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 I5P2026F00000Apu · inoperativeAPU INOP. REPLACED APU PER TASK CARD.SDR UIEA2026050700305Skin · damagedDURING LIGHTNING STRIKE INSPECTION, FOUND 5EA BURN MARKS ON FUSELAGE SKIN AT STA. 522-544, BTWN STRG 39L-39R. REPAIR PARTS HAVE BEEN INSTALLED AS PER SRM 53-00-01-2R-1, REPAIR 1. REV. 131.SDR UIEA2026051300312Bulb · inoperativeR2 DOOR EMERGENCY LIGHT INOP. RELAMPED R2 DOOR EMERGENCY LIGHT IAW AMM 33-51-03. OPS CHECK GOOD.SDR DALA2026051302987Power Supply · failedDURING SVC CHECK FOUND EPSU UNIT BAD LOCATION (11WL). REPLACED EPSU 11WL IAW AMM 33-51-38 OPS CHECK SATISFACTORY. (LP 8700089 - AIRCRAFT WAS GROUNDED)SDR CALA2026051316220Plate · corrodedL1 DOOR CREASE PLATE AT FLOOR BETWEEN STA 290 TO 345 HAS CORROSION IN NUMEROUS PLACES. L-1 DOOR INNER CHORD CORRODED.REMOVED AND REPLACED. NO ISSUES NOTED. ADD EMP:V947134 REMOVED, LOCATED, DRILLED, AND REPLACED NEW INNER CHORD AT L1 DOOR FLOOR STRUCTURE BETWSDR CALA2026051316216Oil System · leakingPOWER PLANT OIL QUANTITY (01=L ENG, 02=R ENG) ZERO, ENGINE OIL P RESSURE WAS (ZERO, LOW) R ENG OIL QUANTITY AND PRESSURE AT 0 AFTER START. ENGINE OIL WAS 22 PRIOR TO START ENG 2 CREW REPORTED THAT RIGHT ENGINE WAS STARTED WITH NORMAL OIL PRESS / QTY, BUT OIL WSDR CALA2026051316214Strap · crackedBULK COMP, CEILING STRAP SUPPORT AT BS 1661, RBL 24.75 IS CRACKED. REPAIRED FLOORBEAM STABILIZER AT STA 1661 RBL 24.75 IAW B757-20 0 SRM 53-00-51-2R-R DETAIL IV.SDR CALA2026051316212Support Angle · corrodedOTBD SIDE OF RIGHT ECS EXHAUST,BODY FAIRING SUPPORT LWR SURFACE HAS FRETTING CORROSION. REMOVED AND REPLACED SUPPORT ANGLE AT O/B SIDE OF RIGHT ECS EXHAUST, BODY FAIRING REF.SRM 51-40-02-0G-0,AND DWG#149A7214SDR CALA2026051316210Gusset · crackedFWD CARGO BS 500I STR - 25L GUSSET BRACKET BROKEN. REMOVED AND REPLACED FWD CARGO STA 500I STR-25L GUSSET PER SRM 51-40-02-0G-0 AND DWG#143A9481,SDR CALA2026051316208Web · dentedDENTS ON FLIGHT DECK FLOOR AT STA 255 LBL 18 TO RBL 3. 241-002. REPAIR ACCOMPLISHED IN ACCORDANCE WITH SRM 53-10-51-2R-2 PAGE 1-9 FIGURE 202 AND SRM 51-40-02-0G-0 PAGE 1-40 FIGURE 202.SDR CALA2026051216192Engine · no discrepancyPOSSIBLE BIRD STRIKE ON NR 2 ENGINE FAN BLADE AND INTAKE LIP. NO ABNORMAL ENGINE INDICATIONS OR ODORS IN THE FLIGHT DECK. FOUND ON WALK AROUND. ACCOMPLISHED BIRDSTRIKE INSPECTION OF ENGINE 2. NO DAMAGE FOUND WITHIN THE ENGINE OR ON THE FAN BLADES. NO INGESTSDR CALA2026051216191Filter · dirtyDURING INSPECTION FOR POSSIBLE ODOR COMING INTO CABIN, FOUND EXCHANGE FILTER FOR ZONAL DRYING SYSTEM CLOGGED/ DIRTY REMOVED AND REPLACED EXCHANGE FILTER TO ZONAL DRYING SYSTEM IAW AMM 21-70-00-400-801-C2. OPS CHK GOOD.SDR DALA2026051302986Terminal · damagedON THE GROUND WHILE ON APU GOT STRONG BURNING SMELL, LOST ELEC POWER. WE SHUT DOWN APU. NO SMOKE OR FIRE INDICATION. T/S FOUND APU TERMINAL DAMAGED. RECIRC FANS AND E/E COMPARTMENT AND CABINS GALLEY OVEN COFFEEMAKER AND LAV HEATERS ALL CHKS