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.
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
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 DALA2026042002499Bottle · low pressureDOOR ASSIST BOTTLES @ 1R, 2L & 4R NEED SERVICING. SERVICED DOOR ASSIST BOTTLES PER A330 52-15. (8162926)SDR 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.SDR 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.SDR 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.SDR 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-SDR IPXA2026042067251Cover · brokenFWD CREW DOOR HAS BROKEN SLIDE ARM/DISARM COVER APPROVEDSDR 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 B75SDR AALA202604204448Girt Bar · looseAIRCRAFT WAS NOT GROUNDED: FOWARD SERVICE DOOR 1R LIFE RAFT ARMED BRACKET LOOSE. TIGHTENED GIRT BAR CLIP.SDR AALA202604201125Life Vest · missingAIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTING MISSING LIFE VEST FROM EMERGENCY CABIN BIN. RESTOCKED LIFE VESTS. PER AMM 25-64-00.SDR 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.SDR AALA202604205094Sign · missingAIRCRAFT WAS NOT GROUNDED: EXIT SIGN IN MIDDLE OF CABIN OVER EXIT ROW MISSING. REPLACED EXIT SIGN. PER AMM 33-51-01.SDR 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 CHESDR 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 CSDR 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.SDR 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.SDR 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.SDR 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 PSDR 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.SDR 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.SDR N6WA2026042004Floor Support · corrodedCORROSION ON FLOOR SILL AT FS280-FS319. REMOVED AND REPLACED RH SILL AT FS280-319.00 IAW CRJ SRM 51-42-06.SDR 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 GRSDR SWAA2026042090850Slide · out of limitsFWD SERVICE DOOR ESCAPE SLIDE PRESSURE OUT OF LIMITS. REPLACED FWD SERVICE DOOR ESCAPE SLIDE IAW MT 725-61-06.SDR SCNA20260420160Girt Bar · out of adjustR1 GIRT BAR BRACKET IS TOO TIGHT. ADJUSTED GIRT BAR TENSION ON R1 DOOR RE. AMM 25-66-00.SDR 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). ASDR 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, (LSDR 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 SDR 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 SDR 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 GROUNDEDSDR 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.SDR IXXA2026041801Web · damagedPUNCTURE DAMAGE ON THE WEB FRONT SPAR LOCATED ON THE RIGHT WING SLAT #12SDR JR2R20260418660Floor Support · corrodedL/H FLOOR SILL AT FR16 LBL40 IS CORRODED. REPLACED PER SRM.SDR JR2R20260418652Floorbeam · corrodedFR14 CROSSBEAM BETWEEN RBL11-RBL24 IS CORRODED. REPAIRED PER SRM.SDR JR2R20260418674Floorbeam · corrodedFWD WET AREA FLOOR SUPPORT AT FR14 RBL14 IS CORRODED. REPLACED PER SRM.SDR 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 - -SDR 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-SDR 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-A01SDR 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 25-33-21SDR 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 25-33-21SDR 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 FSSDR 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.SDR 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. --SDR 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 905SDR 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. - -SDR 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. --SDR 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.SDR 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.SDR 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.SDR VNAA20260418009Beam · crackedCRACK ON LONGITUDINAL BEAM RBL12 FS280. CRACK ON LONGITUDINAL BEAM RBL12 FS280.00 WAS REPAIRED PER REO 690-53-11-2163 REV. --SDR 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 STSDR 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-A01