R (7) Do the leak test of the standby Air Data system (Ref. AMM TASK 34-22-R 25-790-001).

R (8) Do the functional test of the ADM for the CAPT (F/O) circuit (Ref.
R AMM TASK 34-11-00-720-001).

R (a) If one pressure value is different, replace the defective ADM
R (Ref. AMM TASK 34-11-17-000-001) and (Ref. AMM TASK 34-11-17-400-R 001).

R (9) If the fault continues:
R - If there is a report of small airspeed/altitude fluctuations and if
R there are maintenance messages related to the SFCCs in the PFR :
R replace the defective SFCCs (Ref. AMM TASK 24-51-34-000-001) and
R (Ref. AMM TASK 27-51-34-400-001)
R - Do a check of the ADR/SFCC interface wirings (Ref. ASM 34-13/02).
R - Do a check to make sure that there are no impacts on the fuselage
R around the ADMs and the static probes (Ref. SRM 530011P.BLOCK101).

R **ON A/C 001-049, 101-105, 151-199, 201-228,

 D. Do the test given in Para. 3.
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : 001-049, 101-105, 151-199, 201-228, ∞∞34-13-00∞∞∞∞∞∞∞∞∞∞Page B250
 May 01/05 CES

 AIR DATA - TASK SUPPORTING DATA_______________________________
 1. Quick Maintenance Guide of the ADR__________________________________
 **ON A/C 001-049, 101-105, 151-199, 201-203,
R  (Ref. Fig. 301) **ON A/C 051-099, 106-149, 204-299, 301-399, 401-499,
R R  (Ref. Fig. 301A) **ON A/C 106-149, 213-213, 221-299, 301-399, 401-499, 
R R R R  (Ref. Fig. 302) **ON A/C 001-049, 051-099, 101-105, 151-199, 201-220, Post SB 34-1222 For A/C 213-213, Post SB 34-1280 For A/C 213-213, (Ref. Fig. 302A) **ON A/C ALL
 To prevent unjustified ADIRS removals, an ADR MAINTENANCE GUIDE has been created to improve assistance of the line maintenance crews, in making their decisions on ADIRU removals.

 Air Data Reference
 Figure 301

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 101-105, 151-199, 201-203, ∞∞34-13-00∞∞∞∞∞∞∞∞∞∞Page 302
 May 01/05 CES

 Air Data Reference
 Figure 301A

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 051-099, 106-149, 204-299, 301-399, ∞∞34-13-00∞∞∞∞∞∞∞∞∞∞Page 303
 401-499, Aug 01/05 CES

R Altitude/Airspeed Comparison R Figure 302
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 106-149, 213-213, 221-299, 301-399, ∞∞34-13-00∞∞∞∞∞∞∞∞∞∞Page 304
 401-499, Aug 01/05 CES

 Altitude/Airspeed Comparison R Figure 302A
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : 001-049, 051-099, 101-105, 151-199, ∞∞34-13-00∞∞∞∞∞∞∞∞∞∞Page 305
 201-220, Aug 01/05 CES

 AIR DATA - FAULT ISOLATION PROCEDURES
_____________________________________
 TASK 34-13-81-810-801
 Loss of the ADR1 BUS2 Interface with the EFCS2 Identified by the EFCS1
 1. Possible Causes
_______________
 - wiring between the terminal blocks 1860VT and 1840VT
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
R  AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning) AWM 34-11-18
 3. Fault Confirmation
__________________
 A. Test
 (1) Do the BITE test of the EFCS (Ground Scanning) (system 1) (Ref. AMM TASK 27-96-00-740-001).
 4. Fault Isolation
_______________
 A. If the test gives the maintenance message ADR1 BUS 2:
 - do a check and repair the wiring between the terminal blocks 1860VT and 1840VT: between pins 28F, 27F and 76E, 75E (Ref. AWM 34-11-18).
 B. Do the test given in Para. 3.

 TASK 34-13-81-810-802
 Loss of the ADR1 BUS3 Interface with the EFCS1 Identified by the EFCS1

 1. Possible Causes
_______________
 - wiring between the terminal blocks 1851VT and 1831VT
 2. Job Set-up Information
______________________
 A. Referenced Information
　
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