N87, cancelled Dec 24, 2025
Service difficulty reports · 32
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 = 'N87' AND deregistration_id = 'N87-2025-12-24' 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 = 'N87' AND deregistration_id = 'N87-2025-12-24' 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 RU3A2021052101111Selector Valve · faultedGEAR FAILED TO RETRACT AFTER TAKEOFF. 'I/P WOW' LIGHT ILLUMINATED. REPLACED DOOR SELECTOR VALVE AND WEIGHT ON WHEELS HARNESS ON NOSE LANDING GEARSDR RU3A20200108001Warning Light · activatedSTALL PROTECTION SYSTEM FAIL LIGHTS FLASHING IN FLIGHT.SDR RU3A201912065072Wire Harness · damagedR/ OUTBOARD ANTI-SKID FAIL ILLUMINATED AFTER TEST. (AIRBORNE)...TEMP REPAIR #2 MLG HARNESS FOR SFP TO REPAIR STATION. WILL MONITORSDR RU3A20191030060Motor · failedFLAP MOTOR 2 CIRCUIT BREAKER POPPED IN FLIGHT. REPLACING FLAP MOTOR CORRECTED THE DISCREPANCY.SDR RU3A20191030058Charger · failedBATTERY CHARGER CIRCUIT BREAKER TRIPPED IN FLIGHT. CORRECTION: REMOVED AND REPLACED AIRCRAFT BATTERY CHARGER.SDR RU3A20190628026Skin · crackedCRACKS THE WING SKINSDR RU3A20181210050Control Head · burnedDESCENDING THROUGH 5000'MSL CREW NOTICED ACRID SMELL. DONNED OXYGEN MASK AND TURNED AFIS OFF. SMELL SLOWLY DISSIPATED. NO SMOKE WAS VISIBLE. CAUSE WAS FOUND TO BE CVR CONTROL HEAD BURNED INTERNALLY.SDR RU3A2018031200002Crank Assy · crackedPASSENGER DOOR LATCH MECHANISM CRANK CRACKED PART 600-31890-21.SDR RU3A20171205043Display · inoperativeAFIS FAILED IN FLIGHT. DISPLAY WENT DEAD, AND ELECTRICAL FUMES WERE PRESENT. MILTOPE(EIFW IN-FLT WKSTATION)SDR RU3A20171012034Windshield · crackedPILOT SIDE FRONT WINDOW OUTER GLASS HAD A MAJOR CRACK. REMOVED AND REPLACED PILOT'S WINDSHIELD.SDR RU3A20170210003Connector · dirtyRIGHT ENGINE COWL ANTI-ICE FAIL LIGHT ILLUMINATED DURING FLIGHT, PROBLEM WAS CORRECTED AFTER CLEANING OF ELECTRICAL CONNECTORS.SDR RU3A20151021022Anti-Ice System · defectivePILOT LT SIDE WINDSHIELD HEAT FAIL. REPEAT FAILURE.SDR RU3A20150811017Fms · malfunctionedWAAS 1 & WAAS 2 FAILED IN CRUISE FLIGHT. MULTIPLE NAV SYS FAILURES, FD, CDU, FMS 1 & 2 FLAGS ON MFD BOTH SIDE NAV INDICATIONS FAILED. RE-SEATING & RE-LOADING THE FMS DATABASES CORRECTED THE ISSUE.SDR RU3A20140519019Hydraulic Line · looseSUPPLEMENTAL INFORMATION: CORRECT ATA CODE(C) TO 2910, CORRECT HOW DISCOVERED (E) TO V-VISUAL. CORRECTIVE ACTION: FOUND LOOSE B NUT ON HYDRAULIC TUBE ASSY P/N: 601-75238-43 AFT CONNECTION. INSPECTED B-NUT, RE-TORQUED B NUT FITTING. LEAK CHECK SATISFACTORYSDR RU3A20130502006Window · crackedDURING FLIGHT, CREW HEARD LOUD POP. INITIAL INSPECTION DISCOVERED LEFT PILOT SIDE WINDOW WITH LARGE CRACK AND SIGNIFICANT GAP IN OUTER PANE WITH ASSOCIATED "FAIL" LIGHT ON WINDSHIELD HEAT.SDR RU3A1203Thrust Reverser · malfunctionedAT FL150, GOT RIGHT T/R UNLOCK LIGHT. CREW PRESSED T/R EMERGENCY STOW AND COMPLIED WITH CHECKLISTS. DECLARED EMERGENCY AND DIVERTED TO NEAREST AIRPORT WITH ADEQUATE RUNWAY LENGTH.SDR RU3A1119Bulkhead · buckledBULKHEAD AND AIRCRAFT SKIN AT FORWARD FUSELAGE STATION 235 IS CRACKED AND BUCKLED.SDR RU3A1109Proximity Switch · faultyAFTER TAKEOFF THE LANDING GEAR HANDLE WAS MOVED TO THE UP POSITION. BOTH MAIN GEAR RETRACTED BUT THE NOSE GEAR DID NOT RETRACT. THE ONLY INDICATION IN THE COCKPIT WAS ONE GREEN NOSE GEAR DOWN LIGHT. HOLDING WAS COORDINATED WITH ATC. EMERGENCY AND NORMAL CHSDR RU3A1018Unknown · malfunctionedTWO UNCOMMANDED ABRUPT RIGHT