N803FX
Service difficulty reports · 262
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 = 'N803FX' AND registry_match = 'registration' 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 = 'N803FX' AND registry_match = 'registration' 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 COEA2016100276803Skin · corrodedINNER SKIN AT INSULATION STANDOFF AFT OF FRAME 21 HAD CORROSION ABOVE STRINGER 10L. REPAIRED IAW ES-4447/16.SDR COEA2016100275803Frame · corrodedFRAME 24 FLANGE HAD CORROSION, STRINGERS 3 - 3AR. REPAIR IAW ES-4448/16.SDR COEA2016100274803Skin · corrodedINNER SKIN AT INSULATION STANDOFF FWD OF FRAME 24 HAD CORROSION STRINGER 3A - 4R. REPAIRED IAW ES-4448/16.SDR COEA2016100270803Skin · corrodedINNER SKIN AT INSULATION STANDOFF FWD OF FRAME 23 HAS CORROSION BELOW STRINGER 9L. REPAIRED IAW ES-4447/16.SDR COEA2016100269803Skin · corrodedINNER SKIN AT INSULATION STANDOFF FWD OF FRAME 23 HAS CORROSION BELOW STRINGER 7AL. REPAIRED IAW ES-4447/16.SDR COEA2016100268803Skin · corrodedINNER SKIN AT INSULATION STANDOFF AFT OF FRAME 21 HAS CORROSION BELOW STRINGER 9L. REPAIRED IAW ES-4447/16.SDR COEA2016100267803Skin · corrodedINNER SKIN AT INSULATION STANDOFF FWD OF FRAME 21 HAS CORROSION BELOW STRINGER 8L. REPAIRED IAW ES-4447/16.SDR COEA2016100266803Skin · corrodedINNER SKIN AT INSULATION STANDOFF FWD OF FRAME 23 HAS CORROSION BELOW STRINGER 8L. REPAIRED IAW ES-4447/16.SDR COEA2016100265803Skin · corrodedINNER SKIN AT INSULATION STANDOFF FWD OF FRAME 22 HAS CORROSION BELOW STRINGER 9L. REPAIRED IAW ES-4447/16.SDR COEA2016100264803Skin · corrodedINNER SKIN AT INSULATION STANDOFF AFT OF FRAME 22 HAS CORROSION BELOW STRINGER 9L. REPAIRED IAW ES-4447/16.SDR COEA2016100263803Skin · corrodedINNER SKIN AT INSULATION STANDOFF AFT OF FRAME 21 HAS CORROSION BELOW STRINGER 8L. REPAIRED IAW ES-4447/16.SDR COEA2016100262803Skin · corrodedINNER SKIN AT INSULATION STANDOFF FWD OF FRAME 21 HAD CORROSION BELOW STRINGER 7AL. REPAIRED IAW ES-4447/16.SDR COEA2016100261803Skin · corrodedINTERNAL SKIN HAD CORROSION FRAME 21 BELOW STRINGER 9L. REPAIRED IAW ES-4447/16.SDR COEA2016100234803Skin · corrodedHEAVY CHECK/MAJOR REPAIR: INNER SKIN AT INSULATION STANDOFF FWD OF FRAME 23A HAS LEVEL 2 CORROSION BELOW STRINGER 8R. REPAIRED PER SRAS ES-4445/16.10834 DATED 11/25/2016.SDR COEA2016100230803Skin · corrodedHEAVY CHECK/MAJOR REPAIR, INNER SKIN AT THE INSULATION STANDOFF FWD OF FRAME 21 HAS LEVEL 2 CORROSION BELOW STRINGER 8R. REPAIR PER SRAS ES-4429/16.10811 DATED 11/25/2016.SDR COEA2016100229803Skin · corrodedHEAVY CHECK/MAJOR REPAIR, INNER SKIN AT THE INSULATION STANDOFF FWD OF FRAME 17 HAS LEVEL 2 CORROSION STRINGER 11R-10AR. REPAIR PER SRAS ES-4429/16.10811 