
Maximum Tailwind for Takeoff and Landing
|
10 kts
|
|
|
Vfe flaps 15
|
200 KIAS
|
|
|
Vfe flaps 35
|
161 KIAS
|
|
|
Vfe ground flaps 60
|
140 KIAS Intentional selection of ground flaps in flight is prohibited
|
|
|
Vle
|
200 KIAS
|
|
|
Vlo extending
|
200 KIAS
|
|
|
Vlo retracting
|
200 KIAS
|
|
|
Vsb (maximum speed speed break operation)
|
No limit
|
|
|
Maximum Autopilot Speed
|
278 KIAS or .737 Mach
|
|
|
Maximum Altitude for Takeoff
|
10,000 ft
|
|
|
Maximum Turbulent Air Penetration Speed
|
180 KIAS
|
|
|
Maximum Tailwind for Takeoff and Landing
|
10 kts
|
|
|
Minimum Temperature fore take-off
|
-54C
|
|
|
Vfe flaps 15
|
200 KIAS
|
|
|
Vfe flaps 35
|
161 KIAS
|
|
|
Vfe ground flaps 60
|
140 KIAS Intentional selection of ground flaps in flight is prohibited
|
|
|
Vle
|
200 KIAS
|
|
|
Vlo extending
|
200 KIAS
|
|
|
Vlo retracting
|
200 KIAS
|
|
|
Vsb (maximum speed speed break operation)
|
No limit
|
|
|
Maximum Autopilot Speed
|
278 KIAS or .737 Mach
|
|
|
Maximum Altitude for Takeoff
|
10,000 ft
|
|
|
Maximum Turbulent Air Penetration Speed
|
180 KIAS
|
|
|
Maximum Tailwind for Takeoff and Landing
|
10 kts
|
|
|
Minimum Temperature fore take-off
|
-54C
|
|
|
Maximum fuel imbalance
|
200 lbs
(but 600 lbs has been demostrated) |
|
|
Vfe flaps 15
|
200 KIAS
|
|
|
Vfe flaps 35
|
161 KIAS
|
|
|
Vfe ground flaps 60
|
140 KIAS Intentional selection of ground flaps in flight is prohibited
|
|
|
Vle
|
200 KIAS
|
|
|
Vlo extending
|
200 KIAS
|
|
|
Vlo retracting
|
200 KIAS
|
|
|
Vsb (maximum speed speed break operation)
|
No limit
|
|
|
Maximum Autopilot Speed
|
278 KIAS or .737 Mach
|
|
|
Maximum Altitude for Takeoff
|
10,000 ft
|
|
|
Minimum cabin temperature prior to take-off
|
0C (because of the oxygen mask)
|
|
|
Minimum cabin temperature prior to take-off
|
0C (because of the oxygen mask)
|
|
|
Maximum tire speed
|
165 KIAS
|
|
|
Minimum cabin temperature prior to take-off
|
0C (because of the oxygen mask)
|
|
|
Maximum tire speed
|
165 KIAS
|
|
|
Maximum operating altitude
|
45,000 ft
|
|
|
Minimum cabin temperature prior to take-off
|
0C (because of the oxygen mask)
|
|
|
Maximum tire speed
|
165 KIAS
|
|
|
Maximum operating altitude
|
45,000 ft
|
|
|
Maximum generator current
|
300 amps to 41,000ft &
250 amps above 41,000ft |
|
|
Minimum cabin temperature prior to take-off
|
0C (because of the oxygen mask)
|
|
|
Maximum tire speed
|
165 KIAS
|
|
|
Maximum operating altitude
|
45,000 ft
|
|
|
Maximum generator current
|
300 amps to 41,000ft &
250 amps above 41,000ft |
|
|
Maximum altitude to extend flaps or gear
|
18,000 ft
|
|
|
Minimum cabin temperature prior to take-off
|
0C (because of the oxygen mask)
|
|
|
Maximum tire speed
|
165 KIAS
|
|
|
Maximum operating altitude
|
45,000 ft
|
|
|
Maximum generator current
|
300 amps to 41,000ft &
250 amps above 41,000ft |
|
|
Maximum altitude to extend flaps or gear
|
18,000 ft
|
|
|
Load factors
|
Flaps up: -1.52G to +3.6G @ 12,500 lbs
Flaps 15-35: 0G to +2G @ 12,500 lbs |
