N562CP
Registered owner: VANTAGE AIR CORP, MT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
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.
13 reports on file, 2007-11-12 – 2011-06-07.
Part: FIRE DETECTOR — CONTAMINATED (RT NACELLE) · airframe 21,478 hrs · 35,934 cycles
RIGHT ENGINE FIRE LIGHT CAME ON DURING TAKEOFF. INSPECTED RT ENGINE, WHEN OPENING THE LOWER COWLING A LARGE AMOUNT OF WATER POURED OUT, INSPECTED FIRE DETECTORS AND ENGINE RUN NO DEFECTS NOTED IAW MM 26-00. AIRCRAFT WAS SUBJECT TO HEAVY RAIN ON PREVIOUS NIGHT.
Part: ENGINE — SEIZED (ZONE 500) · airframe 20,998 hrs · 34,832 cycles
LEFT PROPELLER DOES NOT TURN, LOCKED, CAUSED BY HOT START. REMOVED LT ENGINE AND PROPELLER. INSTALLED LT ENGINE AND PROP ALL WORK ACCOMPLISHED IAW WORK CARD 72-00. ENGINE RUNS SAT NO LEAKS NOTED.
Earlier reports · 2007–2010 · 11 reports
2010
Part: FIRE LOOP — FALSE ACTIVATION (LT NACELLE) · airframe 20,863 hrs · 24,499 cycles
LT FIRE BELL/ LIGHT ACTIVATED ON TAKEOFF. POWER WAS REDUCED AND INDICATION EXTINGUISHED. RETURNED TO BLOCKS. RAN LT ENGINE AT HIGH POWER SETTING FIRE WARNING ILLUMINATED. R & R BOTH 450C THERMAL FIRE SENSORS. GROUND TEST OK WORK PERFORMED IAW MM 26-10-00. OPS CHECK FLIGHT SATISFACTORY, ACFT RETURNED TO SERVICE
2009
Part: CONTROL HANDLE — ODOR · airframe 20,560 hrs · 33,659 cycles
UNUSUAL ODOR NOTED IN FLIGHT: RETURNED TO DEPARTURE AS A PRECAUTION. FOUND DME INDICATOR HEAD HOT AND SMELLED BURNED. REPLACED INDICATOR, OPS CHECK GOOD IAW INSTALL MANUAL.
Part: ADAPTER — CORRODED (LT ENGINE MOUNT) · airframe 19,492 hrs · 30,255 cycles
LT NACELLE ENGINE MOUNT ADAPTOR PLATE CORRODED. REMOVED AND REPLACED ENGINE MOUNT ADAPTOR PLATE IAW RD6-54-006.
Part: ADAPTER — CORRODED (ZONE 400) · airframe 19,492 hrs · 30,255 cycles
RIGHT NACELLE ENGINE MOUNT ADAPTOR PLATE CORRODED. REMOVED AND REPLACED ENGINE MOUNT ADAPTOR PLATE IAW RD6-54-006.
2008
Part: TURBINE — DAMAGED (RT ENGINE) · airframe 19,244 hrs · 29,573 cycles
RIGHT ENGINE MAKES NOISE WHEN PROP MOVED BY HAND. REMOVED AND REPLACED RIGHT ENGINE AND PROPELLER AS A QEC ASSEMBLY. SPLIT ENGINE AT C-FLANGE AND FOUND POWER TURBINE RUB.
Part: COUNTERWEIGHT — LOOSE (LT PROPELLER) · airframe 19,183 hrs · 29,417 cycles
LEFT PROPELLER BLADE NR 3 COUNTER WEIGHT LOOSE. BOTH MOUNTING BOLTS WERE INSTALLED WITH LOCKING PINS. REMOVED AND REPLACED PROPELLER. SENDING PROPELLER TO REPAIR STATION FOR EVALUATION. INSPECTED ALL AIRCRAFT IN FLEET FOR LOOSE PROPELLER WEIGHTS. NONE FOUND. PROPELLER WAS RETURNED FROM PROP SHOP AND FOUND WEIGHTS WERE UNDER TORQUE.
Part: BELLCRANK — WORN (ELEVATOR) · airframe 18,886 hrs · 28,560 cycles
DURING AD 89-24-06 FOUND ELEVATOR BELL CRANK WORN. REMOVED AND REPLACED ELEVATOR BELL CRANK. NO OTHER DEFECTS NOTED. (S)
Part: BLADE — WORN (NR 2 ENGINE) · airframe 3,834 hrs · 1,155 cycles
UNUSUAL NOISE NOTED IN COMPRESSOR SECTION (NR 2 ENG) UPON START UP. REMOVED ENGINE FROM SERVICE, ENGINE RETURNED TO ENGINE SHOP, FOUND 1ST STAGE BLADE RUB. ENGINE PENDING REPAIR. (K)
Part: COMPRESSOR — NOISY (NR 2 ENGINE)
UNUSUAL NOISE NOTED IN COMPRESSOR SECTION NR 2 ENGINE, UPON START UP, REMOVED ENGINE FROM SERVICE WILL CLOSE SDR WHEN SOURCE OF NOISE IS FOUND AND CORRECTED. (K)
Part: LONGERON — DAMAGED (RT NACELLE) · airframe 18,454 hrs · 27,333 cycles
DURING SCHEDULED 125HR INSPECTION FOUND: RT ENGINE NACELLE IB LONGERON DAMAGED FORWARD OF LEADING EDGE AT STATION 60.8. REMOVED AND REPLACED RT NACELLE IB LONGERON ASSY IAW AC 43-131B CHP7 EMERGENCY MEASURES EXECUTED: NO AIRCRAFT. GROUNDED: BEING REPAIRED DURING 125 HR CAMP INSPECTION, "NO".
2007
Part: WIRE — SHORTED (ZONE 200) · airframe 7,940 hrs · 25,820 cycles
LT GENERATOR WOULD NOT COME ON-LINE AFTER START. FERRIED AC BACK TO BASE SSB. FOUND SHORTED WIRE ON GEN. FIELD RELAY DUE TO LACK OF HEAT SHRINK TUBING ON SOLDERED TERMINAL JOINT.