B767-300 Limitations Flashcards
1
Q
Max certified altitude
A
43100’
2
Q
Max Take off and Landing elevation
A
8400’
3
Q
Rough air penetration speed
A
290 / M0.78
4
Q
Max RWY slope
A
+/- 2%
5
Q
Maximum tailwind component
(non autoland)
A
10 kts
6
Q
Maximum cross wind
(non autoland)
A
Not defined
7
Q
Maximum head wind component
(autoland)
A
25 kts
8
Q
Maximum cross wind component
(autoland)
A
25 kts
9
Q
Maximum tail wind component
(autoland)
A
10 kts
10
Q
Minimum autopilot engagement height
A
200’ RA
11
Q
Maximum flap extension altitude
A
20000’ MSL
12
Q
Minimum speedbrake height
A
800’ AGL
13
Q
Cargo door wind limitations
A
40 kts operations (60 kts open)
14
Q
Max center tank capacity when fuel main tanks are NOT full
A
22050 lbs
(structual limitation)
15
Q
B767 taxi fuel
A
600 lbs
16
Q
B767 MTW (OY-SRU)
A
413,000 lbs
17
Q
B767 MTOW (OY-SYA)
A
412,000 lbs
18
Q
B767 MLW (OY-SYA)
A
326,000 lbs
19
Q
B767 MZFW (OY-SRU)
A
309,000 lbs
