(a)
Protection of the APU exhaust duct
-Put the COVER - EXHAUST DUCT, APU (98D10007512000) in position.
(b)
Protection of the outlet duct of the APU oil cooler
-Put the COVER - OILCOOLER OUTLET, APU (98D10007513000) in position.
(2)
Installation of the Protection Devices on the fuselage
(a) Protection of the 2 total temperature sensors
-Put the COVER - SLIP-ON, TOTAL TEMPERATURE SENSOR (98A10001013000) in position.
(b) Protection of the 3 pitot probes - Put the COVER - SLIP-ON PITOT PROBE (98A10001005000) in position.
(c) Protection of the 3 angle-of-attack sensors - Put the COVER - SLIP-ON, ANGLE OF ATTACK SENSOR (98A10001500000) or COVER - SLIP-ON, AOA (98D10003003000) in position.
(d) Protection of the 6 static probes - Put the COVER-STATIC PROBE (98D10103500001) in position.
(3) Installation of the Protection Devices on the engines
(a) Protection of the engine air intakes - Put the COVER - INLET COWL ENGINE (98D10003002000) in position.
(b) Protection of the engine exhaust nozzles - Put the COVER - COMMON NOZZLE (RSE1132) in position.
(c) Protection of the thrust reverser opening - Put the HALF PLUG, RIGHT-THRUST REVERSER (HIX6002) and HALF PLUG, LEFT-THRUST REVERSER (HIX6003) in position.
R R R (4) Put adhesive tape on all remaining joints and openings where the cleaning products could fall and cause damage. Record the locations where you put adhesive tape.
R R (5) Put protective polyethylene film or equivalent on the tires and brakes.
(6) Remove all the ground support equipment near the aircraft.
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 12-21-11Page 306 1201-299, 301-399, 1Aug 01/05 1 1 1CES 1
R **ON A/C 401-499,
R Subtask 12-21-11-620-052-A
R F. Protection of the Aircraft
R WARNING : USE ONLY THE SPECIFIED TOOLS FOR THE PROTECTION OF THE_______
R AIRCRAFT. DO NOT APPLY ADHESIVE TAPE ON THE PROBES, DUCTS,
R SENSORS (STATIC, PITOT, TAT, AOA).
R THE SPECIFIED TOOLS :
R - GIVE THE CORRECT PROTECTION TO THE AIRCRAFT EQUIPMENT,
R - ARE EASY TO SEE FROM THE GROUND. MAKE AN ENTRY IN THE
R AIRCRAFT LOG BOOK OR ATTACH A TAG ON THE CAPTAIN SIDE STICK TO
R TELL THE CREW THAT PROTECTION COVERS/DEVICES ARE INSTALLED.
R (1) Installation of the Protection Devices on the APU area
R (a) Protection of the APU exhaust duct
R - Put the COVER - EXHAUST DUCT, APU (98D10007512000) in position.
R (b) Protection of the outlet duct of the APU oil cooler
R - Put the COVER - OILCOOLER OUTLET, APU (98D10007513000) in
R position.
R (2) Installation of the Protection Devices on the fuselage
R (a) Protection of the 2 total temperature sensors
R - Put the COVER - SLIP-ON, TOTAL TEMPERATURE SENSOR
R (98A10001013000) in position.
R (b) Protection of the 3 pitot probes
R - Put the COVER - SLIP-ON PITOT PROBE (98A10001005000) in
R position.
R (c) Protection of the 3 angle-of-attack sensors
R - Put the COVER - SLIP-ON, ANGLE OF ATTACK SENSOR
R (98A10001500000) or COVER - SLIP-ON, AOA (98D10003003000) in
R position.
R (d) Protection of the 6 static probes
R - Put the COVER-STATIC PROBE (98D10103500001) in position.
R (e) Protection of the 2 ice detection probes
R - put the COVER - ICE DETECTION PROBE (98D10103501000) in
R position.
R 1EFF : 401-499, 1 12-21-11Page 307 1 1 Aug 01/05 1 1 1CES 1
R (3) Installation of the Protection Devices on the engines
R R (a) Protection of the engine air intakes - Put the COVER - INLET COWL ENGINE (98D10003002000) in position.
R R (b) Protection of the engine exhaust nozzles - Put the COVER - COMMON NOZZLE (RSE1132) in position.
R R R (c) Protection of the thrust reverser opening - Put the HALF PLUG, RIGHT-THRUST REVERSER (HIX6002) and HALF PLUG, LEFT-THRUST REVERSER (HIX6003) in position.
R R R (4) Put adhesive tape on all remaining joints and openings where the cleaning products could fall and cause damage. Record the locations where you put adhesive tape.
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊(cè) AMM SERVICING 1(120)
