Annexes
p. 118
Anne
xes
CRUISE
SPEED LOW
DEGRADED
PERF
AP/OFF
GUIDANCE
INCREASE
SPEED
EGPWS
(or TAWS if T2CAS equipped)
GPWS switch and associated lights:
ON:
All basic GPWS modes are operative
FLAP OVRD:
In reduced flap landing, to
inhib the mode 4 alert
OFF:
All basic GPWS modes inhibited.
OFF:
light come on
FAULT
:
GPWS FAULT ——
> some or all
GPWS basic modes are lost
FAULT
:
TERR FAULT ——
> some or all
enhanced modes are lost
OFF:
All enhanced (TCF&TAD) modes
inhibited
SWITCHING PANEL
When facing to a failure on
the Attitude/ heading or
VOR/ILS or SGU, it permits
to recover the information
from the other side.
Priority is always given to the
captain
MKR
Allows selection of
marker sensitivity
(LO or HI)
A/ERECT FAIL
Associated AHRS loses the
TAS signal from the ADC. The
AHRS is operating in basic
attitude mode.
Aircraft stabilized, gyro fast
erection when pushing on the
P/B for 15s
AUDIO 1/ 2 SEL
FAULT
: When the associated
RCAU part is failed.
ALTN: Affected crew station is
connected directly to:
– VHF1 if CAPT station is
affected.
– VHF2 if F/O station is
affected.
DSP SEL P/B
RDR
: Weather Radar display
on EFIS
TERR
: Terrain display on EFIS
Even if RDR is selected, in
case of terrain warning an
automatic pop out permit to
have the terrain display on
EFIS
ADC SWITCH
To feed either from ADC1 or
ADC2
– EEC1/2
– TAT/SAT/TAS indicator
– GNSS
– FDAU
FAULT
: some or all the
systems here above, are fed
by the ADC 1 when the ADC
2 is selected (relays defect)
Never faulty if selected to
ADC 1
AP OFF
Both lights illuminate or
flash red when autopilot.
associated to the cavalry
charge aural alert
STICK PUSHER
Illuminates when stick
pusher is operating
GUIDANCE
in CAT II, when an
Excess deviation is detected
GPWS
If any mode 1-2-3-4-TCF-TAD
alert of the EGPWS (or TAWS)
is activated
G/S: If mode 5 is activated
Summary of Contents for 42-500
Page 1: ...72 212A 42 500 ...
Page 7: ...A Aircraft general p 6 A Aircraft general p 6 A Aircraft general FCOM 1 00 ...
Page 12: ...A Aircraft general p 11 8 Internal lighting ATA 33 ...
Page 14: ...B Multi Function Computer p 13 B Multi Function Computer FCOM 1 01 ...
Page 16: ...C Centralized crew alerting system p 15 C Centralized crew alerting system FCOM 1 02 ...
Page 22: ...D Air p 21 D Air FCOM 1 03 ...
Page 30: ...E Automatic flight control system p 29 E Automatic flight control system FCOM 1 04 ...
Page 33: ...F Communications FCOM 1 05 p 32 F Communications ...
Page 38: ...G Electrical systems p 37 G Electrical systems FCOM 1 06 ...
Page 52: ...H Emergency equipment p 51 H Emergency equipment FCOM 1 07 ...
Page 57: ...I Fire protection p 56 I Fire protection FCOM 1 08 I Fire protection p 56 ...
Page 60: ...J Flight control p 59 J Flight control FCOM 1 09 ...
Page 65: ...K Flight instruments p 64 K Flight instruments FCOM 1 10 K Flight instruments p 64 ...
Page 74: ...L Fuel system p 73 L Fuel system FCOM 1 11 ...
Page 83: ...M Hydraulic system p 82 M Hydraulic system FCOM 1 12 M Hydraulic system p 82 ...
Page 86: ...N Ice and rain protection p 85 N Ice and rain protection FCOM 1 13 ...
Page 92: ...O Landing gear p 91 O Landing gear FCOM 1 14 ...
Page 95: ...P Navigation system p 94 P Navigation system FCOM 1 15 P Navigation system p 94 ...
Page 98: ...P Navigation system p 97 MODE 4 unsafe terrain clearance MODE 5 below glideslope ...
Page 102: ...Q Power plant p 101 Q Power plant FCOM 1 16 ...
Page 110: ...Annexes p 109 Annexes ...
Page 128: ...p 127 ...