N525CD

CESSNA 525 · 2000 · Fixed-wing multi-engine · 2 engines · 8 seats · Valid Registration

Registered owner: LINCOLN TRANSPORT D LLC, DE (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
Sawyer Aviation LLC (SVGA)Certificate holder—Matched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.

1 report on file, 2021-04-15.

FLUID LOSS · 2021-04-15 Matched by certificate designator
ATA 2910

Part: HOSE — RUPTURED (HYD SYSTEM) · airframe 6,904 hrs · 6,015 cycles

DURING POST FLIGHT INSPECTION BY PILOT LARGE AMOUNT OF HYDRAULIC FLUID VISIBLE ON BOTTOM OF FUSELAGE AND LEFT PYLON. PILOT ALSO REPORTED HYDRAULIC SYSTEM RESERVOIR BELOW ADD LINE. UPON INVESTIGATION BY MAINTENANCE THE LH THRUST ATTENUATOR ACTUATOR EXTEND HOSE LEAKING HYDRAULIC FLUID. HOSE PN AE6203B0185-180, CURE DATE 07-01. HOSE RUPTURED 1/4 INCH FROM ACTUATOR END FITTING. NO ABRASION SLEEVE COVERS THIS AREA OF HOSE. MINOR ABRASION DAMAGE EVIDENT ON SLEEVE APPROX. 5 INCHES FROM ACTUATOR WHICH HAD PREVIOUSLY BEEN COVERED BY SPIRAL WRAP ABRASION PROTECTION. ALL 4 THRUST ATTENUATOR HOSES REPLACED WITH NEW.

Source: SDR 2021F00073