N835EX, cancelled May 30, 2007
Service difficulty reports · 21
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N835EX' AND deregistration_id = 'N835EX-2007-05-30' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N835EX' AND deregistration_id = 'N835EX-2007-05-30' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR HNAA0400109Wire Harness · chafedFLIGHT NR 3822 HAD TO RETURN TO FIELD DUE TO THE RT PROP RPM SURGING ON CLIMB OUT. AIRCRAFT LANDED WITHOUT INCIDENT. CONDITION DID NOT EXIST WITH THE PROP SYNCHROPHASER OFF. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND CHAFED WIRES AT THE ENGINE HARNESS FOR THE SYSDR HNAA0408106Socket · burnedFLIGHT 3980 REPORTED A HOT ELECTRICAL SMELL IN THE CABIN WITH OVERHEAD LIGHTS ON. MAINTENANCE FOUND THE OVERHEAD LIGHT SOCKET BAD. THEN REMOVED AFFECTED BULB AND PULLED AND BANDED ASSOCIATED S1 CIRCUIT BREAKER, AND SCHEDULED TO HAVE THE SOCKET REPLACED.SDR HNAA0408107Power Supply · inoperativeFLIGHT REPORTED THE EMERGENCY EXIT LIGHT OVER THE CABIN DOOR AS BEING INOPERATIVE. MAINTENANCE TROUBLESHOT SYSTEM AND REMOVED AND REPLACED THE BATTERY POWER SUPPLY AT POSITION NR 100. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.SDR PCAA0404192Handle · bentREPORTED THAT THE OUTSIDE AIRSTAIR DOOR HANDLE WAS BENT AND WOULD NOT ALLOW THE DOOR TO BE CLOSED. MAINTENANCE REOMVED AND REPLACED THE HANDLE AS REQUIRED AND THE DOOR WAS RIGGED AS NEEDED. SYSTEM OPERATIONAL CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TO SERVSDR PCAA0402172Smoke Detector · faultyFLIGHT 3982 CREW REPORTED THAT THE NR 2 BAGGAGE BAY SMOKE DETECTOR WOULD NOT TEST. ITEM WAS DEFERRED AFTER VERIFICATION THAT THE NR 1 WAS IN OPERATING ORDER. ONCE IN MAINTENANCE THE DETECTOR WAS REPLACED AND OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TSDR PCAA0303056Brake · failedPHL-FLIGHT 3503 CREW REPORTED NORMAL BRAKES FAILED WHEN TAXIING IN WITH ONLY NR 2 ENGINE OPERATING AND STANDBY PUMPS ON. MAINTENANCE BLED ALL BRAKES, TAXIED AIRCRAFT ON NR 1 ENGINE. NO DEFECTS WERE NOTED. AIRCRAFT RETURNED TO SERVICE.SDR PCAA0301011Wire · damagedDURING ROUTINE MAINTENANCE VISIT 6TH RED FLOOR LEVEL EMERGENCY LIGHT FOUND INOPERATIVE. LEAD WIRE REPAIRED AT ATTACH POINT TO BULB. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR PCAA0212145Windshield · crackedFLIGHT#3636 BTV-LGA. WHILE IN CRUISE FLIGHT FIRST OFFICERS WINDSHIELD BEGAN TO CRACK IN SEVERAL PLACES AND SPARK DUE TO WINDSHIELD HEAT BEING TURNED ON. WINDSHIELD HEAT SELECTED OFF AND SPARKING STOPPED. AIRCRAFT RETURNED TO BTV, AND EMERGENCY DECLARED. MAINTESDR PCAA0208091Wire · crushedDURING ROUTINE MAINTENANCE VISIT FIRST FLOOR LEVEL EMERGENCY LIGHT FOUND INOPERATIVE. CRUSHED WIRE FOUND AND REPAIRED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR PCAA0208085Actuator · crackedPHL-FLIGHT#3686. CREW REPORTED LOSS OF #1 HYDRAULIC SYSTEM FLUID JUST AFTER TAKEOFF.EMERGENCY DECLARD, AND AIRCRAFT RETURNED