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 SWAA2026102113404Tie Clip · crackedCRACK TIE CLIP ON BS 500H, STRINGER 26L AT FWD CARGO COMPARTMENT. REPLACED TIE CLIP LOCATED ON STA 500H AND STR 26L AT FWD CARGO COMPARTMENT IAW SRM 51-40-02, & DWG 143A7505 SHT 151, REV -.Sep 17, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026102193787Tie Clip · crackedCRACKED TIE CLIP ON STA 500H AND STRINGER 26R AT FWD CARGO COMPARTMENT 2026-572636 REPLACED TIE CLIP ON STA 500H AND STR 26R AT FWD CARGO COMPARTMENT IAW SRM 51-10-02 ITEM 9 AND DRAWING# 143A1233 REV-.Sep 17, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026102191183Support Angle · crackedCRACKED SUPPORT ANGLE ON THE FWD FACE OF THE FRAME AT BS 500G, STRINGER 26R. REPLACED THE SUPPORT ANGLE, & FASTENERS IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHEET 152, REV -.Sep 17, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026102111786Tie Clip · crackedCRACKED TIE CLIP, BS 500I, STRINGER 26R IN THE FWD CARGO BAY. REPLACED THE TIE CLIP IAW SRM 51-10-02, ITEM 9, & DWG 143A1234, REV A.Sep 17, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR AALA202610205112Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: AFT CABIN WET AREA STA. 986.5 FLOOR BEAM CORRODED RBL43. REMOVED AND REPLACED T-CHORD MATERIAL DBF-1555-11 IAW SRM 53-70-51-2R-4Sep 17, 2026 · N811NN · Boeing 737823 · Fuselage Main, Floor BeamSDR AALA202610209698Crease Beam · corrodedAIRCRAFT IN BASE MAINTENANCE: AFT CABIN WET AREA RH CREASE ANGLE CORRODED STA 986.5 TO STA987 RBL52. REMOVED AND REPLACED IAW BOEING DRAWING 147A8501AND AARD 51-00-05-1.Sep 17, 2026 · N811NN · Boeing 737823 · Fuselage Main, StructureSDR AALA202610200826Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION STA 986.5 CORRODED AT SCREW HOLES RBL22 TO RBL 39. REMOVED AND REPLACED T-CAP IAW SRM 53-71-51-0GSep 17, 2026 · N811NN · Boeing 737823 · Fuselage Main, Floor BeamSDR AALA202610207237Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: AFT CABIN WET AREA STA 986.5 FLOOR BEAM CORRODED AROUND SCREW HOLES RBL 12 TO 21. REMOVED AND REPLACED T-CAP IAW SRM 53-70-51-OGSep 17, 2026 · N811NN · Boeing 737823 · Fuselage Main, Floor BeamSDR SWAA2026101934509Seat · loosePASSENGER SEAT 16A, FRONT ROW UPPER ESCUTCHEON FOUND LOOSE. TIGHTENED THE SEAT UPPER ESCUTCHEON IAW CMM 25-23-65-4632, PG. 7013, PARA T, STEP 9.Sep 17, 2026 · N8738K · Boeing 7378 · Passenger Compartment EquipmentSDR AALA202610191453Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON Z ANGLE STA 994 LBL36. REMOVED AND REPLACED DAMAGED Z ANGLE IAW AARD 51-00-05-1 AND BOEING DWG 147A5700.Sep 17, 2026 · N811NN · Boeing 737823 · Fuselage Miscellaneous StructureSDR AALA202610190016Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: AFT WET AREA CORROSION AT STATION 986.5 LBL 44. REMOVED AND REPLACED