14 Essential Study and Practice
1. If all engine dri-
1.)Ground operating bus (GOB)
ven generators
2.)APU essential bus
are lost - what DC 3.) Flight Essential DC bus (FEDC)
power is avail- cb will automati- cally power what items?
able?
2. If a GEN
switch must be
left
in the OFF po-
sition because
of a generator
malfunction and
the GEN MECH
light illuminates
- what must
ac-
complished?
3. TRUE OR FALSE
- If the GEN
AUX CONT
C.B.
(FEDC) is out,
and the #2 GEN
OFF light is on,
partial load
mon- itoring will
ac- tivate with
the PROP or
EMP
de-ice
switches
placed to ON?
4. Disruption of the
MEAC bus or
loss of the ES-
SEN IND & LTG
, In-Flight Emergencies: OFM Chapter
14 Essential Study and Practice
4.) EIDS SEDC bus
(Via inverter or
True - the GEN AUX CONT cb will disable GEN 4
without illuminating the GEN 4 off light
Engine Start Selector)
The Emergency
Shutdown Procedure
Pilot and CP red instrument
lighting DCP glare shield control
panel lighting
5.
, In-Flight Emergencies: OFM Chapter
14 Essential Study and Practice
What systems 1.)Bus A - Feeders 2,3,4
are monitored 2.)60 HZ power
during 'Partial 3.)RADAR (66/145)
Load' monitor- 4.)Radiant heaters
ing? 5.)Galley power
6.)Side windshield heat
7.)DC feeder 5
6. How should a You Better Fly Back VFR
crew prepare for 1.)Uncover the boost handles
loss of all 2.)Utility Lights Positioned and on
electri- cal 3.)Flashlights within easy grasp
power - when 4.)Limit EMP and PROP de-ice utilization to de-
forced to ice only and not simultaneously.
operate with one
electri- cal
generator 1.)Boost handles - PULL
2.)Engine Start Selector - Select an engine for
7. With loss of power changes
all engine dri- Future Considerations
ven generators in- 1.)Flaps will remain in position
flight - what 2.)Only Engine Anti-ice is available
actions should 3.)Partial panel with no NAVAIDS
the crew take; 4.)Landing Gear - Free fall
what are fu- 5.)Boost out - no flap landing
ture considera- 6.)Emergency brake operation (3 full - 6 partial)
tions for land- 7.)Flight Idle stops - Extended (More force
ing? required to pull over the ramp)
8.)Maximum reverse speed - 125 KIAS (PL reset
pow- ered by BATT)
9.)Land at the nearest suitable airport as soon as
possi- ble
1.)GEN SW - OFF (Resets under voltage lockout
relay)
8. GEN reset 2.)GEN CONT CB - PULL AND RESET (Resets over
proce- dures? voltage lockout relay).
3.)GEN SW - ON
** Light remains on - un resettable (SFFB)
, In-Flight Emergencies: OFM Chapter
14 Essential Study and Practice
Light off and then
back on - Re occurring
malfunction