Limitations Part 1

Question 1

Do not extend flaps above …

Answer 1

20,000 ft

Question 2

Runway Slope (AFM)

Answer 2

+/- 2 deg

Question 3

QFE Selection

Answer 3

QFE Operations Prohibited

Question 4

Reverse Thrust

Answer 4

• Intentional selection of reverse thrust in flight prohibited
• Backing the airplane with use of reverse thrust is prohibited.

Question 5

Maximum Glideslope Angle

Answer 5

3.25 deg

CAT II and CAT III operations and automatic landing is approved with flaps 25 or 30 only.

Question 6

Maximum Takeoff and Landing Crosswind

Answer 6

30 kts not limiting

Question 7

Maximum Takeoff and Landing Tailwind Component

Answer 7

15 kts

Question 8

Maximum allowable wind speeds when landing weather minima are predicated on auto land operations:

Answer 8

Headwind - 25 kts
Crosswind - 25 kts
Tailwind - 15 kts

Question 9

Maximum Operating Altitude

Answer 9

45,100 ft pressure altitude

Question 10

Turbulent Air Penetration Speed

Answer 10

290-310 kts
or
.82-.85 M whichever is lower

Question 11

The max allowable in flight difference between the CA and F/O altitude displays (altimeters) for RVSM operations is ____ ft.

Answer 11

200 ft

Question 12

Use of aileron trim with autopilot engaged is …

Answer 12

Prohibited

Question 13

Fuel Temp comes from tank #?

Answer 13

1

Question 14

One normal fuel pump can supply fuel to how many engines?

Answer 14

1 - Takeoff

2- Cruise

Question 15

One overriding fuel pump can supply fuel to how many engines

Answer 15

2- Takeoff

2- Cruise

Question 16

Automatic landings may be made with flaps ___ or ___ only.

Answer 16

25

30

Question 17

Do not use FLCH on final approach below ___ ft AFE.

Answer 17

1,000 ft

Question 18

The autopilot must not be engaged below a minimum engage altitude of ___.

Answer 18

250 AGL after T/O

Question 19

Minimum glide slope angle is ___.

Answer 19

2.5 deg

CAT II and III ops and auto land is approved with flaps 25 and 30

Question 20

The A/P must be disengaged before airplane descends more than ___ ft below the MDA unless it is coupled to an ILS glideslopoe and localizer or in go-around mode.

Answer 20

50 ft.

Question 21

The autopilot must be disengaged below ___ ft. AGL, in a non-precision approach.

Answer 21

360 ft.

Question 22

Do not operate HF or WX radar…….

Answer 22

• HF during refueling operations.
• WX radar in a hangar or within 50 ft. of any fueling operations or fuel spill.

Note: Hangar restriction does not apply to the WX Radar Test Mode.

Question 23

Maximum speed operating in Reduced Vertical Separation Minimum (RVSM) airspace.

Answer 23

.90 Mach

Question 24

Cabin Pressurization Limits

Answer 24

Max differential pressure. 9.4 psi

Max allowable cabin pressure differential for T/O and Landing .11 psi

Question 25

Speed Brakes Restriction

Answer 25

Use of speed brakes in flight with flaps more than 20 not recommended.

Question 26

Center wing tank pumps must be .....

Answer 26

Off for taxi, T/O and climb unless the center wing tank contains at least 7,700 kgs of fuel.

Question 27

Pratt & Whitney engine max starting EGT

Answer 27

535 deg C

Question 28

Maximum Field Elevation

Answer 28

9,500 ft

Question 29

Main Deck Occupancy

Answer 29

Occupancy of the main deck cargo area is prohibited during taxi, T/O, in flight and landing.

Question 30

Fuel Dump

Answer 30

Do not extend or retract the flaps between position 1& 5 during fuel jettisoning.

Question 31

GE engine max starting EGT

Answer 31

750 deg C

Question 32

For single channel ILS approaches, the autopilot must be disengaged before the airplane descends below ___ ft. AGL.

Answer 32

100 ft AGL

Question 33

VNAV Selection limitation

Answer 33

If leveling off within 2,000 ft after changing altimeter setting from QNE to QNH, or QNH to QNE, do not use VNAV to execute the level-off if QNH is less than 29.70/1006 hpa. After level-off is completed, VNAV may be re-engaged.

Question 34

RVSM Altimeter Ground Check

Answer 34

Max difference between the CAPT or FO altimeters and field elevation SL-5,000 ft is 75 ft. Max Difference between the CAPT or FO altimeters and field elevation 9,500 ft is 75 ft. Max difference between CAPT and FO altimeters SL-5,000 ft is 35 ft. Max difference between CAPT and FO altimeters 9,500 ft is 40 ft.

Question 35

Maximum Zero Fuel Weight

Answer 35

276,691 kgs

Question 36

Maximum Variable Zero Fuel Weight

Answer 36

288,031 kgs

Question 37

Maximum Taxi Weight

Answer 37

395,986 kgs

Question 38

Maximum Takeoff Weight

Answer 38

394,625 kgs

Question 39

Minimum Flight Weight

Answer 39

166,696 kgs

Question 40

Maximum in flight weight landing flaps

Answer 40

303,906 kgs

Question 41

Maximum Landing Weight

Answer 41

295,742 kgs

Question 42

Maximum Takeoff and Landing Altitude

Answer 42

10,000 ft pressure altitude

Question 43

Continuous Ignition is required on for ....

Answer 43

``` Heavy Rain Severe Turbulence Icing Conditions Volcanic Ash Standing Water or Slush on the runway ``` Continuous Ignition is auto on with nacelle anti-ice on.

Question 44

When should wing anti-ice be on?

Answer 44

Prior to reducing thrust to descent in visible moisture and TAT less than 10 deg C including SAT -40 deg C nacelle anti-ice must be in on position. At or below 22,000 ft wing anti ice selector must be in the on position.

Question 45

Max tank fuel temperature?

Answer 45

Jet A, A1, JP5, or JP8 54 deg C Jet B, JP4 43 deg C In flight tank fuel temp must be maintained at least 3 deg C above the fuel freezing point of fuel being used.

Question 46

Door mounted power assist and escape slides .....

Answer 46

Emergency evacuation slide system must be in Automatic mode and engagement of each escape slide pack extractor must be verified by checking that knob is visible in the automatic viewing port prior to Taxi, T/O, Landing whenever persons occupy the upper deck cabin.

Question 47

Fuel Tanks & Quantities

Answer 47

``` 7 tanks - 163,042 kgs 4 main, 1 center, 2 reserve tanks Main 1&4 - 13,200 kgs ea Main 2&3 - 38,100 kgs ea Center Tank - 52,100 kgs Reserve Tanks - 4,000 kgs ea ```

Question 48

Ground Wind Limits for All Doors

Answer 48

40 kts while opening or closing 65 kts while open