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 CALA2026081118458Light · detachedEMERGENCY LIGHT AT SEAT 28C HAS FALLEN OFF. REMOVED AND REPLACED 28C EMERGENCY LIGHT BOX. OPS CKS GOOD.Aug 10, 2026 · N24706 · Boeing 737724 · Emergency LightingSDR CALA2026081118456Aileron · contaminatedOUTBOARD LT AILERON. THERMOGRAPHIC INSPECTION FOUND WATER INGRESSION INSIDE INBOARD EDGE (STA 910.45). CONSIDERED MAJOR REPAIR. ALL THE STEP OF THE REPAIR WERE ACCOMPLISHED IAW EC/RA 5760-01153.Aug 10, 2026 · N66051 · Boeing 767424ER · AileronsSDR CALA2026081118454Wire · detachedOPERATIONAL TEST OF EMERGENCY LIGHTING SYSTEM. EMERGENCY EXIT SIGN OVER OVERWING EXIT 20A NOT ILLUMINATING. WIRE HAS COME AWAY FROM RING TERMINAL X1. NEW RING TERMINAL CRIMPED ON WIRE W834-012-18 OF L700 EXIT SIGN, LEFT OVER-WING HATCH STA 916, WL 260, LBL Aug 10, 2026 · N667UA · Boeing 767322 · Light System WiringSDR CALA2026081118452Power Supply · damagedONE BANK OF EMERGENCY LIGHTS STAY ILLUMINATED, ROW 22..27 WITNESSED AISLE LIGHTS TURN ON UNCOMMANDED & OFF UNCOMMANDED AFTER A FEW MINS. BATTERY PACKS ARE CHARGED. IAW FIM 33-50 TASK 801. REF IPC 33-51-06-22A. CHKD POWER SUPPLY & BATTERY M1671 IAW AMM 32-09Aug 10, 2026 · N69830 · Boeing 737924ER · Emergency LightingSDR DALA2026081004615Structure · separatedAFTER LANDING, CREW WAS INFORMED THAT A PIECE OF RT TRAILING EDGE FLAP DEPARTED THE ACFT ON ROTATION, VISUAL INSPECTION AFTER PARKING CONFIRMED PART OF FLAP WAS MISSING. FLAP 25 TAKEOFF. R & R OTBD FLAP ASSY IAW AMM 27-51. (8592099) AIRCRAFT WAS GROUNDED.Aug 10, 2026 · N895DN · Boeing 737932ER · Trailing Edge FlapsSDR DALA2026081004611Sign · looseFWD CABIN EXIT SIGN LOOSE. SECURED FWD CABIN EXIT SIGN IAW AMM 33-51. (8801968) AIRCRAFT WAS GROUNDED.Aug 10, 2026 · N921AT · Boeing 717200 · Emergency LightingSDR WX0A2026081032916Bulb · inoperative(AIRCRAFT NOT GROUNDED) LIGHT BULB IN EMERGENCY EXIT LIGHT AT SEAT 16A DOES NOT ILLUMINATE. REMOVED AND REPLACED OVERWING EXIT LIGHT ASSY OPS CHECK GOOD REF 33-21-00-960-802 THIS CLEARS MEL 33-21-01-CAT C MDDR #236344 INOP PLACARD REMOVED.Aug 10, 2026 · N810MG · Boeing 7378200 · Emergency LightingSDR JR2R20260810776Receptacle · chafedL1 DOOR OUTER HANDLE BOX CHAFED INSIDE OF BOX BELOW HANDLE. REPAIRAug 10, 2026 · N86309 · Emb ERJ170200LR · Passenger/Crew DoorsSDR JR2R20260810812Ramp · nickedL1 DOOR BOTH FWD AND AFT DOOR COMMAND RAMPS HAVE MINOR NICKS. REPAIRAug 10, 2026 · N86309 · Emb ERJ170200LR · Fuselage Main, StructureSDR JR2R20260810811Ramp · nickedL1 DOOR BOTH FWD AND AFT DOOR COMMAND RAMPS HAVE MINOR NICKS. REPAIRAug 10, 2026 · N86309 · Emb ERJ170200LR · Fuselage Main, StructureSDR DALA2026081004599Seat Track · corrodedCORROSION SEAT TRACK -Y765 BTW FR64 TO FR66 AT AFT GALLEY AREA (SSI 5 34147). REPLACED SEAT TRACK -Y765 AND FASTENERS LOC. BTW FR64 TO FR66, AS PER SRM 51-72-11, A321 SRM 51-42-11, DWG D53472909, ISSUE: K, AND D53472903, ISSUE: Q. (LP 1748028 - AIRCRAFT WAS Aug 10, 2026 · N107DN · Airbus A321211 · Fuselage, Seat/Cargo Attach FittingsSDR ABXA20260810352Oxygen Bottle · low pressureDURING CREW PREDEPARTURE CHECK, EICAS PRESSURE INDICATION INOP READING 40 PSI. DEFERRED EICAS O2 PRESSOR INDICATION PER MEL 35-11-2-1 MX PROCEDURES COMPLY WITH PLACARD INSTALLED RE-INSPECT O2 PRESSURE BEFORE EA FLIGHT MUST BE COMPLY BY AUG 13, 2026. A/C RETURNAug 10, 2026 · N1361A · Boeing 76731B · Crew Oxygen SystemSDR 2026FA0000633Mixer Box · failedSHORTLY AFTER REACHING CRUISE ALTITUDE OF FL410, AN AUDIBLE POP WITH ASSOCIATED RISE IN CABIN PRESSURE OCCURRED. CREW DESCENDED AND CABIN ALTITUDE AMBER CAS DISPLAYED AND QRH WAS ACCOMPLISHED. ACM O'HEAT AND HEAT EXCHG ONLY DISPLAYED UNTIL QRH PROCEDURE CLEAREAug 10, 2026 · N853Q · Textrn TEXTRON700 · Cabin Cooling SystemSDR FDEA202608101103Seat Track · wornMAIN DECK CARGO COMPARTMENT SEAT TRACK AT BETWEEN BS 695 - 715, X = - 47.5 FOUND CROWN WORN. MAIN DECK CARGO COMPARTMENT WORN CROWN AT SEAT TRACK BS 695 - 715, X = - 47.5, EVALUATED AND FOUND EXCEEDED LIMT IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1Aug 10, 2026 · N605FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202608101102Skin · dentedRIGHT WING OTBD FLAP LWR SURFACE 30 INCHES IB OF NR 7 FLAP SUPPORT FAIRING AND 5 INCHES FROM T/E FOUND DENTED. REPAIRED RHW OB FLAP LWR SURFACE 30 INCHES IB OF #7 FLAP SUPPORT FAIRING AND 5 INCHES FROM T/E DENT AS PER B777 SRM 57-53-01-2R-2 FIGURE 201-204 AAug 10, 2026 · N867FD · Boeing 777F · Trailing Edge FlapsSDR JR2R20250810221Hinge Bracket · gougedRIGHT ELEVATOR HINGE #3 ON HORIZONTAL GOUGED AT O/B SIDE. OUT OF LIMITS. REPAIRED.Aug 10, 2026 · N86311 · Emb ERJ170200LL · Elevator StructureSDR JR2R20250810220Hinge Bracket · gougedR/H ELEVATOR HINGE #2 ON HORIZONTAL GOUGED AT O/B SIDE. OUT OF LIMITS. REPAIRED.Aug 10, 2026 · N86311 · Emb ERJ170200LL · Horizontal Stabilizer StructureSDR CALA2026081018430Battery Pack · no testFOUND R4 FLASHLIGHT NOT TESTING. REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-01, OPS CHECKED OKAug 10, 2026 · N2142U · Boeing 777300ER · Emergency EquipmentSDR IPXA2026102299324Bracket · crackedLH WING, FIXED LEADING EDGE INTERNAL STRUCTURE, ANGLE BRACKET INSIDE FLAP KRUEGER COMPARTMENT HAS A CRACK. LOCATED AND DRILLED NEW ANGLE BRACKET IAW SRM 51-40-44-001.Aug 9, 2026 · N147UP · Airbus A300F4622R · Wing, Control Surface Attach FittingsSDR IPXA2026092998707Fitting · crackedRH FR40 CWB UPPER SKIN TENSION BOLT JUNCTION. MIDDLE FASTENER HOLE (SECOND FROM TOP) HAS MULTIPLE CRACK INDICATIONS THROUGHOUT HOLE. REAMED HOLE "B" (MIDDEL) AT FR 40 R/H 0.6140" IAW A300-600 SRM 57-10-24, FIG 206 SHEET#2, AND SRM 51-40-44. INSTALLED BOLT P/N:Aug 9, 2026 · N147UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026100799313Stiffener · crackedLH WING, FIXED LEADING EDGE INTERNAL STRUCTURE, STIFFENER INSIDE FLAP KRUEGER COMPARTMENT HAS A CRACK .INSTALLED NEW STIFFENER AT INSIDE FLAP KRUEGER COMPARTMENT IAW SRM 