N310DA
Service difficulty reports not matched to an aircraft · 36
They name N310DA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N310DA' AND registry_match IS NULL 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 = 'N310DA' AND registry_match IS NULL 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 DL73S050428Fuse · blownPASSENGER SEAT 25C AND 25D EMERGENCY TRACK LIGHTING INOP. REMOVED AND REPLACED FUSES IN BATTERY PACK CRADLE. OPS CK OK.SDR DL73S041118Bulkhead · crackedINSPECTION OF THE FS 1016 P-DOME BULKHEAD WEB PER AD 99-08- 23 REVEALED 3 CRACKED CHORD ATTACH FASTENER HOLES BETWEEN STRINGERS 5L & 7L. THE CRACKS WERE REMOVED BY TRIMMING THE WEB. THE WEB WAS REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER/A 095482-14AD.SDR DL73S041117Skin · crackedINSPECTION OF THE STRINGER 10R SKIN LAP JOINT PER AD 2003- 08-15 REVEALED A CRACK AT FS 380. THE CRACK WAS REMOVED WITH A 4 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM AND ER/A 095527-14AD.SDR DL73S041116Skin · crackedINSPECTION OF THE STRINGER 4L SKIN LAP JOINT REVEALED A CRACK AT FS 411. THE CRACK WAS REMOVED WITH A 7 INCH CUTOUT IN THE SKIN. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER THE B737 SRM AND PER ER/A 095530-14AD.SDR DL73S041115Skin · crackedINSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003 -08-15 REVEALED A CRACK AT FS 512. THE CRACK WAS REMOVED WITH A 14 INCH LONG CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER B737 SRM AND ER/A 095529-14AD.SDR DL73S041114Skin · crackedINSPECTION OF THE STRINGER 4L SKIN LAP JOINT PER AD 2003 -08-15 REVEALED A CRACK AT FS 432. THE CRACK WAS REMOVED WITH A SKIN CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER B737 SRM AND ER/A 095531-14AD.SDR DL73S041113Skin · crackedINSPECTION OF THE STRINGER 4R SKIN LAP JOINT PER AD 2003- 08-15 REVEALED CRACKS AT FS 470. THE CRACKS WERE REMOVED WITH A 17 INCH LONG SKIN CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER THE B737 SRM AND PER ER/A 095528-14AD.SDR DL73S041105Skin · crackedNUMEROUS SKIN CRACKS FOUND ALONG STRINGER 4L BETWEEN STATION 540 AND 727. REPAIRED IAW ERA 095481-14AD.SDR DL73S041100Skin · crackedFUSELAGE SKIN CRACKED AT MULTIPLE LOCATIONS ALONG STRINGER 4R BETWEEN STA 540 AND 727. REPAIR IAW ER/A 095480-14AD.SDR DL73S031146Engine · malfunctionedAFTER T/O, NR 2 ENGINE WENT TO FULL THEN DROVE TO IDLE. ENGINE DATA READ ON FDR. REPLACED NR 2 ENGINE.SDR DL73S030365Doubler · crackedTHE 'H' DOUBLER AROUND THE LOWER HINGE CUTOUT FOR THE L1 DOOR CUTOUT FWD FRAME WAS FOUND WITH A 3/8 INCH CRACK IN THE CORNER RADIUS. THE CRACK WAS STOP DRILLED AND REPAIRED WITH A TITANIUM REPAIR DOUBLER PER ER/A 384891-14, REV B.SDR DL73K010683Skin · crackedFUSELAGE SKIN AFT GALLEY DOOR CUTOUT AT LOWER HINGE CUTOUT: THE LOWER HINGE CUTOUT OF