Service difficulty reports

1,770,704 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 CALA2026083119015Strap · crackedRIGHT BS 597 INBD STUB BEAM STRAP LOWER AFT FASTENER HOLE HAS A CRACK INDICATION. R & R STUB BEAM STRAP ASSY IAW DWG 144A1703, REV A.Aug 28, 2026 · N23707 · Boeing 737724 · Fuselage Miscellaneous StructureSDR CALA2026083119013Stub Beam · crackedRIGHT BS 616, STUB BEAM 2ND FROM FWD LOWER FASTENER HOLE HAS VISIBLE DAMAGE. R & R STUB BEAM STRAP ASSY IAW DWG 144A1704, REV C.Aug 28, 2026 · N23707 · Boeing 737724 · Fuselage Miscellaneous StructureSDR CALA2026083119011Attach Angle · crackedCRACKED LT VAPOR BARRIER UPPER ATTACH ANGLE, LBL 40. COMPLETED INSTALLATION OF LT VAPOR BARRIER UPPER ATTACH ANGLE IAW SRM 51-40-02-0G-0, & DWG 111A1000.Aug 28, 2026 · N39415 · Boeing 737924ER · Fuselage Main, Attach FittingsSDR DALA2026083104903Seat Track · corrodedCORROSION ON BASE OF SEAT TRACK STA 1640 RBL24 & 48. DAMAGED AREA REPLACED PER B757-300 SRM 51-40-02(1782451)(AIRCRFT GROUNDED)Aug 28, 2026 · N591NW · Boeing 757351 · Fuselage, Seat/Cargo Attach FittingsSDR AALA202608306543Battery Pack · inoperativeAIRCRAFT WAS GROUNDED: WHILE ACCOMPLISHING JC72L00005043 STEP21(B) EPL OPS CHECK FOUND SEAT 2H, 3H, 4H, 5H FWD LIGHTS INOP. MAINTENANCE REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ALL CHECKS OK IAW AMM 33-51-06.Aug 28, 2026 · N789AN · Boeing 777223 · Emergency LightingSDR AALA202608300988Slide Raft · defectiveAIRCRAFT WAS NOT GROUNDED: THERE IS WHAT LOOKS LIKE AND UNCONNECTED WIRE AT THE BOTTOM LEFT OF THE L1 DOOR HANGING OUT. MAINTENANCE REPLACED L1 DOOR SLIDE IAW JOB CARD 08L22125001.Aug 28, 2026 · N962NN · Boeing 737823 · Escape SlideSDR DALA2026083004887Engine · power lossRTO- DUE TO NR 1 ENGINE WOULD NOT MAKE T/O POWER WITH THRUST REVERSER FAULT AND THRUST LEVER DISAGREE. CREW REJECTED AT LOW SPEED. TROUBLESHOOTING IN PROGRESS. (LP: 9489017, AIRCRAFT WAS GROUNDED)Aug 28, 2026 · N343NW · Airbus A320212 · Engine (Turbine/Turboprop)SDR ABXR2026082800015Support · corrodedCORROSION ON THE CUTOUT/ SUPPORT STRUCTURE FOR PANEL 195ML, AT THE LEFT UPPER FILLET AREA, AS VIEWED WITH DOOR OPEN. REMOVED CORROSION FROM PNL 195ML'S SUPPORT STRUCTURE, LH UPR FILLET AREA LOST .037 FROM .080 MATERIAL IS FOUND TO BE OUT OF LIMITS. REPAIRED INAug 28, 2026 · N1373A · Boeing 76731K · Fuselage Structure (General)SDR ABXR082800014Stiffener · crackedSTA. 246 FLOORBEAM HAS CRACKED VERTICAL STIFFENER AT LBL 43 IN LEFT TUNNEL OF MEC .REPAIRED VERTICAL STIFFENER AT STA 246 FLOORBEAM LBL 43 IN LEFT TUNNEL OF MEC IAW B767-300 SRM 53-10-51 REPAIR 3 TABLE 1.Aug 28, 2026 · N1373A · Boeing 76731K · Fuselage Miscellaneous StructureSDR ABXR082800013Stiffener · crackedSTA. 