N267BW
Registered owner: NAMAYA INC, PA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| L. J. Associates, Inc. (ZESA) | 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.
5 reports on file, 2008-07-09 – 2016-01-30.
Part: UNKNOWN — MALFUNCTIONED (AC BAY) · airframe 2,324 hrs · 1,053 cycles
DURING CRUISE FLIGHT, THE PILOTS NOTICED THAT THE RT ENG AIR-CONDITIONING PACK WAS ILLUMINATED IN WHITE RATHER THAN GREEN INDICATION. THEY TRIED TO RESET THE PRV & IT REMAINED WHITE, OFF. THE SYS WAS ABLE TO BE PUT ON MEL BUT THE DECISION WAS MADE TO GO TO THE NEAREST MFG SERVICE CTR & HAVE IT CHECKED. THE ACFT RETURNED, IN DECENT THE SYS TURNED GREEN & OPERATED CORRECTLY. THEY LANDED WITHOUT INCIDENT. THE SYS WAS CHECKED & VERIFIED TO OPERATE NORMALLY. THEY COULD NOT DUPLICATE THE ISSUE & THE ACFT WAS RETURNED TO SERVICE. THE TRIP CONTINUED WITHOUT INCIDENT.
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 1,595 hrs · 743 cycles
DURING PILOTS WALK AROUND ON PREFLIGHT THE PILOTS LT WINDSHIELD WAS FOUND TO BE CRACKED, SHATTERED.
Part: ENGINE — POWER LOSS (NR 2) · airframe 3,008 hrs · 2,140 cycles
APPROXIMATELY 2.5 HRS AT 41,000FT, ENTERED INTO TURBULANCE AND WAVE ACTION. NR 2 ENGINE STARTED COMPRESSOR STALLING, THE N1 STARTED DROPPING AND THE ITT STARTED CLIMBING, THE THROTTLE WAS UNRESPONSIVE AND UPON SURPASSING 988C WITH THE N1 AT 46 PERCENT THE PILOT INITIATED AN ENGINE SHUTDOWN, NGINE SHUTDOWN AS REQUESTED AND THE FAN WINDMILLED AT 20 PERCENT THROUGHOUT THE REST OF THE FLIGHT. ACFT LANDED SAFELY WITHOUT FURTHER INCIDENT.
Part: DIFFUSER — CORRODED (ENGINE)
DURING ENGINE START OIL PRESSURE REMAINED AT ZERO PSI WITH A LOW OIL PRESSURE LIGHT WHEN ENGINE REACHED IDLE. SHUT DOWN ENGINE. INVESTIGATION REVEALED THE ENGINE DRIVEN HYDRAULIC PUMP LOCKED UP DUE TO A PIECE OF METAL THAT HAD DETACHED FROM THE DIFFUSER CASE THAT SUPPORTS THE NR3 MAIN BEARING. GOT INTO THE OIL SYS, SLIPPED BRG THE INLET SCREEN TO THE PUMP. (K)
Part: CASE — CORRODED (DIFFUSER)
ABORTED TAKEOFF, DUE TO RT ENGINE CHIP LIGHT. REMOVED CHIP PLUG FOR INSPECTION, FOUND SMALL DEBRIS, CLEANED, DRAINED AND FLUSHED OIL SYS, INSPECTED OIL FILTER, FOUND NO SIGNIFICANT CONTAMINATION. REINSTALLED FILTER AND SERVICED OIL. GROUND RUN, FOUND NO CHIP LIGHT DURING RUN. DIFFUSER CORRODED. (K)