Limitations - Black (nice to know)

Question 1

Maximum Zero Fuel Weight

Answer 1

32,000 lbs

Question 2

Baggage compartment limit

Answer 2

900 lbs

Question 3

Maximum pressure altitude for takeoff and landing

Answer 3

10,000 ft

Question 4

Maximum altitude landing gear extended

Answer 4

20,000 ft

Question 5

Minimum altitude for use of flight spoilers

Answer 5

300 ft

Question 6

Minimum takeoff temp

Answer 6

-40 C

Question 7

Maximum takeoff/landing temp

Answer 7

ISA +35

Question 8

Maximum tire speed

Answer 8

182 kts

Question 9

Maximum cabin differential pressure

Answer 9

9.2 psi

Question 10

Maximum pressurization - negative relief

Answer 10

-0.5 psi

Question 11

Maximum number of passengers (including lap children) due to number of installed oxygen masks.

Answer 11

14

Question 12

Reserve fuel ( 45-minute IFR)

Answer 12

2,500 lbs

Question 13

Minimum fuel to release

Answer 13

4,000 lbs

Question 14

Fuel quantity - Hot Spare

Answer 14

8,500 lbs

Question 15

Fuel quantity - Emergency

Answer 15

1,500 lbs

Question 16

Minimum Runway Length (Dry)

Answer 16

5,000 ft

Question 17

Minimum Runway Width

Answer 17

75 ft

Question 18

Runway Max Slope (+/-)

Answer 18

2%

Question 19

Runway Ops review if……

Answer 19

Dry: Less than 5,500

Wet/Contaminated: Less than 6,300

Question 20

APU Starting

Using aircraft batteries (on ground or normal in-flight):

Answer 20

Three 30-second start attempts of continuous cranking followed by 20 minutes of cooling time.

Two further 30-second attempts of continuous cranking.

If start is not successful, do not attempt additional start for at least 35 minutes.

Question 21

APU Starting

Using ground power:

Answer 21

Two 15-second start attempts of continuous cranking, followed by 20 minutes of cooling time.

Two further 15-second attempts of continuous cranking.

If start is not successful, do not attempt additional start for at least 35 minutes.

Question 22

APU Limit - Minimum temp for start on ground

Answer 22

• 40 C

Question 23

APU Limit - Maximum temp during start

Answer 23

974 C

Question 24

APU Limit - Single engine inflight restart

Answer 24

APU use prohibited

Question 25

APU Limit - Maximum altitude for bleed air use

Answer 25

15,000 ft

Question 26

Do no use Autopilot for:

Answer 26

Takeoff or Landing

Any approach (precision or nonprecision) with glidepath angle greater than 4 degrees

Question 27

AC Generator load limits - Main

Answer 27

0 to 20,000 ft = 30 kVA

Above 35,000 ft = 25 kVA

Question 28

AC Generator load limits - APU

Answer 28

0 to 20,000 ft = 30 kVA

Question 29

DC TRU load limit

Answer 29

Maximum Continuous: 100 A

Question 30

Fuel Quantities - gravity fueling (Total)

Answer 30

Reduce pressure fueling weight by 7%

Question 31

Minimum go-around fuel

Answer 31

500 lbs per tank

Question 32

Fuel Temperature Limits

Answer 32

Do not takeoff if engine fuel temp is below 5 C

Bulk fuel temperature must remain above fuel freezing point.

Question 33

Fuel Jettison

Answer 33

Flap Setting for Fuel Jettison: 0

Do not jettison fuel in known lightning conditions.

Question 34

Fuel Transfer

Answer 34

Fuel transfer must be off for takeoff.

During normal ops, tail tank transfer system must not be used as a center of gravity control device, it must remain selected to the automatic mode.

Do not manually transfer tail tank fuel with more than 7,000 lb. of fuel in auxiliary tank.

Question 35

Icing conditions exist on the ground when:

Answer 35

SAT is 10 C or below

Visible moisture ( rain, snow, or visibility less than 1 sm) is present

Operating on contaminated surfaces

Question 36

Left main tank quantity

Answer 36

4,860 lbs

Question 37

Right main tank quantity

Answer 37

4,860 lbs

Question 38

Aux tank quantity

Answer 38

7,168 lbs

Question 39

Tail tank quantity

Answer 39

3,112 lbs

Question 40

Display Unit operating temperatures

Answer 40

Do not power Display Units on the ground when flight compartment temperature exceeds 40C for more than 30 minutes, unless at least one pack is operating and pax door is closed.

Question 41

Icing conditions exist in flight when:

Answer 41

EICAS message ICE is displayed, or

TAT is 10C or below, and
Visible moisture (rain, snow, or visiblity is less than 1 sm) is present except when SAT is -40C or below.

Flight in freezing drizzle or freezing rain is prohibited.

Question 42

Electronic Flight Instrument System (EFIS)

Answer 42

Do not use MAP PLAN display for navigation while north of 70N or south of 70S.

OBSTACLE symbols on MFW MAP are for situational awareness only.

Question 43

Synthetic Vision System (SVS)

Answer 43

Do not use SVS for navigation

Deselect SVS prior to FAF when outside WGS-84 or NAD-83 airspace.

De-select SVS when conducting an approach to a runway not in the FMS flight plan (e.g., side-step maneuver).