Limitations Flashcards
Tire speed
204 kts
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
Maximum speed operating in RVSM airspace
0.90 Mach
Ground wind limits for all doors
- 40 knots while opening or closing
* 65 knots while open
Takeoff/Landing Crosswind Guidelines (including peak gust): Good
Dry
Wet
Dry 30/30
Wet 25/25
Takeoff/Landing Crosswind Guidelines (including peak gust)
Medium - Poor
15/10
Maximum Taxi Weight
395.9
Maximum Takeoff Weight
394.6
Maximum Landing Weight
295.7
Maximum Zero Fuel Weight
276.6
Minimum Flight Weight
166.6
Maximum differential pressure (relief valves)
9.4 psi
Maximum allowable cabin pressure differential for
takeoff and landing
0.11 psi
The autopilot must not be engaged below ___ feet after takeoff
250
The autopilot must not be engaged below ___ feet during enroute operation.
500
The autopilot must be disengaged below ___ feet in a single channel ILS approach
150
The autopilot must be disengaged below ___ feet in a non-precision approach.
360
Do not use FLCH on final approach below ___ feet airport field elevation
1,000
Autoland - Flaps
25 or 30 only
Autoland - Glideslope Angle
Maximum 3.25º
Minimum 2.5º
Automatic landings require _ operating hydraulic systems
4
Autoland - Maximum Wind Component
Headwind
Tailwind
Crosswind
25 knots
15 knots
25 knots
Do not operate HF radios during ___
refueling operations
Do not operate the weather radar (3)
in a hangar
within 50 feet of any personnel
within 50 feet of a fuel spill
Remove any power cords from all flight deck PC power outlets before ____
using a hand microphone
Desired Oxygen Pressures - Crew/Pass system
1,200/1,200
Personnel entering main cargo deck during flight ____
will carry a portable oxygen bottle
The smoke barrier door must be closed during ____
taxi, takeoff, flight and landing
EGT Limits -
Starting
Takeoff
Continuous
750 (870 - 40 sec)
960 (5 min)
925
Minimum Oil Pressure
10 psi
Max Oil Temperature -
Continuous
Transient (15 min)
160º C
175º C
Continuous ignition must be ON encountering: (5)
- heavy rain
- severe turbulence
- volcanic ash
- icing conditions
- standing water or slush on runway
APU Limits - Between starts wait: 1 and 2 \_\_ min 2 and 3 \_\_ min 3 and 4 \_\_ min
Between battery starts wait:
1 minute
1 minute
75 minutes
The maximum altitude with flaps extended is ______ feet
20,000
Flight Maneuvering Load Acceleration Limits -
Flaps Up
Flaps Down
+2.5g to -1.0g
+2.0g to 0.0g
Use of speed brakes in flight with flaps extended past __ is not recommended
20
From engine start until shutdown at the completion of flight, _______ are the primary means of alerting the flight crews to non-normal conditions or improper configuration
EICAS Alert messages (Warning, Caution, Advisory)
Maximum speed in RVSM Airspace
0.90 Mach
The maximum allowable in-flight difference between Captain and First Officer altitude displays for RVSM operations is ______
200 feet
The maximum allowable on-the-ground altitude display difference for RVSM between Captain and First Officer -
SL to 5,000 ft - 35 feet
10,000 ft - 40 feet
The maximum allowable on-the-ground altitude display difference for RVSM operations between CA/FO and Field Elevation -
75 feet
IFR approach procedures using VNAV to a DA(H) are not authorized if the path angle is less than ____ or more than ____ degrees
- 75
3. 50
Do not extend or retract the flaps between positions __ and __ during fuel jettison
1 and 5
The use of ___ and ___ fuels are prohibited
Jet B and JP4
In-flight tank fuel temperature must be maintained at least ___ above the fuel freezing point of the fuel being used
3° C
Jet A Freeze Point -
- 40 C
Jet A1 Freeze Point -
-47 C
Nacelle anti-ice must be ON during all ground and flight operations when icing conditions exist or are anticipated, except when the temperature is below ____
-40°C OAT
Icing conditions exist when the OAT on the ground or TAT in-flight, is (4)
10°C or below, and;
- visible moisture in any form is present
- When operating on ramps, taxiways or runways with snow, ice, standing water or slush
- When the difference between the temperature and dew point is less than 3°C
Do not use anti-ice if OAT or TAT exceeds ____
10°C
Ice crystal conditions exist when in visible moisture and one or more of the following indications are present: (4)
- Amber or red weather radar returns below the airplane.
- Appearance of liquid water on the windshield at temperatures too cold for rain (the sound is different than rain).
- The autothrottle is unable to maintain the selected airspeed.
- TAT indication on EICAS remains near 0°C.
TAT should normally increase approximately __°C per ___ feet of descent
2°C per 1,000 feet
Flap Placard Speed (VFE) 1 5 10 20 25 30
1 - 280 5 -260 10 - 240 20 -230 25 -205 30 -180
Landing Gear Operating Speeds:
Retract or Extend (VLO/MLO) -
Extended (VLE/MLE) -
270/0.82
320/0.82
The total number of persons carried, including crew, shall not exceed __
10
Access to the cargo compartment during ___, ___, ___, and ___ is prohibited
Taxi, Takeoff, Flight, and Landing
Mode 4 of the GPWS must be determined to be operational before takeoff by verifying that a ____ status message is not displayed on EICAS before engine start, and a ____ advisory message is not displayed on EICAS after engine start and before takeoff
GND PROX SYS
GND PROX SYS
Above _______ full maneuver capability is not attained until reaching __________
309,000 kgs
VREF 30 + 100 knots.