THE AFT GALLEY DOOR (R2) CUTOUT WAS FOUND WITH A 1 IN CRACK IN THE SKIN AND UNDERLYING BEAR STRAP. THE CRACK WAS ROUTED OUT OF ALL LAYERS OF THE SKIN ASSY AND REPAIRED WITHSDR DL73K010682Skin · crackedFUSELAGE SKIN AFT GALLEY DOOR CUTOUT AT UPPER HINGE CUTOUT. THE UPPER HINGE CUTOUT OF THE AFT GALLEY DOOR CUTOUT (R2) WAS FOUND WITH A .25 CRACK IN THE SKIN. THE CRACK WAS ROUTED OUT AND REPAIRED WITH AN EXTERNAL STEEL DOUBLER. THE REPAIR WAS ACCOMPLISSDR DL73K010041Duct · blownSMOKE IN CABIN, RETURN TO BOSTON. REPLACED LT MIXING CHAMBER AND SUPPLY DUCT, LEAK CHECKED. NEEDS ENGINE RUN AND DUCT BURNOUT. PERFORMED SAME, CHECKS GOOD.SDR DL73K002264Fitting · corrodedTHE VERTICAL STABILIZER ATTACHMENT LUGS WERE FOUND CORRODED AT HMV. ERA 396368-14 REMOVES CORROSION FROM THE BORES AND FACES OF THE LUGS AND REINSTALLS THE BUSHING AND SLEEVES.SDR DL73K002260Door Frame · corrodedTHE FORWARD FRAME OF THE C2 DOOR OPENING WAS FOUND CORRODED ON THE AFT SURFACE UNDERNEATH THE DOOR LATCH FITTING. THE CORROSION WAS CUT OUT AND REPAIRED PER ERA 396463-14AD AT HMV.SDR DL73K002259Fitting · corrodedCORROSION WAS FOUND ON THE HORIZONTAL STABILIZER CLEVIS LUGS IN THE BORES AND FACES. THE DAMAGE WAS REMOVED AND REPAIRED PER ERA 396374-14 AT HMV.SDR DL73K002258Fitting · corrodedCORROSION WAS REMOVED FROM THE HORIZONTAL STABILIZER ATTACH LUGS FROM THE BORE AND FACE. ERA 396375-14 REPAIRED THE AREA AT HMV.SDR DL73K002190Skin · crackedDURING SHOP VISIT THE C-2 DOOR OUTER SKIN WAS FOUND DAMAGED. A CRACK WAS FOUND IN THE UPPER AFT CORNER OF THE DOOR HANDLE LATCH CUTOUT. REPAIRED PER ER/A 396879-14.SDR DL73K002153Floorbeam · crackedTHE BL 0.07 FLOORBEAM WAS FOUND CRACKED FROM FS 700 TO FS 717 IN THE WEB. THE DAMAGE WAS REMOVED AND REPAIRED PER B737 S/B 57-1210 AT HMV.SDR DL73K002151Floorbeam · crackedCRACKS WERE FOUND IN THE BL 0 FLOORBEAM WEB AND CHORD BETWEEN FS 650 AND FS 675. THE DAMAGE WAS REMOVED AND REPAIRED SIMILIARL TO THAT OF S/B 737-57-1210 PER ERA 396377-14 AT HMV.SDR DL73K002106Frame · crackedA CRACK WAS FOUND AT THE LOWER FASTENER ON THE INNER CHORD OF THE LEFT AND RIGHT FS 616 FRAMES AT THE OVERWING FRAME TO BEAM JOINT STUB. ERA 396361-14 AUTHORIZES A REPAIR SIMILIAR TO THAT OF SB 737-53-1182 AT HMV.SDR DL73K001536Transmitter · inaccurateRTO AT EWR DUE TO RIGHT ENGINE DID NOT REACH T/O EPR SETTING. REPLACED RIGHT ENGINE EPR TRANSMITTER. OPERATED RIGHT ENGINE AT T/O POWER PER PFHB AND ALL ENGINE PARAMETERS NORMAL.SDR DL73K001486Generator · inoperativeLT ENGINE GENERATOR FAILED DURING TAKEOFF ROLL AT APPROX 80 KTS. CHECKED NR 1 CSD OIL LEVEL AND FILTER BYPASS, CKS GOOD. REPLACED GCU, RAN ENG FOUND GEN FOLLOWING THROTTLE. REPLACED GENERATOR AND CSD.SDR DL73K000220Coffeemaker · malfunctionedDURING TAXI IN, NOTICED ELECTRICAL FUMES. FUMES SEEMED TO BE COMING