N671BC
Registered owner: IBC AIRWAYS INC, FL (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.
7 reports on file, 2009-06-08 – 2022-12-12.
Part: TRIMMER — FAULTY (RH ENG) · airframe 55,504 hrs · 58,031 cycles
CROSSING 11,000 FT, RIGHT ENGINE ITT INCREASE UNCOMMANDED TO 872C (802C BEFORE INCREASE). PROCEEDED WITH QRH - REDUCING POWER POWER LEVERS BROUGHT TEMPERATURES BACK DOWN TO NORMAL LEVELS. BLEED VALVES HAD NO INFLUENCE ON ENGINE ITT. WHILE DESCENDING , ITT ON RIGHT ENGINE SEEMED TO BALANCE WITH LEFT ENGINE. - SECURED ECU BLACK HARNESS AS NEEDED. PERFORMED ENGINE RUN IAW GE CT7-5, 72-00-00. - PERFORMED FCF THAT WAS UNSATISFACTORY. PASSING THROUGH FL170 RT ENGINE INCREASED FROM 845 TO 901 IMMEDIATELY.AT FL170 UNABLE TO REACH TARGET TORQUE FOR ENGINE TREND DUE TO HIGH ITT. - REPLACED RH ENGINE TRIMMER IAW SA340 AND CT7-5 AMM 72-00-00-16. C/W TRIMMER ADJUSTMENT IAW GE CT7-5 EM 74-00-00.- PERFORMED A SECOND FCF WHICH WAS SATISFACTORY.
Part: PERISEAL — UNSERVICEABLE · airframe 55,503 hrs · 58,030 cycles
#2 ENGINE IN CRUISE, ITT OUT OF LIMITS. C/W QRH. - REMOVED AND REPLACED R/H SIDE UNDER WING FLAP PERI-SEAL IAW SF340A AMM 36-11-40-04. RUN CHECKS SATISFACTORILY.
Part: SMOKE DETECTOR — FALSE ACTIVATION (E/E BAY) · airframe 53,806 hrs · 57,062 cycles
WRITE UP, MASTER WARNING, AVIONICS SMOKE LIGHT ON. MIR STATEMENT, CLIMBING OUT OF 2000 FT DEPARTING FROM KMIA TO MBPV, AVIONICS SMOKE LIGHT ON. THE CREW PERFORMED MEMORY ITEMS AND RETURNED BACK TO MIAMI SAFELY. AFTER LANDING I SMELLED A SMALL HINT OF SMOKE.
Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 48,979 hrs · 54,491 cycles
DURING CRUISE, HYD PUMP FAILED. LANDED WITH NO INCIDENT. R & R MAIN HYD PUMP IAW MM. OPERATIONAL CHECKED SATISFACTORY.
Part: HMU — MALFUNCTIONED (LT ENGINE) · airframe 48,400 hrs · 54,146 cycles
LEFT ENG FAILED ON LANDING ROLL AFTER USING MODERATE REVERSE THRUST. R & R LT ENG HMU IAW APPLICABLE MM. OPERATIONAL CHECKS SATISFACTORY.
Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 48,343 hrs · 54,114 cycles
AIRCRAFT RETURNED DUE TO CARGO SMOKE INDICATION. AFTER TROUBLESHOOTING, FOUND ZONE A CARGO SMOKE DETECTOR INOPERATIVE. R & R ZONE A CARGO SMOKE DETECTOR IAW MM CHAPTER 26. OPERATIONS CHECKED OK.
Part: LATCH — DEFECTIVE (LEFT ENGINE COWL) · airframe 43,226 hrs · 51,225 cycles
ON DEPARTURE FROM MIA THE PILOT NOTED THE LT ENGINE COWLING HAD POPPED OPEN AND WAS COLLAPSED AGAINST THE ENGINE. POWER TO THE AFFECTED ENGINE WAS REDUCED AND A UNEVENTFUL LANDING IN MIA WAS PERFORMED. MX INSPECTED THE AIRFRAME , ENGINE AND COWLING AND SUSPECTED A DEFECTIVE LATCH. THE COWLING ASSY WAS REPLACED WITH A SERVICEABLE UNIT AND THE ACFT WAS RELEASED TO SERVICE. AS A MATTER OF RECORD, AD2009-10-13 WAS PERFORMED ON THIS ACFT MAY 26, 2009 AND NO DEFECTS WERE NOTED AT THAT TIME. THIS PROBLEM IS UNRELATED TO THE REQUIREMENTS OF THAT AD.