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 CALA2026031814644Battery Pack · no testCABIN OVERHEAD L1 DOOR EMERGENCY LIGHT BATTERY PACK, CAPACITY CHK FAILED. THE BATTERY PACK (M33093) WAS REPLACED & TESTED NORMAL IAW AMM 33-51-06.Mar 17, 2026 · N74007 · Boeing 777224 · Emergency LightingSDR CALA2026031814643Battery · no testR2 DOOR EMERGENCY LIGHT BATTERY TEST FAILED. BATTERY REPLACED AND TESTED NORMAL IAW AMM 33-51-06.Mar 17, 2026 · N74007 · Boeing 777224 · Emergency LightingSDR CALA2026031814635Placard · tornRIGHT AFT LAV DOOR EMERGENY SIGN IS TORN AND PARTIALLY FALLING OFF. INSTALLED NEW LAV DOOR EMERGENCY SIGN ON LAV E DOOR. REF. CONFIG DRAWING 1130DD14788.Mar 17, 2026 · N23707 · Boeing 737724 · Placards and MarkingsSDR AALA202603171561Filler · missingAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND FUSELAGE ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER EXISTING REPAIR IS MISSING FILLER. LOCATED AT BS 231 AND S23R. REPAIRED DOUBLER PER SRM 53-10-15-2R-4.Mar 17, 2026 · N871NN · Boeing 737823 · Fuselage Main, Plate/SkinSDR IPXA2026031708053Power Supply · inoperativeINTERIOR EMERGENCY LIGHTS INOP REMOVED AND REPLACED POWER SUPPLY IAW AMM 33-51-07 PB401.Mar 17, 2026 · N431UP · Boeing 75724APF · Emergency LightingSDR IPXA2026031710844Unknown · odorSTRONG ODOR IN FLIGHT DECK. EVEN STRONGER ODOR IN CARGO BAY, CREW NOTICED PHYSIOLOGICAL EFFECTS.Mar 17, 2026 · N370UP · Boeing 767300 · Air Distribution SystemSDR IPXA2026031707108Unknown · odorAIRCRAFT HAS BEEN SERVICED 3 TIMES FOR A STRONG ODOR IN THE COCKPIT. MECHANIC ON ARRIVAL YESTERDAY SMELLED IT OUTSIDE. LAV FUNCTIONS NORMALLY. LOAD CREW COULD SMELL IN THE MAIN DECK. LAV SERVICED. INSPECTED CABIN AND MAIN DECK. REF: AMM 05-41-02. INSPECTED E&EMar 17, 2026 · N370UP · Boeing 767300 · Air Distribution SystemSDR IPXA2026031707927Pawl · inoperativeENTRY DOOR WILL NOT CLOSE UNLESS SECURE LEVER IS ALREADY IN SECURE POSITION. REMOVED AND REPLACED PAWL IAW AMM 52-11-26 OPS CHECKED GOOD.Mar 17, 2026 · N330UP · Boeing 76734AF · Passenger/Crew DoorsSDR FDEA202603170356Skin · crackedDURING PERFORM WORK CARD:EG-5710-E0376285G P12 STEP 3.B.(1) & STEP 5.A.(2) THEN FOUND 02EA CRACK ON UPPER WING SKIN FASTENER NR 5. RH WING UPPER SKIN #5 HOLE CRACK REPAIRED AS PER B777 SRM 51-50-02-0G FIGURE 1, SRM 51-40-02-0G FIGURE 12, SRM 51-10-01-0G FMar 17, 2026 · N854FD · Boeing 777FS2 · Wing, Plate/SkinSDR FDEA202603170355Seat Track · damagedSEAT TRACK DAMAGE TO LOBES ONLY AND WITH IN DEFERAL LIMITS WITH NO EQUIPMENT INSTALLED WITHIN 3 INCHES IAW SRM 53-00-52-1A FIG 101 DETAIL XI SHEET 6. CREATED E.A.#: F-5310-T0387768P1 TITLE: FUSELAGE - MAINFRAME - MAIN CARGO COMPARTMENT SEAT TRACK SPLICE Mar 17, 2026 · N979FD · Boeing 757236 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2026031701853Panel · out of limits(UT) THICKNESS MEASUREMENT WAS ACCOMPLISHED ON LH SIDE PANEL FROM STA 1500+6 TO STA 1530 AT AFT CARGO COMPARTMENT, AREA IS OUT WITHIN LIMITS PER B757-300 SRM 53-00-53-1A PROCEDURE 1 ALLOWABLE DAMAGE 1 DETAIL III NOTE C. AND DETAIL IX. (CORROSION LEVEL 2) LH SMar 17, 2026 · N584NW · Boeing 757351 · Fuselage Miscellaneous StructureSDR K11A2026031700374Battery Pack · inoperativeDURING T/S FOUND L1 DOOR AND FLIGHT DECK ENTRY DOOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED LEFT HAND EMERGENCY LIGHT BATTERY PACK IAW B737 AMM 33-51-51 OPS CHECK GOODMar 17, 2026 · N405CK · Boeing 737436 · Emergency LightingSDR AALA202603174646Light · inoperativeAIRCRAFT WAS NOT GROUNDED: DURING PS CHECK FOUND OVERHEAD