DUMONT AIRCRAFT CHARTER LLC

Part: BLEED AIR SYS — CONTAMINATED (ZONE 100) · airframe 6,920 hrs · 5,264 cycles

ON REPOSITION LEG FROM SFO TO SNA CREW TURNED ON WING ANTI ICE FOR TESTING. AFTER A FEW MINUTES THEY NOTICED WHAT APPEARED TO BE SMOKE IN PAX CABIN. THEY TURNED OFF SYSTEM AND CONTINUED TO SNA. REMOVED CLOSE OUT PANELS AND DETERMINED TO BE SPILLED COFFEE ON BLEED AIR DUCT IN CABIN. CLEANED DUCT AND PERFORMED MAINTENANCE EVALUATION FLIGHT WITH NO FURTHER DEFECTS NOTED.

Part: TUBE — CRACKED (ANTI-ICE SYSTEM) · airframe 14,563 hrs · 9,004 cycles

CRACK IN ANTI-ICE TUBE CAUSED PRESSURE SENSE LINE FITTING TO SEPARATE FROM TUBE AT WELD

Part: STEERING SYS — FAILED (NLG) · airframe 13,810 hrs · 8,726 cycles

NOSE WHEEL STEERING FAILED ON LANDING.

Part: BRAKE SYS — FAILED (NR 1) · airframe 10,458 hrs · 6,263 cycles

BRAKE SYSTEM 1 FAILED AFTER LANDING, SWITCHED TO SYSTEM 2 BRAKES WITH NO ISSUES, TAXIED TO FBO.

Part: ENGINE — FLAMED OUT (NR 2) · airframe 13,797 hrs · 8,721 cycles

NR 2 ENGINE FLAMED OUT DURING TAXI FOR DEPARTURE. TROUBLESHOOTING IN WORK BY GO TEAM WITH AOG SUPPORT.

Part: TIRE — SEPARATED (RT MLG) · airframe 11,000 hrs · 7,326 cycles

RIGHT OUTBOARD TIRE TREAD SEPARATION CAUSING DAMAGE TO MLG DOOR AND ATTACH LINK. ALSO FOUND A SMALL DENT IN LOWER SURFACE OF FLAP.

Part: WARNING LIGHT — ACTIVATED (CABIN PRESSURE) · airframe 12,806 hrs · 6,722 cycles

WHILE DESCENDING FROM FL450, CABIN WARNING LIGHT AND TONE ACTIVATED DUE TO PARTIAL LOSS OF CABIN PRESSURE. CREW DONE MASKS, DECLARED EMERGENCY AND LANDED UNEVENTFULLY AT DESTINATION AIRPORT (BMI).

Part: LANDING GEAR — MALFUNCTIONED · airframe 8,541 hrs · 8,086 cycles

LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. NO MOVEMENT, THREE GREEN INDICATED, RETURNED TO FIELD.

Part: FLAP SYSTEM — FAILED · airframe 11,003 hrs · 6,535 cycles

DURING THE FINAL APPROACH, A FLAPS FAIL LIGHT WHEN THE FLAPS WERE PLACED IN THE 45 DEGREE POSITION. CONTINUED TO AVIATE AND GET THE AIRCRAFT ON THE GROUND. REPORTED A LOSS OF 15-20 KTS DURING THE SHORT FINAL FLARE STAGE. THE LANDING PHASE BECAME UNSTABLE AND IN NEED OF TOO MUCH RUNWAY, AND THE PILOT PERFORMED A O GO-AROUND. DURING THE GO AROUND, THE FLAPS WERE INDEED STUCK IN THE 45 POSITION AND WOULD NOT RETRACT. DID NOT DECLARE AN EMERGENCY AND LANDED.