B777 LIMITATION

1. Under which of the following conditions is operation with assumed temperature reduced takeoff thrust is not permitted?

A wet runway

Inoperative RTO mode

Inoperative anti-skid on two wheels

Contaminated runways

2. What is the maximum crosswind component when basing landing weather minima on autoland operations?

30 knots

25 knots

38 knots

10 knots

3. What is the maximum operating altitude?

45, 100 feet

41,100 feet

47,100 feet

43,100 feet

4. Maximum Flap Extension Altitude is

25,000 feet

15,000 feet

20,000 feet

30,000 feet

5. What is the maximum differential pressure (relief valves)?

11.1 psi

7.3 psi

9.1 psi

8.5 psi

6. Which of the following are maximum allowable wind speeds when landing weather minima are predicate on autoland operations?

Headwind 30 knots

Tailwind 5 knots

Crosswind 38 knots

Crosswind 25 kts

7. What is the minimum altitude for engagement after takeoff?

1000 feet

400 feet

250 feet

200 feet

8. What is the maximum demonstrated takeoff and landing crosswind?

25 knots

38 knots

36 knots

33 knots

9. For an automatic landing, which of the following statements is correct?

The maximum glideslope angle is 3.25 degrees and flap 30 must be used

The minimum glideslope angle is 2.5 degrees and autoland status must display LAND 3

Automatic landings can be made using flaps 20 or 30, with both engines operative or one engine inoperative.

Contact flight dispatch for the landing climbout performance dictated flap setting.

10. What is the maximum runway slope?

Up 2% and down 2%

Up 3.25% and down 2.5%

Up 2.5% and down 2.5 %

There is no slope limitation.

11. What is the maximum difference between Captain’s and First Officer’s altitude display prior to takoff?

0 feet

100 feet

75 feet

50 feet

12. What is the maximum glideslope angle?

3.25 degrees

3.0 degrees

3.5 degrees

3.75 degrees

13. What is the minimum radio altitude for the deployment of the Speedbrakes in flight?

There are no opening limitations on speedbrake operatrion.

400 feet

1500 feet

700 feet

14. Which of the following statements is correct regarding the ground wind limits for doors?

38 knots while opening or closing, 45 knots while open

15 knots while opening or closing, 25 while open

40 knots while opening or closing, 65 while open

There are no ground wind Limits for doors

15. What is the maximum tank fuel temperature?

49 degrees Celsius

3 degrees above the EICAS limit for ‘Jet B’

3 degrees above the EICAS limit for ‘Jet A’

40 degrees Celsius

16. What is the minimum glideslope angle?

3.0 degrees

2.5 degrees

2.25 degrees

2.75 degrees

17. What is the maximum take off and landing altitude?

10,000 feet

14,000 feet

9,800 feet

3,400 feet

18. What is the maximum take off and landing altitude?

10,000 feet

14,000 feet

9,800 feet

8,400 feet

19. What is the severe turbulence airspeed?

0.82 Mach or minimum maneuver speed plus 15 knots, whichever is lower.

280 KCAS /.82M above 10000 feet.

280 KIAS below FL 250 and 270 KIAS /.80 at or above FL250

270 KIAS /.80M above 10000 feet

20. What statement about use of reverse thrust is most correct?

Reverse thrust use below 60 knots is prohibited.

Intentional selection of reverse thrust below 10 feet radio altitude is allowed.

Backing the airplane with the use of reverse thrust is prohibited.

Backing the airplane with the use of reverse thrust and intentional use of reverse thrust in flight are prohibited.

21. At what altitude must the autopilot be disengaged during landing without LAND 2 or LAND 3 annunciated?

None, autoland is always allowed.

50 feet RA

200 feet AGL

22. What is the maximum allowable cabin pressure differential for takeoff and landing?

0.11 psi

11.1 psi

9.1 psi

8.5 psi

23. What is the Maximum takeoff and landing tailwind components?

10 knots

15 knots

18 knots

20 knots

24. What fuel is prohibited for use?

Jet A

Jet B

JP-4

JET B and JP-4

25. What is the maximum airspeed limit with a WINDOW HEAT DL, R EICAS message?

There is no airspeed limit with unserviceable window heat.

280 knots

250 knots below 10000 feet

280 knots below 10000 feet

26. Which statement about the fuel system limitation is most correct?

Main tanks must be maintained full on the ground if center tank fuel is loaded

Main tanks must be scheduled to be full if center tank fuel is loaded.

Fuel crossfeed valves must be close for landing.

Fuel imbalance must not exceed 1000 pounds (500 kilograms)

27. At what altitude must the autopilot be disengaged during landing?

None, autoland is always allowed.

200 feet AGL

28. Which of the following statements is most correct regarding flap position during automatic landings?

Automatic landings may be accomplished using flaps 20, 25 or 30.

Automatic landings may be accomplished using flaps 20 or 30 when LAND 2 or LAND 3 is annunciated.

Automatic landings may be accomplished using flaps 20, 25 or 30 when LAND 2 or LAND 3 is annunciated.

Automatic landings may be accomplished using flaps 20 or 30.

29. Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged before the airplane descends below which altitude?

50 feet AGL

200 feel AGL

200 feet RA

500 feet AGL

30. The Wing Span of the Airplane is

199 feet 11 inches (60.9 meters)

205 feet 10 inches (62.7 meters)

209 feet 1 inch (63.7 meters)

70 feet 7.5 inches (21.5 meters)

31. The use of look-ahead terrain alerting and terrain display functions are prohibited within a range and approaching to land at an airport not contained in the GPWS terrain database. What is that range to the airport?

