What was found
(CAN) RIG TEST HAS SHOWN THAT SFECU WOULD SEND VALID ERRONEOUS SLAT/FLAP POSITION (L127 & L137) DATA TO FBW/CLAWS, IN CASE OF PSU MECHANICAL FAILURE. ++X++ (TCH) (TC# 20190412010)
- Difficulty date
- April 12, 2019
- Submitted
- August 17, 2020
- Operation
- General aviation
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Control Unit
- Part number
- G02701003007G027
- Condition
- Malfunctioned
- Location
- Te Flap
- Stage of operation
- NR
- How discovered
- 9
- Nature of condition
- O
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.