N467CA
Registered owner: VISTA AIRCRAFT LLC, AZ (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| SWEET AVIATION LLC (4SWA) | 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.
20 reports on file, 2002-07-11 – 2008-12-11.
Part: POSITION SENSOR — FALSE INDICATION (TE FLAPS) · airframe 16,179 hrs · 13,841 cycles
FLIGHT 5652, IAH TO ATL - IN CRUISE FLIGHT THE FLIGHT CREW RECEIVED A FLAPS FAIL EICAS MESSAGE. THE FLIGHT CONTROL SYNOPTIC PAGE INDICATED THE FLAPS WERE OUTLINED IN YELLOW SHOWING ZERO DEGREES OF EXTENSION. THE AIRCRAFT LANDED BACK AT IAH WITHOUT INCIDENT. MAINTENANCE PULLED FECU CODES FOR THE RIGHT BRAKE POSITION SENSING UNIT AND THE FECU. THE RIGHT BRAKE POSITION SENSING UNIT WAS REPLACED AND THE FLAP SYSTEM OPERATED NORMALLY.
Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 16,172 hrs · 13,837 cycles
FLIGHT 5637, IAH TO ELP - DURING FINAL SEGMENT OF CLIMB THE FLIGHT CREW RECEIVED A FLAP FAIL MESSAGE ON EICAS. THE FLAPS WERE AT ZERO AND WERE INDICATING ZERO AT THE TIME. THE QRH WAS FOLLOWED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED THE FECU FOR FAULT CODES AND FOUND CODES FOR RT BPSU, FECU, AND WIRING FOR THE RT BPSU. THE SYSTEM WAS RESET AND THE FLAPS OPERATED NORMALLY.
Part: SEAL — LEAKING (ACCY GEARBOX) · airframe 13,767 hrs · 12,090 cycles
IAH TO SRQ - DURING CLIMB, THE CREW RECEIVED A WARNING FOR E1 OIL PRESSURE. E1 OIL PRESSURE WAS NOTED TO FLUCTUATE FROM BELOW 25PSI TO 40PSI. CREW FOLLOWED THE QRH AND REDUCED THRUST ON E1, AFTER WHICH IT WAS NOTED THAT THE OIL PRESSURE HAD STABILIZED AT THE LOWER POWER SETTING. THE FLIGHT RETURNED TO FIELD AT IAH WITHOUT INCIDENT. MAINTENANCE INSPECTED E1 AND FOUND THE SEALS FOR THE ENGINE DRIVEN HYDRAULIC PUMP, INTEGRATED DRIVE GENERATOR, AND THE STARTER WERE LEAKING. THE AIRCRAFT WAS THEN FERRIED TO SDF WHERE THE EDP, IDG, AND STARTER SEALS WERE REPLACED. AFTER REPLACING THE SEALS AND SERVICING WITH OIL, THERE WERE NO FURTHER DEFECTS NOTED.
Earlier reports · 2002–2006 · 17 reports
2006
Part: TRIM SWITCH — MALFUNCTIONED (STAB) · airframe 10,801 hrs · 9,511 cycles
FLIGHT 5261 - AFTER TAKEOFF FROM RIC THE STAB AND MACH TRIM DROPPED OFF, FLIGHT RETURNED TO THE FIELD. CLEANED THE STAB TRIM SWITCHES ON YOKES AND PERFORMED AN OPERATIONAL AND FUNCTIONAL TEST OF STAB TRIM CHANNEL 1 AND 2. DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE.
Part: APU — SHUTDOWN (APU BAY) · airframe 10,687 hrs · 9,410 cycles
FLIGHT 5786 - DURING TAKEOFF ROLL AT HPN RECEIVED AN APU OVER TEMPERATURE WARNING FOLLOWED AUTO-SHUTDOWN OF APU, FLIGHT WAS ABORTED AND RETURNED TO THE GATE. DEFERRED APU PER MEL 49-10-01-01.
2005
Part: DETECTOR — MALFUNCTIONED (TE FLAPS) · airframe 10,141 hrs · 8,932 cycles
FLIGHT 5352 - FLAPS FAIL CAUTION. REPLACED THE RIGHT FLAP SKEW DETECTOR.