10 NM

5 NM15 NM115 NM

20 NM

18 NM

32. Which statement about use of QFE altimeter settings is correct?

The use of look-ahead terrain alerting and terrain display functions are permissible during QFE operations.

A QFE altitude reference for the primary flight display automatic selects QFE reference in the flight management system.

33. The Wing Span of the Airplane is

212 feet 7 inches (64.8 meters)

206 feet 6 inches (63 meters)

119 feet 11 inch (60.9 meters)

239 feet 9 inch (73.1 meters)

34. Do not attempt to make a turn away from an obstacle within what distance?

15 feet (4.6 meters) of the wingtip or 51 feet (15.7 meters) of the nose

15 feet (4.6 meters) of the wingtip of 40 feet (12.2 meters) of the nose

40 feet (12.2 meters) of the wingtip or 15 feet (4.6 meters) of the nose

51 feet (15.7 meters) of the wingtip or 15 feet (4.6 meters) of the nose

35. What the minimum width of pavement for a 180 degree turn?

156 feet (47.5 meters)

182 feet (55.4 meters)

186 feet (56.5 meters)

154 feet (46.8 meters)

36. What is the minimum width of pavement for 180 degree turn?

156 feet (47.5 meters)

182 feet (55.4 meters)

145 feet (44.2 meters)

154 feet (46.8 meters)

37. What is the wingtip turning radius?

129 feet (39.3 meters)

149 feet (45.4 meters)

182 feet (55.4 meters)

154 feet (46.8 meters)

38. Do not attempt to make turn away from an obstacle within what distance?

15 feet (4.6 meters) of the wingtip or 44 feet (13.4 meters) of the nose

15 feet (4.6 meters) of the wingtip or 40 feet (12.2 meters) of the nose

40 feet (12.2meters) of the wingtip or 15 feet (4.6 meters) of the nose

51 feet (15.7 meters) of the wingtip or 15 feet (4.6 meters) of the nose

39. What is the length of the Airplane from nose to tall of fuselage?

239 feet 9 inches (73.1 meters)

199 feet 11 inches (60.9 meters)

206 feet 6 inches (63 meters)

209 feet 1 inch (63.7 meters)

40. What is the length of the Airplane from nose to tail of fuselage?

239 feet 9 inches (73.1 meters)

206 feet 6 inches (63 meters)

199 feet 11 inches (60.9 meters)

102 feet 5 inches (31.2 meters)

41. What is the wingtip turning radius?

152 feet (46.3 meters)

149 feet (45.4 meters)

182 feet (55.4 meters)

160 feet (48.8 meters)

42. Which statement is correct about TCAS?

TCAS information and advisories can not be used when not in radar controlled airspace.

Pilots are authorized to comply with a TCAS II resolution advisory when the airplane transponder is in OFF or STBY.

B777 Limitation

1. Under which of the following conditions is operation with assumed temperature reduced takeoff thrust is not permitted?

2.

What first name or nickname would you like us to use?

2. What is the maximum crosswind component when basing landing weather minima on autoland operations?

3. What is the maximum operating altitude?

4. Maximum Flap Extension Altitude is

5. What is the maximum differential pressure (relief valves)?

6. Which of the following are maximum allowable wind speeds when landing weather minima are predicate on autoland operations?

7. What is the minimum altitude for engagement after takeoff?

8. What is the maximum demonstrated takeoff and landing crosswind?

9. For an automatic landing, which of the following statements is correct?

10. What is the maximum runway slope?

11. What is the maximum difference between Captain’s and First Officer’s altitude display prior to takoff?

12. What is the maximum glideslope angle?

13. What is the minimum radio altitude for the deployment of the Speedbrakes in flight?

14. Which of the following statements is correct regarding the ground wind limits for doors?

15. What is the maximum tank fuel temperature?

16. What is the minimum glideslope angle?

17. What is the maximum take off and landing altitude?

18. What is the maximum take off and landing altitude?

19. What is the severe turbulence airspeed?

20. What statement about use of reverse thrust is most correct?

21. At what altitude must the autopilot be disengaged during landing without LAND 2 or LAND 3 annunciated?

22. What is the maximum allowable cabin pressure differential for takeoff and landing?

23. What is the Maximum takeoff and landing tailwind components?

24. What fuel is prohibited for use?

25. What is the maximum airspeed limit with a WINDOW HEAT DL, R EICAS message?

26. Which statement about the fuel system limitation is most correct?

27. At what altitude must the autopilot be disengaged during landing?

28. Which of the following statements is most correct regarding flap position during automatic landings?

29. Without LAND 2 or LAND 3 annunciated, the autopilot must be disengaged before the airplane descends below which altitude?

30. The Wing Span of the Airplane is

31. The use of look-ahead terrain alerting and terrain display functions are prohibited within a range and approaching to land at an airport not contained in the GPWS terrain database. What is that range to the airport?

32. Which statement about use of QFE altimeter settings is correct?

33. The Wing Span of the Airplane is

34. Do not attempt to make a turn away from an obstacle within what distance?

35. What the minimum width of pavement for a 180 degree turn?

36. What is the minimum width of pavement for 180 degree turn?

37. What is the wingtip turning radius?

38. Do not attempt to make turn away from an obstacle within what distance?

39. What is the length of the Airplane from nose to tall of fuselage?

40. What is the length of the Airplane from nose to tail of fuselage?

41. What is the wingtip turning radius?

42. Which statement is correct about TCAS?