XLS non-red limitations Flashcards
45-minute IFR reserve fuel
1037 Lbs
Hot Spare Fuel
3800 Lbs
Emergency Fuel
900 Lbs
Incliment Wx Fuel
4000 Lbs
Minimum dry runway length and width
3800’/50’
(Required for release only - Pilots may land if LPA computed distance is less than the landing distance available. )
(For wet runway takeoff with thrust reverser credit used to calculate takeoff distance - minimum width is 75’)
Runway Ops review required if:
Dry: Less than 4500’
Wet/Contaminated: Less than 5000’
DAAP: Less than 5000’
If runway is shorter than 3999’ do not:
Takeoff or land when:
- Elevation >3000’
- Contaminated or wet runway
- Tailwind exists
Takeoff with anti-ice on.
land when runway width is less than 75’ and crosswind component exceeds 10 Kts.
Execute circle to land when ceiling less than 1000’ and visibility less than 3 sm.
The following equipment must be operational for flights in RVSM airspace:
1 Autopilot
1 AAD
1 ATC altitude reporting transponder
Static port heaters
Maximum takeoff and landing altitude
14000’
AOM 5.16 for high altitude ops at airfields at or above 8000’ MSL
Mmo
.75
Vmo
305
260 below 8000’
Maximum tire ground speed
165
Vmca flaps 7
90 Kts
Vmca flaps 15
90 Kts
Vmcl Flaps 35
92 Kts
Vmcg flaps 7/15
81 Kts
Max pressurization differential
9.7 PSI
Normal pressurization differential
0-9.6 PSI
Pressure relieve valve opening pressure
9.5 PSI
Lap children may be held in seats:
3,4,10
Crewmember O2 masks not approved for use above:
40,000’ cabin altitude
Passenger O2 masks not approved for use above:
25,000’ cabin altitude
Max number of passengers
7 + 3 lap children (Limit due to O2 masks)
After any APU shutdown, do not attempt restart until __ seconds after APU is at __% rpm.
30 seconds
0%
Do not attempt to start APU after what failure?
Dual generator failure.
Do not operate APU in the following situations:
- When aircraft is unattended
- During ground de/anti-icing procedures
- If APU test has failed
Maximum APU operating altitude
30,000’
Do not use autopilot or yaw damper for ________
Takeoff or landing
Do not manually override autopilot during _____
Normal flight
Do not use autopilot for any of the following:
- Any comparison monitor is activated
- Either PFD is in ATT reversion
Battery limits for engine start:
Three start attempts per hour
Three generator assisted cross starts are equivalent to one engine battery start. Starting the engines using generator cross-start from the APU counts at 1/3 of one normal battery start.
Battery limit for APU start:
9 APU start attempts per hour
Maximum GPU load
1000A
Maximum engine generator load on ground
250A up to 4 minutes
Maximum engine generator load in flight
300A
Maximum APU generator load on ground
200A
Maximum APU generator load in flight
230A
Lav door must be latched open for ______
Taxi, Takeoff, Landing.
Pressure refueling limit:
10-55 PSI
Max defueling pressure:
-10 PSI
Icing conditions exist on the ground when operating on contaminated surfaces and the following conditions are present:
SAT is 10C or below Visible moisture (clouds, precip, <1sm vis)
Icing conditions exist in flight when the following are present:
RAT is 10C or below
Visible moisture.
Operate engine and airframe anti-icing systems in icing conditions, select the following:
WING/ENGINE - ___
TAIL - ____
- On
- AUTO at 10C or less
Flight in _____, ______, or severe conditions of mixed or clear ice is prohibited.
FZRA (Freezing Rain)
FZDZ (Freezing drizzle)
Select ENG-ON at least ________ minutes prior to entering icing conditions.
3-5
Set flaps __ for takeoff when type II, III, or IV fluid has been applied.
7
To prevent cracking of the boot, do not operate the tail deice under any of the following conditions:
Airspeed 150 Kts or greater and RAT -35C of lower
Airspeed less than 150 Kts and RAT -40C or lower
Do not taxi until ______________is completed
altitude and heading ground alignment
Authorized RNAV/RNP for ODP/DP/STAR
RNAV 1/RNP 1 (1 nm)
Authorized RNAV for class I En Route
B-RNAV (5 nm) RNAV 2 (2nm) - Q routes/T routes
When using VNAV for guidance altitude constraints must be displayed on the _____
FMS legs page
Do not use VNAV when altimeter is adjusted to display ________ rather than sea level
QFE (Height above ground)
Do not use the FMS for final approach guidance for ______
ILS, LOC, LOC-BC, LDA, or SDF approaches.
Straight in Vref at Maximum landing weight with anti-ice on is
117 Kts.
Do note use the FMS as primary means of navigation in ______, or __ mode.
Degrade or DR.
Ground idle N2 minimum %
49.3%
Flight idle N2 minimum %
53.2%
Takeoff thrust N1 and N2
N1 - 100%
N2 - 102.8
Transient N1 and N2 limits
N1 - 102 / 20 seconds
N2 - 104 / 20 seconds
N2 - 106.2 / 5 Seconds
Minimum oil pressure for starting
-40
Reverse thrust must be idle below ____ at landing roll or during static operation
60 Kts
thrust reverser deployment is limited to ____ minutes in any ____ minute period
3/10
When APU is operating do not use reverse thrust for longer than ____
30 seconds.