RUDDER INPUTS. AUTOPILOT ON. YAW DAMP ON. AIRCRAFT CLIMBING THROUGH 8000 FEET AT 250 KNOTS. SECOND EVENT 11000 FEET AT 250 KNOTS. NO SERVO MONITOR LIGHT ILLUMINATED. NO INDICATION OF JAM RUDDER. ALL THREE HYDRAULIC SYSTEM PRESDR RU3A1007Windshield · splitAFTER APPROXIMATELY 1.0 HOUR OF FLYING IN THE CLIMBOUT TO NEXT WORK, NOTICED WINDSHIELD SPLITTING FROM A SMALL SCRATCH. LEVELED OFF TO 17,000 FEET, RAN CHECKLIST AND GOT CLEARANCE TO RETURN.SDR RU3A004Hydraulic Line · chafedNUMBER 2 HYDRAULIC SYSTEM LOST PRESSURE ON APPROACH. FOUND PRESSURE HOSE ASSY IN PYLON CHAFED BY HOSE CLAMP WHERE RUBBER LINER WAS ERODED AND THE CLAMP AND HOSE WERE METAL TO METAL. REPLACED HOSE, CLAMP, AND ENGINE DRIVEN HYDRAULIC PUMP. INSPECTED FILTERS, SDR RU3A0710Windshield · crackedFLYING AT FL340 1.5 HOURS INTO FLIGHT THE CO-PILOTS WINDSHIELD OUTER PLY CRACKED. COMING INTO THE TERMINAL AREA WITH -3 DEGREE C AND MOISTURE IN THE AIR, RAIN STARTED TO GET INSIDE THE CRACK. ON A 14 MILE ILS FINAL TO RWY 28 AT ABOUT 3000' HEARD A LOUD POP ASDR RU32006F00001Wing · scratchedUPON POST FLT, DISCOVERED STRATCHES ON RT WINGLET. APPARENTLY WHILE POSITIONING OVER GCP AT RKTP, SCRAPED GCP SIGN. NO INDICATION OF CONTACT WHILE AT RTKP. RETURNED TO RKSO WHERE DAMAGE WAS NOTED. PERFORMED TEMP REPAIR REFERENCE REO. (K)SDR RU3A0419Seal · deterioratedAFTER TAKEOFF FUEL WAS SEEN STREAMING OUT OF LT OVERWING FUEL CAP DURING CLIMB. REPLACED FUEL CAP.SDR 2004F00076Sensor · failedON FINAL APPROACH GEAR EXTENSION AND ANTI-SKID OUTBOARD FAIL MALFUNCTION OCCURRED. GEAR RECYCLED AND SOME TROUBLESHOOTING WAS UNSUCCESSFUL. IN FLIGHT EMERGENCY WAS DECLARED, EQUIPMENT CALLED OUT, ANTI-SKID TURNED OFF AND UNEVENTFUL LANDING CARRIED OUT. NO DASDR RU3A03015Tube · crackedNR 1 HYDRAULIC SYSETM FAILED IN FLIGHT WITH COMPLETE LOSS OF FLUID WITHING THAT SYSTEM. FOUND HYDRAULIC LINE WITH CRACK AT BEND RADIUS. REPLACED HYDRAULIC LINE. ALSO, REPLACED HYDRAULIC PUMP AND FILTERS DUE OT LOSS OF FLUID. (M)SDR R33A03015Line · brokenNR 1 HYDRAULIC SYSTEM FAILED IN FILGHT WITH COMPLETE LOSS OF FLUID WITHIN THAT SYSTEM. FOUND HYDRAULIC LINE SNAPPED OFF. REPLACED HYDRAULIC LINE. ALSO, REPLACED HYDRAULIC PUMP AND FILTERS DUE TO LOSS OF FLUID. (M)SDR RU32003F00003Housing · crackedAPU FUEL FILTER HOUSING ATTACHMENT FLANGES CRACKED. THIS IS THE FIFTH FILTER HOUSING THAT HAS CRACKED SINCE 01/30/99, THREE ON N86 AND TWO ON N87. AFTER INVESTIGATION IT WAS CONCLUDED THAT THE FUEL FILTER HOUSING FAILURES ARE THE RESULT OF FUEL CONTROL UNIT SDR 2003F00235Windshield · crackedDURING CRUISE AT FL330, PILOTS WINDSHIELD, OUTER PLY, POPPED AND THEN CRACKED IMMEDIATELY FROM TOP TO BOTTOM ORIGINATING FROM CENTER. (M)SDR RU3A03003Housing · crackedAPU FUEL FILTER HOUSING ATTACHMENT FLANGES, CRACKED. THIS IS THE 5TH FILTER HOUSING THAT HAS CRACKED SINCE 01/30/99, 3 ON N86, AND 2 ON N87.SDR RU32001F00000Cover · brokenAPU MODEL NUMBER GTCP 36-150RJ. THE LOW PRESSURE FUEL FILTER COVER MOUNTING EAR WAS COMPLETELY BROKEN OFF THE COVER WHERE THE MOUNTING BOLT ATTACHES THE COVER TO THE FUEL CONTROL. APU CONTINUED TO RUN AFTER EAR BROKE OFF.SDR RU3A99007Fuel Cap · dirtyFUEL OBSERVED STREAMING DOWN THE RIGHT-HAND WING DURING FLIGHT. FUEL WAS LEAKING AT THE RIGHT-HAND OUTBOARD FUEL CAP. AIRCRAFT MADE UNSCHEDULED LANDING. THE LOCKING DEVICE ON THE CAP WAS INSPECTED AND FOUND TO BE FUNCTIONING PROPERLY. FOREIGN MATTER WAS FOU
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