N896LL
Registered owner: ANALAR CORP, NJ (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| THE MILTON S HERSHEY MEDICAL CENTER (OLJA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
ENROUTE, NR 2 ENGINE CHIP LIGHT INDICATED ON THE MASTER CAUTION PANEL. ACFT ABORTED FLIGHT. AFTER LANDING, THE ACFT WAS TAKEN OUT OF SERVICE. A CHIP WAS FOUND ON THE ELECTRICAL PLUG. IT WAS WITHIN LIMITS IAW THE MM ONLY ACTION TAKEN WAS AN ENGINE DRAIN AND FLUSH TO RID OF ANY FURTHER DEBRIS FROM THE OIL SYSTEM. AFTER ENGINE FLUSH AND GROUND RUN, NO OTHER CHIPS WERE FOUND IN THE OIL FILTER OR MODULE MAGNETIC CHIP DETECTORS. ACFT RETURNED TO SERVICE. AFTER 4.8 HRS, ELECTRIC CHIP DETECTOR HAD MINOR CHIPS THAT DID NOT ILLUMINATE THE LIGHT. NO OTHER CHIPS WERE FOUND ON THE MODULE CHIP DETECTORS. DUE TO THE HIGH TIME OF THE ENGINE, 63.8 HRS TO OVERHAUL, RETURNED ENGINE TO THE MFG FOR OVERHAUL. MANUFACTURE FOUND MODULE 5 BEARING FRONT INTERNAL GEAR CREATED FLAKES. THIS CAUSED THE CHIPS BEING COLLECTED ON THE CHIP DETECTOR.
RIGHT HAND VERTICAL FIN DEPARTED AIRCRAFT DURING FLIGHT. CAUSE: FATIGUE ON ONE STUD LEADING TO FAILURE OF OTHER STUDS.
FOUND ON DAILY INSPECTION, HYDRAULIC FLUID LEAKING FROM PRESSURE LINE TO NOSE LANDING GEAR ACTUATOR. PRESSURE LINE HOSE REPLACED IN NOSE LANDING GEAR ACTUATOR.
LT HYDRAULIC SYSTEM LEAK DURING AC RUN UP. TROUBLESHOOTING FOUND HYDRAULIC HOSE BETWEEN DISTRIBUTION MANIFOLD AND T FITTING IN HYDRAULIC BAY RUPTURED. REPLACED HOSE.