N925DL, cancelled Mar 19, 2019
Service difficulty reports · 91
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 = 'N925DL' AND deregistration_id = 'N925DL-2019-03-19' 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 = 'N925DL' AND deregistration_id = 'N925DL-2019-03-19' 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 DALA2017062705010Wire · damagedDURING FLIGHT, A RT ENGINE FIRE LOOP MESSAGE DISPLAYED. FOLLOWED QRH, PUT INTO LOOP B. FWD RT ENGINE LOOP A. REPAIRED A DAMAGED WIRE.SDR DALA2017050803632Receptacle · looseTAILCONE ACCESS DOOR CAMLOCK RECEPTICALS LOOSE AND MISSING ON TAILCONE. DOOR CONTAMINATED WITH HYDRAULIC FLUID. REPLACED THE RECEPTICALS. OK FOR SERVICE. FOUND HYD LEAK AND REPAIRED.SDR DALA2017040202667Trim System · bindingAILERON TRIM WHEEL STUCK IN FLIGHT WITH AUTOPILOT ON OR OFF, IT WORKED PRIOR TO DEPARTURE. CHECKED ACTUATOR SCREW ROD END DIMENSION AND DRUM. AILERON TRIM RIG IS GOOD AND NO SIGNS OF BINDING NOTED. COMPLETED IAW AMM 27-10.SDR DALA1702990925Stringer · not reportedWING MAIN FRAME STRINGER 11. REPAIRED IAW 5712-01030, SECT 04.SDR DALA2017020100823Spar · crackedRIGHT WING REAR SPAR CRACKED AT XRS 164 LOWER AFT CORNER OF FLAP HINGE FITTING. REPAIRED THE SPAR IAW DWG J060271 REV T.SDR DALA2017020100822Spar · crackedRIGHT WING REAR SPAR CRACKED AT XRS 164 LOWER AFT CORNER OF FLAP HINGE FITTIING. REPAIRED THE SPAR IAW DWG J060271 REV T.SDR DALA2017020100821Stringer · crackedRIGHT MAIN FUEL TANK STRINGER 11 CRACKED. CUT OUT THE DAMAGED SECTION AND REPAIRED RT WING STRINGER AT XRS 160-164 IAW DWG SR09570100 REV B, AND ERA 553842-14 REV O.SDR DALA2016112909376Switch · failedON APPROACH, RECEIVED NOSE GEAR UNSAFE LIGHT DURING GEAR EXTENSION. COMPLIED WITH QRH AND NORMAL EXTENSION FOLLOWED. IAW MCC, AN EMERGENCY WAS DECLARED. MAINTENANCE REPLACED THE NOSE GEAR INTERLOCK SWITCH WITH POSITIVE RESULTS DURING MULTIPLE NOSE GEAR EXTENSISDR DALA2016112709281Cable · dislodgedLEFT FIRE TEE HANDLE FEELS SPONGY. FOUND CABLE GOING TO HYD SHUTOFF VALVE OFF THE PULLEY. REPOSITIONED IAW AMM 20-10. OPS CHECKED NORMAL. INSPECTED PULLEY AND GUARDS. CHECKED GOOD.SDR DALA2016102807864Psu · malfunctionedDURING CABIN DEPRESSURIZATION EVENT, PSU PANEL DID NOT OPEN AT SEATS 10ABC, 10DE, 13ABC, 12DE, 13DE, 14DE, 15DE, 16DE, 23DE, 24DE, 25ABC, 32ABC, 35ABC, 35DE, 36AB & 36DE. RESET PSU PANELS AND PREFORMED MANUAL EJECT OF OXYGEN MASKS, ALL SEATS AND LAVS PASSED SDR DALA2016102707863Controller · malfunctionedTHE CREW DECLARED AN EMERGENCY DUE TO LOSS OF CABIN PRESSURE. AN EMERGENCY DESCENT WAS MADE TO FL100 AND THE OXYGEN MASKS DEPLOYED. MAINTENANCE FOUND BOTH 1 AND 2 PRESSURE CONTROLLERS SHOWING A CONTROLLER FAULT. THE LEFT ACM LOWER CONNECTING ELBOW DUCT BOOT WASDR DALA2016062004775Battery · dischargedDURING SERVICE CHECK FOUND EMERGENCY LIGHTS AT CEILING ROW 