Service difficulty reports

1,771,708 reports of malfunctions and defects, newest first. Air carriers must report; general aviation reporting is voluntary.

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'
  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.

SDR DALA2026042002499Bottle · low pressureDOOR ASSIST BOTTLES @ 1R, 2L & 4R NEED SERVICING. SERVICED DOOR ASSIST BOTTLES PER A330 52-15. (8162926)Apr 18, 2026 · N431DX · Airbus A330941 · Passenger/Crew DoorsSDR DALA2026042002498Seat Track · corrodedCORROSION FOUND ON LH AFT SEAT TRACK YC1. REPLACED SEAT TRACK PER A330 SRM 51-72-11-911-001. (1550959) AIRCRAFT WAS GROUNDED.Apr 18, 2026 · N414DZ · Airbus A330941 · Fuselage, Seat/Cargo Attach FittingsSDR N6WA2026042006Display · failedBOTH MFDS FAILED ON CLIMBOUT. SWAPPED CAPT'S MFD WITH EICAS SCREEN 2 PER CRJ 550 AMM 31-61-01 AND PERFORMED OPS CHECK OF ALL. DISPLAY SCREENS IAW AMM 31-61-01 ALL SCREENS OPS CHECK OK, AIRCRAFT OK FOR SERVICE.Apr 18, 2026 · N506GJ · Cndair CL6002C11 · Central DisplaySDR IPXA2026042066017Hinge · inoperativeDOOR HINGE COVER NOT RETRACTING REMOVED AND REPLACED CREW DOOR LOCK LATCH COVER HINGE. OPS CHECK GOOD. REMOVED AND REPLACED CREW DOOR LOCK LATCH COVER HINGE. OPS CHECK GOOD.Apr 18, 2026 · N367UP · Boeing 767300 · Passenger/Crew DoorsSDR IPXA2026042071044Control Panel · inoperativeRT FWD WINDOW HEAT INOPERATIVE. INOP LIGHT WILL NOT TEST BUT WHEN SELECTED OFF, WILL ILLUMINATE., REMOVED AND REPLACED WINDOW HEAT CONTROL PANEL PER AMM 30-41-02. ACCOMPLISHED FLIGHT COMPARTMENT WINDOW ANTI-ICING SYSTEM-OPERATIONAL TEST PER AMM 30-41-00-715-Apr 18, 2026 · N361UP · Boeing 76734AF · Windshield/Door Rain/Ice RemovalSDR IPXA2026042067251Cover · brokenFWD CREW DOOR HAS BROKEN SLIDE ARM/DISARM COVER APPROVEDApr 18, 2026 · N163UP · Airbus A300F4622R · Escape SlideSDR DALA2026042002495Hydraulic Line · damagedR SYSTEM HYDRAULIC QUANTITY DROPPED TO .16 RF AND RT HYD SYS PRESS EICAS MSG DISPLAYED AFTER LANDING. R THRUST REVERSER WOULD NOT STOW. R/R HYD FLEX LINE FOR THR PER B757 AMM 78-31. AND SERVICE L/R HYD PER B757 AMM 12-12. LEAK CHK GOOD. CLOSED RT THR PER B75Apr 18, 2026 · N697DL · Boeing 757232 · Hydraulic System, MainSDR AALA202604204448Girt Bar · looseAIRCRAFT WAS NOT GROUNDED: FOWARD SERVICE DOOR 1R LIFE RAFT ARMED BRACKET LOOSE. TIGHTENED GIRT BAR CLIP.Apr 18, 2026 · N998NN · Boeing 737823 · Emergency EquipmentSDR AALA202604201125Life Vest · missingAIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTING MISSING LIFE VEST FROM EMERGENCY CABIN BIN. RESTOCKED LIFE VESTS. PER AMM 25-64-00.Apr 18, 2026 · N855NN · Boeing 737823 · Life JacketSDR AALA202604201442Sign · detachedAIRCRAFT WAS NOT GROUNDED: EXIT SIGN NEAR ROW 16 CAME LOOSE AND IS HANGING. REINSTALLED THE ISLE CENTER CEILING MOUNTED EMERGENCY EXIT SIGN ASSEMBLY AT THE OVER WING EMERGENCY EXITS. PER AMM 33-51-01.Apr 18, 2026 · N952AA · Boeing 737823 · Emergency LightingSDR AALA202604205094Sign · missingAIRCRAFT WAS NOT GROUNDED: EXIT SIGN IN MIDDLE OF CABIN OVER EXIT ROW MISSING. REPLACED EXIT SIGN. PER AMM 33-51-01.Apr 18, 2026 · N966AN · Boeing 737823 · Emergency LightingSDR AALA202604205782Light · no testAIRCRAFT WAS NOT GROUNDED: ALL EMERGENCY LIGHTING INOPERATIVE. FOUND THE AFT FLIGHT ATTENDANT EMERGENCY LIGHT SWITCH OFF CAUSING THE EMERGENCY LIGHTS NOT TO ENGAGE FROM THE FLIGHT DECK. PERFORMED THE EMERGENCY LIGHTS OPERATIONAL TEST. PER AMM 33-51-00. OPS CHEApr 18, 2026 · N338RS · Boeing 7378 · Emergency LightingSDR AALA202604201426Elec Connector · disconnectedAIRCRAFT IN BASE MAINTENANCE: EMERGENCY AISLE LIGHT AT LEFT HAND SEAT ROW 19 INOPERATIVE. T/S EMERGENCY AISLE LIGHT AT SEAT ROW 19, PER B737NG WDM 33-51-13. FOUND CONNECTOR D11100 DISCONNECTED BEHIND OVERHEAD BINS AT LEFT HAND SEAT ROW 19 AND 20. RECONNECTED CApr 18, 2026 · N987AN · Boeing 737823 · Light System WiringSDR CALA2026042015514Oven · odorOVEN 205 HAD STRONG BURNING ODOR COMING FROM IT. STOPPED USING. CHECKED OUT NO ODOR NOTED, PULLED BREAKER. OVEN 205, WAS OFF AND THERE WAS NO ODOR NOTED. R & R G22/205 OVEN IAW AMM 25-32-03, OPS CHECK GOOD, NO ODOR NOTICED.Apr 18, 2026 · N37445 · Boeing 7379 · Buffet/GalleysSDR CALA2026042015512Battery Pack · no testEMERGENCY LIGHT BATTERY PACK M33097,ABOVE DR 2R CTR, FAILED DEEP CAPACITY TEST. EMER LIGHT BATTERY PACK (M33097) REPLACED IAW AMM 33-51-06. INSTALLATION TEST PERFORMED IAW AMM 33-51-06 SATISFACTORY.Apr 18, 2026 · N2142U · Boeing 777300ER · Emergency LightingSDR CALA2026042015487Reservoir · overservicedEXHAUST FUMES ODOR FROM AFTER START UNTIL AFTER LANDING. NOTICED ODOR WHEN ENTERING ACFT. TROUBLESHOT IAW FIM 21-00 TASK 830, FOUND HYD RESERVIOR OVERSERVICED. PERFORMED ENGINE RUN AS PERCAUTIONARY. NO FURTHER FUMES NOTED.Apr 18, 2026 · N17302 · Boeing 7378 · Hydraulic Reservoir, MainSDR CALA2026042015483Floorbeam · corrodedON THE FLOOR STRUCTURE CABIN PAX, PRESSURE DECK AREA WAS FOUND THE FITTING WITH CORROSION AT BS 977, RBL95, WL 189. PERFORMED INTERIM REPAIR OF THE RT BS 977 FRAME AT WL 190 OTBD CHORD CORROSION IAW ECRA 5310-08324, PART 1, IT IS NECESSARY TO ACCOMPLISH THE PApr 18, 2026 · N655UA · Boeing 767322 · Fuselage Main, Floor BeamSDR CALA2026041915479Lamp · inoperativeEMERGENCY LIGHTS - GENERAL VISUAL INSPECTION PROCEDURE. SLIDE EMERGENCY LIGHT DOOR 1R. INOP REPLACED THE LAMPS 1R SLIDE EMERGENCY LIGHT, REF AMM 33-51-06. OP CHECK GOOD.Apr 18, 2026 · N75858 · Boeing 757324 · Emergency LightingSDR ABXA20260418168Fire Loop · warning messageDURING CREW PRE-FLIGHT CHECK, L ENG O/H LP2 STATUS MESSAGE ON GRD. MAINTENANCE DEFERRED IAW MEL 26-11-2-1. C/W MAINT PROCEDURES, PLACARD INSTALLED MBCB 4/28/2026. A/C REMAINS ETOPS 120. AIRCRAFT RETURNED TO SERVICE.Apr 18, 2026 · N371CM · Boeing 767338 · Fire DetectionSDR N6WA2026042004Floor Support · corrodedCORROSION ON FLOOR SILL AT