Pilot's Operating Handbook
Section 3
Emergency procedures
EASA Approved
Edition 0 - March 05, 2019
Rev. 0
Page 3.3.6
Engine regulation discrepancy, power loss,
throttle control loss 2/3
► Continuing
8 - Continue the flight.
► Land as soon as possible ◄
If the available power is weak :
9 - LANDING GEAR lever DN. . . . . . . . . . . . . . . . . . . . . . . . . .
Only on a final approach glide path
10 - FLAPS lever LDG. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Only in short final
▲ CAUTION ▲
When MAN OVRD control is used, the available power may not be
sufficient to ensure a go-around in landing configuration, particularly if
the weight is near the maximum weight.
▲
► Do not perform a go around ◄
► Do not use the reverse ◄
11 - Land normally.
12 - Brakes As required. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
End of procedure ■
If minimum power obtained is excessive :
13 - Airspeed Reduce below 178 KIAS. . . . . . . . . . . . . . . . . . . . . . . .
By setting nose-up attitude
14 - INERT SEP switch ON. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
If ITT > 840°C :
15 - INERT SEP switch OFF. . . . . . . . . . . . . . . . . . . . . . . . . . . .
16 - LANDING GEAR lever DN. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
17 - FLAPS lever TO. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Continue ►
To Next Page
