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PED Power Supply - Schematic Figure 302 (SHEET 1)
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PED Power Supply - Schematic Figure 302 (SHEET 2)
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Aug 01/05 CES ANCILLARY EQUIPMENT (INCLUDING DOOR AREA HEATING PANELS)
________________________________________________________ FAULT ISOLATION PROCEDURES
__________________________
TASK 25-27-00-810-807
EQUIP/FURNIS - DOOR AREA HEATING - One heated floor panel is INOP
1. Possible Causes
_______________
- fuse
- control unit
- heated floor panel
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 25-27-00-740-001 Bite Test of the Heated Floor Panel System. AMM 25-27-34-000-002 Removal of the Control Unit 60DS, 66DS AMM 25-27-34-400-002 Installation of the Control Unit 60DS, 66DS AMM 25-27-51-000-002 Removal of the Heated Floor Panel 31DS (30DS), 33DS
(32DS) AMM 25-27-51-400-002 Installation of the Heated Floor Panel 31DS (30DS),
33DS (32DS) ASM 25-27/01 ASM 25-27/02
3. Fault Confirmation
__________________
A. Do the Bite Test of the Heated Floor Panel System (Ref. AMM TASK 25-27-00-740-001).
4. Fault Isolation
_______________
A. If one test indicator on the related control unit does not come on:
- Do a check of the related fuse. If it is necessary replace the related fuse.
(1) If the fuse is not serviceable:
- Do a check of the aircraft wiring for a short circuit between the related control unit and the inoperative heated floor panel (Ref. ASM 25-27/01) or (Ref. ASM 25-27/02).
(a) If there is a short to ground:
- Repair the aircraft wiring (Ref. ASM 25-27/01) or (Ref. ASM 25-27/02).
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May 01/04 CES
(b) If there is no short to ground:
- Replace the related control unit (Ref. AMM TASK 25-27-34-000-002) and (Ref. AMM TASK 25-27-34-400-002).
(c) If the fault continues:
- Replace the related heated floor panel (Ref. AMM TASK 25-27-51-000-002) and (Ref. AMM TASK 25-27-51-400-002).
(2) If the fuse is serviceable:
- Do a check of the aircraft wiring between the related control unit and the inoperative heated floor panel (Ref. ASM 25-27/01) or (Ref. ASM 25-27/02).
(a) If there is continuity:
- Replace the related control unit (Ref. AMM TASK 25-27-34-000-002) and (Ref. AMM TASK 25-27-34-400-002).
(b) If there is no continuity:
1_ If the fault continues:
- Replace the related heated floor panel (Ref. AMM TASK 25-27-
51-000-002) and (Ref. AMM TASK 25-27-51-400-002).
- Repair the aircraft wiring (Ref. ASM 25-27/01) or (Ref. ASM 25-27/02).
B. Do the test given in para. 3.A.
EQUIP/FURNIS - DOOR AREA HEATING - All heated floor panels are INOP
1. Possible Causes
_______________
- RELAY-GALLEY PWR SPLY (6MC)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-56-00-810-801 Galley Supply Fault AMM 24-56-00-710-001 Operational Test of the Galley Supply AMM 24-56-55-000-002 Removal of the Contactor Located in the Panel 200VU AMM 24-56-55-400-002 Installation of the Contactor Located in the Panel
200VU AMM 25-27-00-740-001 Bite Test of the Heated Floor Panel System.
3. Fault Confirmation
__________________
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