13-15 INOPERATIVE. R & R EMERGENCY LIGHT BATTERIES. OPS CHECK NORMAL. ACFT OK FOR SERVICE.SDR DALA2016032502384Battery Pack · inoperativeTHE CREW FOUND THE AFT LT AND RT OVERWING EXIT SIGNS INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY BATTERIES AND THE LIGHTS CHECKED OK.SDR DALA2016011200207Girt Bar · detachedDURING A FORCASTED SLIDE DEPOYMENT, CVG MAINTENANCE FOUND THAT THE L1 DOOR EMERGENCY ESCAPE SLIDE DID NOT DEPLOY DUE TO THE VELCRO TABS AT THE GIRT BAR BEING UN-ATTACHED. A NEW SLIDE WAS INSTALLED AT POSITION L1; REF LOG SHEET 2305013.SDR DALA2015081805130Floor Support · corrodedENTRANCE DOOR FLOOR SUPPORT FRAME, SIX INCHES FROM DOOR SILL HAS CORROSION. REPLACED THE FLOOR SUPPORT IAW DWG 9936534.SDR DALA2015081805096Support Angle · corrodedCORROSION AT CARGO TRACK SUPPORT ANGLE, BS 1166, TASK 53-139-05. REMOVED AND INSTALLED NEW ZEE CHANNEL IAW SRM 51-01, PARA 4.SDR DALA14032330925Oven · smokeWHILE ENROUTE, THE F/A REPORTED SMOKE FROM FIRST CLASS GALLEY OVEN. OVEN WAS TURNED OFF AND THE CIRCUIT BREAKERS WERE PULLED. THE F/A DISCHARGED A HALON FIRE EXTINGUISHER INTO THE OVEN. SMOKE DISSIPATED AND FLIGHT CONTINUED. REPLACED OVEN.SDR DALA14031380925Wire Harness · damagedDURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY PATH LIGHTING WAS INOPERATIVE AT 27DE. MAINTENANCE REPLACED THE HARNESS AT SEAT 27DE AND THE LIGHTS RETURNED TO AN OPERATIONAL STATE.SDR DALA13072580925Wire · looseDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 27 IN THE CABIN WAS INOPERATIVE. MAINTENANCE FOUND A LOOSE WIRE IN THE CONNECTOR, REPAIRED THE CONNECTOR PIN, AND THE SYSTEM RETURNED TO NORMAL OPERATION.SDR DALA13040780925Rib · crackedRT HORIZONTAL STABILIZER L/E INBD CLOSURE RIB WAS FOUND TO HAVE A CRACK EIGHT INCHES FORWARD OF THE THERMAL ANTI-ICE DUCT. THE CLOSURE RIB WAS REPLACED.SDR DALA13042530925Longeron · crackedLFEC SHOWS INTERNAL CRACK AT BS 1193, LONGERON 3RT. ACCOMPLISHED HFEC INSPECTION IAW NDT 06-10-01.001 NO CRACKS FOUND. REPAIRED IAW ER/A 517907-14AD, REV O.SDR DALA13040530925Inlet · crackedDURING SCHEDULED HEAVY MAINTENANCE, A ONE INCH LONG CRACK WAS FOUND AT THE VERTICAL STABILIZER RAM AIR INLET DUCT RT AFT CORNER. REPAIRED IAW ER/A 517896-14.SDR DALA13039950925Receptacle · wornMX DISCOVERED THAT ALL OF THE TAILCONE RELEASE SYS GUIDE PIN RECEPTACLES WERE WORN BEYOND ALLOWABLE LIMITS. THE RECEPTACLES WERE REPLACED IAW SRM 51-30 AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.SDR DALA13039970925Battery Pack · inoperativeDURING LINE CHECK, MX FOUND THEY HAD NO CONTROL OF THE EMERGENCY ESCAPE LIGHTING AT THE OVERWING EXITS IN THE CABIN, WOULD NOT TURN OFF. MX REPLACED THE BATTERY PACK FOR THE NOTED LIGHTED AREA AND THE LIGHTS RETURNED TO A CONTROLLABLE CONDITION. OPS CHECKEDSDR DALA13026970925Battery Pack · inoperativeDURING LINE CHECK, MX FOUND