06/30/21
Message Overview:
Message Name:
COCKPIT LIGHTS (INTEGRAL) CONTROL PANEL MALFUNCTION
| Message Code: | 331OBS002 |
| Effectivity: | All |
| System: | Panel Integral Lighting |
| System Description: | 33-11-00 |
| Schematic Diagram: | 33-11-00 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wiring Diagram: | 33-11-07 [ Global Express ] [ G5000 ] [ Global XRS ] 33-13-01 [ Global Express ] [ G5000 ] [ Global XRS ] |
Message Description:
A defective COCKPIT LIGHTS (INTEGRAL) Control Panel will cause one of the symptoms that follow:
- A group or groups of Integral/Miscellaneous Lights do not come on
- A DIM/BRT Switch cannot control the intensity of a group of lights
- The DIM/BRT Push Button Annunciator (PBA) Toggle Switch does not change the intensity of the Annunciator Lights
- The MASTER Integral Light Switch has a malfunction
Possible Causes:
- Light Switch
- Cockpit Lights (Integral) Control Panel (AP26)
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin: None
Forum Articles/Infoservice/Newsletter: None
Quick Links:
| Connect Electrical Power to the Aircraft | AMM 24-00-00-861-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Remove the Electrical Power from the Aircraft | AMM 24-00-00-861-802 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Electrical/Electronic Safety Precautions | AMM 24-00-00-910-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Removal of the COCKPIT LIGHTS (INTEGRAL) Control Panel |
AMM 33-11-09-000-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Installation of the COCKPIT LIGHTS (INTEGRAL) Control Panel |
AMM 33-11-09-400-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Operational Test of the COCKPIT LIGHTS (INTEGRAL) Control Panel |
AMM 33-11-09-710-801 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Safety Precautions - Maintenance Practices - ALL | SPM 20-00-01-02 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wire Repair - Maintenance Practices - ALL | SPM 20-12-10-02 [ Global Express ] [ G5000 ] [ Global XRS ] |
Troubleshooting Recommendations:
- Check if DIM/BRT rotary switch or a PBA toggle switch change the intensity of a group of integral lights.
- If DIM/BRT rotary switch or a PBA toggle switch does not change the intensity of a group of integral lights, go to step 5.
- If DIM/BRT rotary switch or a PBA toggle switch change the intensity of a group of integral lights, continue with next step.
- Perform the operational test of the COCKPIT LIGHTS (INTEGRAL) control panel.
- If the test is satisfactory, do close out.
- If the test is unsatisfactory, continue with next step.
- Disconnect the connectors (AP26P1 and AP26P2) from the control panel AP26. Perform a voltage check as follows:
For the L integral lights (28 VDC):From To Result AP26P1-11 AP26P1-12 For the CTR integral lights (28 VDC):
From To Result AP26P1-9 AP26P1-10 AP26P1-13 AP26P1-10 AP26P1-14 AP26P1-10 AP26P1-15 AP26P1-10 For the R integral lights (28 VDC):
From To Result AP26P2-11 AP26P2-12 For the OVHD integral lights (28 VDC):
From To Result AP26P2-9 AP26P2-10 For the CB integral lights (28 VDC):
From To Result AP26P2-13 AP26P2-14 For the AREA lights (28 VDC):
From To Result AP26P1-22 AP26P1-17 For the FLOOR and EYE REF lights (28 VDC):
From To Result AP26P2-22 GROUND - If there is voltage, go step 5.
- If there is no voltage, continue with next step.
- Perform a continuity check at the connectors as follows:
For the MASTER switch:From To Result AP26P1-6 GROUND AP26P1-16 GROUND For the PBA switch:
From To Result AP26P1-33 GROUND AP26P1-34 GROUND AP26P1-36 GROUND AP26P1-37 GROUND AP26P2-7 GROUND AP26P2-8 GROUND - If there is continuity, repair defective wiring as required and do close out.
- If there is no continuity, continue with next step.
- Replace the COCKPIT LIGHTS (INTEGRAL) control panel.
- Connect the disconnected connectors to the integral light control panel (AP26).
- If the problem continues, perform the troubleshooting for CAS Message ELEC SYS FAIL (Amber) and ELEC SYS FAULT (Cyan).
- Do close out.