N651BC
Registered owner: AVIATION INVENTORY RESOURCES INC, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| IBC AIRWAYS, Inc. (OZCA) | 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.
6 reports on file, 2014-03-27 – 2022-11-03.
Part: CHIP DETECTOR — ACTIVATED (ZONE 500) · airframe 50,588 hrs · 51,214 cycles
DURING CRUISE FLIGHT AT 17000 FT LEFT ENGINE CHIP DETECT LIGHT ILLUMINATED A8-15 QRH. NO OTHER ABNORMALITIES. -- REMOVED AND REPLACED LT HAND ENGINE CHIP DETECTOR I/AW GE-CT-5 AMM 79-30-35-04. RUN AND LEAKS CHECK SATISFACTORY
Part: WIRE HARNESS — NONE (LT ENGINE) · airframe 19,968 hrs · 50,837 cycles
WHILE INCRISING POWER LEVERS AT START OF T/O ROLL, L ENGINE TORQUE UNCOMANDED TO 120% ( RED LIGHT ON ) REDUCED POWER LEVER, ENGINE DID NOT RESPOND. SHUT ENGINE DOWN. ASYMETRIC THRUST FROM RUNNING RIGHT ENGINE QUICKLY CAUSED PLANE TO ROTATE TO THE LEFT. RIGHT ENGINE WAS SHUT DOWN. - REPLACED AUTOCOARSEN COMPUTER, CHECKED OUT WIRING FOR 64 DEG SWITCH TO RELAYS 43KA AND 44KA AND TO THE CTOT PANEL CHECKED GOOD. FOUND THE BOTTOM GEVERNOR PREMATURELY ENGAGING REPLACED HMU AND OPS CHECK NORMAL. AFTER A SUCCESSFUL FCF WITHOUT REPEATING THE FAULT, WE DECIDED TO CHANGE THE ENGINE HARNESS AS A PRECAUTION.
Part: UNKNOWN — HAZE (COCKPIT) · airframe 49,139 hrs · 50,380 cycles
CREW REPORTED, ATOMIZED OIL HAZE IN COCKPIT UNABLE TO SEE OUTSIDE OF INSTRUMENTS, AFTER HP'S WERE TURNED ON AND RECIRCLE SWITCH. MAINTENANCE PERFORMED, INSPECTED LT AND RT ACM'S FOR LEAKS AND OPERATIONS CHECK. INSPECTED LT AND RT ENGINE FOR INTERNAL OIL LEAKS, NO FAULTS FOUND. PERFORMED LT AND RT ENGINE RUN, IAW SAAB 340 72-00-00, NO FAULTS FOUND.
Part: RELIEF VALVE — FAULTY (OIL SYSTEM) · airframe 45,442 hrs · 48,031 cycles
ABOUT 10 MINUTES AFTER TAKEOFF, RT ENG OIL TEMP WENT ABOVE RED LINE. REDUCED POWER & FOLLOWED QRH. TEMP SLOWLY STARTED TO REDUCE, OIL PRESS WAS 48 PSI. TROUBLE SHOT SYS & FOUND COLD OIL RELIEF VLV INOPERATIVE. R & R RT COLD OIL RELIEF VLV. GND OPERATIONAL CHECKED SATISFACTORY & CHECK FLIGHT ALSO SATISFACTORY.
Part: CONTROL CABLE — DAMAGED (ZONE 400) · airframe 44,663 hrs · 47,497 cycles
DURING FLIGHT CREW EXPERIENCED A LOSS OF THE NR 2 PROPELLER RPM. ACFT RETURNED BACK TO AIRPORT & LANDED SAFELY. INSPECTED THE ACFT & FOUND THE RT WING TO NACELLE CONTROL CABLE AT FAULT. AFFECTED CABLE WAS REPLACED. RIGGING CHECKS WERE SATISFACTORY & ENG RUNS WERE SATISFACTORY.
Part: CONTROL BOX — FAULTY (FIRE DETECTION) · airframe 44,102 hrs
RIGHT ENGINE FIRE WARNING, RETURNED TO AIRPORT. REPLACED RT FIRE DETECTOR CONTROL BOX WITH AN INSPECTED PART & ACFT WAS RELEASED TO SERVICE.