|
|
Minimum cabin temperature prior to take-off
|
0C (because of the oxygen mask)
|
|
|
Maximum tire speed
|
165 KIAS
|
|
|
Maximum operating altitude
|
45,000 ft
|
|
|
Maximum generator current
|
300 amps to 41,000ft &
250 amps above 41,000ft |
|
|
Maximum altitude to extend flaps or gear
|
18,000 ft
|
|
|
Load factors
|
Flaps up: -1.52G to +3.6G @ 12,500 lbs
Flaps 15-35: 0G to +2G @ 12,500 lbs |
|
|
Normal cabin pressurization
|
0 to 8.9 Psi
|
|
|
Minimum cabin temperature prior to take-off
|
0C (because of the oxygen mask)
|
|
|
Maximum tire speed
|
165 KIAS
|
|
|
Maximum operating altitude
|
45,000 ft
|
|
|
Maximum generator current
|
300 amps to 41,000ft &
250 amps above 41,000ft |
|
|
Maximum altitude to extend flaps or gear
|
18,000 ft
|
|
|
Load factors
|
Flaps up: -1.52G to +3.6G @ 12,500 lbs
Flaps 15-35: 0G to +2G @ 12,500 lbs |
|
|
Normal cabin pressurization
|
0 to 8.9 Psi
|
|
|
N1 redline
|
102.9%
|
|
|
Minimum cabin temperature prior to take-off
|
0C (because of the oxygen mask)
|
|
|
Maximum tire speed
|
165 KIAS
|
|
|
Maximum operating altitude
|
45,000 ft
|
|
|
Maximum generator current
|
300 amps to 41,000ft &
250 amps above 41,000ft |
|
|
Maximum altitude to extend flaps or gear
|
18,000 ft
|
|
|
Load factors
|
Flaps up: -1.52G to +3.6G @ 12,500 lbs
Flaps 15-35: 0G to +2G @ 12,500 lbs |
|
|
Normal cabin pressurization
|
0 to 8.9 Psi
|
|
|
N1 redline
|
102.9%
|
|
|
ITT redline
|
1001C
|
|
|
Minimum cabin temperature prior to take-off
|
0C (because of the oxygen mask)
|
|
|
Maximum tire speed
|
165 KIAS
|
|
|
Maximum operating altitude
|
45,000 ft
|
|
|
Maximum generator current
|
300 amps to 41,000ft &
250 amps above 41,000ft |
|
|
Maximum altitude to extend flaps or gear
|
18,000 ft
|
|
|
Load factors
|
Flaps up: -1.52G to +3.6G @ 12,500 lbs
Flaps 15-35: 0G to +2G @ 12,500 lbs |
|
|
Normal cabin pressurization
|
0 to 8.9 Psi
|
|
|
N1 redline
|
102.9%
|
|
|
ITT redline
|
1001C
|
|
|
ITT redline one engine running
|
878C
|
|
|
Minimum cabin temperature prior to take-off
|
0C (because of the oxygen mask)
|
|
|
N2 redline
|
100.8%
|
|
|
Maximum tire speed
|
165 KIAS
|
|
|
Maximum operating altitude
|
45,000 ft
|
|
|
Maximum generator current
|
300 amps to 41,000ft &
250 amps above 41,000ft |
|
|
Maximum altitude to extend flaps or gear
|
18,000 ft
|
|
|
Load factors
|
Flaps up: -1.52G to +3.6G @ 12,500 lbs
Flaps 15-35: 0G to +2G @ 12,500 lbs |
|
|
Normal cabin pressurization
|
0 to 8.9 Psi
|
|
|
N1 redline
|
102.9%
|
|
|
ITT redline
|
1001C
|
|
|
ITT redline one engine running
|
878C
|
|
|
Oil temp redline
|
149C
|
|
|
Oil pressure redline
|
22 Psi
|
|
|
Oil pressure redline
|
22 Psi
|
|
|
Autopilot minimum altitude ILS
|
70 ft
|
|
|
Oil pressure redline
|
22 Psi
|
|
|
Autopilot minimum altitude ILS
|
70 ft
|
|
|
Autopilot minimum altitude non-precision
|
240 ft
|
|
|
Autopilot minimum altitude cruise
|
1,000 ft
|
|
|
Autopilot minimum altitude cruise
|
1,000 ft
|
|
|
Which mode for a VOR approach?