IAW SRM 53-70-51-2R-6.Sep 17, 2026 · N811NN · Boeing 737823 · Fuselage Main, Floor BeamSDR AALA202610199020Floor Support · corrodedAIRCRAFT IN BASE MAINTENANCE: AFT WET AREA CORROSION AT STATION 951 LBL 25. REMOVED AND REPLACED FLOOR SUPPORT IAW BOEING DWG 147A5650 AND AARD 51-00-05-1.Sep 17, 2026 · N811NN · Boeing 737823 · Fuselage Miscellaneous StructureSDR HNAA2026101600999Skin · chafed55-2502 BOTTOM OF RUDDER I, FRONT SPAR CAP, SKIN CHAFED BTW RIB ZV920 AND RIB ZV1164. REPAIRE IAW ETD 2026-145-016066 AND EO 1-55-26-0500Sep 17, 2026 · N650AE · Emb EMB145LR · Rudder, Plate/SkinSDR AALA202610151493Web · corrodedAIRCRAFT IN BASE MAINTENANCE: RH KWEB CORRODED FASTENER HOLE AT AFT END STA 1015.5 RBL 36. COMPLETED REPAIR IAW EA379163 AND SRM 51-40-02.Sep 17, 2026 · N316SE · Boeing 7378 · Fuselage Miscellaneous StructureSDR AALA202610151378Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: AFT WET AREA AFT DECK CORRODED BS 1020, RBL 32. WORK COMPLETED IAW EA 379266 AND SRM 51-10-02.Sep 17, 2026 · N316SE · Boeing 7378 · Fuselage Miscellaneous StructureSDR SWAA2026101471904Support Angle · crackedCRACKED SUPPORT ANGLE, BS 500I, LBL 7 IN THE FWD CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, AND DWG 143A7505, SHEET 152, REV-.Sep 17, 2026 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026101411876Support Angle · crackedCRACKED SUPPORT ANGLE, BS 500I, RBL 7 IN THE FWD CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02, AND DWG 143A7505, SHEET 152, REV-.Sep 17, 2026 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR AALA202610141774Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CABIN FLOOR CREASE ANGLE AT THE R2 DOOR HAS CORROSION ON TOP FROM APPROX. STA 952 TO STA 986.5. REMOVED AND REPLACED ANGLE IAW 51-00-05-1 AND BOEING DWG 147A8540.Sep 17, 2026 · N316SE · Boeing 7378 · Fuselage Miscellaneous StructureSDR AALA202610143962Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: STA 986.5 FLOORBEAM FLOORBOARD HOLE CORRODED AT STA 986 RBL 22.5 T CAP REPLACED, ALL WORK ACCOMPLISHED AND DOCUMENTED ON 09C20025081/080 NR 575. COMPLETED INSTALLATION OF INTERCOSTAL REPAIR FITTINGS AT LBL 32 STA 986.5-1006 IAWSep 17, 2026 · N316SE · Boeing 7378 · Fuselage Main, Floor BeamSDR AALA202610139994Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: FLOOR CREASE ANGLE AT THE L2 DOOR HAS CORROSION ON TOP FROM STA 955 TO 992 MIGRATING UNDER Z ANGLE. REMOVED AND REPLACED DAMAGE PART IAW AARD 51-00-05-1 AND BOEING DWG 147A8540.Sep 17, 2026 · N316SE · Boeing 7378 · Fuselage Miscellaneous StructureSDR AALA202610123834Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON Z ANGLE (LOCATED BS 991-115 RBL 32) AT BS 1001 AND RBL 31 - INSTALLED Z ANGLE/WALL SUPPORT IAW AARD 51-00-05-1, AND DWG 147A5700.Sep 17, 2026 · N316SE · Boeing 7378 · Fuselage Miscellaneous StructureSDR