Gouge - LIMITATIONS – (400F; GE)

Question 1

What is maximum operating altitude,
maximum altitude for takeoff and landing,
and maximum field elevation?

Answer 1

• 45,100 feet PA – max operating
• 10,000 feet PA – max T/O and LDG altitude.
• 9,500 feet MSL – max field elevation.

Question 2

What is the maximum Takeoff and Landing Tailwind Component?

Answer 2

• 15 knots

Question 3

What is the maximum landing crosswind guideline when reported braking action
is medium?

Answer 3

• 25 knots

Question 4

Are operations allowed when the reported braking action is NIL?

Answer 4

• No

Question 5

What is maximum landing gross weight? (400F)

Answer 5

• 302,092 kilograms

Question 6

What should you do if the -400F ZFW (except N-PA) is greater than 276,691
kgs?

Answer 6

• Comply with decreased maximum weight limits (see table in the Weight
and Balance Manual).

Question 7

While flying an autoland approach without LAND2 or LAND3 annunciated, what
is the minimum altitude to which you can descend while the remaining autopilot
is engaged?

Answer 7

• 100 feet RA

Question 8

When flying a non-ILS approach, the autopilot must be disengaged before The
airplane descends more than___________________feet below the MDA.

Answer 8

• 50 feet or 50 feet below minimums

Question 9

During autoland, what is the assumed touchdown point?

Answer 9

• 2,500 feet from the runway threshold

Question 10

What are maximum and minimum glideslope angles for autoland?

Answer 10

• 3.25 degrees (max); 2.5 degrees (min)

Question 11

What is maximum headwind and crosswind component for autoland?

Answer 11

• 25 knots for both conditions

Question 12

What is maximum crosswind component for autoland on a CAT II/III approach?

Answer 12

• 15 knots

Question 13

What is minimum threshold crossing height for Autoland?

Answer 13

• 44 feet

Question 14

Is it permissible to operate HF radios during refueling operations?

Answer 14

• No

Question 15

While airborne during CPDLC operations, an HF radio fails. How many HF radios are required for you to continue using CPDLC? Reference required.

Answer 15

• One HF radio required for CPDLC, if authorized by DDG.

Question 16

While airborne LUX to HSV, prior to oceanic entry into the North Atlantic MNPS, the autopilot LNAV fails. Can you enter MNPS airspace? (ref req)

Answer 16

• No

Question 17

What are the target oxygen pressures for the crew system?

Answer 17

• Land – 950 psi

* Ocean – 1200 psi

Question 18

At what altitude is minimum oxygen quantity supply for each occupant determined?

Answer 18

• 25,000 feet cabin altitude

Question 19

What is the Boeing equivalent thrust for a CF6-80C2, B1F engine?

Answer 19

• 56,500 lbs

Question 20

What is maximum EGT (GE) for engine starting?

Answer 20

• 870 C (40 secs max transient); 750 C unlimited

Question 21

What is maximum continuous EGT (GE)?

Answer 21

• 925 C

Question 22

What is minimum oil pressure (GE)?

Answer 22

• 10 PSI

Question 23

What are the engine RPM limits for N1 and N2 (GE)?

Answer 23

• 117.5 – N1

* 112.5 – N2

Question 24

What is the maximum altitude for flap extension?

Answer 24

• 20,000 feet

Question 25

After engine start, until shutdown at the completion of the flight, what is the primary means of alerting flight crews to non- normal conditions or improper configuration?

Answer 25

• EICAS Alert messages

Question 26

What is the maximum allowable in-flight difference between Captain and First
Officer altitude displays for RVSM operations?

Answer 26

• 200 feet

Question 27

What is the maximum difference between Captain and First Officer altimeters on
the ground for RVSM operations between sea level and 5,000 feet?

Answer 27

• 35 feet

Question 28

What restriction applies for level-off within 2,000 feet after changing the altimeter setting from QNE to QNH, or QNH to QNE?

Answer 28

• Do not use VNAV for level-off if the QNH is less than 29.70in/1006 hPa.

Question 29

Is it permissible to reset a tripped fuel pump circuit breaker?

Answer 29

• No (Warning!)

Question 30

What is the flap limitation during fuel jettisoning?

Answer 30

• Do not extend or retract the flaps between positions 1 and 5 during fuel jettisoning

Question 31

What fuel tank temperature must we maintain while in flight?

Answer 31

• 3 degrees C above the fuel freeze point of the fuel being used.

Question 32

Nacelle/engine anti-ice must be ON during all ground and flight operations when icing conditions exist or are anticipated except when the temperature is below ______?

Answer 32

• – 40 C OAT.

Question 33

Do not use anti-ice if OAT or TAT exceeds ______?

Answer 33

• 10°C (50°F)

Question 34

What is the flap placard speed for flap position 30 (747-400)?

Answer 34

• 180 knots IAS

Question 35

What is the landing gear operating speed for retracting or extending?

Answer 35

• 270 knots IAS/0.82 Mach

Question 36

What is turbulent air penetration speed (747-400)?

Answer 36

• 290 to 310 KIAS/0.82 to 0.85 Mach, whichever is lower.

Question 37

Intentional selection of reverse thrust in flight is ______

Answer 37

prohibited

Question 38

backing the airplane with use of reverse thrust is ______

Answer 38

Prohibited

Question 39

rapid and large alternating control inputs, especially in combination with large changes in pitch, roll, or yaw (e.g. large side slip angles) as they may result in ___________

Answer 39

in structural failure at any speed, including below Va

Question 40

avoid weather radar operation in a _________

Answer 40

hanger

or within 50 feet of fueling operations

or a fuel spill

Question 41

Continuous ignition must be on when encountering:

Answer 41

Moderate to heavy rain
Moderate to severe turbulence
icing conditions
hail or sleet
volcanic ash
Standing water or slush on runway

Continuous ignition is automatically provided when NAI is ON

L.10.4

Question 42

Runway Slope

Answer 42

+/-2%

Question 43

Max tire speed

Answer 43

204 kt (235mph)

Question 44

Ground Limits for all doors

Answer 44

40 kts while opening and closing

65 knots while open