O - Landing gear
p. 93
GEAR HANDLE RED LIGHT
any gear not sensed down and
locked with some conditions.
CAP.
System 1
UNLK
gear not locked in selected
position or (on GND) uplock box
not opened.
Green
Lt down lock engaged.
OFF
Pb released, system deactivated
F (FAULT)
wheel channel failure. CAP
EMERGENCY BRAKE HANDLE
permits to apply a metered pressure.
The brake accumulator allows at least six
braking applications without any antiskid
operation if the blue hydraulic system is
not available)
BRK TEMP
HOT
Any brake T° > 160°C
TEST pb
(inhibited if speed > 17 kts)
= MC + SC CAP 4F amber lt.
Test duration: 3 sec. in flight and
6 sec. on ground
ANTISKID
Operative if speed > 10 kts.
Activates when speed > 23 kts + 50%
diff between wheels (locked wheel
protection).
Braking action inhibited at touchdown as
long as wheel spin up speed < 35 kts or
5 sec. (touchdown protection).
CAUTION: THE TEST INHIBITS BRAKES
PARKING BRAKE
permits a full pressure on the brakes. When brake
handle is not in the fully released position, amber
PRKG BRK caution light illuminates on CAP and is
taken into account by the T/O CONFIG.
(Springloaded to the off position)
System 2
UNLK
gear not locked in selected
position or (on GND) uplock box
not opened.
Green
Lt down lock engaged
N/W STEERING SW
activates or deactivates the nose wheel
steering system (guarded type in the ON
position)
OFF: unpressurizes the steering system
(91° of deflection)
LDG GEAR EMERGENCY
EXTENSION HANDLE
permits to unlock the landing gear
3. LDG GEAR position indicators
ATA 32
4. Landing gear handles
ATA 32
5. Brakes temperature
ATA 32
and antiskid
6. Emergency parking
ATA 32
brake handle
7. Steering handwheel
ATA 32
THE STEERING HAND WHEEL
controls the nose wheel angle up to 60° in
either direction:
– clockwise: steering to the right
– counter clockwise: steering to the left
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 ...