EMERGENCY LIGHT AT ROW 27 INOPERATIVE. REMOVED AND REPLACED EMERGENCY AISLE LIGHT ABOVE ROW 27. PRT AMM 33-51-03. OPS CHECK GOOD.Mar 17, 2026 · N952AA · Boeing 737823 · Emergency LightingSDR DALA2026031701836Girt Bar · fodDOOR 3L WILL NOT ARM AT DEPARTURE TIME. REMOVED DEBRIS FROM FLOOR FITTING. DOOR ARMS NORMALLY PER A330 AMM 52-11. (8347374)Mar 17, 2026 · N405DX · Airbus A330941 · Emergency EquipmentSDR DALA2026031701833Skin · ground damageFWD CARGO SURROUND SKIN, FR19, STR 37R - 39R, IMPACT DAMAGE. MAJOR REPAIR PER ERA 628935-14 REV A. (1498327)Mar 17, 2026 · N810NW · Airbus A330323 · Fuselage Main, Plate/SkinSDR 2026F00030Skin · corrodedFOUND 9 AREAS OF CORROSION OF RIGHT WING UPPER SKIN, FWD OF AILERON. MECHANICALLY REMOVED 9 AREAS OF CORROSION LOCATED ON RT WING UPPER SKIN, FWD OF AILERON ON WING SKIN TRAILING EDGE IAW SRM 51-70-02. FOUND 8 CORROSION BLENDS TO BE WITHIN LIMITS IAW SRM 51-70Mar 17, 2026 · N339QS · Cessna 680A · Wing, Plate/SkinSDR SWIA2026031677470Stringer Splice · corrodedCORROSION FOUND ON STRINGER SPLICE 24R AT BS 333. REPLACED STRINGER SPLICE AT FS333 , STGR24R REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG SH670-32420, REV E.Mar 16, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026031677447Floorbeam · corrodedLEFT CROSSBEAM AT BS 280 HAS CORROSION. REMOVED AND REPLACED THE CROSSBEAM IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01, AND DWG CC670-34010, REV -K.Mar 16, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2026031677444Stringer Splice · corrodedCORROSION FOUND ON STRINGER SPLICE AT FS333 STR25R. REPLACED STRINGER SPLICE AT FS333 STGR25R IAW SRM 51-42-06-001-001-A01 AND DWG SH670-32420, REV E.Mar 16, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026031677438Stringer Splice · corrodedCORROSION FOUND ON STRINGER SPLICE AT FS333 STR23L. REPLACED STRINGER SPLICE AT FS333 STR23L WITH NEW PART REF DWG SH670-32420 REV E AND SRM 51-42-06-001-001-A01.Mar 16, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026031677426Floorbeam · corrodedRIGHT FLOORBEAM, BS 280 CORRODED. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01, & DWG CC670-34010, REV K.Mar 16, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2026031677409Door Frame · corrodedPAX DOOR FORMER, FS32941, BETWEEN DD5 AND DD6 INTERCOSTAL IS CORRODED MX 31895310 C-CHECK RO 09302026REPLACED WITH NEW PASSENGER DOOR FORMER FS32941 AND CLEAT IAW CRJ700 SRM 51-42-06-001-001-A01 AND DRAWING 601R31702 REV N CMar 16, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2026031677405Skin · damagedREMOVE IN REPLACE RH UPPER SKIN BETWEEN FS169 - FS173 MX 31896724 C-CHECK RO 09302026REMOVED IN REPLACED RH UPPER SKIN BETWEEN FS169 - FS173 PER REF CRJ 700 SRM 51-42-06-001-001-A01, REF CRJ 700 SRM 51-42-13-001-001-A01, DWG CC670-33040, REV G COMPLIED WITMar 16, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2026031677404Stringer · corrodedCORROSION FOUND ON STRINGER SPLICE AT FS333 STR21R C-CHECK RO 09302026REPLACED STRINGER SPLICE AT FS333, STGR21R REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG SH670-32420 REV E COMPLIED WITH TASK CARD 51-900-1002-SKY ALL CHECKS GOODMar 16, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026031677400Stringer · corrodedCORROSION FOUND ON STR19R AT FS379 - FS394 C-CHECK RO 09302026REPLACED STRINGER 19R AT FS349 - FS485 REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG SH670-31070 REV J COMPLIED WITH TASK CARD 51-900-1002-SKY ALL CHECKS GOOD PRESSURE LEAK CHECKED GOODMar 16, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026031677389Drag Angle · brokenVERTICAL STAB RT AFT DRAG ANGLE HAS WORKING FASTENER. REMOVED AND REPLACED FASTENER ON VERTICAL STAB RT AFT DRAG ANGLE REF REO 670-55-31-209 REV -A DATED 2026-05-28COMPLIED WITH 51-900-1002-SKYMar 16, 2026 · N611SK · Cndair CL6002C10 · Fuselage, Stabilizer Attach FittingsSDR SWIA2026031677379Stringer Splice · corrodedCORROSION FOUND ON STRINGER SPLICE 23R, BS 333. REPLACED THE STRINGER SPLICE IAW SRM 51-42-06-001-001-A01, & DWG SH670-32420, REV E.Mar 16, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026031677375Stringer Splice · corrodedCORROSION FOUND ON STRINGER SPLICE 22R, BS 333. REPLACED STRINGER SPLICE IAW SRM 51-42-06-001-001-A01, AND DWG SH670-32420, REV E.Mar 16, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026031677353Stringer Splice · corrodedCORROSION FOUND ON STRINGER SPLICE 24L, BS 333. REPLACED THE STRINGER SPLICE IAW DWG SH670-32420, REV E, AND SRM 51-42-06-001-001-A01.Mar 16, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026031677342Stringer Splice · corrodedCORROSION FOUND ON STRINGER SPLICE AT FS333 STR26R C-CHECK RO 9302026REPLACED STRINGER SPLICE AT FS333, STGR26R REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWG SH670-32420 REV E COMPLIED WITH TASK CARD 51-900-1002-SKY ALL CHECKS GOODMar 16, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2026031677340Stringer Splice · corrodedCORROSION FOUND ON STRINGER SPLICE AT FS333 STR22L. REPLACED STRIMGER SPLICE 22L, BS 333 WITH NEW PART IAW DWG SH670-32420, REV E AND SRM 51-42-06-001-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY ALL CHECKED GOODMar 16, 2026 · N611SK · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR CALA2026090119164Pressure Web · crackedCRACK FOUND AT VERTICAL PRESSURE WEB BETWEEN LBL 40.00 & LBL 31.83, BTWN WL 192.0 AND WL 200.6). CRACK LENGTH 1 INCH. REPAIRED VERTICAL PRESSURE WEB BETWEEN LBL 40 & LBL 31.83, BTWN WL 192.0 & WL 200.6, IAW SRM 57-10-10-2R-3 ALTERNATIVE 1 FIGURE 203.Mar 16, 2026 · N53442 · Boeing 737924ER · Fuselage Main, BulkheadSDR IPXA2026082593903Pawl · wornHE PAWL BEHIND THE CREW ENTRY DOOR EXTERNAL HANDLE IS WORN. (REPLACE) REPLACED THE PAWL I.A.W AMM 52-11-26-004-001 REV.147 AND AMM 52-11-26-404-003 REV.147.TORQUE SCREW TO 35 IN-LB.Mar 16, 2026 · N317UP · Boeing 76734AF · Passenger/Crew DoorsSDR REXA2026080501484Support Bracket · crackedCRACK ON BRACKET SUPPORT OF JB6 AT FWD EQUIPMENT COMPARTMENT BRACKET SUPPORT OF JB6 AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01Mar 16, 2026 · N279PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR COEA2026062505803Skin · dentedEXTERNAL FUSELAGE SKIN DENTED AT FRAME 11 STRINGER 13L. REPAIRED PER SRM 530000-300-808-A01 REV. 122.Mar 16, 2026 · N803FX · Aerosp ATR72212 · Fuselage Main, Plate/SkinSDR U2RA2026051200018Tension Tie · crackedOPEN HOLE NDI INSPECTION FOUND CRACK SIGNALS AT 1120 R/H TENSION TIE. REPAIR CARRIED OUT PER 8100=9 DATED 05/08/2026 REFF BOEING COMMUNICATION CASE 063200880Mar 16, 2026 · N952CA · Boeing 747428 · Fuselage Main, StructureSDR AALA202605110616Dummy Rail · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION RAIL DUMMY Y503.2 BTW FR12 AND FR16 AT FWD GALLEY AREA. CORRODED ARE IS L=1.083 INCH, W=0.821 INCH, D=0.089 INCH. MAINTENANCE REPLACED RAIL DUMMY Y503.2 BTW FR12 AND FR16 AT FWD GALLEY AREA IAW A319 SRM 51-42-11-801, A3Mar 16, 2026 · N9008U · Airbus A319115 · Fuselage, Seat/Cargo Attach FittingsSDR REXA2026050500489Support Bracket · crackedCRACK ON BRACKET SUPPORT OF