Part: COALESCER BAG — DIRTY (LT & RT) · airframe 8,904 hrs · 7,840 cycles
FLIGHT 5462 - STRONG OILY ODOR IN COCKPIT WHEN BLEED AIR SWITCHED FROM APU TO ENGINES. REPLACED COALESOR SOCKS.
Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 8,002 hrs · 7,041 cycles
FLIGHT 5328 RECEIVED A FLAP FAIL CAUTON MESSAGE DURING PREFLIGHT WHEN SELECTING 20 DEGREE POSITION. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.
Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 7,928 hrs · 6,966 cycles
FLIGHT 5393 CARGO SMOKE MESSAGE. BOTTLES DISCHARGED. COULD NOT DUPLICATE. NO EVIDENCE OF SMOKE OR FIRE, REPLACED FIRE BOTTLES AND SMOKE DETECTORS.
2004
Part: DOOR — UNSECURE (CARGO DOOR) · airframe 5,493 hrs · 4,846 cycles
FLIGHT 5917 CABIN ALTITUDE WARNING AND DISPLAY COOL CAUTION. COULD NOT DUPLICATE. INSPECTED AIRCRAFT, FOUND NO DEFECTS. SUSPECT CARGO DOOR NOT CLOSED PROPERLY.
Part: CABLE — BROKEN (PAX DOOR) · airframe 5,273 hrs · 4,670 cycles
PAX DOOR PRESSURE PANEL CABLE (ICE BREAK) IS BROKEN AT THE END OF THE CLEVIS DUE TO RUBBING ON THE FLAP (P/N 601R318122-3). PAX DOOR PRESSURE TO PANEL CABLE WAS REPLACED WITH A SERVICEABLE CABLE (P/N 601R3188127_3). THE FLAP DECOMPRESSION PANEL NEEDS TO HAVE A RECESSION CUT INTO THE INTERIOR LIP TO ALLOW THE CABLE MORE ROOM AND TO PREVENT IT FROM BEING BROKEN FROM NORMAL USE.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 5,273 hrs · 4,670 cycles
CARGO BAY, LEFT AND RIGHT, FLOOR ANGLE SUPPORT CRACKED AT FS 621. REMOVED DAMAGED FLOOR ANGLE ON LEFT HAND AND RIGHT HAND SIDE OF 621 FLOOR ANGLE IN ACCORDANCE WITH BOMBARDIER REO 601R-53-61-004. REPAIRED 621 FLOOR ANGLE, LEFT HAND AND RIGHT HAND SIDE, IN ACCORDANCE WITH BOMBARDIER REO 601R-53-61-004.
Part: PROXIMITY SENSOR — DIRTY (LANDING GEAR) · airframe 5,199 hrs · 4,667 cycles
FLIGHT 5008 GEAR DISAGREE WARNING, NLG DID NOT INDICATE DOWN. CLEANED DIRT FROM NLG PROXIMITY SENSORS. OPERATIONAL CHECK SATISFACTORY.
Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 5,052 hrs · 4,480 cycles
FLIGHT 5347 FLAPS FAIL CAUTION MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.
Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 5,005 hrs · 4,435 cycles
FLIGHT 5886 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU.
Part: BPSU — MALFUNCTIONED (RT TE FLAPS) · airframe 5,003 hrs · 4,438 cycles
FLIGHT 5838 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU.
Part: PDU — MALFUNCTIONED (TE FLAPS) · airframe 4,991 hrs · 4,429 cycles
FLIGHT 5055 FLAPS FAIL MESSAGE. REPLACED THE FLP PDU.
2003
Part: ELEMENT — UNRELIABLE (RT) · airframe 2,825 hrs · 2,571 cycles
FLIGHT 5914 RT 14TH STAGE DUCT OVERHEAT WARNING. REPLACED THE PYLON LEAK SENSIGN ELEMENT.
2002
Part: WARNING SYSTEM · airframe 1,261 hrs · 1,208 cycles
CARGO DOOR CAUTION MESSAGE.INSPECTED CARGO DOOR, NO DEFECTS NOTED, DOOR WARNING SYSTEM WAS PREVIOUSLY ON DEFERRED MAINTENANCE LIST.
Part: BPSU — MALFUNCTIONED (R/H) · airframe 604 hrs · 585 cycles
FLIGHT 5507 FLAPS FAILED CAUTION MESSAGE.REPLACED THE R/H BPSU.