TO FIELD. MAINTENANCE INSPECTED AIRCRAFT AND FOUND INBOARD RIGHT ROLL SPOILER ACTUATOR CRACKED AND LEAKING. INBOARD RIGHT ROLL SPOILER SDR PCAA0207074Connector · loosePHL- FLIGHT 3643. CREW REPORTED FORWARD SEGMENT OF FLOOR EMERGENCY LIGHTING INOPERATIVE. MAINTENANCE RESECURED FORWARD SEGMENT OF EMERGENCY LIGHT PLUGS. AIRCRAFT RETURNED TO SERVICE.SDR PCAA0201015Power Supply · inoperativeDURING ROUTINE MAINTENANCE VISIT RIGHT AFT EMERGENCY LIGHTS FOUND TO BE INOPERATIVE. POWERSUPPLY BOX AT POSITION #400 AND 2 BATTERIES WERE REPLACED, POSITION #400 AND #600. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR PCAA0201010Wire · brokenDURING ROUTINE MAINTENANCE VISIT THE FURTHEST AFT EMERGENCY FLOOR LIGHT WAS FOUND INOPERATIVE. TWO BROKEN WIRES FOUND AND INSULATION PULLED AWAY FROM LIGHT SOCKET. NEW LIGHT ASSEMBLY INSTALLED. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR PCAA0111157Link · wornDURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, FOUND PISTON CAP PIN GOUGED BEYOND LIMITS, TRAILING ARM WORN, AND TRAILING ARM ASSEMBLY WITH A GOUGE. TRAILING ARM ASSEMBLY REPLACED IN ACCORDANCE WITH MAINTENANCE MANUAL 32-20-11, TRSDR PCAA0101002Bulb · failedBGM FLIGHT 3555. ROW 1 RIGHT SIDE EMERGENCY LIGHT INOP ONE BULB. MAINTENANCE REPAIRED WIRING ON FLOOR EMERGENCY LIGHTS. AIRCRAFT RETURNED TO SERVICE.SDR PCAA0011073Skin · crackedBGM- DURING ROUTINE MAINTENANCE INSPECTION STARBOARD SIDE OF FORE RUDDER FOUND TO HAVE A 10 INCH C-SHAPE CRACK. FORE RUDDER ASSEMBLY REPLACED IN ACCORDANCE WITH DEHAVILLAND DASH 8 MAINTENANCE MANUAL CHAPTER 27-20-00. AIRCRAFT RETURNED TO SERVICE.SDR PCAA0002012Windshield · crackedEN ROUTE TO ABE, THE CAPTAINS WINDSHIELD CRACKED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS WINDSHIELD IAW DHC PROCEDURES. AIRCRAFT WAS RETURNED TO SERVICE.SDR PCAA9800765Window · crackedDURING CRUISE FLIGHT OUT OF SYR, THE CAPTAINS SIDE WINDOW CRACKED. AIRCRAFT RETURNED TO SYR AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE SIDE WINDOW IAW DHC PROCEDURES. A/C RETURNED TO SERVICE. (M)SDR PCAA9800718Wire · brokenTWO LIGHTS INOPERATIVE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM. REPAIRED BROKEN WIRE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM. REPAIRED BROKEN WIRE IN FLOOR EMERGENCY PROXIMITY LIGHTING SYSTEM CIRCUIT. OPERATIONAL TEST NORMAL. AIRCRAFT RETURNED TO SDR PCAA9700569Strut · failedLEFT ENGINE OUTBOARD AFT VERTICLE MOUNT STRUT CRACKED COMPLETELY THROUGH ENTIRE STRUT. REMOVED AND REPLACED LEFT ENGINE AFT OUTBOARD VERTICLE MOUNT STRUT WITH SERVICEABLE UNIT. A/C RETURNED TO SERVICE. (M)SDR PCAA9700362O-Ring · failedPHL - DURING CLIMB-OUT, NR 2 ENGINE OIL PRESURE DROPPED TO 40 PSI. THE ENGINE WAS SHUT DOWN AND ACFT LANDED IN ABE WITHOUT INCIDENT. MAINTENANCE INSPECTED ENGINE IAW PWC MANUAL FOR LOW/LOSS OF OIL PRESSURE. FOUND THE PROP CONTROL UNIT ADAPTER FLANGE O-RINGS
Back to N835EX, cancelled May 30, 2007