Limitations Flashcards
Maximum Operating Altitude with Flaps and/or Slats Extended
20,000’
Severe Turbulence Penetration Airspeed - Below 25,000’
290 kts
Severe Turbulence Penetration Airspeed - At or Above 25,000’
310 kts / .84M
Maximum Tailwind Component for Takeoff and Landing
15 kts
Maximum Takeoff Demonstrated Crosswind (-8)
40 kts
Maximum Takeoff Demonstrated Crosswind (-9)
33 kts
Maximum Landing Demonstrated Crosswind (-8)
37 kts
Maximum Landing Demonstrated Crosswind (-9)
40 kts
Weather Radar - Hangar
Avoid weather radar operation:
- In a hangar,
- When personnel are within the area normally enclosed by the aircraft nose radome.
Engine Anti-Ice
Ground.
Engine anti-ice must be selected ON _____ after ____ _____ are started and remain on during all ground operations when icing conditions exists or are anticipated, except when the temperature is below _____.
CAUTION
Do NOT use engine anti-ice when OAT is above ____.
Immediately; both engines; -40°C OAT.
10°C
Engine Anti-Ice
Inflight.
Engine anti-ice must be _____ or ____ when icing conditions exists or are anticipated, except when the temperature is below _____.
CAUTION
Do NOT use engine anti-ice when TAT is above ____.
AUTO or ON; -40°C SAT
15°C
Minimum Height for Autopilot Use after Takeoff
200’ AGL
Minimum Height for Autopilot Use Without LAND 2 or LAND 3 Annunciated
135’ AGL
Minimum Height for Autopilot Use In Go-Around Mode - Autopilot Already Engaged
None
Minimum Height for Autopilot Use In Go-Around Mode - Autopilot NOT Yet Engaged
200’
Autoland capability may only be used for operations into runways at or below _____ airport field elevation.
8,400’
Maximum Autoland Glideslope Angle
-3.25°
Minimum Autoland Glideslope Angle
-2.5°
HF Radio Operation During Refueling
Do NOT operate during refueling operations.
Oil Temperature must be greater than _____ for enigne start
-40°C
Minimum Oil Quantity for Dispatch Indicated on ENG Display
20 quarts
Reverse Thrust
Intentional selection of reverse thrust inflight is
Prohibited.
Backing the aircraft with reverse thrust is
Prohibited.
Flight Loads
Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g., large slideslip angles) as they may result in structural failures at any speed, including below VA.