246 FLOORBEAM HAS A CRACKED VERTICAL STIFFENER ON FWD SIDE AT LBL 28 IN LEFT TUNNEL OF MEC . REPAIRED VERTICAL STIFFENER ON FWD SIDE FLOORBEAM OF STA 246 LBL 28 IN LEFTTUNNEL OF MEC IAW B767-300 SRM 53-10-51 REPAIR 3 TABLE 1.Aug 28, 2026 · N1373A · Boeing 76731K · Fuselage Miscellaneous StructureSDR AALA202608282199Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: RIGHT FORWARD EMERGENCY EXIT DOOR (843) INDICATES LOW PRESSURE. REQUIRES SERVICING. MAINTENANCE SERVICED RIGHT FORWARD EMERGENCY EXIT DOOR (843) PER AMM 52-22-00.Aug 28, 2026 · N142AN · Airbus A321231 · Emergency ExitsSDR 2026F00189Slide Raft · malfunctionedDURING THE SCHEDULED TIME-CHANGE OF THE L1 DOOR ESCAPE SLIDE/RAFT ON N276GX AT ALEXANDRIA (AEX), MAINTENANCE PERSONNEL FOUND THE TRANSPORTATION (SHIPPING) SAFETY PIN STILL INSTALLED FROM THE UNIT'S PRIOR INSTALLATION AT MIAMI (MIA). WITH THE PIN INSTALLED, THEAug 28, 2026 · N276GX · Airbus A320214 · Escape SlideSDR QR9R2026082800001Reu · failedWHILE AT HOVER, COMM #2 WOULD NOT TRANSMIT FROM COPILOTS STATION, NO SIDE TONE OR TX INDICATED PILOTS STATION COULD XMIT BUT EXTREMELY GARBLED. RETURNED TO PARKING, AVIONICS ADJUSTED RADIO COMM AND CHECKED OK UNTIL ATTEMPT TO HOVER, THEN FAILED AGAIN. REMOVED Aug 28, 2026 · Bolkms BK117C2 · Communications SystemSDR IPXA2026082867237Handle · bindingENTRY DOOR EXTERIOR HANDLE TAKES EXCESSIVE FORCE TO OPEN.Aug 28, 2026 · N630UP · Boeing 7478F · Passenger/Crew DoorsSDR FDEA202608281248Strut · crackedNR 2 NACELLE STRUT, RIGHT SIDE SKIN, THROUGH ACCESS 443AR, SHOWS A CRACK WITH NO VISIBLE STOP HOLE. THIS ITEM HAS BEEN ACCOMPLISHED ON EA F-5430-T0388382 P1.Aug 28, 2026 · N993FD · Boeing 7572Q8 · Nacelle/Pylon, Main FrameSDR FDEA202608281247Skin · debondedLEFT WING INBD T/E MAIN FLAP, AFT PANEL, REAR EDGE HAD DEBONDING. APPLIED PERMANENT REPAIR ON THE LT WING FLAP AFT PANEL IAW SRM 57-53-01-2R, REP 1, DETAIL I, FIG 201, SHEET 2, IAW IAW SRM 51-70-10-2R, REP 4.Aug 28, 2026 · N993FD · Boeing 7572Q8 · Trailing Edge FlapsSDR FDEA202608281246Window · arcedAFTER INITIATING DESCENT FROM FL300, WITH PRESENCE OF ST. ELMO S FIRE, L1 WINDOW ARCING OCCURRED FOLLOWED BY SHATTERING. QRH ACTIONED AND EMERGENCY DECLARED. REMOVED AND REPLACED L1 WINDSHIELD IAW AMM 56-11-01-4-0 SECTION E, STEP 13, FIRST TORQUE APPLIED SECAug 28, 2026 · N963FD · Boeing 75728A · Flight Compartment WindowsSDR FDEA202608281245Skin · dentedFOUND LT WING, T/E, OTBD FLAP LOWER SURFACE, HAD ONE DENT AT CROSS OTEF, 315 INCHES AND T/E 5 INCHES. REPAIRED LH WING T/E O/B FLAP LOWER SURFACE 01 EA DENT AT CROSS OTEF 315 INCHES AND T/E 5 INCHES AS PER B777 SRM 57-53-01-2R-2 FIGURE 201-204 AND SRM 51-70Aug 28, 2026 · N840FD · Boeing 777F · Trailing Edge FlapsSDR FDEA202608281244Extinguisher · dischargedWHEN ACFT WAS TOWED INTO GATE AND MX INSP. FOUND