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74 Cards in this Set
- Front
- Back
Manufacturer Maximum Altitude
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FL 410
|
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AWAC Maximum Altitude
|
FL 370
|
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Maximum Takeoff and Landing Altitude
|
10,000 ft
|
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Minimum Takeoff and Landing
|
-1,000 ft
|
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Can you fly in RVSM with 1 Autopilot?
|
Yes
|
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Can you fly in RVSM with 1 Transponder (Altitude reporting kind)?
|
Yes, but Autopilot/FD must be on the working Transponders side.
|
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Can you fly in RVSM with 1 Air Data Computer?
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No, both must be operational.
|
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Required Equipment for flight into RVSM?
|
Autopilot (1)
Altitude Alerting System Altitude Reporting Transponder (1) Air Data Computer (2) |
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Maneuvering Limits (g-loads)
Flaps Retracted |
-1g to +2.5g
|
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Maneuvering Limits (g-loads)
Flaps extended (all positions) |
0g - +2.0G
|
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Minimum Takeoff Temp. (ambient)
|
-40C
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Maximum Takeoff Temp. (-1,000 to sea level)
|
+50C
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Maximum Takeoff Temp. (sea level to 10,000 ft)
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ISA +35C
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Maximum Enroute Temp. (sea level to 10,000 ft)
|
ISA +35C
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Maximum Enroute Temp. (above 10,000ft)
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ISA +30C
|
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Max speed to operate Flaps 8
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200 KIAS
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Max speed to operate Flaps 20
|
200 KIAS
|
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Max speed to operate Flaps 30
|
185 KIAS
|
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Max speed to operate Flaps 45
|
170 KIAS
|
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Max Landing gear Extension speed (VLOE)
|
250 KIAS
|
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Max Landing gear Retraction speed (VLOR)
|
200 KIAS
|
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Turbulence penetration speed
|
Most restrictive of 280 KIAS or .75 Mach
|
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Tire Limit speed
|
182 KIAS
|
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Max Ramp Weight
|
53,250 lbs
|
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Max Takeoff Weight
|
53,000 lbs
|
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Max Landing Weight
|
47,000 lbs
|
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Max Zero Fuel Weight
|
44,000 lbs
|
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Min Flight Weight
|
33,000 lbs
|
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ADG (A/C 401-404, 431, 432, 433)
Max speed for Flight test/Training Deployment |
215 KIAS
Time limit - None |
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ADG (A/C 401-404, 431, 432, 433)
Max speed following accidental or manual deployment |
250 KIAS
Time limit - None |
|
ADG (A/C 401-404, 431, 432, 433)
Max speed when Operationally Necessary (windmilling air-starts) |
251 - 330 KIAS
Time limit - 12min 331 - 335 KIAS Time limit - 4 min |
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Maximum Runway slope
|
+2%
|
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Minimum Runway slope
|
-2%
|
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Maximum Crosswind on
Wet Runway |
24 knots
|
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Maximum Crosswind on
Dry Runway |
27 knots
|
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Maximum Crosswind on
Snow or ice covered Runway |
15 knots
|
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Maximum Tailwind for Takeoff
|
10 knots
|
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Max Contaminated Runway Operation Depths for Takeoff
Standing water |
0.50"
|
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Max Contaminated Runway Operation Depths for Takeoff
Slush |
0.50"
|
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Max Contaminated Runway Operation Depths for Takeoff
Wet snow |
1.00"
|
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Max Contaminated Runway Operation Depths for Takeoff
Dry snow |
3.00"
|
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Max Contaminated Runway Operation Depths for Landing
Standing water |
0.75"
|
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Max Contaminated Runway Operation Depths for Landing
Slush |
0.88"
|
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Max Contaminated Runway Operation Depths for Landing
Wet snow |
1.50"
|
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Max Contaminated Runway Operation Depths for Landing
Dry snow |
3.75"
|
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Maximum Rotation rate during Takeoff
|
3º per second
|
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During a Precision Approach, when can the Flaps be extended out of 0?
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Reported visibility(or RVR) is confirmed to be at or above the landing minima for the approach and can be reasonably expected to remain above until after landing.
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During a Non-Precision Approach when can the Flaps be extended out of 0?
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Reported ceiling and visibility(or RVR) is confirmed to be at or above the landing minima for the approach and can be reasonably expected to remain above until after landing.
|
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Single engine taxi Maximum N1 limitation
|
55%
|
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Can you Single engine taxi on taxiways contaminated with snow?
|
No. Not authorized on surfaces contaminated with snow or ice.
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2 Airports that Single engine taxi are prohibited?
|
DCA and HPN
|
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If cargo is in the cargo compartment how far away must a suitable airport be during flight?
|
45 min
|
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Minimum amount of static wicks (trailing dischargers) on the CL-65?
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Top (outboard most) (2) trailing dischargers on each winglet and horizontal tail end cap must be intact.
|
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When is a tactile check required during a Preflight walkaround?
|
OAT is 5°C; or
wing fuel temp is 0°C; or atmospheric conditions have been conducive to frost formation. |
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Max differential pressure
Positive |
8.7 psi
|
|
Max differential pressure
Negative |
-0.5 psi
|
|
Max differential pressure
During taxi, takeoff, and landing |
0.1 psi
|
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Auto-Flight restricted modes
|
PITCH
DES during approach |
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On a Visual Approach what is the Minimum Altitude for autopilot use?
|
400 ft AGL
AWAC policy is to disconnect the A/P at 50 ft below the approved MDA or DH, or the limit above which ever is higher. |
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On a Non-Precision Approach what is the Minimum Altitude for autopilot use?
|
400 ft AGL
AWAC policy is to disconnect the A/P at 50 ft below the approved MDA or DH, or the limit above which ever is higher. |
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On a Precision Approach what is the Minimum Altitude for autopilot use?
|
80 ft AGL
AWAC policy is to disconnect the A/P at 50 ft below the approved MDA or DH, or the limit above which ever is higher. |
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APU EGT Limit
|
743ºC
|
|
APU EGT Limit (starting)
|
974ºC
|
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APU RPM % Limit
|
107%
|
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Maximum Altitude for APU Bleed air extraction
|
15,000 ft MSL
|
|
During flight, can you use the APU to start an engine?
|
Only during a double engine failure.
Limited to below 13,000 ft MSL for bleed air extraction. |
|
Max permissible load on APU Generator in flight.
|
30kVA
|
|
Max Altitude to start APU
|
FL300
|
|
Minimum ambient temp for starting a cold-soaked APU on the ground
|
-40ºC
|
|
APU Starting
Max Continuous Cranking times using the GPU |
15 seconds
|
|
APU Starting
Max Continuous Cranking times using the Battery |
30 seconds
|
|
APU Starting
How much rest time in between start attempts |
After 1st - 2 minutes
After 2nd - 20 minutes After 3rd - 2 minutes After 4th - No further attempts for at least 40 minutes. |
|
AC Electrical Load Limits for
APU |
0 to FL370 - 30kVA
|
|
AC Electrical Load Limits for
Engine Driven Generator |
0 to FL350 - 30kVA
FL350 to FL370 - 25kVA |