04/02/21
Message Overview:
Message Description:
TAWS is indicating a flaps input fault.
Possible Causes:
- Terrain-Avoidance Warning System (TAWS) Computer (A34)
- FLAP Lever (A120)
- TAWS/Landing Gear Control-Panel (PL10)
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin: None
Forum Articles/Infoservice/Newsletter: None
Quick Links:
| Removal of the FLAP Lever | AMM 27-51-01-000-801 |
| Installation of the FLAP Lever | AMM 27-51-01-400-801 |
| Removal of the TAWS/LANDING GEAR Control-Panel | AMM 34-42-09-000-801 |
| Installation of the TAWS/LANDING GEAR Control-Panel | AMM 34-42-09-400-801 |
| Standard Practices - Replace Wiring | SPM 20-12-00-02 |
| Standard Practices - Repair Wiring | SPM 20-12-10-02 |
Troubleshooting Recommendations:
- Reset TAWS (CB2-A6) circuit breaker or push in the TAWS TEST/RESET switch on the center pedestal.
- If system check passes, do close out.
- If fault remains, continue with next step.
- Verify the operation of the Flap Override Input circuitry as per drawing. Repair/replace as required.
- If system check passes, do close out.
- If fault remains, continue with next step.
NOTE: The TAWS FLAP switch will provide, when pushed in (light ON), a ground to pin C9 of TAWS computer connector A34BP1. The Flap lever will provide a ground when selected at 30 degree at the same pin, since both are wired in parallel through Junction Box 2.
- Replace the TAWS computer.
- Do close out.