THAT THE LT WING EXTERIOR EMERGENCY LIGHT WAS MALFUNCTIONING IN THAT IT WOULD REMAIN ON AFTER SELECTOR WAS CHANGED TO "ARMED". MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPS CONDITION.SDR DALA12011160925Lanyard · misinstalledTAILCONE SLIDE DEPLOYMENT LANYARD WAS NOT LOOPED AROUND THE TAILCONE RELEASE MECHANISM CAM. DISCONNECTED THE LANYARD FROM CLEVIS AT THE SLIDE BOX AND RECONNECTED THE TAILCONE SLIDE DEPLOYMENT LANYARD IAW AMM 25-62-01-201. INSPECTION OF LANYARD INSTALLATION WASSDR DALA1233670925Pin · wornDURING FUNCTIONAL CHECK OF TAILCONE RELEASE SYSTEM OPS 6908, MAINTENANCE FOUND THE TEE PIN, BUSHING, AND CABLE WORN BEYOND THE TEE PIN 11, CAM ASSEMBLY, AND CABLE WERE ALL REPLACED AND THE RII COMPLETED.SDR DALA1213520925Battery · dischargedDURING LINE CHECK, MAINTENANCE FOUND THAT BOTH OF THE FORWARD OVERWING EMERGENCY EXIT SIGNS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPERATIONAL CHECK WAS GOOD.SDR DALA1212040925Skin · corrodedDURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN STA Y=773 BTW LONGERON 27 TO 28RT. FUSELAGE SKIN WAS BLENDED AND DOUBLER INSTALLED PER REPAIR IAW MD88 SRM 53-04D PARA 57.SDR DALA1210850925Support Fitting · corrodedCORROSION ON RT GEAR SUPPORT FITTING BUSHING BORE I/B SIDE AND NICKS ON LOWER AND UPPER SURFACE, ALSO WEAR ON VERTICAL WALL. REPAIRED PER ERA 500108-14AD ORIG REV.SDR DALA1211940925Fastener · missingDURING HMV LOOSE AND MISSING FASTENERS WERE FOUND ON UPPER AND LOWER ROWS OF FASTENERS ABOVE AND BELOW THE SPLICE AT STATION ZFS=52.26 AT VERTICAL STABILIZER LEADING EDGE. LEADING EDGE SKIN/SPLICE WAS REPAIRED IAW ERA 500113-14AD REV ORIG.SDR DALA1211920925Skin · crackedDURING HMV THREE CRACKS WERE FOUND ON FUSELAGE SKIN AT THE UPPER FWD DOOR JAMB CORNER AND BTW LONGERON 20 AND 21RT OF THE FWD CARGO COMPARTMENT:0.125"LENGTH;0.437" LENGTH AND 0.468 LENGTH. FUSELAGE SKIN WAS REPAIRED IAW ERA 500104-14AD ORIG.SDR DALA1210600925Skin · damagedLIGHTNING STRIKES ON FWD /AFT EDGE OF WINDOW BELT FRAME BTW STA Y=427 AND 446, 465 AND 484, 541 AND 560 AT FUSELAGE SKIN. REPAIRED PER ERA 500106-14 REV ORIG.SDR DALA1210590925Skin · scratchedSCRATCHES ON FUSELAGE SKIN UPPER FORWARD CORNER OF THE WINDOW BELT PANEL BTW STA Y=693 AND Y=712. REPAIRED PER ERA 500106-14 REV ORIG.SDR DALA1210540925Skin · damagedDURING HMV LIGHTNING STRIKE WAS FOUND ON AFT UPPER CORNER IN STA Y=769 AND 750 FUSELAGE SKIN WINDOW BELT FRAME_RT. REPAIRED PER ERA 500111-14.SDR DALA1210530925Structure · damagedDURING HMV LIGHTNING STRIKE WAS FOUND ON FWD LOWER CORNER AND AFT EDGE OF WINDOW BELT FRAME BTW STA Y=731-750 RT. SUPPLEMENT TO N/R T0237100 WITH CORRECTIVE ACTION REPAIRED PER ERA 500111-14.SDR DALA1209310925Skin · corrodedDURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN STA Y=1103-1110 LONGERON 28RT REF MD88 SRM 53-04D FIG 53 FOR