GOOD. RAN BOTH ENGISDR DALA2026051302985Oil System · leakingDESCENDING THROUGH 4000 CA AND FO BOTH BEGAN TO SMELL A DIRTY SOCK FUME. THE SMELL BECAME STRONGER AND SLIGHTLY MORE ACRID DURING THE REMAINDER OF THE DESCENT. FWD FA'SQUIRED BUT DID NOT SMELL THE ODOR. UPON LANDING THE COCKPIT WINDOWS WERE OPENED AND THE ODORSDR SCNA20260513197Battery Pack · inoperativeAFT R/H SECTION OF EMERGENCY LIGHTS INOP - - R/R AFT R/H BATTERY PACK IAW AMM 33-51-06-960-805. OPS CHECK GOOD AT THIS TIMESDR SCNA20260513196Girt Bar · no discrepancyFA REPORTS DIFFICULTY WITH UNSEATING FWD ENTRY GIRT BAR FROM HANGER DURING ARMING PROCEDURE - - REMOVED AND INSTALLED GIRT BAR SMOOTH OPERATION IAW AMM 25-66-01SDR DALA2026051302981Floor Support · corrodedLEVEL 2 CORROSION, A319 TASK 5320-6010, CPCP 2021-2001. PAX CABIN, AFT SECTION, FLOOR STRUCTURE AT FR68 Y-765MM, LONGITUDINAL BEAM WITH CORROSION. C/A: REPLACED LONGITUDINAL BEAM P/N: D5347219320000 IAW A319 SRM 51- 72-11-911-001 REV 157.00 DATED 15/PR/26. (LPSDR DALA2026051302980Hydraulic System · lowAT APPX 70KTS "HYD SYS B LO PRESS" ECAM WARN MESSAGE.REJECTTED TAKE OFF. FOUND BLUE SYST ACCUM VERY LOW.SERVICED SAME PER A320 AMM 29-14. PERFORMED OP CHECK OF BLU SYST BUT FOUND THAT ACCUM HAD LEAKED OUT MOST OF ITS PRE CHARGE.DETERMINED ACCUMULATOR BAD.REPLSDR 2026FA0000360Frame · gouged9V-OJB IS IN THE HANGAR FOR “C” CHECK BETWEEN 21 APR TO 09 JUN2026. WHILE PERFORMING ADSI IB78S550001 INSPECTION, FOUND GOUGE IN VTP TENSION BOLT #6 HOLE ALUMINIUM CROWN FRAME AT 2 O’CLOCK (VIEWING UPWARDS). DIMENSION APPROX CIR LENGTH: 10.0MM AND HEIGHT 5.0MMSDR 2026FA0000357Stiffener · shearedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF AND/OR CRACKEDSDR VNAA20260512038Skin · crackedCRACK WAS FOUND ON EXTERNAL SKIN LH UPPER ENGINE TRANSCOWL. CRACK WAS FOUND ON EXTERNAL SKIN LH UPPER ENGINE TRANSCOWL WAS REPAIRED PER REO 670-54-21-1818 REV. -A.SDR VNAA20260512037Acoustic Panel · crackedIN REF TO NRC 0254 AFTER REMOVAL OF COAMING LATCH CRACK ON ACUSTIC PANEL WAS FOUND UPPER LH TRANSCOWL. ACOUSTIC PANEL WAS FOUND UPPER LH TRANSCOWL WAS REPAIRED PER REO PER REO 670-54-21-1818 REV. -A.SDR VNAA20260512036Intercostal · corrodedAFTER CORROSION REMOVAL REWORKED AREA ON INTERCOSTAL STGR 21LH BTW FS=310 TO FS= 333 WAS FOUND OUT OF LIMITS E/E BAY. CORROSION ON INTERCOSTAL STGR 20LH BTW FS=319 TO FS= 333 (FWD E/E BAY) WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01, WAS EVALUATED, THERESDR VNAA20260512035Fitting · corrodedCORROSION ON BORE LUG L2, L5 AND L6 AT LH AILERON CENTRAL FITTINGS. HINGE FITTING AILERON LH BORE LUGS L2, L5 AND L6 WERE REPAIRED PER REO 670-57-61-237 REV - .SDR VNAA20260512034Fitting · corrodedCORROSION ON LUG BORES ON R3 AND R5 AT RH AILERON CENTRAL FITTING. CORROSION ON LUG BORE R5 AT RT AILERON CENTRAL FITTING WAS REPAIRED PER REO 670-57-61-237 REV:-- AND LUG R3 WAS CLEANING PER SRM 51-26-00-001-001-A01 CLEANING.