Limitations 747 Flashcards

1
Q

Runway slope

A

+/- 2 %

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Maximum T/O and LDG tailwind component

A

10 kts (15 IFK & IFM)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Maximum Operating Altitude

A

45,100 feet

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Maximum T/O & LDG Altitude

A

10,000 feet pressure altitude

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Maximum Field Elevation

A

9,500 feet

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Maximum speed operating in RVSM

A

0.90 Mach

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Turbulent air penetration speed

A

290-310 kts
.82-.85 M
Whichever is lower

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Maximum difference between altimeters
(Sea level to 5,000 feet & 9,500 feet; between Capt - FO & between altimeter and field elevation)

A

35 ft between Capt - FO sea level to 5,000
40 ft between Capt - FO 9,500 feet

75 ft between Capt/FO - Field elevation

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Maximum differential pressure

A

9.4 psi

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Maximum allowable cabin pressure for T/O or LDG

A

0,11 psi

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Minimum altitude for engagement A/P

A

250 ft AGL

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Minimum altitude for disengagement A/P

A

50 ft below MDA
In case if single channel ILS, minimum 100 ft AGL

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Maximum headwind component Autoland

A

25 kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Maximum crosswind component Autoland

A

25 kts

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

Maximum tailwind component Autoland

A

10 kts (15 kts for IFK & IFM)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Maximum glideslope angle

A

3,25°

17
Q

Minimum glideslope angle

A

2,5°

18
Q

Minimum altitude for FLCH

A

1,000 feet AFE

19
Q

Continuous ignition

A

-Heavy rain
-Severe turbulence
-Volcanic ash
-Icing conditions
-Standing water or slush on runway

20
Q

Vnav selection within 2,000 feet

A

QNH is less than 29,70 in/1006 hPa

21
Q

Maximum altitude for flaps extension

A

20,000 feet

22
Q

Minimum fuel

A

20T for T/O
5500 Kg for LDG