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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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Quick Links

10/06/23

Message Overview:

Message Name:

PACK TEMP HIGH

Message Code:

B3-007409

Associated CAS:

PACK TEMP HIGH
(Caution)

Reporting LRU: Integrated Air System Controller (IAS) 1A
System Description: 21-61-00 - Temperature Control and Indication
Schematic Diagram: 21-61-00-101 - Temperature Control and Indication
Wiring Diagram: 21-52-17-1 - Sheet 1 - Compressor Discharge Temperature-Sensor - ALL

Message Description:

The compressor discharge temperature of the pack has been detected over its maximum allowed limit of 240°C. Run both Integrated Air System Controller (IASC) #1 power-up tests.

Possible Causes:

  • RAM Air Duct
  • Precooler
  • Precooler Heat Exchanger
  • Pack Overheat
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin:

  • AW300-21-0413 - Air Cycle Machine (ACM) - Investigation of Failures Causing Smoke/Smell Events

Forum Articles/Infoservice/Newsletter: None

  • SIL LS3471-21-01 - Failure of Air Cycle Machine PN 3471A020000 potentially causing smoke/smell event

Fault Confirmation Procedure:

  1. Message# = 1
  2. Fault Logged = AIR, TAXI
  3. Status = OVERHEAT
  4. Message Type = Fault Message
  5. {Term Definitions}

    1. IAS1A-59 XX 353 00 EXCT XXXX-XXXT XXXX-XXXX XXXX-XXXX 353A: 25; PACK OVERHEAT
    2. IAS2A-64 XX 353 10 EXCT XXXX-XXXT XXXX-XXXX XXXX-XXXX 353A: 25; PACK OVERHEAT

Quick Links:

Removal of the Covers and Plugs AMM 10-12-00-020-802
Standard Aircraft Configuration for Maintenance AMM 12-00-00-867-803
Operational Test of the Cabin Pressure Control System AMM 21-31-00-710-801
Component Location AMM 21-31-00-992-801
Removal of the Integrated Air System (IAS) Controller AMM 21-31-01-000-801
Installation of the Integrated Air System (IAS) Controller AMM 21-31-01-400-801
Removal of the Outflow Valve AMM 21-31-05-000-801
General Visual Inspection of the Outflow Valve AMM 21-31-05-210-801
Installation of the Outflow Valve AMM 21-31-05-400-801
Removal of the Air Cycle Machine AMM 21-52-13-000-801
Installation of the Air Cycle Machine AMM 21-52-13-400-801
Removal of the Compressor Discharge Temperature-Sensor AMM 21-52-17-000-801
Installation of the Compressor Discharge Temperature-Sensor AMM 21-52-17-400-801
Removal of the Pack Discharge Temperature-Sensor AMM 21-52-37-000-801
Installation of the Pack Discharge Temperature-Sensor AMM 21-52-37-400-801
Removal of the Ram-Air Intake Upper-Duct AMM 21-53-13-000-801
General Visual Inspection of the Ram-Air Inlet Ducting AMM 21-53-13-210-801
Installation of the Ram-Air Intake Upper-Duct AMM 21-53-13-400-801
Removal of the Ram-Air Intake Lower-Duct AMM 21-53-17-000-801
Installation of the Ram-Air Intake Lower-Duct AMM 21-53-17-400-801
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
Electrical/Electronic Safety Precautions AMM 24-00-00-910-801
Electrostatic-Discharge Safety Precautions AMM 24-00-00-910-802
Removal of the Lower Precooler Inlet-Duct AMM 36-11-45-000-801
Installation of the Lower Precooler Inlet-Duct AMM 36-11-45-400-801
Removal of the Upper Precooler Inlet-Duct AMM 36-11-47-000-801
Installation of the Upper Precooler Inlet-Duct AMM 36-11-47-400-801

Troubleshooting Recommendations:

  1. The compressor discharge temperature of the pack has been detected over its maximum allowed limit of 240°C. Run both IASC #1 power-up tests. If no problem is detected, clean RAM air ducting, Precooler and Precooler Heat Exchanger.
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