|
Approach mode
|
|
|
Autopilot minimum altitude cruise
|
1,000 ft
|
|
|
Which mode for a VOR approach?
|
Approach mode
|
|
|
Icing conditions exist when the RAT...
|
is +10C or below and visible moisture is present
|
|
|
Autopilot minimum altitude cruise
|
1,000 ft
|
|
|
Which mode for a VOR approach?
|
Approach mode
|
|
|
Icing conditions exist when the RAT...
|
is +10C or below and visible moisture is present
|
|
|
Minimum speed for flight in icing conditions
(except approach ans landing) |
160 KIAS
|
|
|
Autopilot minimum altitude cruise
|
1,000 ft
|
|
|
Which mode for a VOR approach?
|
Approach mode
|
|
|
Icing conditions exist when the RAT...
|
is +10C or below and visible moisture is present
|
|
|
Minimum speed for flight in icing conditions
(except approach ans landing) |
160 KIAS
|
|
|
What position should flaps be in icing conditions?
(except app & ldg) |
Zero degrees, flaps UP
|
|
|
Autopilot minimum altitude cruise
|
1,000 ft
|
|
|
Which mode for a VOR approach?
|
Approach mode
|
|
|
Icing conditions exist when the RAT...
|
is +10C or below and visible moisture is present
|
|
|
Minimum speed for flight in icing conditions
(except approach ans landing) |
160 KIAS
|
|
|
What position should flaps be in icing conditions?
(except app & ldg) |
Zero degrees, flaps UP
|
|
|
Minimum N2 speed for effective wing anti-icing
|
80% N2
|
|
|
Autopilot minimum altitude cruise
|
1,000 ft
|
|
|
Which mode for a VOR approach?
|
Approach mode
|
|
|
Icing conditions exist when the RAT...
|
is +10C or below and visible moisture is present
|
|
|
Minimum speed for flight in icing conditions
(except approach ans landing) |
160 KIAS
|
|
|
What position should flaps be in icing conditions?
(except app & ldg) |
Zero degrees, flaps UP
|
|
|
Minimum N2 speed for effective wing anti-icing
|
80% N2
|
|
|
Minimum temperature for operation of tail deicing boots
|
-35C RAT
|
|
|
Autopilot minimum altitude cruise
|
1,000 ft
|
|
|
Which mode for a VOR approach?
|
Approach mode
|
|
|
Icing conditions exist when the RAT...
|
is +10C or below and visible moisture is present
|
|
|
Minimum speed for flight in icing conditions
(except approach ans landing) |
160 KIAS
|
|
|
What position should flaps be in icing conditions?
(except app & ldg) |
Zero degrees, flaps UP
|
|
|
Minimum N2 speed for effective wing anti-icing
|
80% N2
|
|
|
Minimum temperature for operation of tail deicing boots
|
-35C RAT
|
|
|
Kinds of Equipment for single pilot operations
|
1. Operating autopilot
2. Headset/microphone 3. FAA approved abbreviated checklist 4. Accessible charts |
|
|
Autopilot minimum altitude cruise
|
1,000 ft
|
|
|
Which mode for a VOR approach?
|
Approach mode
|
|
|
Icing conditions exist when the RAT...
|
is +10C or below and visible moisture is present
|
|
|
Minimum speed for flight in icing conditions
(except approach ans landing) |
160 KIAS
|
|
|
What position should flaps be in icing conditions?