NR 1 CARGO FIRE BOTTLE DISCHARGED. AMM: 26-23-02-4 R & R NR 1 CARGO FIRE BOTTLE AND TEST IAW MM 26-23-02-4 WITH SAT RESULTS, OK FOR SERVICE.Aug 28, 2026 · N995FD · Boeing 7572Q8 · Fire Bottle, FixedSDR FDEA202608281243Skin · noneEXISTING REPAIR AT FUSELAGE SKIN - MAIN DECK CARGO DOOR CUTOUT - FORWARD LOWER CORNER STATION 623.065, LONGERON 27 LEFT HAND. EXISTING REPAIR AT FUSELAGE SKIN - MAIN DECK CARGO DOOR CUTOUT - FORWARD LOWER CORNER STATION 623.065 LONGERON 27 LEFT HAND EVALUAAug 28, 2026 · N617FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA202608281242Skin · noneEXISTING REPAIR AT FUSELAGE SKIN AT STATION 1894 TO STATION 1914 LONGERON 47 LEFT HAND TO LONGERON 50 RIGHT. FUSELAGE SKIN AT STATION 1894 TO STATION 1914 LONGERON 47 LEFT HAND TO LONGERON 50 RIGHT HAND CARRIED OUT REPAIR IN ACCORDANCE WITH EA 1-5330-T03Aug 28, 2026 · N617FE · Doug MD11F · Fuselage Main, Plate/SkinSDR DALA2026082804885Lamp · inoperativeSEAT 30 H/J EMERGENCY LIGHT INOP. REPLACED LAMP ASSEMBLY PER AMM 33-51. OK FOR SERVICE. (9189034) AIRCRAFT WAS GROUNDED.Aug 28, 2026 · N802NW · Airbus A330323 · Emergency LightingSDR DALA2026082804884Lamp · inoperativeSEAT 33H/J EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP ASSEMBLY IAW AMM 33-51. OK FOR SERVICE. (9189035) AIRCRAFT WAS GROUNDED.Aug 28, 2026 · N802NW · Airbus A330323 · Emergency LightingSDR DALA2026082804881Control Rod · out of adjustL1 DOOR (FAULTS). REMOVED L1 DOOR SLIDE ON AMDS W/C 2560-4425. REMOVED L1 DOOR LINING IAW AMM 52-11-31. ADJUSTED L1 DOOR UPPER GATE CONTROL ROD AND CONTROL ROD TO UPPER LATCH TORQUE TUBE PER B737 AMM 52-11-00. REINSTALLED L1 DOOR LINING IAW AMM 52-11-31. REIAug 28, 2026 · N826DN · Boeing 737932ER · Passenger/Crew DoorsSDR IXXA2026082800002Cowling · out of toleranceNR 1 ENGINE INBD CORE COWL GAPS ARE OUT OF LIMITS ON TRAILING EDGE IAW AMMAug 28, 2026 · N761CX · Boeing 767223 · Nacelle/Pylon, Main FrameSDR IXXA2026082800001Cowling · out of toleranceNR 1 ENGINE OTBD CORE COWL GAPS ARE OUT OF LIMITS ON TRAILING EDGE IAW AMM.Aug 28, 2026 · N761CX · Boeing 767223 · Nacelle/Pylon, Main FrameSDR SWIA2026082777804Skin · dentedDURING BIRD STRIKE INSPECTION, FOUND UPPER NOSE SKIN, BS 202. 75, SUBZONE 221-212, UNDER CO-PILOT WINDSHIELD TO BE DENTED MEASURING 6875 IN HEIGHT, 8375 IN WIDTH, AND HAVING A DEPTH OF 0114. DAMAGE IS GOING ACROSS AIRCRAFT STRINGER AND RIVETS, NO SHARP EDGES Aug 27, 2026 · N717EV · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR SWIA2026082777803Skin · dentedDURING BIRD STRIKE INSPECTION, FOUND ON THE RT SIDE RVSM AREA, BS 235, SUBZONE 212, NEXT TO RT PITOT-STATIC TUBE TO BE DAMAGED FROM IMPACT IMPACT OR DENT FOUND TO MEASURE 4228 IN HEIGHT, 346 IN WIDTH WITH A DEPTH OF 145. DAMAGED AREA INCLUDES RIVETED