-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
R  98D10103501000  1 COVER - ICE DETECTION PROBE
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R  **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 10-11-00-991-001  Fig. 202 
R  **ON A/C 401-499, 
R  10-11-00-991-001-A  Fig. 202A 
R  **ON A/C ALL
 10-11-00-991-004 10-11-00-991-005 10-11-00-991-006  Fig. 203Fig. 204Fig. 205
 3. Job Set-up__________
 Subtask 10-11-00-941-056
 A. Safety Precautions
 (1) Put an ACCESS PLATFORM 5M (16 FT)- ADJUSTABLE in position near the aircraft.
 (2) Put a WARNING NOTICE in position in the cockpit to tell persons not to operate the systems while you install the protective devices on the aircraft.

 4. Procedure_________ 
R  **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
 Subtask 10-11-00-555-069
 A. Installation of the Protection Devices on the Fuselage (Ref. Fig. 202/TASK 10-11-00-991-001)
 (1) Protection of the 2 total temperature sensors - Put the COVER - SLIP-ON, TOTAL TEMPERATURE SENSOR (98A10001013000) in position.
 (2) Protection of the 3 pitot probes - Put the COVER - SLIP-ON PITOT PROBE (98A10001005000) in position.
 (3) 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.
 (4) Protection of the 6 static probes - Put the COVER-STATIC PROBE (98D10103500001) in position. 
R  **ON A/C 401-499, 
R  Subtask 10-11-00-555-069-A 
R R  A. Installation of the Protection Devices on the Fuselage (Ref. Fig. 202A/TASK 10-11-00-991-001-A) 
R R R  (1) Protection of the 2 total temperature sensors - Put the COVER - SLIP-ON, TOTAL TEMPERATURE SENSOR (98A10001013000) in position. 
R R  (2) Protection of the 3 pitot probes - Put the COVER - SLIP-ON PITOT PROBE (98A10001005000) in position. 
R R R  (3) 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. 
R R  (4) Protection of the 6 static probes - Put the COVER-STATIC PROBE (98D10103500001) in position.

 Protective Equipment
 Figure 202/TASK 10-11-00-991-001

R EFF : 001-049, 051-099, 101-149, 151-199,  10-11-00Page 243 201-299, 301-399, Aug 01/05   CES

R  Protective Equipment 
R  Figure 202A/TASK 10-11-00-991-001-A 
R EFF :  401-499,    10-11-00 Page 244 
    Aug 01/05
   
 CES  

R (5) Protection of the 2 ice detection probes
R - Put the COVER - ICE DETECTION PROBE (98D10103501000) in position.

R **ON A/C ALL

 Subtask 10-11-00-555-070
 B. Installation of the Protection Devices on the Engines (Ref. Fig. 203/TASK 10-11-00-991-004, 204/TASK 10-11-00-991-005)
 (1)
 Protection of the engine air intakes

 -Put the COVER - INLET COWL ENGINE (RSE1244) or COVER - INLET COWL ENGINE (98D10003002000) in position.

 (2)
 Protection of the engine exhaust nozzles

 -Put the COVER - COMMON NOZZLE (RSE1132) in position.

 (3)
 Protection of the thrust reverser opening

 -Put the HALF PLUG, RIGHT-THRUST REVERSER (HIX6002) and HALF PLUG, LEFT-THRUST REVERSER (HIX6003) in position.
 Subtask 10-11-00-555-071
 C. Installation of the Protection Devices on the APU Area
 (Ref. Fig. 205/TASK 10-11-00-991-006)

 (1)
 Protection of the APU exhaust duct

 -Put the COVER - EXHAUST DUCT, APU (98D10007512000) in position.

 (2)
 Protection of the outlet duct of the APU oil cooler

 -Put the COVER - OILCOOLER OUTLET, APU (98D10007513000) in position.
 5. Close-up
________
 Subtask 10-11-00-942-058

 A. Close-up
 (1) Remove all the fixtures, tools, test and support equipment used during this procedure.

 Protective Equipment Figure 203/TASK 10-11-00-991-004
　
中國航空網(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 AMM PARKING, MOORING, STORAGE & RETURN TO S(16)