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 C. Manually turn the AOA sensor from the maximum to the minimum mechanical stops (+ 85. to - 35.) and make sure that there is no hard point. 
R  **ON A/C 001-049, 101-105, 151-199, 201-228,
 5. Close-up________ 
R  **ON A/C 001-049, 101-105, 151-199, 201-228, 
R  Post SB  34-1222 For A/C 001-049,101-105,151-199,201-228,
 Subtask 34-11-19-860-054
 A. Put the aircraft back to its initial configuration.
 (1) Install the AOA sensor slip-on cover.
 (2) Make sure that the work area is clean and clear of tool(s) and other items.
 (3) Remove the access platform(s). 

R 1EFF : 001-049, 101-105, 151-199, 201-228, 1 34-11-19Page 604 1 1 May 01/05 1 1 1CES 1

 Subtask 34-11-19-865-054
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------FOR 3FP1 49VU ANTI ICE/PROBES/AOA/1 4DA1 D04 49VU NAV PROBES/ADIRU 1/AND AOA 1/26VAC 5FP1 F07 49VU NAV PROBES/ADIRU1/115VAC 4FP1 F06 
R  **ON A/C 001-049, 101-105, 201-203,
 121VU ADIRS/ADIRU/3PWR/SWTG  9FP  N10
 **ON A/C 151-199, 204-228,
 121VU ADIRS/ADIRU/3PWR/SWTG  9FP  N09 
R  **ON A/C 001-049, 101-105, 151-199, 201-228, 
R  Post SB  34-1222 For A/C 001-049,101-105,151-199,201-228,
 FOR 3FP2 
R  **ON A/C 001-049, 101-105, 201-203,
 121VU ADIRS/ADIRU/2PWR/SHED 121VU ADIRS/ADIRU/2/26VAC AND AOA 121VU ADIRS/ADIRU/2/115VAC  10FP 5FP2 4FP2  N11N09N07
 **ON A/C 151-199, 204-228,
 121VU ADIRS/ADIRU/2PWR/SHED 121VU ADIRS/ADIRU/2/26VAC AND AOA 121VU ADIRS/ADIRU/2/115VAC  10FP 5FP2 4FP2  N10N08N06 
R  **ON A/C 001-049, 101-105, 151-199, 201-228,
 122VU ANTI ICE/PROBES/2/AOA  4DA2  Y13 

R 1EFF : 001-049, 101-105, 151-199, 201-228, 1 34-11-19Page 605 1 1 May 01/05 1 1 1CES 1

R  -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------**ON A/C 001-049, 101-105, 151-199, 201-228, 
R  Post SB  34-1222 For A/C 001-049,101-105,151-199,201-228,
 FOR 3FP3 
R  **ON A/C 001-049, 101-105, 201-203,
 121VU ADIRS/ADIRU/3PWR/SWTG 121VU ADIRS/ADIRU/3/26VAC AND AOA 121VU ADIRS/ADIRU/3/115VAC  9FP 5FP3 4FP3  N10N08N06
 **ON A/C 151-199, 204-228,
 121VU ADIRS/ADIRU/3PWR/SWTG 121VU ADIRS/ADIRU/3/26VAC AND AOA 121VU ADIRS/ADIRU/3/115VAC  9FP 5FP3 4FP3  N09N07N05 
R  **ON A/C 001-049, 101-105, 151-199, 201-228,
 122VU ANTI ICE/PROBES/3/AOA  4DA3  Z15 

R 1EFF : 001-049, 101-105, 151-199, 201-228, 1 34-11-19Page 606 1 1 May 01/05 1 1 1CES 1

 AIR DATA/INERTIAL REFERENCE SYSTEM (ADIRU & CDU) - DESCRIPTION AND OPERATION
____________________________________________________________________________
 1. General
_______ The Air Data/Inertial Reference System (ADIRS) provides the main air data and heading/attitude/navigation data to the aircraft systems. The main computers of the ADIRS are the three Air Data/Inertial Reference Units (ADIRU) which are controlled by the ADIRS Control and Display Unit (CDU). The ADIRS is a three channel system. Each channel is isolated from the others and provides independent information as defined in ARINC 738. Each ADIRU contains:
 -
an Air Data Reference (ADR) portion. Its operation is described in 34-13

 -
an Inertial Reference (IR) portion. Its operation is described in 34-14. Power supply is common for ADR and IR and described in 34-11.

 2. Component Location
__________________
 (Ref. Fig. 001, 002)
 The three ADIRUs are installed in the avionics compartment.
 The ADIRS CDU is installed in the cockpit.

 -------------------------------------------------------------------------------FIN | FUNCTIONAL DESIGNATION | PANEL|ZONE|ACCESS | ATA | | | | DOOR | REF.
 -------------------------------------------------------------------------------1FP1 ADIRU-1 127 824 34-12-34 1FP2 ADIRU-2 128 824 34-12-34 1FP3 ADIRU-3 127 824 34-12-34 2FP CDU-ADIRS 20VU 211 831 34-12-12
R 1EFF : 001-049, 101-105, 151-199, 201-203, 1 34-12-00Page 1 1 1 Config-1 May 01/05 1 1 1CES 1

 ADIRS - Component Location
 Figure 001

R 1EFF : 001-049, 101-105, 151-199, 201-203, 1 34-12-00Page 2 1 1 Config-1 May 01/05 1 1 1CES 1
　
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