Black Limitations Flashcards
Maximum tire ground speed:
182 Knots.
Max defueling pressure:
-10 PSI.
Maximum (VMO) Above 8000 feet and below 8000 feet:
305 above, 270 below.
Maximum takeoff and landing altitude:
14,000 feet.
Icing conditions exist on the ground when operating on Contaminated runway surfaces or the following conditions are present:
- SAT is 10C or below.
- Visible moisture (Clouds, precipitation, or fog with visibility less than 1 am) is present.
Passenger oxygen mask are not approved for sustained operation above ____ feet.
25,000 feet.
Zero fuel weight:
21,430 pounds.
Maximum APU generator electrical load in flight or on ground:
275 AMPS.
Do not operate APU under the following conditions:
- During Ground de/anti-Icing procedure.
- MAX COOL ON while manually operating cockpit and cabin temp controls.
Minimum 45-minute IFR Reserve Fuel Quantity:
1464 pounds.
Required Equipment for RVSM operations:
- Autopilot (1)
- Altitude Alerting Device (1)
- ATC Altitude reporting Transponder (1)
- Air Data Computers (ADC) (2)
- Pitot probe heaters (2) on the probes linked to the ADC in use.
- Minimum Airspeed in RVSM 160 Knots.
Minimum speed brakes extended Airspeed:
VREF +15.
Maximum runway slope requirements:
+/- 2%.
Maximum engine limit for continuous thrust in cruise:
10 minutes.
Maximum engine limit for continuous static ground operation at TO thrust:
2 minutes.
Battery power only limitation for engine start:
3 start attempts per hour.
Crew member oxygen Masks are not approved above ____ feet.
40,000 feet.
Ops review required runway requirements:
1) Dry: Less than 4500 Feet.
2) Wet/Contaminated: Less than 5000 feet.
3) DAAP: Less than 4500 feet.
4) Width: Less than 75 feet.
Maximum GPU electrical load:
1500 AMPS.
Maximum Oil consumption:
1 quart per hour.
Maximum engine generator electrical load limit in flight or on ground:
300 AMPS.
Minimum width runway requirements:
70 feet.
Maximum gear extended altitude:
18,000 feet.
Minimum Release Fuel Quantity:
2564 pounds.
Flight in freezing rain is:
Prohibited.
Maximum (MMO) Operating Mach:
Mach 0.80
How many APU start attempts allowed following a duel generator failure?
1.
Icing conditions exist in flight when the following conditions are present:
- RAT is 10C or below.
- Visible moisture (Clouds, precipitation, or visibility less than 1 SM) is present.
Normal Differential Pressurization:
0-10.2 PSI
Fuel pressure refueling limits:
10-55 PSI.
Following any APU shutdown, do not attempt restart until ____ seconds after APU is at 0% RPM.
30 Seconds.
Minimum Emergency Fuel Quantity:
1100 pounds.
Maximum number of Pax:
8 plus 2 lap children.
Minimum Dry Length Runway Requirements:
4000 feet.
Maximum Differential Overpressure Pressurization:
10.3 PSI
Maximum Flaps Extended Altitude:
18,000 feet.
Maximum engine generator electrical load above 35,000 feet:
275 AMPS.
Minimum Hot Spare Fuel Quantity:
6000 pounds.
Minimum Fuel Inclement Weather
6000 pounds
Maximum Operating Speed Below 8000
270 kts
Min Battery Temp for APU Start
-20C
Min Battery Temp for Engine Start
-10C
Maximum Fuel Quantity
11,390 lbs
Do not use AUX HYD
In flight or when SAT is -40C
