問題一覧
1
Flight Maneuvering Load Acceleration Limits: Clean Configuration
-1g to +2.5g
2
Runway altitude:
9,200 ft
3
Maximum wind for FWD and AFT cargo door operation if aircraft nose is into the wind, or if the FWD and AFT cargo doors are on the leeward side:
50 kts
4
Wipers maximum operating speed:
230 kts
5
Minimum weight:
37,230 kg
6
Maximum zero fuel weight:
61,000 kg
7
Maximum landing weight:
64,500 kg
8
Maximum takeoff weight (brake release):
73,500 kg
9
Maximum taxi weight:
73,900 kg
10
Minimum control speed for landing (VMCL):
113 kts
11
Maximum ground speed:
195 kts
12
Maximum speed at which the landing gear may be retracted (VLO retraction):
220 kts/M 0.54
13
Maximum speed at which the landing gear may be extended (VLO extension):
250 kts/M 0.60
14
Maximum speed with the landing gear extended (VLE):
280 kts/M 0.67
15
MMO
M 0.82
16
VMO:
350 kts
17
Max speed for Flaps lever configuration: CONF FULL
177 kts
18
Max speed for Flaps lever configuration: CONF 3
185 kts
19
Max speed for Flaps lever configuration: CONF 2
200 kts
20
Max speed for Flaps lever configuration: CONF 1+F
215 kts
21
Max speed for Flaps lever configuration: CONF 1
230 kts
22
Max speed for Flaps lever configuration: CONF 0
VM0/MMO
23
Cockpit window open maximum speed:
200 kts
24
Maximum wind for FWD and AFT cargo door operation:
40 kts
25
Maximum wind for passenger door operation:
65 kts
26
Maximum tailwind (takeoff and landing):
15 kts
27
Maximum demonstrated crosswind (takeoff and landing):
38 kts
28
Minimal runway width:
30 meters
29
Nominal runway width:
45 meters
30
Runway slope (mean):
±2 %
31
Flight Maneuvering Load Acceleration Limits: Other Configuration
0g to +2g
32
Electric power supply must be limited during ground operations. In normal avionics ventilation system configuration: OAT ≤ 49 °C
No limitation
33
Electric power supply must be limited during ground operations. In normal avionics ventilation system configuration: 49 °C < OAT ≤ 55 °C
2 h
34
Electric power supply must be limited during ground operations. In normal avionics ventilation system configuration: 55 °C < OAT ≤ 60 °C
1 h
35
Electric power supply must be limited during ground operations. In normal avionics ventilation system configuration: 60 °C < OAT ≤ 64 °C
0.5 h
36
Maximum positive differential pressure
9.0 PSI
37
Maximum negative differential pressure
-1.0 PSI
38
Safety relief valve setting
8.6 PSI
39
Maximum wind condition for ILS/MLS (CAT II or CAT III and for GLS) CAT I: Headwind:
30 kts
40
Maximum wind condition for ILS/MLS (CAT II or CAT III and for GLS) CAT I: Tailwind:
10 kts
41
Maximum wind condition for ILS/MLS (CAT II or CAT III and for GLS) CAT I: Crosswind:
20 kts
42
APU ROTOR SPEED: Maximum N speed:
107%
43
Maximum EGT for APU start (below 35 000 ft):
1090 °C
44
Maximum EGT for APU start (above 35 000 ft):
1120 °C
45
Maximum EGT for APU running:
675 °C
46
Thrust Setting/EGT Limits: Takeoff and Go-around - All engines operative:
5 mins - 950°C
47
Thrust Setting/EGT Limits: Takeoff and Go-around - One engines inoperative:
10 mins - 950°C
48
Thrust Setting/EGT Limits: Maximum Continuos Thrust (MCT)
Not limited - 915°C
49
Thrust Setting/EGT Limits: Starting (On ground/In flight):
725°C
50
APU BLEED: Max altitude to assist engine start:
20 000 ft
51
APU BLEED: Max altitude for air conditioning and pressurization (single pack operation):
22 500 ft
52
APU BLEED: Max altitude for air conditioning and pressurization (dual pack operation):
15 000 ft
53
ENGINES: Maximum N1
104%
54
ENGINES: Maximum N2
105%
55
OIL TEMPERATURE: Maximum continuous temperature
140 °C
56
OIL TEMPERATURE: Maximum transient temperature (15 min)
155 °C
57
OIL TEMPERATURE: Minimum starting temperature
-40 °C
58
OIL TEMPERATURE: Minimum temperature before takeoff
-10 °C
59
OIL QUANTITY: Minimum oil quantity
9.5 qt + estimated consumption
60
Maximum operating altitude with slats and/or flaps extended
20 000 ft
61
Minimum fuel quantity for takeoff
1 500 kg
62
Maximum brake temperature for takeoff
300 °C