Maximum Range Descent - After Engine Fail
3-8-02
continued
CAUTION
Monitor BAT 1 and BAT 2 amps. If one indication is positive, switch OFF
affected battery. After 5 minutes battery can be switched ON again. If
indication still positive switch battery OFF.
Note
During extended glide period
Engine Oil Level
and/or
Engine Oil Temp
may
appear - disregard for air start.
12.
Engine.........................................
Restart as soon as possible (if applicable)
(refer to
)
If engine restart was not successful or not applicable:
13.
Rate of descent...........................
Adjust to achieve cabin altitude of 10,000
ft before oxygen supply exhausted
Below 10,000 ft:
14.
ACS EMER shut off.....................
PULL (cabin ventilation)
15.
Aircraft.........................................
---------- END -----------
Maximum Rate Descent
3-8-03
(Refer to
)
1.
PCL.............................................
IDLE
2.
Landing gear...............................
Below 180 KIAS, down
3.
Aircraft speed..............................
M
MO
/V
MO
4.
All occupants...............................
Check seat lap and shoulder belts are
fastened and the lap belt tightened.
5.
Main OXYGEN lever...................
Confirm ON
Continued on next page
Section 3 - Emergency Procedures (EASA Approved)
Emergency Descent
Pilot's Operating Handbook
Report No: 02406
Issue date: Mar 06, 2020
Page 3-8-3
12-C-A15-40-0308-00A-141U-A
FOR
GENERAL
AND
FAMILIARIZATION
PURPOSES
ONLY
