Limitations Flashcards
Maximum Runway Slope
+/- 2%
Maximum Takeoff and Landing Tailwind Component
15 Knots
Maximum Operating Altitude
45,100 feet pressure altitude
Maximum Takeoff and Landing Altitude
10,000 feet pressure altitude
Maximum Field Elevation
9,500 feet pressure altitude
Maximum speed Operating in RVSM Airspace
0.90 Mach
Turbulent Air Penetrating Speed
290 KIAS to 310 KIAS or
0.82 Mach to 0.85 Mach
Whichever is LOWER
Maximum Takeoff and Landing Crosswind
30 KIAS (not limiting)
DO NOT USE H.F. Radio’s During _________
refueling
Avoid Weather Radar use within ___ of Fuel Spill
50’
Maximum in-flight Difference between Captain and F/O Altitudes for RVSM
200 feet
Maximum on-ground difference between Captain and F/O Altitudes for RVSM
Field Elevation Max. Difference between Captain and F/O Max Difference between Captain, F/O and Field Elevation Sea Level to 5,000’ 35 feet 75 feet 9,500 feet 40 feet 75 feet
Emergency evacuation slide must be in ________ mode and knob must be visible prior to Taxi, Takeoff and Landing
AUTOMATIC
Maximum Taxi Weight
395,986 Kilograms
Maximum Takeoff Weight
394,625 Kilograms
Maximum Landing Weight
295,742 Kilograms
Maximum Zero Fuel Weight
276,691 Kilograms
Maximum Differential Pressure
9.4 psi
Maximum Allowable Cabin Differential Pressure for Takeoff and Landing
0.11 psi
If Pack _ available, Do NOT move the Pack 3 Control Lever to ___ during normal ground operations unless Pack _ and _ are selected OFF
3, OFF, 1 and 2
Use of aileron trim with autopilot engaged is ______
prohibited
Autopilot must NOT be engaged below
250’ AGL after takeoff
Autopilot must be disengaged before descending more than
50’ below MDA unless coupled to ILS glideslope or in GA mode
For Single channel ILS approach, autopilot must be disengaged before descending below
100’ AGL
Do NOT use FLCH on Final Approach below
1000’ AFE
Maximum allowable wind speeds when weather minima are predicted on autoland operations:
Headwind 25 Knots
Tailwind 15 Knots
Crosswind 25 Knots
Maximum and Minimum Glideslope angles:
Maximum: 3.25 degrees
Minimum: 2.5 degrees
Autoland with Flaps
25 or Flaps 30 ONLY
Maximum Fuel
Temperature: (Jet A, Jet A-1, JP-5 or JP-8)
54°C (130°F)
Must be maintained at least 3°C above Fuel Freezing point
Continuous Ignition must be ON for:
- Heavy Rain
- Severe Turbulence • Volcanic Ash
- Icing Conditions
- Standing Water or Slush on Runway
Thrust Reversers in Flight is _________?
Prohibited
Backing airplane with use of Thrust Reversers is ____?
Prohibited
If leveling off within _____ after changing altimeter setting from QNE to QNH, or QNH to QNE, do NOT use _____ to execute level off if QNH is less than __.__ in / 1006 hPa.:
2,000’, VNAV, 29.70
Avoid rapid and large alternating control inputs, especially in combination with large changes in _____
pitch, roll or yaw
Maximum Flap extension:
20,000 ‘
Use of Speedbrakes in flight with flaps extended beyond ____ is NOT recommended
20
Do NOT use terrain display for
Navigation
The use of Look-ahead terrain alerting and terrain display function is prohibited within
15 nm of takeoff, approach or landing at airport or runway not contained in GPWS database.