(except app & ldg) |
Zero degrees, flaps UP
|
|
|
Minimum N2 speed for effective wing anti-icing
|
80% N2
|
|
|
Minimum temperature for operation of tail deicing boots
|
-35C RAT
|
|
|
Kinds of Equipment for single pilot operations
|
1. Operating autopilot
2. Headset/microphone 3. FAA approved abbreviated checklist 4. Accessible charts |
|
|
Engine failure below V1
|
1. Brakes as required
2. Throttles IDLE 3. Speed brakes EXTEND |
|
|
Autopilot minimum altitude cruise
|
1,000 ft
|
|
|
Which mode for a VOR approach?
|
Approach mode
|
|
|
Icing conditions exist when the RAT...
|
is +10C or below and visible moisture is present
|
|
|
Minimum speed for flight in icing conditions
(except approach ans landing) |
160 KIAS
|
|
|
What position should flaps be in icing conditions?
(except app & ldg) |
Zero degrees, flaps UP
|
|
|
Minimum N2 speed for effective wing anti-icing
|
80% N2
|
|
|
Minimum temperature for operation of tail deicing boots
|
-35C RAT
|
|
|
Kinds of Equipment for single pilot operations
|
1. Operating autopilot
2. Headset/microphone 3. FAA approved abbreviated checklist 4. Accessible charts |
|
|
Engine failure below V1
|
1. Brakes as required
2. Throttles IDLE 3. Speed brakes EXTEND |
|
|
Engine failure above V1
|
1. Maintain directional control
2. Accelerate to Vr 3. Rotate at Vr 4. LDG gear UP 5. Wing X/Flow switch if anti ice is on 6. At 1,500 AGL retract flaps at V2+10 and accelerate to Venr |
|
|
Autopilot minimum altitude cruise
|
1,000 ft
|
|
|
Engine failure during final approach
|
1. Thrust- Increase as required
2. Airspeed Vapp 3. Flaps- Takeoff and Approach |
|
|
Which mode for a VOR approach?
|
Approach mode
|
|
|
Icing conditions exist when the RAT...
|
is +10C or below and visible moisture is present
|
|
|
Minimum speed for flight in icing conditions
(except approach ans landing) |
160 KIAS
|
|
|
What position should flaps be in icing conditions?
(except app & ldg) |
Zero degrees, flaps UP
|
|
|
Minimum N2 speed for effective wing anti-icing
|
80% N2
|
|
|
Minimum temperature for operation of tail deicing boots
|
-35C RAT
|
|
|
Kinds of Equipment for single pilot operations
|
1. Operating autopilot
2. Headset/microphone 3. FAA approved abbreviated checklist 4. Accessible charts |
|
|
Engine failure below V1
|
1. Brakes as required
2. Throttles IDLE 3. Speed brakes EXTEND |
|
|
Engine failure above V1
|
1. Maintain directional control
2. Accelerate to Vr 3. Rotate at Vr 4. LDG gear UP 5. Wing X/Flow switch if anti ice is on 6. At 1,500 AGL retract flaps at V2+10 and accelerate to Venr |
|
|
Autopilot minimum altitude cruise
|
1,000 ft
|
|
|
Engine failure during final approach
|
1. Thrust- Increase as required
2. Airspeed Vapp 3. Flaps- Takeoff and Approach |
|
|
Engine Fire
|
1. Throttle- Affected Eng to IDLE
IF LIGHT REMAINS ON 2. Engine fire switch- Lift cover and PUSH 3. Either bottle illuminated BOTTLE ARMED light push |
|
|
Which mode for a VOR approach?
|
Approach mode
|
|
|
Icing conditions exist when the RAT...
|
is +10C or below and visible moisture is present
|
|
|
Minimum speed for flight in icing conditions
(except approach ans landing) |
160 KIAS
|
|
|
What position should flaps be in icing conditions?
