XLS non-red limitations

Question 1

45-minute IFR reserve fuel

Answer 1

1037 Lbs

Question 2

Hot Spare Fuel

Answer 2

3800 Lbs

Question 3

Emergency Fuel

Answer 3

900 Lbs

Question 4

Incliment Wx Fuel

Answer 4

4000 Lbs

Question 5

Minimum dry runway length and width

Answer 5

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’)

Question 6

Runway Ops review required if:

Answer 6

Dry: Less than 4500’
Wet/Contaminated: Less than 5000’
DAAP: Less than 5000’

Question 7

If runway is shorter than 3999’ do not:

Answer 7

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.

Question 8

The following equipment must be operational for flights in RVSM airspace:

Answer 8

1 Autopilot
1 AAD
1 ATC altitude reporting transponder
Static port heaters

Question 9

Maximum takeoff and landing altitude

Answer 9

14000’

AOM 5.16 for high altitude ops at airfields at or above 8000’ MSL

Question 10

Mmo

Answer 10

.75

Question 11

Vmo

Answer 11

305

260 below 8000’

Question 12

Maximum tire ground speed

Answer 12

165

Question 13

Vmca flaps 7

Answer 13

90 Kts

Question 14

Vmca flaps 15

Answer 14

90 Kts

Question 15

Vmcl Flaps 35

Answer 15

92 Kts

Question 16

Vmcg flaps 7/15

Answer 16

81 Kts

Question 17

Max pressurization differential

Answer 17

9.7 PSI

Question 18

Normal pressurization differential

Answer 18

0-9.6 PSI

Question 19

Pressure relieve valve opening pressure

Answer 19

9.5 PSI

Question 20

Lap children may be held in seats:

Answer 20

3,4,10

Question 21

Crewmember O2 masks not approved for use above:

Answer 21

40,000’ cabin altitude

Question 22

Passenger O2 masks not approved for use above:

Answer 22

25,000’ cabin altitude

Question 23

Max number of passengers

Answer 23

7 + 3 lap children (Limit due to O2 masks)

Question 24

After any APU shutdown, do not attempt restart until __ seconds after APU is at __% rpm.

Answer 24

30 seconds

0%

Question 25

Do not attempt to start APU after what failure?

Answer 25

Dual generator failure.

Question 26

Do not operate APU in the following situations:

Answer 26

- When aircraft is unattended - During ground de/anti-icing procedures - If APU test has failed

Question 27

Maximum APU operating altitude

Answer 27

30,000'

Question 28

Do not use autopilot or yaw damper for ________

Answer 28

Takeoff or landing

Question 29

Do not manually override autopilot during _____

Answer 29

Normal flight

Question 30

Do not use autopilot for any of the following:

Answer 30

- Any comparison monitor is activated | - Either PFD is in ATT reversion

Question 31

Battery limits for engine start:

Answer 31

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.

Question 32

Battery limit for APU start:

Answer 32

9 APU start attempts per hour

Question 33

Maximum GPU load

Answer 33

1000A

Question 34

Maximum engine generator load on ground

Answer 34

250A up to 4 minutes

Question 35

Maximum engine generator load in flight

Answer 35

300A

Question 36

Maximum APU generator load on ground

Answer 36

200A

Question 37

Maximum APU generator load in flight

Answer 37

230A

Question 38

Lav door must be latched open for ______

Answer 38

Taxi, Takeoff, Landing.

Question 39

Pressure refueling limit:

Answer 39

10-55 PSI

Question 40

Max defueling pressure:

Answer 40

-10 PSI

Question 41

Icing conditions exist on the ground when operating on contaminated surfaces and the following conditions are present:

Answer 41

``` SAT is 10C or below Visible moisture (clouds, precip, <1sm vis) ```

Question 42

Icing conditions exist in flight when the following are present:

Answer 42

RAT is 10C or below | Visible moisture.

Question 43

Operate engine and airframe anti-icing systems in icing conditions, select the following: WING/ENGINE - ___ TAIL - ____

Answer 43

- On | - AUTO at 10C or less

Question 44

Flight in _____, ______, or severe conditions of mixed or clear ice is prohibited.

Answer 44

FZRA (Freezing Rain) | FZDZ (Freezing drizzle)

Question 45

Select ENG-ON at least ________ minutes prior to entering icing conditions.

Answer 45

3-5

Question 46

Set flaps __ for takeoff when type II, III, or IV fluid has been applied.

Answer 46

7

Question 47

To prevent cracking of the boot, do not operate the tail deice under any of the following conditions:

Answer 47

Airspeed 150 Kts or greater and RAT -35C of lower | Airspeed less than 150 Kts and RAT -40C or lower

Question 48

Do not taxi until ______________is completed

Answer 48

altitude and heading ground alignment

Question 49

Authorized RNAV/RNP for ODP/DP/STAR

Answer 49

RNAV 1/RNP 1 (1 nm)

Question 50

Authorized RNAV for class I En Route

Answer 50

``` B-RNAV (5 nm) RNAV 2 (2nm) - Q routes/T routes ```

Question 51

When using VNAV for guidance altitude constraints must be displayed on the _____

Answer 51

FMS legs page

Question 52

Do not use VNAV when altimeter is adjusted to display ________ rather than sea level

Answer 52

QFE (Height above ground)

Question 53

Do not use the FMS for final approach guidance for ______

Answer 53

ILS, LOC, LOC-BC, LDA, or SDF approaches.

Question 54

Straight in Vref at Maximum landing weight with anti-ice on is

Answer 54

117 Kts.

Question 55

Do note use the FMS as primary means of navigation in ______, or __ mode.

Answer 55

Degrade or DR.

Question 56

Ground idle N2 minimum %

Answer 56

49.3%

Question 57

Flight idle N2 minimum %

Answer 57

53.2%

Question 58

Takeoff thrust N1 and N2

Answer 58

N1 - 100% | N2 - 102.8

Question 59

Transient N1 and N2 limits

Answer 59

N1 - 102 / 20 seconds N2 - 104 / 20 seconds N2 - 106.2 / 5 Seconds

Question 60

Minimum oil pressure for starting

Answer 60

-40

Question 61

Reverse thrust must be idle below ____ at landing roll or during static operation

Answer 61

60 Kts

Question 62

thrust reverser deployment is limited to ____ minutes in any ____ minute period

Answer 62

3/10

Question 63

When APU is operating do not use reverse thrust for longer than ____

Answer 63

30 seconds.