IPXA2026100101667Frame · crackedMAJOR REPAIR. CENTER FUSELAGE BASE FRAME FITTING FR44 LT HAS SIGNS OF CRACK. CRACK EXTENDS ENTIRE TOP SURFACE AND STOPS JUST PAST EDGE ON FWD SURFACE OF FRAME. ACCOMPLISHED REPAIR IAW EO 46789-JIC 7 AND EO-46789-REQ 6 (APPX J).Sep 17, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, FrameSDR IPXA2026100101697Frame · crackedMAJOR REPAIR. CENTER FUSELAGE BASE FRAME FITTING FR45 LH SIDE HAS SIGNS OF CRACK. AFTER FURTHER EVALUATION FOUND CRACK LENGTH IS 0.100". ACCOMPLISHED REPAIR IAW EO 46789-JIC 7 AND EO-46789-REQ 6 (APPX J).Sep 17, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, FrameSDR CALA2026101220277Gusset · crackedFRAME 68, STRINGER 14L GUSSET PLATE 2ND HOLE FROM BOTTOM IS VISIBLY OUT OF ROUND. THE GUSSET PLATE WAS R & R IAW SRM 53-41-12-300-018, FIGURE 1.Sep 17, 2026 · N836UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2026101220275Gusset · crackedFRAME 68, STRINGER 12R, GUSSET PLATE MIDDLE HOLE IS VISIBLY ELONGATED IN GUSSET PLATE LAYER. GUSSET PLATE R & R IAW SRM 53-41-12-300-018, FIGURE 1.Sep 17, 2026 · N836UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2026101220271Gusset · crackedFR 66, STR 16L GUSSET PLATE TOP HOLE HA S A REJECTABLE INDICATION. GUSSET PLATE REMOVED AND REPLACED IAW SRM 53-41-12-300-018, FIGURE 1. FLOWCHART SOLUTION 1. GVI & HFEC INSPECTION COMPLETED PER NTMS 51-90-00, 5110-08 AND 51-10-01. NO DAMAGE FOUND ON FRAME ISep 17, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR SWAA2026100781953Support Angle · crackedCRACKED SUPPORT ANGLE, BS 867, STR 3R. REPLACED THE SUPPORT ANGLE IAW SRM: 51-10-02-0G-0 146A7901, SHEET 19, REV-.Sep 17, 2026 · N208WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026100606701Support Angle · crackedCRACKED SUPPORT ANGLE, BS 867, STR 3R REPLACED SUPPORT ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, PARAGRAPH 9, & DWG 146A7901, SHEET 66, REV A.Sep 17, 2026 · N8309C · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026100663323Plate · crackedCRACK ON CORRUGATED PLATE, TRAILING EDGE ORSS 327 RT WING. REPLACED CORRUGATED PLATE AND FASTENERS LOCATED TRAILING EDGE ORSS327 AT RT WING IAW SRM 51-40-02-0G-0, DWG 115A3700, SHEET 60, REV-, AND SRM 51-10-0G-0, PARAGRAPH 9.Sep 17, 2026 · N8309C · Boeing 7378H4 · Wing Main, Frame StructureSDR SWAA2026100666204Plate · crackedCRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE ORSS297 AT RT WING. REPLACED CORRUGATED PLATE AND FASTENERS LOCATED TRAILING EDGE ORSS297 AT RT WING I.A.W B737-800 SRM 51-40-02-0G-0 DWG 115A3700 SHEET: 60 REV: - AND B737-800 SRM 51-10-02-0G-0 PARAGRAPH 9.Sep 17, 2026 · N8309C · Boeing 7378H4 · Wing Main, Frame StructureSDR SWAA2026100622622Plate · crackedCRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE ORSS307 AT RT WING. REPLACED CORRUGATED PLATE AND FASTENERS