LIMITATIONS

Question 1

VMO:

Answer 1

Winglets: 0.86 / 340 (Placard beside right RDMI)

Non winglets 0.86 / 360

Question 2

VA:

Answer 2

300kts at sea level
320kts at FL150
0.86 above FL280

Question 3

Flap placard speeds: (5kts between 300 and 300ER/F) (15 and 20 positions are the same)

Answer 3

300: 1 / 245 5 / 225 15 / 205 20 / 205 25 / 175 30 / 165

300ER / F 1 / 250 5 / 230 15 / 210 20 / 210 25 / 180 30 / 170

Question 4

VLO:

Answer 4

Retraction: 270kts
Normal extension: 270 / 0.82
Alternate extension: 250 / 0.75

Question 5

VLE:

Answer 5

Extended: 270 / 0.82

Question 6

Max take-off and landing tailwind: (Runway length dependant)

Answer 6

2001m or above: 15kts

2000m or below: 10kts

Question 7

Runway slope limit:

Answer 7

+/- 2%

Question 8

Max operating altitude:

Answer 8

43,100ft

Question 9

Max take-off and landing pressure altitude:

Answer 9

8,400ft

Question 10

Maximum cabin differential pressure:

Answer 10

9.1psi

Question 11

Minimum height for autopilot engagement:

Answer 11

200ft AGL

Question 12

Maximum allowable wind conditions for autoland: (Runway length dependant for tailwind)

Answer 12

Headwind: 25kts
Tailwind: 15kts (2001m or above) / 10kts (2000m or below)
Crosswind: 25kts

Question 13

Max N1:

Answer 13

117.5% (Found on SEI)

Question 14

Max N2:

Answer 14

112.5% (Found on SEI)

Question 15

Max EGT

Answer 15

Take-off: 960c (5 minutes) (Found on SEI)
Continuous: 925c
Starting: 750c (870c for 40 seconds)

Question 16

Min oil pressure:

Answer 16

10psi

Question 17

Max oil temperature:

Answer 17

15 minutes: 175c

Continuous: 160c

Question 18

Maximum allowable in flight difference between Captain and Co-pilot altimeters:

Answer 18

Maximum allowable in flight difference between Captain and Co-pilot altimeters:

Question 19

Maximum allowable on ground difference between Captain and Co-pilot altimeters:

Answer 19

40ft

Question 20

Maximum difference between Captain / Co-pilot altimeter and field elevation:

Answer 20

75ft

Question 21

Maximum tank fuel temperature:

Answer 21

49c

Question 22

Minimum tank fuel temperature:

Answer 22

Fuel freezing point + 3c

Question 23

Fuel freezing points:

Answer 23

Jet A = -40c
Jet A-1 = -47c
JP5 = -46c
JP8 = -47c

Question 24

Maximum number of passengers without infants:

Answer 24

Shall not exceed 290 because of emergency evacuation

Question 25

Engine flameout protection: (Bulletin 05-05)

Answer 25

Thrust reduced for a descent or speed reduction, TAT at or below 10c, in visible moisture,
regardless of SAT:
- Engine anti-ice ON
- At or below 22,000ft, Wing anti-ice ON (increases bleed extraction)

Question 26

Engine operation in hail and / or heavy rain: (Bulletin 94-02)

Answer 26

Engine start selectors: CONT
TAT at or below 10c: Engine anti-ice ON
TAT higher than 10c: Autothrottle disengage (descent only)
Thrust levers: 50% N1 minimum above 10,000ft, or 45% N1 minimum below 10,000ft

Question 27

Maximum take-off weights:

Answer 27

• 300 = 288,700lbs
• 300ER = 400,000lbs
• 300F = 412,000lbs
• 300BCF = 407,000lbs

Question 28

Maximum landing weights:

Answer 28

• 300 = 280,000lbs
• 300ER = 320,000lbs
• 300F = 326,000lbs
• 300BCF = 326,000lbs

Question 29

Max crosswind:

ICE or SNOW
Braking Action:

Answer 29

Dry / Damp = 33kts
Wet grooved = 25kts
Wet ungrooved = 20kts
Flooded= 10kts

Good= 20kts
Med to Good=20(15)*
Medium=20(15)*
Med to Poor=15(10)*
Poor= 10kts
*less than 2500m rwy

Question 30

Turbulence penetration speed:

Answer 30

290kts / 0.78 whichever is lower

Question 31

Maximum fuel imbalance:

Answer 31

2500lbs until 48,000lbs total
1500lbs above 79,800lbs total
Linear scale between 48,000lbs (1500) and 79,800lbs (2500lbs)

Question 32

APU starter cycle:

Answer 32

A Maximum of three consecutive starts or attempts within a 60 minute period

Question 33

Engine starter cycle:

Answer 33

Five minutes on, followed by 30 seconds per minute on