FAA incident reports · 3
FAA accident and incident reports matched to this aircraft by N330SB and the event date: up to this one’s cancellation.
Incident 19980310005679ITo Aborted (Fixed Wing) · Honolulu, HINarrative: aircraft ground aborted due to #2 engine fuel flow indication problem. During rollout #2 engine fuel flow dropped and there were no other abnormal indications. As a precautionary measure, the crew taxied aircraft back. Discrepancy was deferred per…Incident 19820308007519IFinal Approach · Boston, MARight main gear unsafe light. Visual gear down check. Normal landing. Struck micro switch.Incident 19800221027009IInitial Approach-IFR · Albany, NYFlight got left gear unsafe light when gear was lowered. Down light switch was out of adjustment.
Service difficulty reports · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR HSYA 2013072013Cable · brokenFLT 248, PILOT REPORTED THAT WHILE DESCENDING FROM 8000 TO 3000 FT APPROX 30 NM OF DESTINATION, THE ELEVATOR TRIM FAILED. DECLARED AN EMERGENCY, PILOT REPORTED THAT THE CREW "MUSCLED" THE ACFT WHERE THEY LANDED WITHOUT FURTHER INCIDENT. FOUND TRIM CABLE BSDR HSYA2013041113Governor · failedPILOT REPORTED LT ENGINE WOULD ONLY PRODUCE 1600 LBS OF TORQUE AT MOST. THE TAKEOFF WAS ABORTED AND ACFT RETURNED TO THE PARKING RAMP WITHOUT FURTHER INCIDENT AND MX WAS NOTIFIED. MX TROUBLESHOT ACFT AND PERFORMED THE FOLLOWING MX. TROUBLESHOOT PY LINES ANDSDR HSYA2013012800012Structure · corrodedDURING MX, CORROSION INSPECTION, FOUND CORROSION ON LT WING OTBD SIDE OF NR 1 NACELLE INBD T/E BETWEEN WS 160 & 175. MX REMOVED LT WING UPPER SKIN DOUBLERS AT WS 160 AT APPROX 7.5" FROM L/E SPAR AND APPROX 7.5" FROM THE REAR EDGE SPAR. ON REMOVAL AND FURTHESDR HSYA2012100512Engine · failedAFTER LEVELING OFF AT 9,000 FT, CREW OBSERVED A FLAME COME OUT OF NR 1 ENGINE, FOLLOWED BY THE GENERATOR LIGHT ILLUMINATING, AND ENGINE SPOOLING DOWN. FOLLOWED EMERGENCY CHECKLIST AND SHUTDOWN NR 1 ENGINE IN-FLIGHT. ATTEMPTED TO RESTART NR 1 ENGINE PER EMERGENSDR HSYA2012050412Bolt · failedDURING TAXI, RT POWER LEVER HAD SEVERE VIBRATION. RETURNED TO RAMP. INSPECTED NR 2 ENG & PROP. FOUND 3 PROP BOLTS FRACTURED AND/OR SHEARED. ACFT GROUNDED. PERFORMED ENGINE VIBRATION INSPECTION CHECK IAW MM 5-51-13. NR 2 ENG REDUCTION GEARBOX PROP MOUNTSDR HSYA2011082511Lamp · burned outON APPROACH, THE PILOT PUT THE LANDING GEAR HANDLE DOWN FOR LANDING AND THE RT MAIN GEAR INDICATOR FAILED TO ILLUMINATE. THE CREW EXECUTED A GO AROUND AND REQUESTED VECTORS IN ORDER TO ACCOMPLISH ABNORMAL CHECKLIST (DID NOT DECLARE AN EMERGENCY). AFTER A SUCSDR HSYA20100721102Skin · corrodedLT AND RT CEILING STA 584.93 HAS SKIN CORROSION, APPROX SIZE (5" X 