51-40-21. REVIEWED.Aug 9, 2026 · N147UP · Airbus A300F4622R · Leading Edge DevicesSDR IPXA2026100692769Plate · crackedNR 2 PYLON RH SIDE PANEL SUPPORT BETWEEN 422DR AND 424CR HAS CRACKED PLATE. NEW FISH PLATE INSTALLED IAW A300-600 SRM 51-40-21. REVIEWED.Aug 9, 2026 · N147UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR SIMA20260809008Seat Track · corrodedSSI 53-10-027: FWD GALLEY LH SEAT TRACK DOUBLER CORRODED. (MAJOR REPAIR) (LEVEL 2 CORROSION) RAR DOUBLER AND FILLER ON FWD GALLEY LH SEAT TRACK IAW ERJ 170 SRM 53-10-10/REPAIR 01P.Aug 9, 2026 · N749BM · Emb ERJ170100SE · Fuselage, Seat/Cargo Attach FittingsSDR SIMA20260809006Floorbeam · corrodedFWD GALLEY CROSBEAM CORRODED BTWN RH FLOOR BEAM AND SERV DOOR CUTOUT AT FR 1. (MAJOR REPAIR). INSTALLED REPAIR PARTS (FILLER & INNER DOUBLER) ON FWD GALLEY CROSSBEAM FR 17 IAW ERJ-170 SRM 53-00-10 RE03.Aug 9, 2026 · N749BM · Emb ERJ170100SE · Fuselage Main, Floor BeamSDR SIMA20260809007Seat Track · corrodedSSI 53-10-027: RH LWR SEAT TRACK CORRODED BTWN FR 17-18. (LVL 2 CORROSION) (MAJOR REPAIR). RAR RH LOWER #1 SEAT TRACK BEAM IAW ERJ 170 SRM 51-40-08.Aug 9, 2026 · N749BM · Emb ERJ170100SE · Fuselage Main, StructureSDR REXA2026092101857Latch · crackedFWD LAV SERVICING DOOR TOP HINGE AND BOTTOM LATCH BROKEN TOP HINGE AND BOTTOM LATCH AT FWD LAV SERVICING DOOR WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ9-00 SRM 51-41-02-001-001-A01.Aug 9, 2026 · N480PX · Cndair CL6002D24 · Service DoorsSDR REXA2026092101856Hinge · crackedFWD LAV SERVICING DOOR TOP HINGE AND BOTTOM LATCH BROKEN TOP HINGE AND BOTTOM LATCH AT FWD LAV SERVICING DOOR WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ9-00 SRM 51-41-02-001-001-A01.Aug 9, 2026 · N480PX · Cndair CL6002D24 · Fuselage, Door HingeSDR REXA2026092101831Floorbeam · corrodedRT BS 280 BEAM HAS CORROSION UNDER UPPER SPLICE STRIP. BLENDED CORROSION ON RT BEAM UNDER UPPER SPLICE STRIP IAW SRM 51-21-06-001-001-A01 & FOUND TO HAVE 100% MATERIAL LOSS. BEAM REQUIRES REPLACEMENT. LOCATED & DRILLED NEW SERVICEABLE RT CROSSBEAM IAW SRM 5Aug 9, 2026 · N549CA · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR REXA2026092101830Floorbeam · corrodedLT FS280 BEAM HAS CORROSION ON FWD SIDE UNDER J-ANGLE. BLENDED CORROSION ON LH FS280 BEAM UNDER J-ANGLE & UNDER UPPER SPLICE STRIP IAW SRM 51-21-06-001-001-A01 & FOUND TO HAVE 100% MATERIAL LOSS. LT 280 BEAM REQUIRES REPLACEMEMNT. INSTALLED UPPER SPLICE STRIP Aug 9, 2026 · N549CA · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR SIMA20260809004Shear Panel · corrodedCENTER SHEAR PANEL LOCATED FROM FR87 TO FR88 CROSSBEAMS IS CORRODED. (LEVEL 2 CORROSION). R & R CENTER SHEAR PANEL LOCATED FROM FR87 TO FR88 CROSSBEAMS IAW SRM 51-40-08.Aug 9, 2026 · N749BM · Emb ERJ170100SE · Fuselage Miscellaneous StructureSDR SIMA20260809005Shear Panel · corrodedRH SHEAR PANEL LOCATED FROM FR87 TO FR88 CROSSBEAMS IS CORRODED. (LEVEL 2 CORROSION) R & R RT SHEAR PANEL LOCATED FROM FR87 TO