N1327J
Registered owner: ABSOLUTE ALTITUDE LLC, OH (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Skyway Aviation Services, Inc. (B90A) | 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.
2 reports on file, 2018-12-10 – 2020-06-12.
Part: GARLOCK SEAL — DAMAGED (LT HYD PUMP) · airframe 6,049 hrs · 5,171 cycles
CLIMBING THROUGH APPROXIMATELY 7,000 FEET WHEN THE OIL PRESSURE DROPPED SIGNIFICANTLY AND WAS IMMEDIATELY FOLLOWED BY A RED MASTER WARNING INDICATOR AND A MESSAGE FOR LEFT ENGINE OIL PRESSURE. AN EMERGENCY WAS DECLARED AND REQUESTED AN IMMEDIATE RETURN TO DEPARTURE IAW THE EMERGENCY CHECKLIST, THE LEFT ENGINE WAS SHUTDOWN AND SECURED. CREW PERFORMED A SINGLE-ENGINE VISUAL APPROACH AND LANDING WITH NO FURTHER ISSUES. AIRCRAFT WAS ABLE TO TAXI UNDER ITS OWN POWER TO THE FBO. MAINTENANCE HAD REPLACED THE HYDRAULIC PUMP AND AFT OIL BREATHER GARLOCK SEAL PREVIOUSLY. AIRCRAFT HAD NOT FLOWN UNTIL THIS OCCURRENCE. MAINTENANCE FOUND A SINGLE BURR ATTACHED TO THE MAGNETIC SIDE OF AFT OIL BREATHER GARLOCK SEAL AND FOUND A SLIGHT GOUGE IN THE INNER HOUSING OF THE HYDRAULIC PUMP MOUNTING FLANGE AT GARLOCK SEAL. BOTH THE HYDRAULIC PUMP GARLOCK SEAL AND AFT OIL BREATHER GARLOCK SEAL WERE REPLACED WITH NEW. LEAK CHECKED AND ONE HOUR OIL CONSUMPTION CHECK WERE PERFORMED WITH SATISFACTORY RESULTS.
Part: LINER — CRACKED (RT ENGINE) · airframe 5,834 hrs · 5,004 cycles
DURING SCHEDULED FJ44 CHECKS 1 AND 2, RT ENGINE INLET LINER FOUND DAMAGED/CRACKED. PERFORMED IP AND HP COMPRESSOR (BORESCOPE) INSPECTION IAW FJ44-1A LMM TASK 71-00-30 FOR POSSIBLE FOD DAMAGE. NO EVIDENCE OF FOD DAMAGE FOUND. RT ENGINE INLET ASSEMBLY WAS REPLACED WITH NEW P/N: 6352100-205.