FROM CB PANEL BEHIND F/O SEAT. ALSO, NOTICED BT LEAD. FLIGHT ATTENDANT FOUND R1 GALLEY COFFEEMAKER OVERHEATING. REPLACED SAME, PERFORMED OPS AND CHECK ALL OK. INSPECTED ALL CB PANELS AND SDR DL73K992170Yaw Damper · malfunctionedUNCOMMANDED ROLL/YAW AT 31000 FT, 77 MACH AUTOPILOT ENGAGED, A/C ROLLED HARD LEFT. REQUIRED 40-50 DEGREE AILERON TO TO RIGHT TO COUNTER COMMAND ROLL. POM COMPLIED WITH YAW DAMPER DISENGAGED. A/C RETURNED TO NORMAL FLIGHT. REPLACED YAW DAMPER COUPLER AND RUDSDR DL73K980113Valve · stuck openF/A REPORTED, DENSE ACRID SMOKE IN CAB AFTER T/O. SMOKE CONCENTRATED FROM ROWS 4 TO 10. DENSE FROM 4 FT ABOVE FLOOR TO CEILING CAB LIGHTS WERE LOW. SMOKE APPEARED TO BE GREY OR WHITE. CHANGED LT 35 DEGREE VLV AND SENSOR. RUN UP BOTH PACKS WITH ENGINE. FOSDR DL73K971642Skin · crackedDUE TO FATIGUE, THE L-2 DOOR LOWER CUTOUT HAS BEEN FOUND TO HAVE A 1.5 TYPICAL CRACK IN THE BEAR STRAP, OUTER SKIN AND THE DOUBLER. THE CRACK CAN BE REPAIRED PER THE B737-200 SRM 53-30-3, FIGURE 24. A TIME LIMITED REPAIR WILL BE INSTALLED WITH BLIND FASTENERSDR DL73K971594Bearings · wornON TAKEOFF/CLIMBOUT, STAB TRIM NOISY MAKING CLICKING NOISE. FLIGHT DIVERTED TO BOS. FOUND STAB TRIM WHEEL BEARING WORN ON RT SIDE OF PEDESTAL. REPLACED BEARINGS AND CROSS SHAFT, CHECKED NORMAL.SDR DL73K971432Fire Detector · malfunctionedAPU FIRE AURAL WARNING AND FIRE HANDLE LIGHT ABOUT 2-3 MINS AFTER START ATTEMPT ON FINAL TO 17 AT MCO. DECLARED EMERGENCY, PULLED AND ROTATED FIRE HANDLE AND WARNING WENT OUT. CKD APU EXHAUST INLET AND OPENED BATHTUB, NO EVIDENCE OF FIRE ALL CKS NML. REPLACSDR DL73S962481Bulkhead · crackedSTATION 178 BULKHEAD WAS FOUND CRACKED IN SEVERAL LOCATIONS. DAMAGE CUTOUTS ARE: 1INCH BY 2.5 INCH FOR RBL 5, WL 194, AND 1INCH BY 2.0 INCH FOR LBL 5, WL 194. REPAIRED PER ERA 304373-14 REV A.SDR DL73S962518Mount · corrodedTHE FWD ENGINE MOUNT HAS TWELVE BOLT HOLES THAT ARE USED TO ATTACH TWO COVER PLATES TO EITHER END OF THE MOUNT, SIZE HOLES PER COVER PLATE. THE TWELVE BOLT HOLES WERE FOUND WITH CORROSION IN THEM. THE BOLT HOLES WERE OVERSIZED TO .400/.407 TO REMOVE THE CORRSDR DL73S954800Press Line · leakingHYD SYS-A LOST QTY AND INDICATES ZERO. REPLACED LEFT MLG UPLOCK PRESS LINE.SDR DL73S953297Eel Bulb · failedEXTERIOR EMERGENCY LIGHT INOP AT L2 DOOR. RELAMPED, OPERATION NORMAL.SDR DL73S951109Skin · corrodedDURING HMV INSPECTION, THE SKIN AT STA 480 WAS FOUND CORRODED IN TWO LOCATIONS BETWEEN STR 26R-28R. THE DAMAGE CONSISTED OF A 1.125 INCH CUTOUT NEAR STR 27R AND A 3.25 INCH BY 2.5 INCH CUTOUT AT THE STA 480 BUTT SPLICE. IN ACCORDANCE WITH B727 SRM 53-30-3, FSDR DL73S950757Valve · leakingON TAXI OUT LOST ALL HYDRAULIC FLUID. FOUND BRAKE SHUTTLE VALVE LEAKING. REPLACED VALVE, OPERATION NORMAL.
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