FS280-FS319. REMOVED AND REPLACED RH SILL AT FS280-319.00 IAW CRJ SRM 51-42-06.Apr 18, 2026 · N583GJ · Cndair CL6002C11 · Fuselage Miscellaneous StructureSDR DALA2026042002485Pump · failedDECLARED EMERGENCY DUE TO HYD PUMP 2B FAIL. REPLACED HYD PUMP 2B, RT EDP AND RUDDER PCU. R & R CASE DRAIN FILTER, PRESSURE FILTER ELEMENT, HYDRAULIC LINE AND O-RING. REPLACED PRESSURE COIL LINE OF THE MIDDLE PCU. OPS CHECK OKAY. (LP# 8717840; AIRCRAFT WAS GRApr 18, 2026 · N102DU · Airbus BD5001A10 · Hydraulic Pump (Electric/Engine), MainSDR SWAA2026042090850Slide · out of limitsFWD SERVICE DOOR ESCAPE SLIDE PRESSURE OUT OF LIMITS. REPLACED FWD SERVICE DOOR ESCAPE SLIDE IAW MT 725-61-06.Apr 18, 2026 · N8324A · Boeing 7378H4 · Escape SlideSDR SCNA20260420160Girt Bar · out of adjustR1 GIRT BAR BRACKET IS TOO TIGHT. ADJUSTED GIRT BAR TENSION ON R1 DOOR RE. AMM 25-66-00.Apr 18, 2026 · N814SY · Boeing 7378BK · Emergency EquipmentSDR DALA2026042002470Web · corrodedCORROSION WEB FRAME 16 RH SIDE AT FWD GALLEY AREA. REPLACED WEB, LOC. BTW FR12 TO 16 RH SIDE AT FWD GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11 AND DWG D53112780, & DWG D53918884. TOOK MEASURES OF CORROSION ON WEB ARE: L= 3.832IN W=1.570 IN. (LP: 1551636). AApr 18, 2026 · N336NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2026042002469Seat Track · crackedCORRODED SEAT TRACK -Y1292 LOCATED AT FR 66 AT AFT GALLEY AREA. REPLACED SEAT TRACK -Y1292 LOC BTW FR64 TO FR66 AT AFT GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11, AND DWG 10N01036. TOOK MEASURE CORROSION WERE: L: 0.620 INCH, W: 0.450 INCH, D: 0.035 INCH, (LApr 18, 2026 · N336NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026042002468Fitting · crackedCRACKED FITTING. LOCATED BTW FR 11 TO FR 12 AND -Y 765 IN COCKPIT. REPLACED FITTING (1 EA) LOCATED BTW FR 11 TO FR 12 AND -Y 765 IN COCKPIT TOOK MEASURES OF CRACK L:0.468 INCH IAW SRM 51- 42-11, SRM 51-72-11, AND DWG D53110097. (LP: 1551630). AIRCRAFT WAS Apr 18, 2026 · N336NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2026042002463Repair · not reportedREMOVE EXISTING EXTERNAL REPAIR LOCATED BTWN FR1 AND FR3 STRG 34R AND RT LOWER STRG AND PERFORM VISUAL INSPECTION OF THE UNDERLYING STRUCTURE. REPAIRED R/H NOSE FWD FUSELAGE SKIN BETWEEN FRI-FR3 BETWEEN STRG -34R-36R I/A/W DELTA ER/A 633282-14AD REV: ORIGINAL Apr 18, 2026 · N325NB · Airbus A319114 · Fuselage Main, Plate/SkinSDR DALA2026041902459Sensor · inoperativeDECLARED EMERGENCY DUE LANDING GEAR NOT EXTENDING ON FIRST ATTEMPT DURING THE APPROACH. GEAR EXTENDED AFTER CYCLING THE HANDLE. MAINTENANCE IN PROGRESS. LP: 8339716) AIRCRAFT WAS GROUNDEDApr 18, 2026 · N370NW · Airbus A320212 · Landing Gear Position and WarningSDR R61A2026041800108Skin · crackedDURING OVERNIGHT MAINTENANCE A CRACK WAS FOUND IN THE RH WING SKIN AT SPAR II RIB 4. REPAIR WAS PREFORMED IAW EMB ETD 2026-170-006470. CRACK CUT OUT, FILLER INSTALLED, AND