STRINGERAug 27, 2026 · N717EV · Cndair CL6002C11 · Fuselage Main, Plate/SkinSDR REXA2026102001968Doubler · crackedCRACK ON THE PULL IN CAM DOUBLER ON FRAME 338 BTWN MEMBER UPPER EDGE AND INTERCOSTAL DD1 ON THE PAX DOOR. PULL IN CAM DOUBLER WAS REPLACED IAW SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01, & SRM 51-42-13-001-001-A01.Aug 27, 2026 · N479PX · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2026102001967Panel · crackedCRACKED DOOR STAIR, AFT SIDE PANEL ON BOTTOM STEP AREA OF THE PAX DOOR. THE DOOR STAIR AFT SIDE PANEL ON BOTTOM STEP AREA WAS REPAIRED IAW SRM 52-11-04-201-004-A01.Aug 27, 2026 · N479PX · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2026102001965Support Angle · corrodedCORRODED FWD SUPPORT ANGLE BTWN INTERCOSTAL DD4 AND INTERCOSTAL DD6 AT THE PASSENGER DOOR. SUPPORT ANGLE WAS REPAIRED IAW EA CRJ952-23231, REV IR.Aug 27, 2026 · N479PX · Cndair CL6002D24 · Passenger/Crew DoorsSDR REXA2026102001964Structure · crackedCRACKED TOP EDGE MEMBER AT THE LT AFT EMERGENCY EXIT DOOR. THE TOP EDGE MEMBER WAS REPAIRED IAW REO 670-52-21-103, REV -.Aug 27, 2026 · N479PX · Cndair CL6002D24 · Emergency ExitsSDR REXA2026102001963Drag Angle · crackedCRACKED VERTICAL STABILIZER TO FUSELAGE LT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO 67.5% REAR SPAR DATUM. THE VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.Aug 27, 2026 · N479PX · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026101601932Floorbeam · corrodedAFTER FLOORBEAM REMOVAL IAW NRC 200, THE LT FLOORBEAM AT FS280 WAS FOUND CORROSION. THE FLOORBEAM WAS REPLACED IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, & SRM 51-42-22-001-001-A01.Aug 27, 2026 · N296PQ · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026101601888Hinge · corrodedSECONDARY NRC FROM RC 900-27-900-910: AFTER LT AILERON BUSHINGS REMOVAL, WEAR ON L1, L2, L3, L4, L5, & L6 LUG BORE AT LH AILERON. LUG BORES L1, L2, L5 AND L6 AT LH AILERON WERE REPAIRED PER REO 670-57-61-237 REV - - & LUG BORES L3 AND L4 AT LH AILERON WERE REAug 27, 2026 · N296PQ · Cndair CL6002D24 · AileronsSDR JR2R20260827633Floorbeam · corrodedFWD CABIN FLOOR ATTACH ANGLE AT APPROX RBL30 AT THE AFT SIDE OF FR12 IS CORRODED. REPLACEDAug 27, 2026 · N89357 · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR HNAA2026101500988Doubler · gougedPILOTS' BULKHEAD UPPER OTBD GUIDE PIN HOLE IS GOUGED. INSTALLED THE NEW FABRICATED DOUBLER AND SACRIFICIAL PLATE FOR THE REPAIR ON PILOTS' BULKHEAD UPPER OTBD GUIDE PIN HOLE IAW EMB 145 SRM 53-21-02 ITEM 4 FIG. 204 AND PIEDMONT EO1-53-26-0443.Aug 27, 2026 · N670AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026101500987Shear Tie · crackedSHEAR TIE IS CRACKED AT FR 68 BETWEEN STGR. 6L AND 7L. RAR SHEAR TIE AT FR 68 BETWEEN