-.SDR VNAA20260512033Fitting · gougedGOUGE ON LATERAL FACE OF LUG R1 AND R2 AT RH AILERON CENTRAL FITTINGS. LATERAL FACE OF LUG R1 AND R2 AT RH AILERON CENTRAL FITTINGS WERE REPAIRED PER REO 670-57-61-237 REV -SDR VNAA20260512032Angle · crackedCRACK ON OUTBD ANGLE ON CROSSBEAM FS 280 LBL-12 AT PAX CABIN FLOOR STRUCTURE. ANGLE WAS REPLACED ON CROSSBEAM FS 280 LBL-12 AT PAX CABIN FLOOR STRUCTURE PER CRJ700 SRM 51-42-21-001-001-A01.SDR VNAA20260512031Support · crackedCRACKS ON DIAPHRAGM SUPPORT (ABOVE DOOR NET STRUCTURE) OF AFT BAGGAGE BAY STRUCTURE. DIAPHRAGM SUPPORT (ABOVE DOOR NET STRUCTURE) OF AFT BAGGAGE BAY STRUCTURE WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01 PAR. AND SRM 51-41-02- 001-001-A01.SDR VNAA20260512030Skin · corrodedDURING EXTERNAL ZONAL INSPECTION OF THE REAR FUSELAGE: FS977.00 TO FS1098.00, ABOVE WL72.50, SEVERAL DENTS WERE FOUND ON EXTERNAL FUSELAGE SKIN BTW FS1015.00 TO FS1069.00 BTW STGR27 TO STGR 22 RH. AFTER REMOVAL OF PAINT, DVI WAS PERFORMED PER CRJ-700 NDT PARTSDR VNAA20260512029Structure · corrodedCORROSION ON SETTLEMENT SUPPORT STRUCTURE AT AFT C-CHANNEL ALONG AFT WING-TO-FUSELAGE FAIRING (196DR). SETTLEMENT SUPPORT STRUCTURE (STRAP) WAS REPLACED PER CRJ-700 SRM 51-42-10-001-001-A01.SDR VNAA20260512028Seat Track · corrodedCORROSION ON SEAT TRACK OF FS 582.00 TO FS 669.00 AND RBL 9 OF THE FUSELAGE FLOOR STRUCTURE. CORROSION ON SEAT TRACK OF FS 582.00 TO FS 669.00 AND RBL 9 OF THE FUSELAGE FLOOR STRUCTURE WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND THEREFORE OUT OF LIMSDR VNAA20260512027Seat Track · corrodedCORROSION ON SEAT TRACK OF FS 486.00 TO FS 581.00 AND LBL 9 OF THE FUSELAGE FLOOR STRUCTURE. CORROSION ON SEAT TRACK OF FS 486.00 TO FS 581.00 AND LBL 9 OF THE FUSELAGE FLOOR STRUCTURE. AT PASSENGER CABIN WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01, WAS SDR VNAA20260512026Intercostal · crackedCRACK ON INTERCOSTAL, TIRE BURST COVER BEHIND PANEL 542AZ OF LH WING. INTERCOSTAL, TIRE BURST COVER BEHIND PANEL 542AZ OF LH WING WAS REPLACED PER CRJ-700 SRM 51-42-21-001-001-A01 PAR.6.C AND SRM 51-42-13-001-001-A01 PAR.6.C AND SRM 51-42-06-001-001-A01 PAR.SDR JR2R20260512738Skin · chafedRIGHT ENGINE CORE COWL 427AL EXTERIOR SKIN HAS CHAFE MARKS. REPAIRSDR VNAA20260512025Seat Track · corrodedCORROSION WAS FOUND AT SEAT TRACK ON FS 364.00 TO 469.00 LBL 25 OF THE FUSELAGE FLOOR STRUCTURE. SEAT TRACK ON FS 364.00 TO 469.00 LBL 25 OF THE FUSELAGE FLOOR STRUCTURE WERE REPLACED PER CRJ700 AMM 53-00-49-400-801 (CONFIG A03)SDR VNAA20260512024Floorbeam · corrodedCORROSION ON BRACKETS FLOOR BEAM AT FS 284.00 RBL16 AND RBL36, ON BRACKET FLOOR BEAM FS 295.00 AND RBL 5 OF THE FUSELAGE FLOOR STRUCTURE. FLOORBEAM TEE REMOVED PER SRM 51-21-06-001-001-A01 AND AREAS IS OUT LIMITS PER CRJ700 SRM 53-21-43-101-001-A01 AND SRM 53SDR VNAA20260512023Bracket · crackedCRACK ON OXYGEN SERVICE PANEL BRACKET (LOWER AFT CORNER) AT FWD FUSELAGE. PANEL BRACKET ON OXYGEN SERVICE (LOWER AFT CORNER) AT FWD FUSELAGE WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01 "SDR VNAA20260512022Angle · corrodedAFTER REMOVAL OF MIDCAP ANGLE, CORROSION ON KICKPLATE ANGLE WAS FOUND AT SURROUND STRUCTURE OF PASSENGER DOOR. CORROSION ON KICKPLATE ANGLE WAS FOUND AT SURROUND STRUCTURE OF PASSENGER DOOR WAS REMOVED PER SRM 51-21-06-001-001-A01 AND AREA WAS FOUND OUT LIMISDR VNAA20260512021Angle · crackedCRACK ON ANGLE OF SETTLEMENT AREA OF ACCESS PANEL 642AZ (ATTATCHED TO REAR SPAR) AT RH WING. ANGLE OF SETTLEMENT AREA OF ACCESS PANEL 642AZ (ATTATCHED TO REAR SPAR) AT LH WING. WAS REPLACED PER SRM 51-42-21-001-001-A01.SDR VNAA20260512020Angle · crackedCRACK ON ANGLE OF SETTLEMENT AREA OF ACCESS PANEL 542AZ (ATTATCHED TO REAR SPAR) AT LH WING. ANGLE OF SETTLEMENT AREA OF ACCESS PANEL 542AZ (ATTATCHED TO REAR SPAR) AT LH WING. WAS REPLACED IAW SRM 51-42-21-001-001-A01.SDR VNAA20260512019Frame · crackedCRACK ON LH UPPER/LOWER THRUST REVERSER TORQUE BOX FWD FRAME AT LH ENGINE. LT UPPER/LOWER THRUST REVERSER TORQUE BOX FWD FRAME AT LH ENGINE.WERE REPAIRED PER REO 670-54-22-154 REV-- AND REO 670-54-22-155 REV-.SDR VNAA20260512018Support Beam · chafedCHAFE DAMAGE UPPER/LOWER CASCADE SUPPORT BEAM AT LT/RT ENGINE. CHAFE DAMAGE UPPER/LOWER CASCADE SUPPORT BEAM AT LH/RH ENGINE WERE REPAIRED PER REO 670-54-22-160 REV- -, REO 670-54-22-161 REV- -. REO 670-54-22-159 REV- -. AND PER REO 670-54-22-162 REV- -.SDR ABXA20260512196Charger · malfunctionedDURING TAXI OUT,LE SLAT ASYM CAUTION MSG AND LIGHT ON AFTER START CHECKLIST. SEEMS TO HAPPEN WHEN SELECTING APU OFF WHILE FLAPS ARE IN TRANSIT.A/C RETURNED TO THE GATE AND MTX GROUNDED A/C MTX T/S LE SLAT ASYM MSG PER B767 FIM 27-81 FT 809 FOUND MAIN BATTERY ISDR VNAA20260512017Angle · crackedCRACKED INTERNAL ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT STRUCTURE. ANGLE OF EXTERNAL POWER RECEPTACLE SUPPORT WAS REPLACED PER SRM 51-42-06-001-001-A01.SDR VNAA20260512016Striker · corrodedCORROSION ON LOWER STRIKER OF CARGO DOOR SURROUND STRUCTURE. REPLACED PER CRJ 700 SRM 51-42-21-001-001-A01.SDR DALA2026051202974Spar Web · crackedDURING TEST FLIGHT SPOILER ACTUATOR, CRACKED REAR SPAR WEB STA XRS=295-324 AT LT WING. REPAIRED PRI 633829-14 REV 8 AND ER/A 633829-14 (1589343) (AIRCRAFT GROUNDED)SDR IPXA2026051241708Warning Message · illuminatedAIR TURN BACK, FWD CARGO DOOR MESSAGE ILLUMINATED IN CLIMB OUT. DEFERRED PER MEL 52-71-1-1B. PLACARD INSTALLED.SDR JR2R20260512855Doubler · corrodedFWD WET AREA FWD RH DOUBLER BETWEEN FR12 AND FR14 CORRODED. REPLACEDSDR 2026F00105Wedge · corrodedDURING SANDING OF THE RH WING FOR PAINT REFURBISHMENT, FOUND CORROSION ON RH WING OUTBOARD TRAILING EDGE STRUCTURE NEAR WS 257.47. AFTER EVALUATION, IT WAS DETERMINED THAT THE RH WING TRAILING EDGE WEDGE IS OUT OF LIMITS AND REQUIRES REPLACEMENT.SDR DALA2026051202970Oxygen Mask · unwanted deploySEAT 22C - O2 GENERATOR PANEL DROPPED. RE-PACKED MASKS IAW AMM 35-21. OK FOR SERVICE. (8716434) AIRCRAFT WAS GROUNDED.