1
Q
Ambient temperatures
A
Max for take-off & landing +50°C, ISA +40°C above 2525 ft
Min ground -40°C
2
Q
Max wind component take-off & Landing
A
Tail: 15
Cross (Demonstrated): 35
3
Q
Flexible thrust on runways
A
Approved
4
Q
Max altitude
A
31,000 ft
8000 ft for take-off & landing
5
Q
Max ∆P
A
6.75 psi
6
Q
T/O with packs & eng air on
A
Approved
7
Q
T/O with 33° flap
A
Not approved
8
Q
APU start
A
EXT DC start not approved
9
Q
Bird impact
A
250 kt IAS below 8000 ft
10
Q
VMO/MMO
A
295/0.72
11
Q
VA flap zero
A
235
12
Q
VA flap 18
A
175
13
Q
VFE flap 18
A
210 kt
18 en-route 175 kt
14
Q
VFE 24
A
180 kt
15
Q
VFE 30
A
170 kt
16
Q
VFE 33
A
150 kt
17
Q
Max alt for flaps
A
19,000 ft
18
Q
Gear
A
Max 205 kt
19
Q
Max weights
A
Ramp - 43,318 kg
Zero fuel - 35,153 kg
Take-off - 43,091 kg
Landing - 37,648 kg
BAe 146 Louis
flashcards
Decks in class (5)
# Cards
