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R  (Ref. AMM TASK 49-61-34-000-003) and (Ref. AMM TASK 49-61-34-
R  400-003). 
R  D. If the PD is more than 8 psig lower than PT (ECS or MES mode): 
R  NOTE : PD = main engine precooler inlet air pressure (source BMC).____ 
R  NOTE : As a rule of thumb, the pressure drop accross the cross bleed____ 
R  valve is 3 psig, therefore PD (RTL mode) shows approx. 3 psig 
R  higher than PD (ECS or MES mode). 
R  - check on the MCDU the load control valve position (the ADW1 parameter 
R  shows a 9 in the last position i.e. 08509 = load control valve open). 
R  (1) If the ADW1 shows that the load control valve is not open (e.g. ADW1 
R  = 08108): 
R  - replace the LOAD CONTROL VALVE P12 (Ref. AMM TASK 49-51-51-000-004) 
R  and (Ref. AMM TASK 49-51-51-400-004). 
R  (2) If the ADW1 shows that load control valve is fully open (e.g. ADW1 = 
R  08109): 
R  - in the APU compartment, do a check of the load control valve 
R  position. 
R  (a) If the load control valve is fully open: 
R  - do a check of the APU bleed system for leaks. 
R  1_  If the fault continues:
R  - do the trouble shooting procedure of low air pressure in the 
R  right crossbleed duct (Ref. TASK 36-12-00-810-804). 
R  E. If the LCIT is more than 10 deg.C higher than the outside air temperature 
R  (TAT): 
R  - check for hot gas ingestion (make sure that the main engine exhaust is 
R  not blown into the APU air intake), 
R  - check for hot gas leaks at the APU compressor split lines.

 201-207, Config-1 Aug 01/05 CES

R (1) If the fault appears to be intermitted:
R - do a check and repair of the aircraft wiring
R from the ECB (59KD) AB/H3,H4 to the electrical connector P1/7,6
R and
R from P1/7,6 to the Inlet Temp Sensor P6/B,A
R (Ref. ASM 49-61/02)
R - replace the INLET TEMP SENSOR (P6) (Ref. AMM TASK 49-23-14-000-001)
R and (Ref. AMM TASK 49-23-14-400-001).

R (a) If the fault continues:
R - replace the ECB (59KD) (Ref. AMM TASK 49-61-34-000-001) and
R (Ref. AMM TASK 49-61-34-400-001).

R F. If the LCIT is more than 10 deg.C lower than the outside air temperature
R (TAT):
R - do a check and repair of the aircraft wiring
R from the ECB (59KD) AB/H3,H4 to the electrical connector P1/7,6
R and
R from P1/7,6 to the Inlet Temp Sensor P6/B,A
R (Ref. ASM 49-61/02)
R - replace the INLET TEMP SENSOR (P6) (Ref. AMM TASK 49-23-14-000-001) and
R (Ref. AMM TASK 49-23-14-400-001).

R (1) If the fault continues:
R - replace the ECB (59KD) (Ref. AMM TASK 49-61-34-000-001) and (Ref.
R AMM TASK 49-61-34-400-001).

R (a) If the fault continues:
R - do a check and repair of the aircraft wiring from the ECB
R (59KD) AB/4H,3H to the INLET TEMP SENSOR studs/alumel,chromel
R (Ref. ASM 49-62/02) (Ref. ASM 49-62/04).

R **ON A/C 001-049, 101-105, 151-199, 201-210,

R Post SB 49-1062 For A/C 001-049,101-105,151-154,201-207,

R A. If the self test gives the maintenance message:
R
R - CHECK PRESS XDCR WIRING/ECB 59KD (Ref. TASK 49-00-81-810-852),
R - DIFFERENTIAL PRESS XDCR (8043KM) (Ref. TASK 49-00-81-810-853),
R - TOTAL PRESS XDCR (8044KM) (Ref. TASK 49-00-81-810-854),
R - SURGE CTL VALVE (8058KM) (Ref. TASK 49-00-81-810-871),
R - INLET GUIDE VANE ACTR (8014KM) (Ref. TASK 49-00-81-810-851) or
R (Ref. TASK 49-00-81-810-858).
R - LOAD CTL VALVE (8050KM) (Ref. TASK 49-00-81-810-861).
R - INLET TEMP SENSOR (8010KM) (Ref. TASK 49-20-00-810-803).
R - INLET OVERHEAT/CHECK APU INLET (Ref. TASK 49-00-81-810-843).

 「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, 107-107, 151-199, ∞∞49-00-81∞∞∞∞∞∞∞∞∞∞Page B259
 201-210, Config-1 Aug 01/05 CES

R B. If the IGV parameter values are out of range:
R - check that the EGT increase during a mode change (i.e. RTL to ECS).

R NOTE : RTL = Ready To Load

____
R (1) If the EGT does not increase:
R - remove the IGV ACTUATOR 8014KM (Ref. AMM TASK 49-23-51-000-004).
R - do a push/pull test on the IGVs to check the IGV movement.
R .make sure that the IGV has a travel range of 1 in. (25.3999 mm),
R .measure the force of the IGV movement.

R (a) If a force less than 20 lbf.ft (2.7116 m.daN) is necessary to
R move the IGVs:
R - replace the IGV ACTUATOR 8014KM (Ref. AMM TASK 49-23-51-000-R 004) and (Ref. AMM TASK 49-23-51-400-004).
　
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