9"). LT UPPER SIDE WALL STA 514 HAS SKIN CORROSION. REMOVED CORROSION, TREATED AREA AND INSTALLED 5.25" X 7.25" FABRICATED DOUBLER FROM 2024T3 .032. CLEANED ALODINED AND PRIMED, INSTALLED ISDR HSYA20100721101Strap · corrodedDURING 4800/9600 HOUR STRUCTURAL INSP THE FOLLOWING ITEMS WERE FOUND. RT FWD TENSION STRAP AT STA 238.17 HAS CORROSION DAMAGE. REMOVED CORROSION,TREATED AREA AND INSTALLED DOUBLER FABRICATED FROM 2024 T351 .190- SIZE (26" X 4"). REPAIRED IAW ENGINEERING REPORTSDR HSYA2010072110Window Frame · corrodedDURING 4800/9600 HOUR STRUCTURAL INSP THE FOLLOWING ITEM WAS FOUND. RT LOWER WINDOW FRAME RAIL-STA 30 HAS CORROSION DAMAGE. REMOVED CORROSION, TREATED AREA AND INSTALLED DOUBLER FABRICATED FROM 2024 T3 .063-SIZE (7" X 4"). REPAIRED IAW ENGINEERING REPORT NR 84SDR HSYA20100720101Skin · corrodedDURING 4800/9600 HOUR STRUCTURAL INSP, THE FOLLOWING ITEMS WERE FOUND. CORROSION DAMAGE ON FUSELAGE SKIN FOUND AT STA 213.2-FUEL TANK RT OF CENTERLINE. REMOVED CORROSION, TREATED AREA AND INSTALLED DOUBLER FABRICATED FROM 2024 T3 .032 - 6" X 9" IN SIZE AT STA SDR HSYA2010072010Skin · corrodedDURING 4800/9600 HOUR STRUCTURAL INSP, FOUND CORROSION ON FUSELAGE SKIN FOUND AT STA 146.2-FUEL TANK RT OF CENTERLINE. REMOVED CORROSION, TREATED AREA AND INSTALLED DOUBLER FABRICATED FROM 2024T3 .032 -10" X 6" IN SIZE AT STA 146.2 - (7) INCHES RT OF CENTERLINSDR HSYA2010071910Seat Track · corrodedLT FWD SEAT TRACK CORRODED AT STA 117.6 REQUIRES A 11 INCH SPLICE REPAIR- (REF SRM 53-00-00 PAGES 62 &64). LT FWD SEAT TRACK CORRODED AT STA 187.2 AND STATION 213.2 - REQUIRES A 36 INCH SPLICE REPAIR- (REF SRM 53-00-00 PAGES 62 & 64). LEFT AFT SEAT TRACK CORROSDR HSYA20080101Line · rupturedJUST AFTER TAKEOFF, THE CREW REPORTED THAT THE NOSE LANDING GEAR WOULD NOT LOCK IN THE UP POSITION. SHORTLY AFTERWARDS BOTH OF THE HYDRAULIC SYSTEM LOW PRESSURE LIGHTS ILLUMINATED. THE CREW DECLARED AN EMERGENCY AND PERFORMED THE ABNORMAL PROCEDURES LIST FOR HSDR HSYA20070601Proximity Switch · out of adjustFLT 120-DURING APPROACH, CREW REPORTED RT MLG UNLOCK INDICATION AFTER SELECTING GEAR HANDLE TO THE DOWN POSITION. THE AIRCRAFT WAS DIVERTED, ATC DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MX FOUND THE RT MLG DOWNLOCK PROXIMITY SWITCH OUT OSDR 20000426SH031Skin · corrodedHNL - LOWER FUSELAGE SKIN CORRODED THROUGH CORRUGATED SKIN AT STA 350 - STA 364 AT CENTER LINE ZERO TO 4 LEFT. HIGHLY CORROSIVE OPERATING ENVIRONMENT, AGING AIRCRAFT. REPAIRED WITH INSERTION REPAIR PER THE SD3-30 SRM AND 43.13-1B. DOCUMENTED ON FORM 337. (
Other aircraft with N330SB · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. N330SB is registered now to the first aircraft listed.