CTRL Systems
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Aviation Use Case • Boeing 737-700 LE Flap & Boeing 757-200 TE Flap

Hydraulic Systems

Isolate faulty actuators, control valves, and bypass valves without shotgun swaps.

Hydraulic Systems

What the UL101 delivered

  • LE flap B737-700: 96 → 36 hrs troubleshoot (60 hrs saved)
  • LE flap AOG: $74,400 total savings vs. replacing all 8 actuators
  • TE flap B757-200: pinpointed #4 & #5 transmissions vs. trial-and-error swaps
  • Detects friction, internal leakage, blockages & fluid bypass

The problem

On a Boeing 737-700 with an AOG-grounding leading-edge flap defect, the traditional troubleshooting workflow would have replaced all eight leading-edge actuators — the only way to be certain the failing unit was among them. On a separate Boeing 757-200 with a trailing-edge flap disagree, the same shotgun approach would have required trial-and-error swaps of four flap transmissions until the defect cleared.

How the UL101 solved it

Using the UL101 with a solid contact probe, technicians listened to each actuator and transmission under load. Friction, internal leakage, blockages and fluid bypass each produce distinct ultrasonic signatures that make a failing hydraulic component obvious against its silent, healthy neighbors. On the 737-700, the failing actuator was isolated within one troubleshoot cycle. On the 757-200, transmissions #4 and #5 were pinpointed directly instead of swapping components at random.

The outcome

The 737-700 troubleshoot dropped from 96 hours to 36 hours (60 hours saved), and $74,400 in unnecessary actuator swaps was avoided — a 1,078% ROI on a single UL101 for this one AOG event. On the 757-200, the flap disagree cleared in a single targeted repair rather than a multi-step trial-and-error swap.

Run this diagnosis on your fleet

The CTRL UL101 Aviation Troubleshooter is the sensor that made this case study possible.