Aircraft Operations Manual
EXTENDED WINGTIPS
PAGE
3
Dec 01/20
SE/CH/SU
REASON FOR CHANGE
CODE
PAGES
32/2.1
19
−
20
New pages with new tables for all engines climb gradient (metric).
32/2.2
19
−
20
New pages with new tables for all engines climb gradient (impe-
rial).
37/3.5
E4
−
1
15
Text added to highlight who controls the aircraft after pitch discon-
nect.