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C - Stays as it is.
With both engine anti-ice pushbuttons set to ON,
does the N1 limit change ?
A - Yes.
B - No.
TMUICE306 LEVEL 1
EFFECTIVITY 30-21-00 Page 4
Sep 30/97
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 30 ICE & RAIN PROTECTION
UF94200
EFFECTIVITY Page 34
ALL
30 - ICE AND RAIN PROTECTION
30-21-00 ENGINE AIR INTAKE ICE PROTECTION
SYSTEM WARNINGS
CONTENTS:
Engine 1 or Engine 2 Valve Open
Engine 1 or Engine 2 Valve Closed
TMUIC1201 LEVEL 3
EFFECTIVITY 30-21-00 Page 1
Aug 06/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 30 ICE & RAIN PROTECTION
UF94200
EFFECTIVITY Page 35
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TMUIC1201-P01 LEVEL 3
ENGINE AIR INTAKE ICE PROTECTION SYSTEM WARNINGS
EFFECTIVITY 30-21-00 Page 2
Aug 06/99
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 30 ICE & RAIN PROTECTION
UF94200
EFFECTIVITY Page 36
ALL
30 - ICE AND RAIN PROTECTION
30-21-00 ENGINE AIR INTAKE ICE PROTECTION
SYSTEM INTERFACES
CONTENTS:
Pushbutton Switch
System Data Acquisition Concentrator
Zone Controller
TMUIC5001 LEVEL 3
EFFECTIVITY 30-21-00 Page 1
Sep 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 30 ICE & RAIN PROTECTION
UF94200
EFFECTIVITY Page 37
ALL
ENGINE AIR INTAKE ICE PROTECTION SYSTEM INTERFACES
PUSHBUTTON SWITCH
The pusbutton switch sends a discrete signal to the
solenoid to open or close the valve, this information
is also sent to the System Data Acquisition
Concentrators (SDACs).
The "FAULT" light comes on either during valve transit
or in case of disagreement between valve position and
system selection.
SYSTEM DATA ACQUISITION CONCENTRATOR
The SDACs acquire the pusbutton switch configuration
and the "FAULT" condition information to display system
status on ECAM warning page and ECAM MEMO page.
ZONE CONTROLLER
The Zone Controller acquires the "valve not closed"
position information from the valve position switch
for bleed air management.
TMUIC5001-T01 LEVEL 3
EFFECTIVITY 30-21-00 Page 2
Sep 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 30 ICE & RAIN PROTECTION
UF94200
EFFECTIVITY Page 38
ALL
ENGINE AIR INTAKE ICE PROTECTION SYSTEM INTERFACES
TMUIC5001-P01 LEVEL 3
EFFECTIVITY 30-21-00 Page 3
Sep 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 30 ICE & RAIN PROTECTION
UF94200
EFFECTIVITY Page 39
ALL
THIS PAGE INTENTIONALLY LEFT BLANK
TMUIC5001 LEVEL 3
EFFECTIVITY 30-21-00 Page 4
Sep 30/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 30 ICE & RAIN PROTECTION
UF94200
EFFECTIVITY Page 40
ALL
30 - ICE AND RAIN PROTECTION
30-21-00 ENGINE AIR INTAKE ICE PROTECTION
SYSTEM COMPONENTS
CONTENTS:
Engine Anti-Ice Valve
TMUIC3E03 LEVEL 2
EFFECTIVITY 30-21-00 Page 1
Aug 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 30 ICE & RAIN PROTECTION
UF94200
EFFECTIVITY Page 41
ALL
ENGINE AIR INTAKE ICE PROTECTION SYSTEM COMPONENTS
ENGINE ANTI-ICE VALVE
IDENTIFICATION
FIN: 4000DN
LOCATION
ZONE: (LH) 435, (RH) 446
COMPONENT DESCRIPTION
The engine anti-ice valve is a butterfly shut off
valve of the on/off type.
The valve is spring loaded to the closed position
in case of no air pressure.
A solenoid allows the valve to :
- close, if energized,
- open, if deenergized and air pressure from the
9th stage is high enough.
CUT VIEW
Two microswitches monitor the OPEN and CLOSE position.
LOCATED VIEW
The valve can be manually operated from an external
nut connected to the butterfly shaft.
In addition, the butterfly can be locked in closed or
open position by means of a pip pin. Visual valve
position is also provided.
TMUIC3E03-T01 LEVEL 2
EFFECTIVITY 30-21-00 Page 2
Aug 31/96
_A319/A320/A321 TECHNICAL TRAINING MANUAL
MECHANICS / ELECTRICS & AVIONICS COURSE 30 ICE & RAIN PROTECTION
UF94200
EFFECTIVITY Page 42
ALL
ENGINE AIR INTAKE ICE PROTECTION SYSTEM COMPONENTS - ENGINE ANTI-ICE VALVE -
CUT VIEW/LOCATED VIEW
TMUIC3E03-P01 LEVEL 2
　
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