LOCATED TRAILING EDGE ORSS307 AT RT WING IAW SRM 51-40-02-0G-0, DWG 115A3700, SHEET 60, REV -, & SRM 51-10-02-0G-0, PARAGRAPH 9. ISep 17, 2026 · N8309C · Boeing 7378H4 · Wing Main, Frame StructureSDR SWAA2026100601040Beam · crackedCRACK ON BEAM LOCATED TRAILING EDGE ORSS279 AT LT WING. REPLACED BEAM LOCATED TRAILING EDGE ORSS279 AT LT WING IAW SRM 51-10-02, ITEM 9, SRM 51-40-02 AND DWG 115A3700 SHEET 60 REV -.Sep 17, 2026 · N8309C · Boeing 7378H4 · Wing Main, Frame StructureSDR SWAA2026100649708Plate · crackedCRACKED PHENOLIC OF CORRUGATED PLATE LOCATED TRAILING EDGE ORSS 245 AT LT WING. REPLACED CORRUGATED PLATE AND FASTENERS LOCATED TRAILING EDGE ORSS245 AT LT WING IAW DWG 115A2001 SHEET 67, REV -, SRM 51-40-02-0G-0, AND SRM 51-10-02-0G-0, PARAGRAPH 9.Sep 17, 2026 · N8309C · Boeing 7378H4 · Wing Main, Frame StructureSDR SWAA2026100649568Plate · crackedCRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE IRSS217 AT RT WING. REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE IRSS 217 AT RT WING IAW SRM 51-10-02-0G-0 ITEM 9, AND SRM 51-40-02-0G-0 DWG 115A2001, SHEET 67 REV - .Sep 17, 2026 · N8309C · Boeing 7378H4 · Wing Main, Frame StructureSDR SWIA2026091777523Flap Track · out of limitsLH WING FLAP TRACK 1A HAS THICKNESS REDUCTION DAMAGE MAX DEPTH OF DAMAGE IS 030 REQUIRES 200 FC RE-INSPECT UNTIL DEPTH OF DAMAGE EXCEED 068, PER SRM 57-52-03AD01 TABLE 101. REMOVED AND REPLACED LH WING FLAP TRACK 1A REF EMB AMM 57-54-25Sep 17, 2026 · N185SY · Emb ERJ170200LR · Trailing Edge FlapsSDR IPXA2026100102772Panel · crackedPANEL 423BL LOWER AREA WITH 2 CRACKS. REMOVED (IEA) SEAL AND SEAL RETAINER AT PANEL 423BL IAW SRM 51-40-21. REINSTALLED SEAL AND SEAL RETAINER AT PANEL 423BL IAW SRM 51-40-21.Sep 17, 2026 · N158UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2026100101699Shear Tie · crackedMAJOR REPAIR. CENTER FUSELAGE BASE FRAME FITTING FR46 LH SIDE HAS SIGNS OF CRACK. ACCOMPLISHED EO-46789-JIC007.Sep 17, 2026 · N158UP · Airbus A300F4622R · Fuselage Internal Mounting StructureSDR IPXA2026100102793Panel · crackedPANEL 423BL EXTERNAL SURFACE WITH A CRACK. VERIFIED RECEIVED THE REPAIRED PANEL 423BL BY WELDING ON TRAVELER # T26/1879228, NOTE: THE INSTALLATION WILL BE ACCOMPLISED ON TASKCARD: T3F18E007EGD6.Sep 17, 2026 · N158UP · Airbus A300F4622R · Nacelle/Pylon, Plate/SkinSDR IPXA2026100102892Access Panel · crackedPANEL 413BL, EXTERNAL SURFACE WITH A CRACK DOT 53-024. RECEIVED THE REPAIRED PANEL 413BL BY WELDING ON TRAVELER # T26/1879227, NOTE: THE INSTALLASION WILL BE ACCOMPLISED ON TASK CARD T3F18E007EGD6.Sep 17, 2026 · N158UP · Airbus A300F4622R · Nacelle/Pylon, Plate/SkinSDR SWAA2026092919759Seal · damagedLEFT HORIZONTAL STAB SEAL, TRAILING EDGE PANEL 334EB, SCREW HOLES ELONGATED. REPLACED THE PANEL 334EB IAW SRM 51-10-02. PANEL INSTALLATION PERFORMED ON TTG8Q01E2Q7K.Sep 