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Require immediate crew attention. These messages are accompanied by flashing master warning, triple chime attenson with or without voice message or dedicated tone. Require immediate crew awareness and future crew action may be required in the form of alternate system selection or performance limitation. These message are accompanied by flashing master caution and a single chime. Indicate safe or normal system operation which require crew awareness, over and above the dark cockpit philosophy. Indicate minor failures or reduction in systems capability, which require no crew action.

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01/21/25

Message Overview:

Message Name:

SHORT CIRCUIT

Message Code:

B3-008031

Associated CAS:

PACK LOOP FAIL
(Caution)

BLEED LOOP FAULT
(Advisory)

Reporting LRU: PACK LOOP B
System Description: 36-20-00 - Indicating System
Schematic Diagram: 36-21-00 - Bleed-Air Leak-Detection System
Wiring Diagram: 36-21-11Pack Loop

Message Description:

The PACK LOOP B is detected shorted to ground by the IASC-2 during the system self-test. Check the loop and wiring isolation to ground.

350_pack-loops

Possible Causes:

  • Pack Duct Leaking
  • Bleed Loop Routing
  • Pack Loop Sensor 1B (MT141)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Full Throttle Blog/Forum Articles/Infoservice/Newsletter: None

Flight Operation Notifications Manual (FONM): None

NOTES:

Quick Links:

Standard Aircraft Configuration for Maintenance AMM 12-00-00-867-803
Electrical/Electronic Safety Precautions AMM 24-00-00-910-801
Electrostatic-Discharge Safety Precautions AMM 24-00-00-910-802
Connect Electrical Power to the Aircraft AMM 24-00-00-861-801
Remove the Electrical Power from the Aircraft AMM 24-00-00-861-802
Component Location AMM 36-21-00-992-801
Bleed-Air Leak-Detection and Warning-System Safety Precautions AMM 36-21-00-910-801
Operational Test of the Bleed-Air Leak-Detection and Warning System AMM 36-21-00-710-801
Initiation Test of the Bleed-Air Leak-Detection Loops AMM 36-21-00-740-801
Resistance Check of the Bleed-Air Leak-Detection Loops AMM 36-21-00-760-801
Removal of the Left Bleed-Loop Element AMM 36-21-01-000-801
Installation of the Left Bleed-Loop Element AMM 36-21-01-400-801

Troubleshooting Recommendations:

  1. Gain access to IASC #2 located behind the lavatory sink just forward of the water pallet.
  2. Disconnect connector A56P4 from the IASC and check resistance between pins 10 and 11. Resistance should be approximately 15.4 Ω at room temperature.
  3. Isolate a system short through standard practices by isolating the different loop and wiring from the IASC. Repair faulty wire segment or replace loop as required.
  4. NOTE: Measure Insulation resistance and line resistance of the detection loops as per the Leak Detection Elements Troubleshooting Sheet. Make sure line resistance & insulation values are within the specified limits.

    Perform resistance checks on the applicable loop per AMM 36-21-00-760-801.

    NOTE: Before replacing a loop always look at the loop for routing, ensure loop is not too close to the plumbing or the bleed hole on a valve. Review AMM 36-21-00-992-801 for component location. See individual loops for specific routing information.

    NOTE: Often while troubleshooting this discrepancy the CAS is not usually present. However what you may find is higher than normal resistance such as 10 Ω or higher above nominal. It is not high enough to trip a bleed loop fault CAS message but high enough to assist in troubleshooting. When you get the resistance value down to nominal values then it is safe to say you've corrected the discrepancy.

    20_pack_air_loop10_2iasc_location

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