REPAIR. CORROSION WAS REMOVED AND ARE WITHIN LIMITS PER SRM53-04D.SDR DALA1209300925Skin · corrodedDURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING STA Y=1084-1089 ON L29L, Y=1124-1133 BTW LONGERON 23-26L, Y=1115 BTW LONGERON 20-21L AND Y=1105 BTW LONGERON 19-20L REF MD88 SRM 53-04D FIG 53 FOR REPAIR. FUSELAGE SKIN WAS SDR DALA1209320925Skin · corrodedDURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING STA Y=1043 AND Y=1060-1068 BTW LONGERON 18-19LT REF MD88 SRM 53-04D FIG 53. FUSELAGE WAS BLENDED OUT AND WITHIN LIMITS REF MD88 SRM 53-0 4D PARA 57.SDR DALA1209290925Skin · corrodedDURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN STA Y=998-1041 BETWEEN LONGERONS 18-17LT. REF MD88 SRM 53-04D FIG 53 FOR REPAIR. FUSELAGE SKIN WAS BLENDED OUT AND WITH LIMITS REF MD88 M 53-04D PARA 57.SDR DALA1209270925Rudder · damagedDAMAGED FLAME SPRAY ON SEVERAL AREAS AT RT RUDDER SURFACE. FLAME SPRAY WAS REPAIRED IAW MD88 SRM 51-70-1AD. 0-1AD PARA 23.SDR DALA1209160925Skin · crackedDURING HMV A CRACK WAS FOUND OF 0.093" ON FUSELAGE SKIN AT STA Y=1212 BTW LONGERON 1 AND 2LT. REPAIRED PER ERA 500114-14AD REV ORIG.SDR DALA1208530925Plate · corrodedHIDDEN DAMAGE; CORROSION AND SCRATCHES ON BARREL NUTS AND HOLES AT RT/LT HORIZONTAL STABILIZER UPPER PLATE AFT EDGE. HORIZONTAL STABLIZER UPPER PLATE WAS REPAIRED IAW ERA 499479-14 REV ORIG.SDR DALA1206630925Skin · corrodedDURING HMV CORROSION WAS FOUND BETWEEN INNER FUSELAGE SKIN AND PRODUCTION DOUBLER STA Y=575 AT MID CARGO COMPARTMENT BETWEEN LONGERON 28L AND 28R. REF ERA 483854-14 REV C FOR REPAIR. REPAIRED PER ERA 500664-14.SDR DALA1206640925Fastener · missingDURING HMV LOOSE AND MISSING FASTENERS WERE FOUND ON UPPER AND LOWER ROWS OF FASTENERS ABOVE AND BELOW THE SPLICE AT STATION ZFS=52.26 AT VERTICAL STABLIZER LEADING EDGE REF EA 09-470871-12.SDR DALA1206560925Panel · debondedDURING HMV DISBONDED CARBON SHEET WAS FOUND ON RT WING GROUND SPOILER PANEL OUTBD EDGE. REF MD-88 SRM 51-70-1B PARA12 FOR REPAIR.SDR DALA1206550925Skin · nickedDURING HMV NICKS WERE FOUND ON EXTERNAL FUSELAGE SKIN ALTERNATE STATIC PORT STA Y=454 BTW LONGERON 27RT AND 28RT REF MD88 SRM 53-04D FIG 12C FOR REPAIR.SDR DALA1206230925Doubler · corrodedDURING HMV CORROSION WAS FOUND ON FUSELAGE SKIN INTERNAL DOUBLE AT STA Y=244 BTW LONGERON 16L TO 17L. DOUBLER WAS REPLACED IAW MD88 SRM 53-04D FIG 12B.SDR DALA1202680925Beam · corrodedDURING HMV CORROSION WAS FOUND ON LOWER DOOR JAMB BEAM FROM STA Y=642-687 AT MID CARGO COMPARTMENT REF MD88 SRM 53-05 FIG 123 FOR REPAIR.SDR DALA1208260925Skin · crackedCRACK EXT FUSELAGE STA 1437 BETWEEN LONGS 4RT AND 5RT DAMAGED AREA TRIMMED OUT. REPAIR DOUBLER AND FILLER WERE INSTALLED IAW DC9/MD80 SRM 53-04D FIG 27. AIR DOUBLER AND FILLER WERE INSTALLED IAW DC9/MD80 SRM 53-04D FIG 27.
Back to N925DL, cancelled Mar 19, 2019