DATED 11/25/2016.SDR COEA2016100228803Skin · corrodedHEAVY CHECK/MAJOR REPAIR INNER SKIN AT THE INSULATION STANDOFF FRAMES 13-14 HAS LEVEL 2 CORROSION BELOW STRINGER 4R. REPAIR PER SRAS ES-4429/16.10811 DATED 11/25/2016.SDR COEA2016100227803Skin · corrodedHEAVY CHECK/MAJOR REPAIR, INNER SKIN AT THE INSULATION STANDOFF FRAMES 13-14 HAS LEVEL 2 CORROSION BELOW STRINGER 9R. REPAIR PER SRAS ES-4429/16.10811.SDR COEA2016100206803Stringer · crackedSTRINGER 1AR IS CRACKED BY FRAME 15. STRINGER SPLICED IAW SRM 530000-300-824-A01.SDR COEA2016100205803Stringer · crackedSTRINGER 2L IS CRACKED BY FRAME 20. STRINGER SPLICED IAW SRM 530000-300-824-A01.SDR COEA2016100204803Skin · corrodedSKIN AT THE INSULATION STANDOFF AFT OF FRAME 16 HAS CORROSION ABOVE STRINGER 16AR. REPAIRED IAW SRM 530000-300-805-A01.SDR COEA2016062303803Skin · damagedAFT CARGO DOOR INNER SKIN IS DAMAGED AT LOWER CORNERS AND HAS OVERSIZED HOLES. REPAIRED IAW SRAS DO/TS-5345/05.SDR COEA2016030902803Master Cylinder · inoperativeAFTER ARRIVAL FROM FLIGHT 8299, THE CREW NOTED THE RT FIRST OFFICERS BRAKE WAS INOPERATIVE. REPLACED THE FIRST OFFICERS MASTER CYLINDER, BLED BRAKES. OPERATIONS CHECKED GOOD.SDR COEA2016030801803Unknown · malfunctionedFLIGHT 7299 BRAKE INOPERATIVE WO 159364 DISCREPANCY. DURING TAXI, THE FIRST OFFICERS RT BRAKE FAILED. ACFT WAS TAXIED BACK TO RAMP. OPERATIONS CHECKED BRAKES IAW JIC 32-42-00 OPT 10000-001 & ENG RUN & TAXI CHECKLIST. NO FAULT FOUND. OPERATIONS CHECKED GOOSDR COEA2015062502803Fitting · crackedFLIGHT 7299 EN ROUTE, EMER DECLARED, DISCREPANCY. WHILE AT CRUISE EN ROUTE, THE CREW RECEIVED A GREEN HYD SYS LOW LEVEL INDICATION & CCASS ALERT. WHILE RUNNING THE QRC, THE CREW ALSO RECEIVED A LOW PRESS INDICATION ON THE SAME SYS. AN EMER WAS DECLARED & THSDR COEA2015050701803A/C Pack · damagedFLIGHT 8277 EN-ROUTE, SMOKE IN COCKPIT. APPROX 60 MILES OUT, THE CREW DETECTED A STRONG SMOKE SMELL IN THE COCKPIT. THE CREW DECLARED AN EMER AS SMOKE BEGAN TO BUILD IN THE COCKPIT. WHILE RUNNING THRU THEIR CHECKLIST, FOR SMOKE IN THE COCKPIT, THE SMOKE LIFSDR COEA2014120310803Wire · chafedAIR TURN BACK. ON DEPARTURE DURING CLIMB, THE NR 1 ACW GEN FAULTED. THE QRH WAS CONSULTED & THE CREW ELECTED TO RETURN. NO EMER WAS DECLARED. THE ACFT LANDED WITHOUT INCIDENT. DUE TO ICING CONDITIONS ENROUTE THE ACW GEN WAS NOT DEFERRABLE. AFTER EXTENSIVESDR COEA2014102709803Contactor · faultedSHORTLY AFTER TAKEOFF THE NR 1 ACW GEN FAULTED & WOULD NOT RESET. DUE TO ICING CONDITIONS, THE ACFT WAS RETURNED, NO EMER WAS DECLARED. AFTER TROUBLESHOOTING, MAINTENANCE WAS ABLE TO GET THE GEN BACK ONLINE BY REPLACING THE NR 1 ACW CONTACTOR. OPERATIONS CHESDR COEA2014100208803Frame · damagedWORK ORDER 139727 NR 2 HEAVY CHECK POST CHECK INSPECTION COE & MAJOR REPAIR. EDGE DAMAGE TO RT FRAME 13 INNER FLANGE ABOVE STRINGER 12. REPAIR IAW SRAS DT S-5916 14 8742 DATED 10/6/2014.SDR COEA2014090806803Panel · corrodedWORK ORDER 137960 NR 500025. HEAVY CHECK COE, MAJOR REPAIR. PANEL 521DT FOIL HAS FRETTING. REPAIR IAW DO TS 4828 10 6020 ISSUE B DATED 9/22/14.SDR COEA2014090804803Housing · corrodedWORK ORDER 137960 NR 600017. HEAVY CHECK COE, MAJOR REPAIR. RT CTR WING ACCESS PANEL HOUSING FOR PANEL 622CT HAS FRETTING. REPAIR IAW DOTS 4828 10 6020 ISSUE B DATED 9/22/14.SDR COEA2014090405803Skin · galledWORK ORDER 137960 NR 500017. HEAVY CHECK COE, MAJOR REPAIR. LT CTR WING FEEDER TANK ACCESS DOOR CUT OUT HAS GALLING. REPAIR IAW DOTS 4828 10 6020 ISSUE B DATED 9/22/14.SDR COEA2014090203803Stringer · damagedWORK ORDER 137960 NR 200010. HEAVY CHECK COE, MAJOR REPAIR. STRINGER 7A AT FRAME 20 RT HAS TOOLING DAMAGE. STRINGER SPLICE BETWEEN FRAME 19 - 21 IAW SRM 53-00-00 REPAIR 422.SDR COEA2014083007803Skin · peelingWORK ORDER 137960 NR 500004 HEAVY CHECK COE MAJOR REPAIR. LT WING HAS TWO SPOTS OF COMPOSITE PEELING ON THE LOWER SURFACE NEAR THE LE, OTBD OF RIB 19 & INBD OF RIB 21. REPAIR IAW SRAS DT S-5621 4 8730 DATED 9/30/14.SDR COEA2014053001803Heat Exchanger · crackedSMOKE IN CABIN & AFW. DISCREPANCY, WHILE RUN & TAXI TRAINING WAS BEING CONDUCTED, THE CABIN WAS DISCOVERED TO BE FULL OF SMOKE. THE ACFT WAS SHUT DOWN. THE FIRE DEPARTMENT WAS NOTIFIED & THE THREE OCCUPANTS EGRESSED THE AIRPLANE. THE FWD & AFT DOORS WERE OSDR COEA2012102907803Skin · dentedHEAVY CHECK COE/MAJOR REPAIR: DENT OUT OF LIMITS 2.3 INCHES AFT OF FRAME 15-1.3 INCHES ABOVE RIGHT STR 19. REPAIR PER SRM.SDR COEA2012102906803Skin · dentedHEAVY CHECK COE/MAJOR REPAIR: LEFT LOWER FUSELAGE SKIN HAS A CREASE & DENT FWD OF FRAME 32 BETWEEN STRINGERS 15L & 17L-MARKED. REPAIR PER SRM.SDR COEA2012102904803Skin · dentedHEAVY CHECK COE/MAJOR REPAIR: DENT OUT OF LIMITS 3.8 INCHES AFT OF FRAME 36-0.6 INCHES ABOVE LEFT STR 18. REPAIR PER SRM.SDR COEA2012102903803Skin · dentedHEAVY CHECK COE/MAJOR REPAIR: DENT OUT OF LIMITS 3.5 INCHES FWD OF FRAME 33-1.1 INCHES. ABOVE RIGHT STR 19. REPAIR PER SRM.SDR COEA2012102902803Skin · dentedHEAVY CHECK COE / MAJOR REPAIR: DENT OUT OF LIMITS 9.5 INCHES FORWARD OF FRAME 23A - 1.6 INCHES BELOW LEFT STRINGER 19. REPAIRED PER SRM.SDR COEA2012071001803Sensor · wornAIR TURNBACK: JNU FLT 8216: AFTER DEPARTURE FROM JNU THE NR 2 DC GENERATOR FAULTED TWICE AND CREW WAS UNABLE TO RESET. CREW ELECTED TO RETURN TO JNU FOR MAINTENANCE. MAINTENANCE REMOVED AND REPLACED THE HALL EFFECT SENSOR. AIRCRAFT RETURNED TO SERVICE.SDR COEA2011121004803Starter Gen · failedFLT 8902 FOR MAINTENANCE: ON DESCENT INTO SIT PILOT RECEIVED A DC GEN 1, DC BUS 1 AND AN AC BUS 2 FAILURE. DUE TO FAILURES THE NAVIGATION SYSTEM WAS AFFECTED. PILOTS ELECTED TO RETURN TO JNU FOR MAINTENANCE. AN EMERGENCY WAS DECLARED AND AIRCRAFT LANDED WISDR COEA2011082003803Static Inverter · failedAIR TURNBACK / SEA: SHORTLY AFTER ROTATION ON CLIMBOUT FROM SEA ALL MECHANICAL CAPT SIDE GAUGES FLAGGED OFF, ALL EFIS DATA WAS LOST, STBY ATTITUDE INDICATOR FLAGGED OFF. FOR 5 SEC. INTERVALS 4-5 TIMES. PILOT ELECTED TO RETURN TO SEA. AIRCRAFT LANDED WITHOUTSDR COEA2011081902803Engine · power lossFLT 7202 AIR TURNBACK / SEA: PILOT EXPERIENCED MOMENTARY POWER LOSS ON NR 2 ENGINE ON CLIMBOUT. MAINTENANCE PERFORMED INSPECTION OF ENGINE ELECTRICAL WIRING HARNESS CONNECTOR SLEEVES AND PERFORMED ENGINE GROUND RUN WITH NO DEFECTS NOTED. PERFORMED FDAU AND SDR COEA2011042501803Skin · damagedMAJOR REPAIR: FOUND FASTENER TRAPPED BETWEEN OUTER SKIN AND SUBSTRUCTURE AT APPRX FR 36LT. (UNUSED PILOT HOLE IN SKIN AND DOUBLER AT FR 36) REMOVED GILLINER TO ACCESS. REPAIRED SKIN AND DOUBLER IAW SRM AND SRI DO/TS1741/11-14956 ISSUE A. REINSTALLED GILLINESDR COEA2010121763803Support Beam · crackedP-F MODIFICATION BY M7 AEROSPACE IN SAT / CRACK OF PAX / CREW DOOR SURROUND / 2 EACH AFT DOOR BEAM SUPPORTS: 1 WITH A 0.50, CRACK AND THE OTHER WITH A 0.25, CRACK ALSO LOCATED IN THE RADIUS. THE PART NUMBER FOR THESE DOOR BEAM SUPPORTS ARE THE SAME P/N S 52176SDR COEA2010121762803Intercostal · crackedP-F MODIFICATION BY STC BY M7 IN SAT / CRACK OF PAX / CREW DOOR SURROUND / LOCATED FROM TOP OF DOOR, BETWEEN 6 AND 14 DOWN, AND FROM FRONT TO BACK. 1 EACH INTERCOSTAL RECEIVED WITH 1 EACH CRACK IN RADIUS AT 0.75 IN LENGTH P/N S 52176205202-01.SDR COEA2010121761803Frame · damagedATR STRUCTURAL REPAIR INSTRUCTION DO/TS-6714/10-14653 SAT P-F MODIFICATION PER STC/ MIS-DRILLED HOLES / MAJOR REPAIR OF MIS-DRILLED HOLES IN FRAME 23 WEB AT STRINGER 5A. REPAIRED IN ACCORDANCE WITH REFERENCED ATR SRI WITH CUTOUT AND LOCALIZED DOUBLER REPAIR. SDR COEA2010121760803Seat Track · corrodedWO 97861 NR 100011 COE HEAVY CK / LEVEL 2 CORROSION / MAJOR REPAIR: RT OUTBOARD SEAT TRACK HAS AREAS OF BARE METAL WITH CORROSION BETWEEN FRAMES 29 & 36. BLENDED RIGHT O/B SEAT TRACK FOUND FR 34.5 TO 36 OUT OF LIMITS. REC'D NEW SEAT TRACK AFT END FR 34.5 -36SDR COEA2010120959803Threshold · corrodedLEVEL 2 CORROSION / MAJOR REPAIR: AFT RT SERVICE DOOR THRESHOLD PLATE UPPER SURFACE HAS LEVEL 2 CORROSION BETWEEN FRAMES 36 & 39. REMOVED THRESHOLD PLATE, INTERCOSTALS, ETC. REMOVED CORROSION FROM THRESHOLD WEB, FOUND OUT OF LIMITS (LENGTH 4 INCH, WIDTH 3 I
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