(except app & ldg) |
Zero degrees, flaps UP
|
|
|
Minimum N2 speed for effective wing anti-icing
|
80% N2
|
|
|
Minimum temperature for operation of tail deicing boots
|
-35C RAT
|
|
|
Kinds of Equipment for single pilot operations
|
1. Operating autopilot
2. Headset/microphone 3. FAA approved abbreviated checklist 4. Accessible charts |
|
|
Engine failure below V1
|
1. Brakes as required
2. Throttles IDLE 3. Speed brakes EXTEND |
|
|
Engine failure above V1
|
1. Maintain directional control
2. Accelerate to Vr 3. Rotate at Vr 4. LDG gear UP 5. Wing X/Flow switch if anti ice is on 6. At 1,500 AGL retract flaps at V2+10 and accelerate to Venr |
|
|
Single engine enroute climb speed
|
Venr
|
|
|
Engine restart-two engines
|
1. L/R Boost switches- BOTH ON
2. Throttle-OFF, then IDLE 3. If altitude allows, INCREASE to 230KIAS |
|
|
Electrical fire or smoke
|
1. Oxygen Mask- DON & EMER
2. Mic switch- MIC OXY MASK |
|
|
Electrical fire or smoke
|
1. Oxygen Mask- DON & EMER
2. Mic switch- MIC OXY MASK |
|
|
Enviromental system smoke or odor
|
1. Oxygen mask-DON & EMER
2. Mic switch- MIC OXY MASK |
|
|
Electrical fire or smoke
|
1. Oxygen Mask- DON & EMER
2. Mic switch- MIC OXY MASK |
|
|
Enviromental system smoke or odor
|
1. Oxygen mask-DON & EMER
2. Mic switch- MIC OXY MASK |
|
|
Smoke removal
|
1. Oxygen Mask-DON
2. Mic switch- MIC OXY MASK |
|
|
Electrical fire or smoke
|
1. Oxygen Mask- DON & EMER
2. Mic switch- MIC OXY MASK |
|
|
Enviromental system smoke or odor
|
1. Oxygen mask-DON & EMER
2. Mic switch- MIC OXY MASK |
|
|
Smoke removal
|
1. Oxygen Mask-DON
2. Mic switch- MIC OXY MASK |
|
|
Cabin Altitude Light
|
1. Oxy Mask- DON & 100%
2. Mic switch- MIC OXY MASK 3. Emer Desc- AS REQUIRED 4. Pax Oxy down or manual deploy |
|
|
Electrical fire or smoke
|
1. Oxygen Mask- DON & EMER
2. Mic switch- MIC OXY MASK |
|
|
Enviromental system smoke or odor
|
1. Oxygen mask-DON & EMER
2. Mic switch- MIC OXY MASK |
|
|
Smoke removal
|
1. Oxygen Mask-DON
2. Mic switch- MIC OXY MASK |
|
|
Cabin Altitude Light
|
1. Oxy Mask- DON & 100%
2. Mic switch- MIC OXY MASK 3. Emer Desc- AS REQUIRED 4. Pax Oxy down or manual deploy |
|
|
Emergency Descent
|
1. AP TRIM DISC button-press & release
2. Throttles-IDLE 3. Speed brakes- EXTEND 4. Airplane pitch attitude- INITIALLY TARGET 20 DEGREE PITCH DOWN |
|
|
Electrical fire or smoke
|
1. Oxygen Mask- DON & EMER
2. Mic switch- MIC OXY MASK |
|
|
Enviromental system smoke or odor
|
1. Oxygen mask-DON & EMER
2. Mic switch- MIC OXY MASK |
|
|
Smoke removal
|
1. Oxygen Mask-DON
2. Mic switch- MIC OXY MASK |
|
|
Cabin Altitude Light
|
1. Oxy Mask- DON & 100%
2. Mic switch- MIC OXY MASK 3. Emer Desc- AS REQUIRED 4. Pax Oxy down or manual deploy |
|
|
Emergency Descent
|
1. AP TRIM DISC button-press & release
