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 EE4Y2026042124344Box Beam · crackedDURING THE EXECUTION OF ALLEGIANT WORK CARD A32X—53-240-001_P1-OP-UP-UF IT WAS FOUND AT THE UPPER FUSELAGE AT FR43 S15 AREA AND Y+1650.0 SIDE BOX BEAM, OPEN FASTENR HOLE WITH CRACK INDICATION. REPAIRED UPPER FUSELAGE AT FR 43,STR 15 LH AND Y+1650.0 SIDE BOXApr 22, 2026 · N292NV · Airbus A320214 · Fuselage Main, StructureSDR EE4Y2026042124343Box Beam · crackedDURING THE EXECUTION OF ALLEGIANT WORK CARD A32X—53-240-001_P1-OP-UP-UF IT WAS FOUND AT THE UPPER FUSELAGE AT FR43 S15 AREA AND Y-1650.0 SIDE BOX BEAM, OPEN FASTENR HOLE WITH CRACK INDICATION. REPAIRED UPPER FUSELAGE AT FR 43,STR 15 RH AND Y-1650.0 SIDE BOX Apr 22, 2026 · N292NV · Airbus A320214 · Fuselage Main, StructureSDR FDEA202604220492Slat System · faultedLEADING EDGE SLAT DISAGREE CAUTION MESSAGE APPEARED WHEN FLAPS WERE SELECTED FROM ZERO TO ONE. WE DECLARED AN EMERGENCY OUT OF AN ABUNDANCE OF CAUTION. RAN THE QRH FOR THE PROCEDURE. THE SLATS WERE RESTORED IN THE ALTERNATE MODE. LANDING UNEVENTFUL AT Apr 22, 2026 · N182FE · Boeing 7673S2F · Leading Edge Slat Control SystemSDR AALA202604229933Power Supply · no testAIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT 13WL FAILED BITE TEST IN REFERENCE WITH JOB CARD 26L00005005. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 13WL IN REFERENCE WITH AMM 33-51-38,Apr 22, 2026 · N665AW · Airbus A320232 · Emergency LightingSDR QR9R2026042200001Bleed Valve · no indicationDURING START RUN-UP ENG NR 2 BLEED VALVE WOULD NOT INDICATE ON CAD BEFORE TAKEOFF. MTF MOC REVEALED #2 BLEED VALVE INDICATED CLOSED AFTER START. DURING THE BLEED VALVE CHECK, THE LIGHT DID NOT INDICATE THE VALVE OPENING OR CLOSING. REMOVED AND REPLACED BLEED VApr 22, 2026 · Bolkms BK117C2 · Compressor Bleed ValveSDR 2026FA0000282Brake Disc · crackedATTACHMENT FLANGE CRACKED THROUGH 270+ DEGREES OF CIRCUMFERENCE - DURING ANNUAL INSPECTION, RT BRAKE DISC/ROTOR DISCOVERED TO HAVE 5 SIZEABLE HOLES AT 90 BEND FROM BODY TO ATTACHMENT FLANGE. SIGNS OF HEAVY CORROSION IN BEND ALSO PRESENT. CRACKS RUNNING BETWEENApr 22, 2026 · N621FW · Cirrus SR22 · Landing Gear Brake SystemSDR JR2R20260422730Panel · corrodedPANEL 195ML HAS EVIDENCE OF CORROSION AROUND SCREW HOLES. REPAIRED PER ETD.Apr 22, 2026 · N89313 · Emb ERJ170200LL · Aerodynamic FairingsSDR SWIA2026042176717Web · crackedCRACKED FLOOR WEB IN FWD EQUIPMENT COMPARTMENT, RIGHT SIDE ADJACENT TO THE ADG PUMP. PERFORMED A REPAIR OF CRACKED FLOOR WEB IN FWD EQUIPMENT COMPARTMENT IAW REO 670-53-11-509 REV -E, AND AMM 20-70-00.Apr 21, 2026 · N614QX · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2026042176430Drag Angle · crackedLH FUSELAGE - TO - VERTICAL STAB FORWARD DRAG ANGLE POSSIBLE CRACK IN THE RADIUS AREA. REPAIRED LT FUSELAGE TO VERTICAL STAB FORWARD DRAG ANGLE IAW SRM 55-31-00-201-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.Apr 21, 2026 · N770SK · Cndair CL6002C10 · Fuselage, Stabilizer Attach FittingsSDR SWIA2026042176379Drag Angle · crackedRIGHT FUSELAGE - TO - VERTICAL STAB FORWARD DRAG ANGLE POSSIBLE CRACK IN THE RADIUS AREA. REPAIRED RT