Limitations Flashcards
Maximum Takeoff and Landing Tailwind Component
15 knots
Severe turbulent air penetration speed (in severe turbulence) is defined as:
270 knots below 25,000 feet,
280 knots or 0.82 Mach whichever is lower at 25,000 feet and above.
Maintain a minimum speed of 15 knots above the minimum maneuvering speed at all altitudes when airspeed is below 0.82 Mach.
Do not operate HF radios
during refueling operations
Avoid weather radar operation in a hangar or within…….. of fueling operations or a fuel spill.
50 feet (15.25 meters)
The autopilot must not be engaged below a minimum engage altitude of
200 feet AGL after takeoff.
Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged
below 200 feet AGL.
Maximum allowable Headwind for an Autoland is
25 knots
Maximum allowable Tailwind for an Autoland is
15 knots
Maximum allowable crosswind for an Autoland is
25 knots (USA – 15 knots)
The maximum glideslope angle for an Autoland is
3.25 degrees.
The minimum glideslope angle for an Autoland is
2.5 degrees.
Automatic landings can be made using flaps 20 or 30, with both engines operative or one engine inoperative. The autopilot flight director system (AFDS) autoland status annunciation must display LAND 2 or LAND 3 and the ………message must not be present.
…………….must not be displayed.
SLATS DRIVE EICAS
SGL SOURCE DISPLAYS, RAD ALT or ILS
Do not use FLCH on final approach below
1,000 feet AFE.
G-YMMA - G-YMMU # Oil temperature must be greater than .......for engine start and ..........before advancing thrust levers to takeoff power.
-40 degrees C
50 degrees C
Intentional selection of reverse thrust in flight is.
prohibited
Backing the airplane with use of reverse thrust is.
prohibited
Avoid rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g. large side slip angles) as they may
result in structural failure at any speed, including below VA.
The maximum altitude with flaps extended is
20,000 feet.
Land climb limit weight:-
There is no requirement to check the Landing Climb Limit Weight chart if you are making a normal weight approach below the WAT limit.
Neither would it be necessary if you are planning to land with Flap 20. Eg SE
So, when should the LCW chart be checked?
IF Landing Overweight AND a Flap 25 or Flap 30 landing is planned.
Or as above with a normal landing above the WAT limit
When you do the Overweight Landing NNC you will notice that at weights over approximately 267T for a -200 and 310T for a -300 you will not be able to use Flap 30.
