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-------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------- 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power TSM 30 PB 101 (for corrective action) 3. Job Set-up __________ Subtask 30-31-00-861-057 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
Subtask 30-31-00-941-057 B. Aircraft Maintenance Configuration (1) On the panel 25VU: -push the PROBE/WINDOW HEAT pushbutton switch (the ON legend comes on). 4. Procedure _________ Subtask 30-31-00-810-052 A. Reactivation of the Heating of the Static Probes (1) Do the trouble-shooting of the system (Ref. TSM 30 PB 101) and do the applicable corrective steps. 1EFF : ALL 1 30-31-00Page 427 1 1 May 01/05R 1 1 1CES 1
5. Close-up ________ Subtask 30-31-00-942-054 A. Put the aircraft back to its initial configuration. (1) On the panel 25VU: -release the PROBE/WINDOW HEAT pushbutton switch (the ON legend goes off). Subtask 30-31-00-862-056 B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
1EFF : ALL 1 30-31-00Page 428 1 1 May 01/05R 1 1 1CES 1
TASK 30-31-00-040-004 Deactivation of the Heating of the Angle of Attack Sensors 1. Reason for the Job__________________ Refer to the MMEL TASK: 30-31-04 Probe Ice Protection Angle-of-attack Probe Heating 2. Job Set-up Information______________________ R A. Fixtures, Tools, Test and Support Equipment R R R -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION ------------------------------------------------------------------------------- R No specific circuit breaker(s) safety clip(s) R B. Referenced Information -------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------- R 30-31-00-710-001 32-69-00-860-001 34-13-00-740-002 34-13-00-740-003 Operational Test of the Probe Ice Protection Simulation of Flight, with the Aircraft on the GroundINTERFACE TEST of the ADRSYSTEM TEST of the ADR 3. Job Set-up__________ Subtask 30-31-00-941-058 A. Safety Precautions (1) On the panel 25VU: - make sure that the PROBE/WINDOW HEAT pushbutton switch is released (the ON legend is off).
4. Procedure _________ R **ON A/C 001-049, 101-105, 151-199, 201-210, 301-399, 401-499, Subtask 30-31-00-710-059-A A. Test (1) Do an operational test of the available probe ice protection systems (Ref. TASK 30-31-00-710-001). (2) Do a SYSTEM TEST of the ADR (Ref. TASK 34-13-00-740-003). **ON A/C 051-099, 106-149, 211-299,
Subtask 30-31-00-710-059 A. Test (1) Do an operational test of the available probe ice protection systems (Ref. TASK 30-31-00-710-001). (2) Do an INTERFACE TEST of the ADR (Ref. TASK 34-13-00-740-002). **ON A/C ALL
Subtask 30-31-00-750-053 B. Check of ECAM Warning Messages (1) Do a check of the ECAM warning messages related to the systems that operate correctly. Subtask 30-31-00-865-122 C. Open, safety and tag this(these) circuit breaker(s): -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 6DA1 49VU ANTI ICE/PROBES/AOA/1 4DA1 D04 49VU ANTI ICE/PROBES/PITOT/1 3DA1 D02
R Subtask 30-31-00-869-103 R D. Check R (1) On the upper ECAM DU: R - make sure that the R ANTI ICE CAPT PITOT R ANTI ICE CAPT AOA R indications come into view. R Subtask 30-31-00-865-123 R E. Remove the safety clip(s) and the tag(s) and close this(these) circuit R breaker(s): R FOR 6DA1 R 3DA1, 4DA1. R Subtask 30-31-00-865-124 R F. Open, safety and tag this(these) circuit breaker(s): R ------------------------------------------------------------------------------- R PANEL DESIGNATION IDENT. LOCATION www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM ICE AND RAIN PROTECTION 防冰和排雨2