NEW DESIGN DOUBLER INSTALLED.Apr 18, 2026 · N857RW · Emb ERJ170200LR · Wing, Plate/SkinSDR IXXA2026041801Web · damagedPUNCTURE DAMAGE ON THE WEB FRONT SPAR LOCATED ON THE RIGHT WING SLAT #12Apr 18, 2026 · N227AZ · Boeing 767323 · Wing Miscellaneous StructureSDR JR2R20260418660Floor Support · corrodedL/H FLOOR SILL AT FR16 LBL40 IS CORRODED. REPLACED PER SRM.Apr 18, 2026 · N89313 · Emb ERJ170200LL · Fuselage Miscellaneous StructureSDR JR2R20260418652Floorbeam · corrodedFR14 CROSSBEAM BETWEEN RBL11-RBL24 IS CORRODED. REPAIRED PER SRM.Apr 18, 2026 · N89313 · Emb ERJ170200LL · Fuselage Main, Floor BeamSDR JR2R20260418674Floorbeam · corrodedFWD WET AREA FLOOR SUPPORT AT FR14 RBL14 IS CORRODED. REPLACED PER SRM.Apr 18, 2026 · N89313 · Emb ERJ170200LL · Fuselage Main, Floor BeamSDR VNAA20260418022Skin · dentedTOOL MARKS AND DENTS ON SETTLEMENT AREA OF VENTRAL FIN FAIRINGS BTW FS 997 TO FS1162, STGRS 21LH-22LH AND BTW STRGS 21RH-22RH. REPAIRED PER PER REO 690-53-61-1762 REV. - - AND REO 690-53-61-1761 REV - -Apr 18, 2026 · N605NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA20260418021Skin · dentedTOOL MARKS AND DENTS ON SETTLEMENT AREA OF VENTRAL FIN FAIRINGS BTW FS 1162 TO REAR SPAR DATUM 67.50%, STGRS 21LH-22LH AND BTW STRGS 21RH-22RH. TOOL MARKS AND DENTS ON SETTLEMENT AREA OF VENTRAL FIN FAIRINGS BTW FS 1162 TO REAR SPAR DATUM 67.50%, STGRS 21LH-Apr 18, 2026 · N605NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA20260418020Retainer · corrodedDURING TO AFTER REMOVE THE TORN PRESSURE SEAL ON MAIN AVIONICS COMPARTMENT DOOR, CORROSION WAS FOUND ON FWD & AFT SEAL RETAINERS. SEAL RETAINERS FWD & AFT ON MAIN AVIONICS COMPARTMENT DOOR WERE REPLACED PER SRM 51-42-06-001-001-A01Apr 18, 2026 · N605NN · Cndair CL6002D24 · Cargo/Baggage DoorsSDR VNAA20260418019Fitting · corrodedCORROSION FLOOR FITTING P/N 9331091-3 IN FWD ACCESS 109 (1EA) ON GALLEY 1. FLOOR FITTING P/N 9331091-3 IN FWD ACCESS 109 (1EA) ON GALLEY 1 WAS REPLACED PER CMM 25-33-21Apr 18, 2026 · N605NN · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR VNAA20260418018Fitting · corrodedCORROSION FLOOR FITTING IN FRONT ACCESS 107 (1EA) ON GALLEY 1. FLOOR FITTING IN FRONT ACCESS 107 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-21Apr 18, 2026 · N605NN · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR VNAA20260418017Web · corrodedWEAR AND CORROSION ON WEB BTW STGR 26L TO 25L AND FS 517.00 TO FS 565.00 ALSO STGR 26L TO 25L & FS 629.00 TO FS 661.00+ 16.00 AT FWD AND CENTER BAGGAGE BAY DOOR AREA. WEB BTW STGR 26L TO 25L AND FS 517.00 TO FS 565.00 ALSO STGR 26L TO 25L AND FS 629.00 TO FSApr 18, 2026 · N605NN · Cndair CL6002D24 · Fuselage Main, StructureSDR VNAA20260418016Seat Track · wornWEAR ON SIDE SEAT TRACK BTW BS 533 AND 549, STGR 15L. EVALUATED, DUE TO EXCESS DAMAGE ALONG THE ON SIDE SEAT RAIL BTW FS533.00 AND FS549.00 STGR 15L AT CAB PAX PER SRM 53-31-49-101-001-A02 