Limitations Flashcards
Maximum take-off tailwind
10kts
Maximum landing tailwind
15 kts
Crosswind PVD take-off
15kts
Bird strike Protection speed
Do not exceed 313kts below 8,000ft
Turbulent air penetration speed
290kts / .78 Mach, whichever is lower.
After take-off, the autopilot must not be engaged below
500 feet AGL.
Use of aileron trim with autopilot engaged
Is prohibited.
Max autoland Headwind
25kts
Max autoland Tailwind
15kts
Max autoland crosswind
25kts
Max autoland crosswind USA Ops
15kts
In an approach using v/s mode, the autopilot must be disengaged
At or above 250 feet ARTE (above runway threshold elevation)
On a single channel ILS approach, disengage the autopilot at
Not less than 150 feet ARTE
Maximum operating altitude?
43,100 feet
The Autopilot must be disengaged in severe turbulence
Unless CWS is installed and selected.
The maximum & minimum glide slope angle for automatic landings are
3.1 degrees & 2.5 degrees
Automatic landings may be made with flaps
25 or 30 only.
For automatic landings how may hydraulic systems must be operating?
All three.
For automatic landing how many electrical systems must be operating?
Two electrical systems (the APU generator may be used to power one system.
For automatic landing the inertial reference system IRS associated with the engaged autopilots
Must be in NAV mode.
For automatic landing what autoland status annunciations and how many autopilots engaged below 600 feet?
At least 2 autopilots & LAND 2 or LAND 3
Do not use FLCH
on final approach below 1000 feet AFE.
The auto throttle on a single engine approach
must not be used.
Continuous ignition must be on (engine start selector in the CONT position)
while operating in severe turbulence.
[Note: continuous ignition is automatically provided in icing conditions when engine anti-ice is on.]
Max engine EGT TAKEOFF
785 degrees C 5 mins
[increased to 10 mins provides this use is restricted to situations where an engine failure actually occurs, and there is an obstacle in the takeoff flight path.]
Max engine EGT Maximum Continuous
733 degrees C
Max engine EGT Starting
600 degrees C
Max engine EGT Overtemperature
805 degrees C 20 seconds
Fuel imbalance, wing tanks less than 21,773 kg
1134 kg
[linear reduction between figures[
Fuel imbalance, wing tanks more than 36,200 kg
680 kg
[linear reduction between figures]
Reverse thrust
Ground use only.
The maximum altitude for flap extension is
20,000 feet