2. Throttles-IDLE 3. Speed brakes- EXTEND 4. Airplane pitch attitude- INITIALLY TARGET 20 DEGREE PITCH DOWN |
|
|
Battery Overtemp
|
1. Volt/Amp- NOTE
2. Battery switch- EMER 3. Volt/Amp- NOTE |
|
|
Electrical fire or smoke
|
1. Oxygen Mask- DON & EMER
2. Mic switch- MIC OXY MASK |
|
|
Enviromental system smoke or odor
|
1. Oxygen mask-DON & EMER
2. Mic switch- MIC OXY MASK |
|
|
Smoke removal
|
1. Oxygen Mask-DON
2. Mic switch- MIC OXY MASK |
|
|
Cabin Altitude Light
|
1. Oxy Mask- DON & 100%
2. Mic switch- MIC OXY MASK 3. Emer Desc- AS REQUIRED 4. Pax Oxy down or manual deploy |
|
|
Emergency Descent
|
1. AP TRIM DISC button-press & release
2. Throttles-IDLE 3. Speed brakes- EXTEND 4. Airplane pitch attitude- INITIALLY TARGET 20 DEGREE PITCH DOWN |
|
|
Battery Overtemp
|
1. Volt/Amp- NOTE
2. Battery switch- EMER 3. Volt/Amp- NOTE |
|
|
Autopilot malfunction
|
1. AP TRIM DISC Button- PRESS & REALEASE
|
|
|
Electrical fire or smoke
|
1. Oxygen Mask- DON & EMER
2. Mic switch- MIC OXY MASK |
|
|
Enviromental system smoke or odor
|
1. Oxygen mask-DON & EMER
2. Mic switch- MIC OXY MASK |
|
|
Smoke removal
|
1. Oxygen Mask-DON
2. Mic switch- MIC OXY MASK |
|
|
Cabin Altitude Light
|
1. Oxy Mask- DON & 100%
2. Mic switch- MIC OXY MASK 3. Emer Desc- AS REQUIRED 4. Pax Oxy down or manual deploy |
|
|
Emergency Descent
|
1. AP TRIM DISC button-press & release
2. Throttles-IDLE 3. Speed brakes- EXTEND 4. Airplane pitch attitude- INITIALLY TARGET 20 DEGREE PITCH DOWN |
|
|
Battery Overtemp
|
1. Volt/Amp- NOTE
2. Battery switch- EMER 3. Volt/Amp- NOTE |
|
|
Autopilot malfunction
|
1. AP TRIM DISC Button- PRESS & REALEASE
|
|
|
Electric Elevator Trim Runaway
|
1. AP TRIM DISC Button- PRESS & RELEASE
2. Throttles- AS REQUIRED 3. Speed brakes- AS REQUIRED 4. Manual Elevator Trim- AS REQUIRED 5. PITCH TRIM Circuit Breaker (L Panel) PULL |
|
|
Electrical fire or smoke
|
1. Oxygen Mask- DON & EMER
2. Mic switch- MIC OXY MASK |
|
|
Enviromental system smoke or odor
|
1. Oxygen mask-DON & EMER
2. Mic switch- MIC OXY MASK |
|
|
Smoke removal
|
1. Oxygen Mask-DON
2. Mic switch- MIC OXY MASK |
|
|
Cabin Altitude Light
|
1. Oxy Mask- DON & 100%
2. Mic switch- MIC OXY MASK 3. Emer Desc- AS REQUIRED 4. Pax Oxy down or manual deploy |
|
|
Emergency Descent
|
1. AP TRIM DISC button-press & release
2. Throttles-IDLE 3. Speed brakes- EXTEND 4. Airplane pitch attitude- INITIALLY TARGET 20 DEGREE PITCH DOWN |
|
|
Battery Overtemp
|
1. Volt/Amp- NOTE
2. Battery switch- EMER 3. Volt/Amp- NOTE |
|
|
Autopilot malfunction
|
1. AP TRIM DISC Button- PRESS & REALEASE
|
|
|
Electric Elevator Trim Runaway
|
1. AP TRIM DISC Button- PRESS & RELEASE
2. Throttles- AS REQUIRED 3. Speed brakes- AS REQUIRED 4. Manual Elevator Trim- AS REQUIRED 5. PITCH TRIM Circuit Breaker (L Panel) PULL |
|
|
Emergency Evacuation
|
1. Parking brake-SET |
