Other Limitations Flashcards
Takeoff/Landing Pressure Altitude
Maximum
10,000 feet
Runway Slope
Maximum
+/- 2%
Runway Width
Normal
Narrow
Minimum
148 feet wide or greater
Less than 148 feet but not less than minimum runway width
100 feet
Maximum Airspeed
VMO
MMO
Indicated by max airspeed pointer on airspeed indicated
.82 Mach
Maximum Airspeed
Maximum gear retraction speed
Maximum gear extension speed
Maximum gear operating/extended speed
235 knots
270 knots/.82 Mach
320 knots/.82 Mach
Flap Speeds
1 2 5 10 15 25 30 40
250 250 250 210 or 205 (9ER) 200 or 195 (700) 170, 190, 195 165-180 156-171
QFE Altimetry
Pilots are prohibited from operating with a QFE altimeter setting selected.
VA is defined as:
the speed above which maneuvers involving full application of rudder, ailerons, or elevator, or maneuvers involving angles of attack near stall, should be avoided
Minimum Ground Time After Landing
Steel brakes
Carbon brakes
67 minutes
48 minutes
Portable Oxygen Bottles
Minimum
At least one for each assigned flight attendant
Pressurization
Maximum cabin pressure differential
Maximum differential pressure for takeoff and landing
9.10 PSI
.125 PSI
Duct Pressure
Maximum cooling
20-25 PSI
When engine bleeds are on (either one or both), do not:
operate air conditioning packs in high for takeoff, approach, and landing
Duct Pressure For Two Pack Operation From One Bleed Source
Minimum
Do not operate more than _____ from one engine.
20-25 PSI
one pack (MAX, applies only on the ground)
Engine Anti-Ice
Must be ON during all ground operations, including after landing, when:
Must be ON during all flight operations when icing conditions exist or are anticipated, except during climb and cruise when the temperature is below:
Must be ON prior to and during descent in:
Engine ignition must be selected to ____ prior to and during engine anti-ice operation.
icing conditions exist or are anticipated.
-40°C SAT
all icing conditions, including temperatures below -40°C SAT
CONT
Wing Anti-Ice
Use wing anti-ice during all operations between engine start and takeoff when:
Do not operate wing anti-ice on the ground when the OAT is above:
Do not use wing anti-ice as a substitute for:
Use of wing anti-ice above approximately ____ may cause ____ and possible loss of cabin pressure.
icing conditions exist or are anticipated, unless the aircraft is or will be protected by the application of Type II or Type IV fluid.
10°C/50°F
ground deicing/anti-icing
FL 350, bleed trip off
Autolandings
Autoland capability may only be used to runways at or below:
The ILS autoland capability may only be used with flaps ____ and ____ with both ____ operative.
Maximum and minimum glideslope angles for autoland are :
The autoland system shall not be used for:
Autolands with the ____ as Pilot Flying are not authorized.
8400 feet pressure altitude.
30, 40, engines
3.25° and 2.5°
overweight landings.
First Officer
Wi-Fi System
Do not operate the KA GND TX ENABLE switch in the OVERRIDE position or the WIFI COMM ENABLE/BROADBAND SYSTEM switch in the ON position during:
deicing, when maintenance is being performed in the vicinity of the WiFi radome, or in a hangar
Battery Voltage For APU Start
Minimum
23 volts
Engine Ignition
Ignition must be on for:
Takeoff, Landing, Engine anti-ice operation, Heavy rain
Engine Oil Pressure
Oil pressure must be in the normal range for takeoff.
Minimum
13 PSI, 17.4 (MAX)
Engine Oil Temperature
Minimum starting (MAX)
Minimum takeoff (MAX)
Maximum
-40°C
31°C
155°C