17, 2026 · N8548P · Boeing 7378H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2026092854256Cover · delaminatedLEFT ELEVATOR HINGE COVER PANEL 334KB IS DELAMINATED AT SCREW HOLE. REMOVED AND REPLACED LT ELEVATOR LOWER HINGE COVER 334KB IAW AMM 27-31-31. INSP C/WSep 17, 2026 · N8548P · Boeing 7378H4 · Elevator StructureSDR SWAA2026092890689Strap · looseAFT LT GALLEY DOOR SAFETY YELLOW STRAP ASSEMBLY FOUND BROKEN. ATTACHED THE STRAP AND TIGHTENED AFT ENTRY DOOR ASSIST HANDLE IAW AMM 25-21-25-420-801 AND AIPC 25-66-10-02.Sep 17, 2026 · N8502Z · Boeing 7378H4 · Emergency EquipmentSDR IPXA2026092801699Shear Tie · crackedMAJOR REPAIR. CENTER FUSELAGE BASE FRAME FITTING FR46 LT SIDE HAS SIGNS OF CRACK. ACCOMPLISHED THE FOLLOWING STEPS: 58 TO 63 IAW EO-46789-JIC007.Sep 17, 2026 · N158UP · Airbus A300F4622R · Fuselage Internal Mounting StructureSDR IPXA2026092801667Shear Tie · crackedMAJOR REPAIR. CENTER FUSELAGE BASE FRAME FITTING FR44 LH SIDE HAS SIGNS OF CRACK. VERIFIED C/W STEPS: 41 AND 42 OF EO-46789-JIC007 (T3F18E009P8WZ)Sep 17, 2026 · N158UP · Airbus A300F4622R · Fuselage Internal Mounting StructureSDR IPXA2026092801697Shear Tie · crackedMAJOR REPAIR. CENTER FUSELAGE BASE FRAME FITTING FR45 LH SIDE HAS SIGNS OF CRACK. ACCOMPLISHED ROTPROBPROBE INSPECTION IAW NTM 51-10-01 PART 6. CRACK TERMINATES AT STOP DRILL.Sep 17, 2026 · N158UP · Airbus A300F4622R · Fuselage Internal Mounting StructureSDR SIMA20260917004Bearing · wornSSI# 32-11-001 RH MLG FWD TRUNNION BEARING HAS PLAY. (MAJOR REPAIR). REMOVED AND REPLACED RH MLG FWD TRUNNION BEARING PN ABC44G-401 REF ERJ175 AMM 57-50-00.Sep 17, 2026 · N306DD · Emb ERJ170200LR · Trailing Edge FlapsSDR SIMA20260917003Bolt · rustedRH MLG AFT PINTLE PIN HAS PITTING AT MULTIPLE LOCATIONS. (MAJOR REPAIR) (LEVEL 1 CORROSION) REMOVED RT MLG AFT PINTLE PIN P AND INSTALLED A NEW RT MLG AFT PINTLE PIN IAW AMM 32-11-01.Sep 17, 2026 · N306DD · Emb ERJ170200LR · Main Landing GearSDR SIMA20260917002Pintle Pin · corrodedRIGHT MLG FWD PINTLE PIN HAS PITTING & CORROSION AT BOTH BOLT HOLES. (MAJOR REPAIR) (LEVEL 1 CORROSION) REMOVED RT MLG FWD PINTLE PIN AND INSTALLED A NEW RT MLG FWD PINTLE PIN IAW AMM 32-11-01.Sep 17, 2026 · N306DD · Emb ERJ170200LR · Main Landing GearSDR DALA2026092805373Shaft · damagedREPAIR TO R4 DOOR LOWER HINGE ARM STUB SHAFT REQUIRES REPLACEMENT IAW ERA 636926-14. PERMANENT REPAIR IAW ERA 636926-14. (1818551) (AIRCRAFT GROUNDED)Sep 17, 2026 · N595NW · Boeing 757351 · Service DoorsSDR CALA2026092819916Shade · brokenDURING CABIN CHECK, FOUND WINDOW SHADES BROKEN AT SEATS 20A, 21A. APPLIED TAPE AND SECURED AFFECTED WINDOW SHADES IN THE FULL OPEN POSITION. WINDOW SHADES DO NOT POSE ANY HAZARD TO PASSENGERS OR CREW. STICKER APPLIED ON FWD ATTENDANTS PANEL.Sep 17, 2026 · N37531 · Boeing 7379 · Passenger Compartment Equipment