FR88 CROSSBEAMS IAW ERJ 170 SRM 51-40-08Aug 9, 2026 · N749BM · Emb ERJ170100SE · Fuselage Main, StructureSDR AALA202609175155Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: FWD CARGO RH TRANSITION PANEL 500C-500E MULTIPLE AREAS OF CORROSION AT FASTENER HOLES. INSTALLED NEW RH TRANSITION PANEL IAW IPC 53-42-11-11 AND AARD 51-00-05-1.Aug 9, 2026 · N905AN · Boeing 737823 · Fuselage Miscellaneous StructureSDR AALA202609154414Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: FWD CARGO LEFT TRANSITION PANEL 500A-500C MULTIPLE AREAS OF GALVANIC CORROSION AT FASTENER HOLES. INSTALLED OF NEW LT TRANSITION PANEL AND SPLICE IAW IPC 53-42-11-11 AND AARD 51-00-05-1 AND SRM 53-00-53-2R-5.Aug 9, 2026 · N905AN · Boeing 737823 · Fuselage Miscellaneous StructureSDR AALA202609152914Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: FWD CARGO- LT TRANSITION PANEL 500C-500I MULTIPLE AREAS OF EXFOLIATION CORROSION AT FASTENER HOLES. NEW L/H TRANSITION PANELAug 9, 2026 · N905AN · Boeing 737823 · Fuselage Miscellaneous StructureSDR AALA202609152091Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: FWD CARGO RH TRANSITION PANEL 500E-500I MULTIPLE AREAS OF CORROSION AT FASTENER HOLES. INSTALLED NEW RH TRANSITION PANEL IAW IPC 53-42-11-11 AND AARD 51-00-05-1.Aug 9, 2026 · N905AN · Boeing 737823 · Fuselage Miscellaneous StructureSDR REXA2026091101805Angle · crackedCRACKS ON UPPER ANGLES (FIRE PROTECTION KIT 2EAS) FWD CORNERS AT FWD/CENTER BOTH BAGGAGE BAY DOORS. UPPER ANGLES (FIRE PROTECTION KIT 2EAS) FWD CORNERS AT FWD/CENTER BOTH BAGGAGE BAY DOORS WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND 51-42-13-001-001-Aug 9, 2026 · N930XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026091101804Angle · crackedCRACKS ON UPPER ANGLES (FIRE PROTECTION KIT 2EAS) FWD CORNERS AT FWD/CENTER BOTH BAGGAGE BAY DOORS. UPPER ANGLES (FIRE PROTECTION KIT 2EAS) FWD CORNERS AT FWD/CENTER BOTH BAGGAGE BAY DOORS WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND 51-42-13-001-001-Aug 9, 2026 · N930XJ · Cndair CL6002D24 · Cargo/Baggage DoorsSDR IPXA2026082799311Bracket · crackedLEFT CENTER FLAP, OTBD FACE, AFT BRACKET BROKEN. REMOVED AND REPLACED ONE BRACKET AT LT CENTER FLAP, OTBD FACE IAW SRM 51-40-21-001.Aug 9, 2026 · N147UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026083199328Structure · chafedLEFT WING, FIXED LEADING EDGE INTERNAL STRUCTURE, RIVETS AND STRUCTURE ABOVE THE PNEUMATIC DUCT HAVE CHAFE MARKS. REMOVED WEB AT LH WING LEADING EDGE INTERNAL STRUCTURE IAW SRM 51-40-21-001. INSTALLED NEW WEB AT LT WING LEADING EDGE INTERNAL STRUCTUR IAW SRM Aug 9, 2026 · N147UP · Airbus A300F4622R · Wing Main, Frame StructureSDR REXA2026090401772Frame · corrodedSTRINGER 21L CORRODED FWD OF BS 319. REMOVED CORROSION FROM FS319 BETWEEN STR 21L AND STR 20L IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS MEASUREMENTS OF REWORKED AREAS IAW NDTM PART 1, 51-20-004-270-A01, REV-37. FOUND LOWEST REMAINING THICKNESS TO Aug 9, 2026 · N810SK · Cndair CL6002D24 · Fuselage Main, FrameSDR SWAA2026090143085Support Angle · crackedCRACKED SUPPORT ANGLE, BS 500, STR 26L IN THE FWD CARGO COMPARTMENT. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02 TEM 9 AND DWG 143A7505 SHEET:119 REV:-.Aug 9, 2026 · N954WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026090182195Shield · crackedCRACKED SHIELD WEB LOCATED BTW BS 492.5 TO BS 500A, STR 26R IN FWD CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS LOCATED BTW BS 492.5 TO BS 500A AT LVEL STR 26R AT FWD CARGO COMPARTMENT IAW SRM 51-40-02-0G-0 SRM 51-10-02-0G-0 ITEM 9 AND DWG 143A0080 Aug 9, 2026 · N954WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026090184084Scuff Plate · crackedCRACK ON SCUFF PLATE LOCATED FWD POSITION CUT OUT DOOR AT AFT CARGO COMPARTMENT. REPAIRED SCUFF PLATE LOCATED FWD POSITION CUT OUT DOOR AT AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.Aug 9, 2026 · N954WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026090160750Support Angle · crackedCRACKED SUPPORT ANGLE BS 500C FWD POSITION AT LEVEL STR 26L ON FWD CARGO COMPARTMENT. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS 500C FWD POSITION AT LEVEL STR 26L ON FWD CARGO COMPARTMENT IAW SRM 51-40-02-0G-0 AND DWG 143A7505 SHEET: 117 AND SHEET: 118Aug 9, 2026 · N954WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR IPXA2026082792230Channel · crackedCRACKED SPLICE CHANNEL, LT BODY GEAR WHEEL WELL, OTBD STRUT INTERCOSTAL UPPER ATTACHMENT AT BS 1372. REMOVED THE DAMAGE CHANNEL IAW SRM 51-40-02-0G, REV 49. INSTALLED A NEW CHANNEL IAW SRM 51-40-02-0G, REV 49, & DWG 65B15001, SH 6, REV B.Aug 9, 2026 · N612UP · Boeing 7478F · Fuselage Miscellaneous StructureSDR IPXA2026082792256Channel · crackedCRACKED SPLICE CHANNEL, RT BODY GEAR WHEEL WELL OTBD STRUT INTERCOSTAL UPPER ATTACHMENT AT BS 1372. REMOVED THE DAMAGED CHANNEL IAW SRM 51-40-02-0G, REV 49. INSTALLED A NEW CHANNEL IAW SRM 51-40-02-0G, REV 49, & DWG 65B15001, SH 6, REV B.Aug 9, 2026 · N612UP · Boeing 7478F · Fuselage Miscellaneous StructureSDR MASA20260824215Gusset · corrodedDURING HEAVY CHECK, INSPECTIONS OF CF ILL, CORROSION ON GUSSET PLATE AT FR 90, RIH, RBL 23 REPLACED WITH NEW GUSSET PLATE IAW ERJ 175 SRM 51-41-02. NRC# 4502709-1000-0105, REV 45 DATED MAY-28-2021.Aug 9, 2026 · N84307 · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR AALA202608249832Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 2 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42Aug 9, 2026 · N578UW · Airbus A321231 · Elevator StructureSDR AALA202608244630Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 5 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42Aug 9, 2026 · N578UW · Airbus A321231 · Elevator StructureSDR AALA202608246879Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 2 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42Aug 9, 2026 · N578UW · Airbus A321231 · Elevator Structure