Limitations Flashcards
Immediate Action Items for:
Cabin Altitude Warning or Rapid Depressurization / Emergency Descent
- Oxygen Masks and Regulators - On, 100%
- Crew Communications - Establish
- Seatbelt sign - On
Ref: QRC
Immediate Action Items for:
Engine Start - Aborted Start
Engine start lever (affected engine) - CUTOFF
Ref: QRC
Landing Crosswind Component - Runway CC 6
37 knots
Ref: FM 1.20.7
Landing Crosswind Component - Runway CC 5
37 knots
Ref: FM 1.20.7
Takeoff Crosswind Component - Runway CC 6
33 knots
Ref: FM 1.20.7
Takeoff Crosswind Component - Runway CC 5
25 knots
Ref: FM 1.20.7
Maximum Cabin Pressure Differential
9.10 PSI
Ref: FM 1.30.3
Minimum duct pressure for two pack operation from one bleed source
20-25 PSI
Ref: FM 1.30.3
Icing conditions exist on the ground and for takeoff when:
OAT is 10C or below with visible moisture, standing water, slush, or snow
Ref: FM 1.30.4
Icing conditions exist in flight when:
TAT is 10C or below with visible moisture
Ref: FM 1.30.4
Window heat must be on ____ minutes prior to takeoff.
10
Ref: FM 1.30.5
Autopilot minimum engagement height
400 feet AGL
Ref: FM 1.30.6
Autoland maximum headwind
25 knots
Ref: FM 1.30.5
Autoland maximum crosswind
15 knots
Ref: FM 1.30.7
Autoland maximum tailwind
10 knots (except 900[401-412] with flaps 30)
Ref: FM 1.30.5
Autopilot use prohibited ____ feet radio altitude at airport pressure altitudes above ____ feet.
100; 8400
Ref:
Minimum altitude for autopilot use on approach for
- ILS/GLS coupled approaches
- Non-precision approaches
50 feet AGL
50 feet below MDA/DA
Ref:
Maximum runway pressure altitude for autoland
8400 feet
Ref:
Maximum and minimum glideslope angles for autoland
2.5 - 3.25 degrees
Ref:
Do not use LVL CHG on final approach below ____
1000 ft AFE
Ref: FM 1.30.10
Minimum battery voltage for APU start
23 volts
Ref:
Minimum Oil Pressure for NG, MAX
NG - 13 PSI
MAX - 17.4 PSI
Ref:
Maximum EGT for Start - NG, MAX
NG - 725C
MAX - 753C
Ref: FM 1.30.13
Maximum continuous EGT - NG, MAX
NG - 925C
MAX - 1013C
Ref: FM 1.10.13
Minimum Engine Oil Quantity for Start
70%
Ref:
Wait a minimum of ____ for APU shutdown cycle to complete, then turn ____ switch to OFF (NG)
120 seconds
Ref:
Maximum Flap Extension Altitude
20,000 feet
Ref: FM 1.30.17
In flight, the speed brake lever should not be extended beyond the _______ detent with greater than flaps ___ selected.
ARMED; 10
Ref: FM 1.30.18
Maximum airspeed to extend the flaps with the alternate system
230 knots
Ref: FM 1.30.18
Maximum speed with Mach Trim Fail
280 knots / 0.82 mach
Ref:
Minimum inflight fuel temperature for Jet A and Jet A-1
-37C and -44C, respectively
Ref:
Maximum tire groundspeed
NG - 195 knots
MAX - 204 knots
Ref:
Maximum Operating Pressure Altitude
41,000 feet
Ref:
Autobrake action for RTO occurs above ____ wheel speed.
90 knots for NG, 88 knots for MAX
Ref:
G Limits for Flaps up and Flaps down
Flaps up: -1.0 - 2.5
Flaps down: 0 - 2.0
Ref: FM 1.20.2
Maximum takeoff/landing pressure altitude
10,000 feet
Ref:
Minimum Runway Width
100 feet
Ref:
Maximum Takeoff/Landing Tailwind Component
15 knots
Ref:
MMO
0.82 Mach
Ref: FM 1.20.4
Maximum Gear Retraction Speed
235 knots
Ref:
Maximum Gear Extension Speed
270 knots / 0.82 Mach
Ref:
Maximum Gear operating/extended speed
320 knots / 0.82 Mach
Ref:
Maximum severe turbulence penetration speed - cruise
TURB N1 setting from cruise page
Ref:
Recommended Severe Turbulence Penetration Speed - climb and descent
280 knots / 0.76 Mach
Ref:
Minimum Ground Time After Landing - Carbon Brakes
48 minutes
Ref:
Do not deploy the speed brakes at radio altitudes less than _____
1000 feet
Ref:
While extending or retracting the flaps with the ALTERNATE FLAPS position switch, allow _____ seconds after releasing the ALTERNATE FLAPS position switch before moving the switch again.
15
Ref:
A fully charged battery can supply standby power for a minimum of _____ minutes.
30
Ref:
The battery provides ____ volts DC.
28
Ref:
Battery voltage range is ____ to ____ volts
22, 30
Ref:
The Transformer Rectifiers convert ____ volt _____ to ____ volt ____
115 volt AC, 28 volt DC
Ref:
What busses are powered by the standby power system?
DC standby bus, AC standby bus, battery bus
Ref:
Fuel LOW Alert illuminates when fuel quantity is less than ______ lbs in the related main tank, and remains until fuel tank quantity is increased to ______ lbs.
2000, 2500
Ref:
The Fuel CONFIG Alert displays when either engine is running, both center tank pump switches are OFF, and center tank fuel quantity is greater than ______ lbs.
1600
Ref:
The Fuel IMBAL Alert displays when main tanks differ by more than ______ lbs and remains until the imbalance is reduced to ____ lbs.
1000; 200
Ref:
