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 ABXA20260222077Warning Message · false activationEICAS MSG TRAILING EDGE FLAPS DISAGREE DURING INITIAL TAXI AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC . MTX PERFORMED FLAP OPERATION MULTIPLE TIMES IN ELECTRIC AND THEN HYDRAULIC AND NO FAULTS NOTED IAW AMM 27-51-00. AND RETURNED AC TO SERVICE.Feb 22, 2026 · N774AX · Boeing 767281 · Trailing Flap Position Indicating SystemSDR IXX2026F00001Panel · delaminatedLT SIDE VERTICAL STAB PNL DELAMINATED P/N 175T2001-3Feb 22, 2026 · N307AZ · Boeing 767338 · Vertical Stabilizer, Plate/SkinSDR JR2R20260222526Frame · corrodedRH MLG WHEEL WELL AILERON QUADRANT ASSY LOWER BRACKET IS CRACKED. REPLACEDFeb 22, 2026 · N88310 · Emb ERJ170200LL · Fuselage Main, FrameSDR JR2R20260222854Panel · corroded633FB HAS EVIDENCE OF CORROSION. REPAIREDFeb 22, 2026 · N88310 · Emb ERJ170200LL · Wing, Plate/SkinSDR MAS2026F00002Panel · corroded633FB HAS EVIDENCE OF CORROSION. REPAIRED.Feb 22, 2026 · N88310 · Emb ERJ170200LL · Wing, Plate/SkinSDR JR2R20260222773Pin · chafedFWD AVIONICS DOOR AFT SIDE ALONG SEAL ABOVE LT LOCKING PIN CHAFED. REPAIRED.Feb 22, 2026 · N88310 · Emb ERJ170200LL · Electrical/Electronic Compartment DoorsSDR IXXA20260222002Pressure Deck · corrodedRIGHT WHEEL WELL PRESSURE DECK CORRODED STA1160 RBL3 P/N 144N8142-10Feb 22, 2026 · N752CX · Boeing 7572G5 · Fuselage Main, StructureSDR IXXA20260222001Support Web · corrodedLW FUEL BOOST PUMP CUTOUT CORROSION IRSS 183Feb 22, 2026 · N752CX · Boeing 7572G5 · Wing Miscellaneous StructureSDR REXA2026080601516Stiffener · crackedCRACK ON STIFFENER (1EA) ON ACCESS PANEL 171CL STIFFENER ON ACCESS PANEL 171CL WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01Feb 21, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026080601502Stand Off · crackedCRACKED INNER SUPPORT ANGLE (STANDOFF 1 EA) ON RH UPPER TRANSCOWL. INNER SUPPORT ANGLE (STANDOFF 1 EA) ON RH UPPER TRANSCOWL WAS REPLACED PER CRJ-900 SRM 51-42-28-001-001-A01 AND SRM 51-42-21-001-001-A01Feb 21, 2026 · N297PQ · Cndair CL6002D24 · Engine Thrust ReverserSDR CALA2026050816072Skin · ground damageAIRCRAFT STRUCK BY WATER SERVICING TRUCK. AFT OF WATER SERVICING DOOR. LOCATION OF DAMAGE IS AFT OF THE LAV VACUME WASTE ACCESS PANEL, UNDER BULK CARGO LAV WASTE TANKS. WASTE TANK RINSE LINE FITTING ASSEMBLY - REMOVAL IAW AMM DMC-B787-A-38-32-14, FOR CLOSEST Feb 21, 2026 · N16009 · Boeing 78710 · Fuselage Main, Plate/SkinSDR SWIA2026022175985Hinge · gougedPASSENGER DOOR HINGE, DOOR SIDE, ALL LUGS GOUGED. REPAIRED PASSENGER DOOR HINGE, DOOR SIDE, ALL LUGS IAW SRM 52-11-01-201-007-A01.Feb 21, 2026 · N795SK · Cndair CL6002C10 · Fuselage, Door HingeSDR REXA2026042800396Web · crackedCRACKED FLOOR WEB RIGHT SIDE AT_ ELECTRICAL BAY (BELOW ADG SUPPORT DOUBLER) FS193.00. FLOOR WEB RIGHT SIDE AT_ ELECTRICAL BAY (BELOW ADG SUPPORT DOUBLER) FS193.00 WAS REPAIRED PER CRJ-900 SRM 53-11-43-201-001-A01.Feb 21, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026042800372Web · crackedCRACKED FLOOR WEB LEFT SIDE AT_ ELECTRICAL BAY (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) FS193.00. FLOOR WEB LEFT SIDE AT_ ELECTRICAL BAY (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) FS193.00 WAS REPAIRED PER CRJ900 SRM 53-11-43-201-001-A01Feb 21, 2026 · N297PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWIA2026022175743Skin · gougedLEFT INBD FLAP AT WS 97.009 INNER SKIN AND DOUBLER HAS GAUGES. REPAIRED LT INBD FLAP AT WS 97.009 INNER SKIN AND DOUBLE IAW REO 601R-57-52-2545, REV-. CHECKS GOOD.Feb 21, 2026 · N952SW · Cndair CL6002B19 · Trailing Edge FlapsSDR IPXA2026030639575Seat Track · corrodedMAJOR REPAIR. MAIN CABIN COMPARTMENT FLOOR STRUCTURE, FR 79-80 Y0 SEAT TRACK CORRODED. INSTALLED NEW SECTION OF SEAT TRACK, MAIN CABIN COMPARTMENT FLOOR STRUCTURE, FR 79-80 Y-0ÂFeb 21, 2026 · N135UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026031635090Floorbeam · corrodedMAJOR REPAIR. UPON REMOVAL OF DAMAGED ON DECK PLATE, FOUND FLOORBEAM UPER FLANGE EXFOLIATED BS 1681, LBL 28 - 33. REMOVED THE DAMAGE. CUT OUT THE FLOORBEAM UPPER TEE AND CUT AWAY ANY DAMAGE ON FLOORBEAM VERTICAL WEB AS REQUIRED IAW E.A. 757-5310-01-B0703Feb 21, 2026 · N422UP · Boeing 75724APF · Fuselage Main, Floor BeamSDR IPXA2026040136279Skin · crackedL/H WING-I/B FLAP I/B TOP SKIN APPROX 6"FROM I/B END AND 3' FROM T/E HAS DENT IN SKIN AND RUB STRIP (RUB STRIP CRACKED AT DENT) NOT IN MAPPING-109-210-VWV VERIFIED L/H I/B FLAP WAS REPLACED ON T/C T3F18E008AETA. NO FURTHER ACTION REQ.Feb 21, 2026 · N135UP · Airbus A300F4622R · Trailing Edge FlapsSDR IPXA2026032038490Floor Support · corrodedAFT CARGO COMP. FLOOR STRUCT. FLOOR STRINGER HAS EVIDENCE OF CORROSION AROUND MULTIPLE NUT PLATE HOLE BTW STA 1440 AND STA 1480 APPROX LBL/RBL 16.10, ID STICKER NUM. (085-002). REMOVED 2 EA NUTPLATES AND REMOVED CORROSION AT STA 1470 AFT CARGO COMP FLOOR STRUCFeb 21, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026030939628Profile · crackedMAIN CABIN COMPARTMENT FLOOR STRUCTURE, FR 74-75 LH O/B "Z" PROFILE HAS (2EA) CRACKS. INSTALLED PENDING AREA OF NEW PROFILE AT FR 73-75 LH O/B I.A.W. A300-600 SRM 51-40-21 INSTALLED WEB 73-74 LH O/B ON T3F18E008BQLAFeb 21, 2026 · N135UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026031839266Profile · crackedMAIN CABIN COMPARTMENT FLOOR STRUCTURE, FR 80 - 82 LT BETWEEN Y1221.2 AND Y1580.5 ZEE PROFILE CRACKED. ZEE PROFILE WAS REMOVED IAW SRM 51-40-21. INSTALLED A NEW ZEE PROFILE AT MAIN CABIN COMPARTMENT FLOOR STRUCTURE, FR80/82 LH BETWEEN Y1221.2 & Y 1580.5 IAW SFeb 21, 2026 · N135UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026032539278Bracket · gougedRIGHT WING T/E SHROUD BOX AREA INBD OF AILERON DROP DOWN PANEL HAS A GOUGED BRACKET. REMOVED THE BRACKET IAW SRM 51-40-21-001. INSTALLED THE BRACKET IAW SRM 51-40-21-001.Feb 21, 2026 · N135UP · Airbus A300F4622R · Wing Miscellaneous StructureSDR IPXA2026031039440Seat Track · corrodedMAIN CABIN COMPARTMENT FLOOR STRUCTURE, FR 79-80 LH Y1137.1 SEAT TRACK CORRODED. REMOVED CORROSION STR-ZONE-200. MAIN CABIN COMPARTMENT FLOOR STRUCTURE, FR 79-80 LH Y1221.2 SEAT TRACK. IAW SRM 51-74-10 AND EVALUATED AND FOUND OUT LIMITS IAW SRM 53-10-16 PAR 2Feb 21, 2026 · N135UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202602210372Actuator · faultedCARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDCD) ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24 - AOT A52W016-24. COMPLIED WITH EO 6-5230-E0378588 C P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIFeb 21, 2026 · N746FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR SWAA2026032472998Support Angle · crackedCRACKED SUPPORT ANGLE, BS 291.5 - 294.5, RBL 54. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, SRM 51-40-02, & DWG 141A8310, SHEET 25, REV- .Feb 21, 2026 · N920WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032472992Stub Frame · crackedCRACK SERVICE DOOR CUTOUT LOWER STUB FRAME, BS 294.5, RBL 54. REPLACED THE STUB FRAME IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, & DWG 141A8370, SHEET 10, REV D.Feb 21, 2026 · N920WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2026032473118Web · crackedCRACK WEB ON CEILING INTERNAL STRUCTURE, BS 847 - 867, LBL 21. REPLACED THE WEB IAW SRM 51-10-02, ITEM 9, & DWG 149A8100, SHEET 1, REV-.Feb 21, 2026 · N920WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032472997Stringer Clip · crackedCRACKED STRINGER CLIP, BS 277, STRINGER 10R. REPLACED THE STRINGER CLIP IAW SRM 51-40-02 & DWG 141A1110, SHEET 18, REV-.Feb 21, 2026 · N920WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2026032473119Angle · crackedCRACKED ANGLE ON LT WING NR 2 SLAT. REPLACED THE ANGLE IAW SRM 51-40-02-0G-0.Feb 21, 2026 · N920WN · Boeing 7377H4 · Leading Edge DevicesSDR SWAA2026032372978Stringer · crackedCRACKED STRINGER 23R, BS 540. PERFORMED PERMANENT REPAIR ON STRINGER 23R, BTWN BS 500D TO 540 IAW SRM 53-00-03-2R-1, REPAIR 1.Feb 21, 2026 · N245WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2026032373102Support · corrodedCORRODED SUPPORT ZEE, BS 727D - 767, RBL 21, WL 155. REPLACED SUPPORT ZEE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 146A7502, SHEET 26, REV -, DWG 146A7500, SHEET 85, REV A.Feb 21, 2026 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032373103Shield · corrodedCORRODED SHIELD WEB, BS 767 - 794.3, WL 155, (4 POINTS). REPLACED SHIELD WEB IAW SRM 51-40-02-0G, SRM 51-10-02-0G, PARAGRAPH 9, & DWG 146A0081, SHEET 31, REV -.Feb 21, 2026 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032372981Glowstrip · deterioratedDETERIORATED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA). REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (10EA) IAW AMM 33-51-15-400-802;Feb 21, 2026 · N7889A · Boeing 73779L · Emergency EquipmentSDR SWAA2026032373109Tie Clip · corrodedCORRODED TIE CLIP, BS 747, STRINGER 26R, WL 152. REPLACED THE TIE CLIP IAW SRM-51-10-02, ITEM (9), SRM-51-40-02, & DWG 146A1220, SHEET 50, REV-.Feb 21, 2026 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032372977Support Angle · crackedCRACKED SUPPORT ANGLE, BS 500D, STRINGER 28R. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, SRM 51-40-02, AND DWG 143A7902, SHEET 126, REV A.Feb 21, 2026 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032072976Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED STA 500D AND STR 28L FWD CARGO BAY. REPLACED ANGLE - SUPPORT LOCATED STA 500D AND STR 28L FWD CARGO BAY IAW SRM 51-10-02; SRM 51-40-02 AND DWG 143A7902 SHEET:126 REV:A.Feb 21, 2026 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032073100Support · corrodedCORROSION SUPPORT ZEE LOCATED BTW STA 727 TO STA 847 LBL 21 AND WL 155 AFT CARGO (12 POINTS). PERFORMED REPAIR ON SUPPORT ZEE LOCATED BTW STA 727 TO STA 847 LBL 21 AND WL 155 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-6 AND DWG 146A7500 SHEET 85 REV Feb 21, 2026 · N245WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR IPXA2026032036304Adapter · corrodedUPPER MAIN CARGO AFT OF FLOOR PANEL 222DG AND FWD OF 232EF FRAME BEAM HAS CORROSION . INSTALLED CLS ADAPTER IAW A300-600 SRM 51-40-21Feb 21, 2026 · N135UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026031939258Profile · crackedMAIN CABIN COMPARTMENT FLOOR STRUCTURE, FR80/82 RH BETWEEN -Y1221.2 AND -Y1580.5 "Z" PROFILE CRACKED. INSTALLED NEW Z PROFILE P#A5398140120100 BATCH #0004466723 AT MAIN CABIN FLOOR STRUCTURE FR80/82 R/H IAW A300-600 SRM 51-40-21-001.Feb 21, 2026 · N135UP · Airbus A300F4622R · Fuselage Main, Longeron/StringerSDR IPXA2026030939549Seat Track · corrodedMAJOR REPAIR. MAIN CABIN COMPARTMENT FLOOR STRUCTURE, FR 79-80 RH -Y1137.1 SEAT TRACK CORRODED. INSTALLED REPAIR AT SEAT TRACK BTWN FR 79-80 RH -Y1137.1 IAW SRM 51-10-16-201 PAR. 4 C (16) TO (20). WITH FASTENERS AND COLLARS.Feb 21, 2026 · N135UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026030739698Support Plate · crackedMAIN CABIN COMPARTMENT FLOOR STRUCTURE, FR 73-74 RH O/B WEB LOWER SURFACE HAS (1EA) CRACK. INSTALLED NEW SUPPORT PLATE (WEB) AT MAIN CABIN COMPARTMENT FLOOR STRUCTURE, FR 73-74 RH O/B (1EA) IAW SRM 51-40-21-001Feb 21, 2026 · N135UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR QXEA2026031700057Placard · damaged812ALW UP ARROW PLACARD DAMAGED ON PASSENGER DOOR. REMOVED AND REPLACED 812ALW UP ARROW PLACARD IAW AMM E175 20-10-09-400-801-A, 20-10-09-000-801-AFeb 21, 2026 · N655QX · Emb ERJ170200LR · Placards and MarkingsSDR IPXA2026030739689Support Plate · crackedMAIN CABIN COMPARTMENT FLOOR STRUCTURE, FR 73-74 LT OTBD WEB LOWER SURFACE HAS (1EA) CRACK. REMOVED WEB AT MAIN CABIN COMPARTMENT FLOOR STRUCTURE, FR 73-74 LT OTBD AND THE WEB IS CRACKED IAW SRM 51-40-21. INSTALLED NEW SUPPORT PLATE (WEB) AT MAIN CABIN COMPARFeb 21, 2026 · N135UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR SWIA2026031175506Skin · dentedAFT FUSELAGE SKIN, BS 700 BTWN STRINGERS 20L-24L DENTED. ACOMPLISHED WHIT REO 601R-53-61-8482, FOR REPAIR ON AFT FUSELAGE SKIN.Feb 21, 2026 · N913EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR IPXA2026030838490Floor Support · corrodedAFT CARGO COMP. FLOOR STRUCT. FLOOR STRINGER HAS EVIDENCE OF CORROSION AROUND MULTIPLE NUT PLATE HOLE BTW STA 1440 AND STA 1480 APPROX LBL/RBL 16.10, INSTALLED 4 EA NUTPLATES AT AFT CARGO COMP. FLOOR STRUCT. FLOOR STRINGER BTW STA 1440 AND STA 1480 LBL 16.10 IFeb 21, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026031138732Floor Support · corrodedAFT CARGO COMP. FLOOR STRUCT. FLOOR STRINGER HAS EVIDENCE OF CORROSION AROUND MULTIPLE NUT PLATE HOLE BTW STA 1440 AND STA 1480 APPROX LBL/RBL 7.55, ID STICKER NUM. (085-004). ATA 53-10 VERIFIED STEP 24, C/W B757-200PF AMM 51-24-09-377-001.Feb 21, 2026 · N422UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026030639394Profile · crackedMAIN CABIN COMPARTMENT FLOOR STRUCTURE, FR79-80 O/B LH Y1580.5 "Z" PROFILE CRACKED. REMOVED PROFILE AT -STR-ZONE-200. MAIN CABIN COMPARTMENT FLOOR STRUCTURE, FR79-80 O/B LH Y1580.5 "Z" IAW 51-40-21. INSTALLED NEW PROFILE IAW SRM 51-40-21.Feb 21, 2026 · N135UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026030239504Shear Web · crackedMAIN CABIN COMPARTMENT FLOOR STRUCTURE, FR 76-77 RH O/B WEB CRACKED. REMOVED WEB AT STR-ZONE 200. MAIN CABIN COMPARTMENT FLOOR STRUCTURE, FR 76-77 RH O/B AND THE WEB IS BROKEN IAW SRM 51-40-21. INSTALLED WEB MAIN CABIN COMPARTMENT FLOOR STRUCTURE, FR 76-77 Feb 21, 2026 · N135UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026030637030Adapter · corrodedUPPER MAIN CARGO CTR RH SIDE OF FLOOR PNL # 232EF SEAT TRACK HAS CORROSION . REMOVED CLS ADAPTER AT UPPER MAIN CARGO CTR RH SIDE OF FLOOR PNL # 232EF IAW A300-600 SRM 51-40-21-001. INSTALLED NEW CLS ADAPTER IAW A300-600 SRM 51-40-21-001.Feb 21, 2026 · N135UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026030501527Sensor · erraticDIVERTED TO SEA DUE TO LEFT ENGINE OIL QUANTITY INDICATION INOP. INSPECTED WIRING AND REPLACED OIL QUANTITY TRANSMITTER. OK FOR SERVICE. (8416515)Feb 21, 2026 · N813NW · Airbus A330323 · Engine Oil Quantity