Latitude All Other Limitations

Front 1

Max altitude flaps extended

Back 1

18,000 ft

Front 2

Gear extended max altitude

Back 2

18,000

Front 3

Zero fuel weight

Back 3

21,430 lbs

Front 4

Max altitude for takeoff And landing

Back 4

14,000

Front 5

Minimum temp between FL350 and FL450

Back 5

-75 SAT

Front 6

Max tire speed

Back 6

182 kts

Front 7

Min speed, speed brakes out

Back 7

Vref+15

Front 8

Vmca (minimum controllable speed - air): Flaps 1

Back 8

88

Front 9

Vmca (minimum controllable speed - air): Flaps 2

Back 9

83

Front 10

Vmcl (minimum controllable speed - Landing): Flaps 2

Back 10

83

Front 11

Vmcl (minimum controllable speed - Landing): Flaps FULL

Back 11

78

Front 12

Vmcg (minimum controllable speed - Ground): Flaps 1

Back 12

88

Front 13

Vmcg (minimum controllable speed - Landing): Flaps 2

Back 13

91

Front 14

Normal differential pressure:

Back 14

0-10.2 psi

Front 15

Max differential pressure:

Back 15

10.3

Front 16

Min o2 for dispatch:

Back 16

0 occupants: 520psi, 10 occupants, 1000psi. AOM ref 12.7

Front 17

One apu start Attempt allowed after:

Back 17

A dual generator failure

Front 18

Following any APU shutdown:

Back 18

Do not attempt restart until after 30 seconds after 0% rpm is indicated.

Front 19

Do not operate the apu under the following conditions:

Back 19

-During ground deicing procedures

- MAX COOL ON while manually operating cockpit temp controls

Front 20

After 45 minutes of APU operation in ambient temp of 30c or higher:

Back 20

Keep main door closed except to get on or off

Front 21

Autopilot limitations:

Back 21

- For takeoff or landing

- do not manually override Ap in normal flight

- do not use when, 1, any comparison monitor is activated. 2, either PFD att or hdg is in reversion

- either ahrs has failed

Front 22

Do not ______ autothrottle during _______. _______ only when cleared for takeoff.

Back 22

Do not ARM autothrottle during TAXI. ARM only when cleared for takeoff.

Front 23

Do not use autothrottle when:

Back 23

There's any monitor miscompare and the appropriate sensor reversion is not selected.

Front 24

Red EICAS message __ _______ _______ is displayed when AT fails to:

Do not ______ _________.

Back 24

AT HOLD FAIL. It's displayed when a or both throttles didn't reach TO in time or the servo is still powered. Do not take off.

Front 25

AT RETARD mode is unavailable when:

Back 25

The radio Altimeter is inop

Front 26

To use AT during an approach, set the speed to?

Back 26

Vref+3

Front 27

If: on battery only, how many engine start attempts?

Back 27

Three per hour

Front 28

If: using a GPU to assist battery start, how many engine start attempts?

Back 28

3 GPU start attempts drawing 1000A or more are equivalent to 1 battery start.

1 GPU start attempt that draws LESS THAN 1000A is equivalent to one battery start.

Front 29

If: starting the second engine using the running generator to assist the batteries, how many engine start attempts?

Back 29

Three generator assisted cross starts are equivalent to one engine battery start.

Front 30

What is the battery limitation for starting the APU?

Back 30

Nine attempts per hour

Front 31

The battery temp indicating system must be?

Back 31

Operational

Front 32

Minimum battery temp for APU startup?

Back 32

-20c

Front 33

The minimum battery temperature for engine start is?

Back 33

-10C

Front 34

Battery voltage for engine start?

Back 34

23-32V

Front 35

Max GPU load?

Back 35

1500A

Front 36

Max Gm engine gen load?

Back 36

300A

Front 37

Max engine gen load above FL350?

Back 37

275A

Front 38

Max APU load?

Back 38

275A

Front 39

Pressure refueling limits?

Back 39

10-55psi

Front 40

Max defuel pressure?

Back 40

-10PSI

Front 41

Total fuel weight?

Back 41

11,390 lbs

Front 42

Do not use the Auxiliary hydraulic pump when?

Back 42

In flight OR sat is -40 or less

Front 43

Auxiliary hydraulic pump run time limit?

Back 43

2 minutes cumulative in 15 consecutive minutes. After 2 minutes cumulative it needs a 15 minute cooldown.

Front 44

When to turn on ENG/STAB anti ice?

Back 44

+10 to -35C

Front 45

Select L&R wing anti ice on when?

Back 45

5 through -35C

Front 46

Icing conditions exist on the ground when:

Back 46

Operating on a contaminated runway or SAT is below 10 and visible moisture (clouds, precip, less than 1sm vis)

Front 47

Icing is present in flight when:

Back 47

RAT is 10 or less c and visible moisture

Front 48

If type 2, 3, or 4 is used DO NOT:

Back 48

Select setting anti ice on just prior to takeoff