R -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU CLOCK/NORM/SPLY 6FS F11 49VU CAPT/LOUD/SPKR 5WW F10 49VU NAV PROBES/ADIRU3/PWR/SWTG 8FP F09 49VU SDAC/1 AND 2/28VDC/ESS BUS 12WV F05 49VU COM/RMP/1 2RG1 G10 49VU COM/VHF/1 2RC1 G09 49VU COM/AUDIO/FLT/INTPH 9RN G08 49VU COM/AUDIO/ACP/F/O 5RN G07 49VU COM/AUDIO/ACP/CAPT 4RN G06 49VU LIGHTING/EMER LT/CABIN 79WL H07 49VU LIGHTING/ICE AND STBY/COMP/LIGHT 1LF H04
R **ON A/C 106-149, 213-213, 221-299, 301-399, 401-499,
49VU STBY/INST 5FN F12
R **ON A/C 106-149, 151-199, 301-399, 401-499,
49VU COM DIR ESS/1 150RH G01
R **ON A/C 401-499,
R 49VU ABCU &/Y BRK/PRESS IND 61GG C10
R R **ON A/C 001-049, 051-052, 054-056, 058-059, 061-099, 101-101, 103-149, 151-199, 201-299, 301-399, 401-499, Post SB 30-1037 For A/C 001-049,051-052,054-056,
49VU ANTI ICE/RAIN/RPLNT/CAPT 1DB1 D01
**ON A/C ALL
105VU ELEC/CSM/G /EV AUTO/SPLY 121VU ENGINE/IGN/ENG2/SYS B 121VU ENGINE/IGN/ENG1/SYS B 121VU ENGINE/IGN/ENG2/SYS A BAT 121VU ENGINE/IGN/ENG1/SYS A BAT 121VU ENGINE/ENG1/FADEC B/AND EIU 1 7XE 3JH2 3JH1 2JH2 2JH1 4KS1 C01P42P41P40P39R41
D. Flight Configuration Precautions
WARNING : OPEN THE PITOT-PROBE HEATER CIRCUIT-BREAKERS 3DA1, 3DA2 AND
_______ 3DA3 BEFORE YOU OPEN THE PHC CIRCUIT BREAKERS 2DA1, 2DA2 AND 2DA3. IF YOU DO NOT OBEY THIS SEQUENCE:
-
THE PITOT PROBES WILL BECOME TOO HOT,
-
THE PITOT PROBE COVERS WILL MELT AND,
-THERE IS A RISK OF INJURY TO MAINTENANCE PERSONNEL.
WARNING : OPEN THE WINDOW HEAT CIRCUIT-BREAKERS 4DG1 AND 4DG2, AND THE
_______ WINDSHIELD HEATER CIRCUIT-BREAKERS 1DG1 AND 1DG2, BEFORE YOU OPEN THE WHC CIRCUIT-BREAKERS 5DG1 AND 5DG2. IF YOU DO NOT OBEY THIS SEQUENCE:
-THE WINDOWS AND WINDSHIELDS WILL BECOME TOO HOT,
-THIS CAN CAUSE DAMAGE TO EQUIPMENT AND INJURY TO PERSONNEL.
WARNING : OPEN CIRCUIT BREAKERS 1JH, 2JH1, 2JH2, 3JH1 AND 3JH2 (ENGINE 1
_______ AND 2 IGNITION SYSTEMS). THEN OPEN CIRCUIT BREAKERS 2KS1 AND 2KS2 (FADEC A AND EIU 1 AND 2) AND 4KS1 (FADEC B AND EIU 1). IF YOU DO NOT OBEY THIS SEQUENCE, THE ENGINE AUTOMATIC IGNITION- SYSTEM WILL OPERATE. THIS CAN CAUSE INJURY TO MAINTENANCE PERSONNEL.
R (1) Do the flight configuration precautions with electrical power R (Ref. TASK 32-00-00-860-001).
(2) On the panel 35VU, make sure that:
-the GEN1, GEN2, APU GEN, EXT PWR and GALLEY pushbutton switches are pushed in.
Subtask 32-31-00-860-097
E. Aircraft Maintenance Configuration
(1) Disconnect the isolation coupling of the PTU (Ref. TASK 29-23-00-860-001).
WARNING : MAKE SURE THAT THE CONTROLS AGREE WITH THE POSITION OF THE
_______ ITEMS THEY OPERATE BEFORE YOU PRESSURIZE A HYDRAULIC SYSTEM.
(2) Use the Ground Power Cart to pressurize the Green Hydraulic System (Ref. TASK 29-10-00-863-001).
1EFF : ALL 1 32-31-00Page 541 1 1 May 01/05 1 1 1CES 1 1EFF : ALL 1 32-31-00Page 542 1 1 May 01/05 1 1 1CES 1 1EFF : ALL 1 32-31-00Page 543 1 1 May 01/05 1 1 1CES 1
(3) On the panel 35VU, make sure that: - the GEN1, GEN2, APU GEN, EXT PWR and GALLEY pushbutton switches are released (out).
(4) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
Subtask 32-31-00-860-098
F. Energize the Aircraft Electrical Circuits from the Batteries
(1) On the panel 35VU:
(a) Make sure that the voltage of the battery 1 and 2 is more than 25.5 VDC.
(b) Push (in) the BAT1 and BAT2 pushbutton switches.
(2) On the section INT LT of the panel 25VU:
(a) Put the DOME switch in the position DIM or BRT. Make sure that the dome lights come on.
(b) Put the DOME switch in the OFF position. Make sure that the dome lights go off.
Subtask 32-31-00-480-064
R R G. Installation of the Test Equipment (Ref. Fig. 505/TASK 32-31-00-991-025)
R R CAUTION : REMOVE THE PROTECTIVE COVERS FROM THE PROBES BEFORE YOU DO THE_______ TEST.
R (1) Remove the slip covers from the static and pitot probes.
R R (2) Connect the GENERATOR - GROUND PRESSURE (87202126V15) to the static and pitot probes as follows:
R R R (a) Use the ADAPTER COVER-STATIC PORT (98D34003500000) equipment to connect the GROUND PRESSURE GENERATOR to the static probes 7DA1 and 8DA1.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM LANDING GEAR 起落架4(68)