STGR 6L AND 7L IAW EMB 145 SRM 53-31-04RE FIGURE 205.Aug 27, 2026 · N670AE · Emb EMB145LR · Fuselage Internal Mounting StructureSDR HNAA2026101500986Shear Tie · crackedSHEAR TIE IS CRACKED AT FRAME 16 BETWEEN STRINGERS 15R-16R. R & R SHEAR TIE AT FRAME 16 BETWEEN STRINGERS 15R-16R IAW EMB 145 SRM 51-40-02.Aug 27, 2026 · N670AE · Emb EMB145LR · Fuselage Internal Mounting StructureSDR HNAA2026101500985Shear Tie · crackedSHEAR TIE IS CRACKED AT FRAME 15 BETWEEN STRINGERS 15R-16R. R & R SHEAR TIE AT FRAME 15 BETWEEN STRINGERS 15R-16R IAW EMB 145 SRM 51-40-02.Aug 27, 2026 · N670AE · Emb EMB145LR · Fuselage Internal Mounting StructureSDR HNAA2026100900967Gusset · corrodedRIGHT CROSSBEAM GUSSET HAS CORROSION AT FR57. REMOVED AND REPLACED RT CROSSBEAM AT FR 57 IAW SRM 51-40-02.Aug 27, 2026 · N670AE · Emb EMB145LR · Fuselage Main, StructureSDR HNAA2026100900974Floor Support · corrodedPAX ENTRYWAY FWD FLOOR SUPPORT HAS CORROSION. REMOVED AND REPLACED PAX ENTRYWAY FWD FLOOR SUPPORT IAW SRM 51-40-02.Aug 27, 2026 · N670AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026100900973Floor Support · corrodedRIGHT FLOOR SUPPORT HAD CORROSION AT MULTIPLE LOCATIONS FROM FR52-59. RAR CENTER FUSELAGE IV RT FLOOR SILL IAW EMB 145 SRM 51-40-02.Aug 27, 2026 · N670AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026100900972Floor Support · corrodedLEFT FLOOR SUPPORT HAD CORROSION AT FR 57. R & R CENTER FUSELAGE IV, THE LT FLOOR SUPPORT NR 7 IAW IAW SRM 51-40-02.Aug 27, 2026 · N670AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026100900971Shear Tie · corrodedTHERE IS CORROSION ON A SHEAR TIE, IN-LINE WITH FR65, STR 20-21L. R & R SHEAR TIE IN-LINE WITH FR65 AT STR 20-21L IAW SRM 51-40-02.Aug 27, 2026 · N670AE · Emb EMB145LR · Fuselage Internal Mounting StructureSDR HNAA2026100900969Floor Support · corrodedL3 OTBD FLOOR SUPPORT CORRODED. R & R L3 OTBD FLOOR SUPPORT IAW SRM 51-40-02.Aug 27, 2026 · N670AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026100900968Floor Support · corrodedLEFT NR 4 OTBD FLOOR SUPPORT CORRODED. R & R L4 OTBD FLOOR SUPPORT IAW SRM 51-40-02.Aug 27, 2026 · N670AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026100900697Gusset · corrodedRH CROSSBEAM GUSSET HAS CORROSION AT FR57. REMOVED AND REPLACED RH CROSSBEAM AT FR 57 IAW SRM 51-40-02.Aug 27, 2026 · N670AE · Emb EMB145LR · Fuselage Main, StructureSDR HNAA2202610090096Gusset · corrodedRH CROSSBEAM GUSSET HAS CORROSION AT FR 57. REMOVED AND REPLACED RT CROSSBEAM AT FR 57 IAW SRM 51-40-02.,Aug 27, 2026 · N670AE · Emb EMB145LR · Fuselage Main, StructureSDR HNAA2026100500947Angle · crackedRIGHT WING STUB, FUSE TO WING BOX ANGLE CRACKED AT FR 46. R & R ANGLE IAW SRM 51-40-02Aug 27, 2026 · N653AE · Emb EMB145LR · Aerodynamic Fairings