# SDR 2026F00139

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: June 7, 2026
- Submitted: July 2, 2026
- Operation: General aviation
- Aircraft: [N325GH](https://openairdocs.org/aircraft/N325GH), registered now
- Make and model: Cessna 525A
- Registry model: [Cessna 525A](https://openairdocs.org/model/cessna-525a) (OpenAirDocs)
- Aircraft serial: 525A0087
- Aircraft time: 5,281 hours, 4,172 cycles
- System (JASC): [2910 · Hydraulic System, Main](https://openairdocs.org/jasc/2910)
- Part: Flex Hose
- Part number: AE3663919E0355
- Part serial: NA
- Condition: Ruptured
- Location: Zone 400
- Part time: 5,281 hours, 4,172 cycles
- Component: Thrust Attenuat, Cessna
- Component part number: NA
- Stage of operation: CL
- How discovered: V
- Nature of condition: O
- Precautionary procedure: D
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/2026F00139

## Discrepancy

DURING CLIMBOUT FROM HOME BASE THE CREW NOTED THE HYDRAULIC PRESSURE ON ANNUNCIATION AND THE LEFT HAND THRUST ATTENUATOR LAMP BLINKING.THE CREW EMERGENCY DEPLOYED THE MAIN LANDING GEAR DUE TO HYDRAULIC LOSS. LANDING WAS NORMAL POST FLIGHT WALK AROUND HYDRAULIC FLUID WAS NOTED DRIPPING IN THE AREA OF THE LEFT ENGINE PYLON.

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