AND REPLACED PER AMM 53-00-49.Apr 18, 2026 · N605NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20260418015Rib · crackedCRACK ON MACHINED RIB OF LEADING EDGE SS15.50 AT RH WING. MACHINED RIB OF LEADING EDGE SS15.50 AT RH WING WAS REPAIRED PER REO 690-57-41-587 REV. --Apr 18, 2026 · N605NN · Cndair CL6002D24 · Wing, Rib/BulkheadSDR IXX2026F00006Frame · corrodedCORROSION EVIDENCE NOTED AT APU COMPARTMENT DOOR 315AL (L/H SIDE) INTERNAL SIDE FRAME STA 1840.2 CLOSE TO I/B EDGE REFERENCE XTREME WO 014592 NRC 905Apr 18, 2026 · N255CM · Boeing 767223 · Auxiliary Power Unit (APU) DoorsSDR VNAA20260418014Rib · crackedCRACK ON MACHINED RIB OF LEADING EDGE SS58.41 AT RH WING. CRACK ON MACHINED RIB OF LEADING EDGE SS58.41 AT RH WING WAS REPAIRED PER REO 690-57-41-240 REV. - -Apr 18, 2026 · N605NN · Cndair CL6002D24 · Wing, Rib/BulkheadSDR VNAA20260418013Rib · crackedCRACK ON MACHINED RIB OF LEADING EDGE SS57.16 AT LH WING. MACHINED RIB OF LEADING EDGE SS57.16 AT LH WING WAS REPAIRED PER GREO 690-57-41-240 REV. --Apr 18, 2026 · N605NN · Cndair CL6002D24 · Wing, Rib/BulkheadSDR VNAA20260418012Bracket · crackedCRACKS ON SUPPORT BASE MAIN BATTERY DIRECT BUS AT FWD EQUIPMENT COMPARTMENT. SUPPORT BASE MAIN BATTERY DIRECT BUS AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ 900 SRM 51-42-06-001-001-A01.Apr 18, 2026 · N605NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA20260418011Web · crackedCRACK ON WEB BTW FS195 TO FS205 AND WL79.50 INTERNAL STRUCTURE AT FWD EQUIPMENT COMPARTMENT. CRACK ON WEB BTW FS195 TO FS205 AND WL79.50 INTERNAL STRUCTURE AT FWD EQUIPMENT COMPARTMENT. WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01.Apr 18, 2026 · N605NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA20260418010Bracket · crackedCRACK FWD ANGLE SUPPORT (2EAS) ON ACUMULATOR AT INTERNAL NOSE HYD COMPARTMENT. CRACK FWD ANGLE SUPPORT (2EAS) ON ACUMULATOR AT INTERNAL NOSE HYD COMPARTMENT WERE REPLACED PER CRJ900 SRM 51-42-21-001-001-A01 AND SRM 51-41-02-001-001-A01.Apr 18, 2026 · N605NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA20260418009Beam · crackedCRACK ON LONGITUDINAL BEAM RBL12 FS280. CRACK ON LONGITUDINAL BEAM RBL12 FS280.00 WAS REPAIRED PER REO 690-53-11-2163 REV. --Apr 18, 2026 · N605NN · Cndair CL6002D24 · Fuselage Main, StructureSDR VNAA20260418008Stiffener · crackedCRACK ON UPPPER STIFFENER ATTACHED TO POWER-ASSIST MOTOR BTW DATUM 4 AND DATUM 5 (AFT SIDE PANEL) OF PASSENGER DOOR INTERNAL STRUCTURE. (SM). UPPER STIFFENER ATTACHED TO POWER-ASSIST MOTOR BTW DATUM 4 AND DATUM 5 (AFT SIDE PANEL) OF PASSENGER DOOR INTERNAL STApr 18, 2026 · N605NN · Cndair CL6002D24 · Passenger/Crew DoorsSDR VNAA20260418007Hinge · gougedGOUGE ON LUG OF THE PIANO HINGE (DOOR SIDE) AT PASSENGER DOOR. :PIANO HINGE (DOOR SIDE) AT PASSENGER DOOR WAS REPLACED PER CRJ900 SRM 52-11-01-201-007-A01Apr 18, 2026 · N605NN · Cndair CL6002D24 · Fuselage, Door Hinge