JB6 AT FWD EQUIPMENT COMPARTMENT BRACKET SUPPORT OF JB6 AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01Mar 16, 2026 · N279PQ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR SWAA2026042880250Angle · crackedCRACKED GUSSET ANGLE, BS 500I, STR 19R IN THE FWD CARGO COMPARTMENT. REPLACED GUSSET ANGLE IAW SRM 51-40-02-0G-0, AND DWG 143A7902, SHEET 257, REV B.Mar 16, 2026 · N8640D · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042880251Angle · crackedCRACKED ANGLE, FWD FACE BS 500H, STR 26R IN THE FWD CARGO COMPARTMENT. REPLACED THE ANGLE IAW SRM 51-40-02 AND DWG: 143A7505 SHEET: 138 REV -.Mar 16, 2026 · N8640D · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042880253Angle · crackedCRACKED ANGLE, FWD FACE BS 500G, STR 26R IN THE FWD CARGO COMPARTMENT. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 143A7505, SHEET 138, REV-.Mar 16, 2026 · N8640D · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042880254Angle · crackedCRACKED ANGLE, AFT FACE BS 500G, STR 26R IN THE FWD CARGO COMPARTMENT. REPLACED THE ANGLE IAW SRM 51-40-02, AND DWG 143A7502, SHEET 37, REV -.Mar 16, 2026 · N8640D · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042880255Angle · crackedCRACKED GUSSET ANGLE, BS 500I, STR 21L AT FWD CARGO COMPARTMENT. REPLACED THE GUSSET ANGLE IAW SRM 51-40-02-0G-0, AND DWG 143A7902, SHEET 257, REV B.Mar 16, 2026 · N8640D · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042880259Angle · crackedCRACKED ANGLE, FWD FACE BS 500G AT LEVEL STR 26L IN THE FWD CARGO COMPARTMENT. REPLACED ANGLE AND FASTENERS IAW SRM 51-40-02, AND DWG 143A7505, SHEET 138 REV-.Mar 16, 2026 · N8640D · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042880423Angle · crackedCRACKED ANGLE, LOCATED AFT FACE BS 400 AT LEVEL STR 26L IN THE FWD CARGO COMPARTMENT. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, STEP 9, AND DWG 143A7505 SHEET 137 REV-.Mar 16, 2026 · N8640D · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042880256Angle · crackedCRACKED ANGLE, LOCATED AFT FACE BS 500H AT LEVEL STR 26L AT FWD CARGO COMPARTMENT. REPLACED ANGLE-CLIP LOCATED AFT FACE BS 500H AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW SRM 51-40-02 AND DWG 143A7502 SHEET:37 REV-.Mar 16, 2026 · N8640D · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042880257Angle · crackedCRACKED ANGLE, LOCATED FWD FACE BS 500H AT LEVEL STR 26L AT FWD CARGO COMPARTMENT. REPLACED ANGLE-CLIP LOCATED FWD FACE BS 500H AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW SRM 51-40-02 AND DWG 143A7505 SHEET:138 REV-.Mar 16, 2026 · N8640D · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042780252Intercostal · crackedCRACKED INTERCOSTAL LOCATED BTW BS 500A - 500B, STR 26R, FWD CARGO COMPARTMENT. REPLACED THE INTERCOSTAL IAW SRM 51-40-02-0G-0, AND DWG 143A7505, SHEET 137, REV -.Mar 16, 2026 · N8640D · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042780424Web · crackedCRACK ON WEB LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 26L AT FWD CARGO COMPARTMENT. REPLACED WEB LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW SRM 51-40-02 AND 143A7505 SHEET 137, REV-.Mar 16, 2026 · N8640D · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026042780258Angle · crackedCRACKED ANGLE LOCATED AFT FACE BS 500G AT LEVEL STR 26L AT FWD CARGO COMPARTMENT. REPLACED ANGLE AND FASTENERS LOCATED AFT FACE BS 500G AT LEVEL STR 26L AT FWD CARGO COMPARTMENT IAW SRM 51-40-02 AND DWG 143A7502 SHEET 37 REV-.Mar 16, 2026 · N8640D · Boeing 7378H4 · Fuselage Miscellaneous Structure