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时间:2010-06-09 00:05来源:蓝天飞行翻译 作者:admin
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the landing gear is downlocked.
BRAKE FANS
The impeller creates a flow of air from the heat pack
to the exterior through the debris guard.
Each fan includes a three phase type motor, an impeller
and a shroud with a debris guard.
TMULDWW01-T01 LEVEL 1
EFFECTIVITY 32-48-00 Page 2
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 178
ALL
BRAKE COOLING SYSTEM PRESENTATION
TMULDWW01-P01 LEVEL 1
EFFECTIVITY 32-48-00 Page 3
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 179
ALL
THIS PAGE INTENTIONALLY LEFT BLANK
TMULDWW01 LEVEL 1
EFFECTIVITY 32-48-00 Page 4
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 180
ALL
32 - LANDING GEAR
32-42-00 WHEEL AND BRAKE ECAM PAGE
PRESENTATION
CONTENTS:
Wheel/Brake Release Indications
Anti-Skid Indication
Auto Brake Indications
Alternate Braking Indication
Brake Temperature Indications
TMULDA4ZZ LEVEL 1
EFFECTIVITY 32-42-00 Page 1
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 181
ALL
WHEEL AND BRAKE ECAM PAGE PRESENTATION
The ECAM WHEEL page displays landing gear and door
positions, as well as brake and steering indications.
WHEEL/BRAKE RELEASE INDICATIONS
The wheel and brake release indications are displayed
as shown on the table below.
ANTI-SKID INDICATION
"A/SKID" indication appears amber in case of failure
of Braking and Steering Control Unit system 1 and
system 2 or when the anti-skid and nose wheel steering
switch (A/SKID & N/W STRG) is set to "OFF".
AUTO BRAKE INDICATIONS
"AUTO BRK" (Green) : Steady when auto brake is armed.
Flashing for 10 sec after auto
brake disengagement.
"AUTO BRK" (Amber) : If arming conditions are not met.
If a failure occurs with the
system armed.
"MED", "LO" or "MAX" (Green) : Selected auto brake
rate.
ALTERNATE BRAKING INDICATION
"ALTN BRK" indication appears if the braking system
is in alternate mode.
During normal braking operation, if a master lever is
set to OFF, normal braking is momentarily lost and
alternate braking becomes operative.
This to avoid any jerks during braking when the
electrical generator is shut down.
BRAKE TEMPERATURE INDICATIONS
The various brake temperature indications are
displayed as shown on the table below.
TMULDA4ZZ-T01 LEVEL 1
EFFECTIVITY 32-42-00 Page 2
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 182
ALL
WHEEL AND BRAKE ECAM PAGE PRESENTATION
TMULDA4ZZ-P01 LEVEL 1
EFFECTIVITY 32-42-00 Page 3
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 183
ALL
THIS PAGE INTENTIONALLY LEFT BLANK
TMULDA4ZZ LEVEL 1
EFFECTIVITY 32-42-00 Page 4
Oct 31/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 184
ALL
32 - LANDING GEAR
32-42-00 WHEEL AND BRAKE SYSTEM WARNINGS
CONTENTS:
Config Parking Brake ON
Brakes Hot
Auto Brake Fault
Anti Skid NWS Fault
Anti Skid/NWS Off
Hydraulic Selector Valve Fault
Braking And Steering Control Unit System 1 (2) Fault
TMULDB6ZZ LEVEL 3
EFFECTIVITY 32-42-00 Page 1
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 185
ALL
TMULDB6ZZ-P01 LEVEL 3
WHEEL AND BRAKE SYSTEM WARNINGS
EFFECTIVITY 32-42-00 Page 2
Sep 30/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 32 LANDING GEAR
UF94200
EFFECTIVITY Page 186
ALL
32 - LANDING GEAR
32-42-00 NORMAL BRAKING COMPONENTS
CONTENTS:
BSCU
Brake Selector Valve
Filter
Automatic Selector
Throttle Valve
Manifold Normal Brake Servovalves
Normal Brake Servovalves
Pressure Transducers
Hydraulic Fuses
 
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