2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R  ESPM 204416W01
 AMM 34-36-00-720-001  Functional Test of the ILS
R  AMM 34-36-18-000-001 AMM 34-36-18-400-001 AMM 34-36-31-000-001 AMM 34-36-31-400-001 ASM 34-36/01  Removal of the Glide/Slope Antenna (4RT)Installation of the Glide/Slope Antenna (4RT)Removal of the ILS Receiver (2RT1,2RT2)Installation of the ILS Receiver (2RT1,2RT2)
 3. Fault Confirmation__________________
 A. Test

 Do the functional test of the ILS (Ref. AMM TASK 34-36-00-720-001).
 4. Fault Isolation
_______________
 A. If the G/S indication does not come into view on the CAPT PFD and F/O ND during the test:
 - replace the RECEIVER-ILS, 1 (2RT1) (Ref. AMM TASK 34-36-31-000-001) and (Ref. AMM TASK 34-36-31-400-001).
 (1) If the fault continues:
 - do a check of the wiring from the glide/slope 1/2 antenna (4RT) to R the ILS receiver 1 (2RT1) (Ref. ASM 34-36/01) and (Ref. ESPM R 204416W01).
 (a) If there is no continuity:

 - repair the above wiring.

 (b) If there is continuity:

 - replace the ANTENNA-GLIDE/SLOPE 1/2 (4RT) (Ref. AMM TASK 34-36-18-000-001) and (Ref. AMM TASK 34-36-18-400-001).
 「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 : ALL ∞∞34-36-00∞∞∞∞∞∞∞∞∞∞Page 244
 May 01/05 CES

 B. If the G/S indication does not come into view on the F/O PFD and CAPT ND during the test:
 - replace the RECEIVER-ILS, 2 (2RT2) (Ref. AMM TASK 34-36-31-000-001) and (Ref. AMM TASK 34-36-31-400-001).
 (1) If the fault continues:
 - do a check of the wiring from the glide/slope 1/2 antenna (4RT) to R the ILS receiver 2 (2RT2) (Ref. ASM 34-36/01) and (Ref. ESPM R 204416W01).
 (a) If there is no continuity:

 - repair the above wiring.

 (b) If there is continuity:

 - replace the ANTENNA-GLIDE/SLOPE 1/2 (4RT) (Ref. AMM TASK 34-36-18-000-001) and (Ref. AMM TASK 34-36-18-400-001).
 C. If the G/S indication does not come into view on the two PFDs and the two NDs during the test:
 - replace the ANTENNA-GLIDE/SLOPE 1/2 (4RT) (Ref. AMM TASK 34-36-18-000-001) and (Ref. AMM TASK 34-36-18-400-001).
 D. Do the test given in Para. 3.

 Loss of the LOC Indication on the PFD(s) and ND(s)
 1. Possible Causes
_______________
 - RECEIVER-ILS, 1 (2RT1)

 - ANTENNA-LOCALIZER 1/2 (3RT)

 - RECEIVER-ILS, 2 (2RT2)

 - wiring from the localizer 1/2 antenna (3RT) to the ILS receiver 1 (2RT1)

 - wiring from the localizer 1/2 antenna (3RT) to the ILS receiver 2 (2RT2)

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R  ESPM 204416W01
 AMM 34-36-00-720-001  Functional Test of the ILS
R  AMM 34-36-11-000-001 AMM 34-36-11-400-001 AMM 34-36-31-000-001 AMM 34-36-31-400-001 ASM 34-36/01  Removal of the Localizer Antenna (3RT)Installation of the Localizer Antenna (3RT)Removal of the ILS Receiver (2RT1,2RT2)Installation of the ILS Receiver (2RT1,2RT2)
 3. Fault Confirmation__________________
 A. Test

 Do the functional test of the ILS (Ref. AMM TASK 34-36-00-720-001).
 4. Fault Isolation
_______________
 A. If the LOC indication does not come into view on the CAPT PFD and F/O ND during the test:
 - replace the RECEIVER-ILS, 1 (2RT1) (Ref. AMM TASK 34-36-31-000-001) and (Ref. AMM TASK 34-36-31-400-001).
 (1) If the fault continues:
 - do a check of the wiring from the localizer 1/2 antenna (3RT) to R the ILS receiver 1 (2RT1) (Ref. ASM 34-36/01) and (Ref. ESPM R 204416W01).
 (a) If there is no continuity:

 - repair the above wiring.

 (b) If there is continuity:

 - replace the ANTENNA-LOCALIZER 1/2 (3RT) (Ref. AMM TASK 34-36-11-000-001) and (Ref. AMM TASK 34-36-11-400-001).
 「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 : ALL ∞∞34-36-00∞∞∞∞∞∞∞∞∞∞Page 246
 May 01/05 CES

 B. If the LOC indication does not come into view on the F/O PFD and CAPT ND during the test:
　
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