FUSELAGE - TO - VERTICAL STAB FORWARD DRAG ANGLE IAW SRM 55-31-00-201-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.Apr 21, 2026 · N770SK · Cndair CL6002C10 · Fuselage, Stabilizer Attach FittingsSDR SWIA2026042176253Floor Support · out of limitsREMOVE AND DISCARD OLD ANGLE ASSEMBLY. REPLACE WITH NEW SAME AS CC670-33199(-4 OPP) REMOVED AND REPLACED L/H COCKPIT FLOOR SUPPORT ANGLE (CC670-33199-4) WITH NEW PER REF CRJ 550 SRM 51-42-06-001-001-A01 DWG# CC670-33052, REV -G. COMPLIED WITH TASK CARD 51-900Apr 21, 2026 · N703SK · Cndair CL6002C11 · Fuselage Miscellaneous StructureSDR IPXA2026052712905Sidewall Panel · damagedPANEL EXT SURFACE DAMAGED. 5 ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-97691-REQ1 AND VT-MAE EA 300-2555-27-A4503. REV. _.Apr 21, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR VNAA202606060008Web · crackedCRACK ON FLOOR WEB RIGHT SIDE(BELOW ADG PUMP SUPPORT) FS193.00 AT ELECTRICAL BAY. CRACK ON FLOOR WEB RIGHT SIDE(BELOW ADG PUMP SUPPORT) FS193.00 AT ELECTRICAL BAY WAS REPAIRED PER SRM 53-11-43-201-001-A01.Apr 21, 2026 · N606NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202606060007Bracket · crackedCRACK FWD BRACKET SUPPORT OF UPPER ACCUMULATOR. CRACK FWD BRACKET SUPPORT OF UPPER ACCUMULATOR AT FWD EQUIPMENT COMPARTMENT WAS REPLACED CRJ-900 SRM 51-42-21-001-001-A01 AND SRM 51-41-02-001-001-A01.Apr 21, 2026 · N606NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202606060006Bracket · crackedCRACK ON FWD/AFT INBD/OTBD CORNER OF BOX JB6 SUPPORT STRUCTURE AT FWD EQUIPMENT COMPARTMENT. BRACKET ASSY OF BOX JB6 SUPPORT STRUCTURE AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER SRM 51-42-06-001-001-A01.Apr 21, 2026 · N606NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR AALA202606030520Shear Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11.Apr 21, 2026 · N9013A · Airbus A319115 · Fuselage Miscellaneous StructureSDR AALA202606034148Shear Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SHEAR PLATE AT FR 69 AND S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.Apr 21, 2026 · N9013A · Airbus A319115 · Fuselage Miscellaneous StructureSDR ASAA2026042166368Transition Panel · corrodedRH SIDEPLATE TRANSITION PANEL IS CORRODED IN MULTIPLE SPOTS FROM STA 500 - 500K. GROUNDED - YES. REMOVED AND REPLACED R/H TRANSITION PANEL I.A.W. B737-900 SRM 53-00-53-2R-6W= 1" 2= .040 R= .030 L= 1' D= .010.Apr 21, 2026 · N464AS · Boeing 737990ER · Fuselage Miscellaneous StructureSDR 2026FA0000463Stiffener · crackedR/H WING FWD LWR I/B SKIN, AFT STIFFENER CRACKED. REPLACED WITH NEWApr 21, 2026 · N612G · Piper PA28181 · Wing Miscellaneous StructureSDR 2026FA0000454Skin · crackedR/H WING AFT WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITHNEWApr 21, 2026 · N612G · Piper PA28181 · Wing, Plate/SkinSDR 2026FA0000450Skin · crackedR/H WING FWD WING WALK SKIN CRACKED ON CORRUGATED SKIN. REPLACED WING WALK SKIN ASSY WITHNEWApr 21, 2026 · N612G · Piper PA28181 · Wing, Plate/SkinSDR 2026FA0000435Stringer · bentAIRCRAFT FAILED THE INSPECTION CRITERIA OUTLINED IN TEXTRON SERVICE LETTER SEL-53-04, DATED JANUARY 14, 2026. BOTH UPPER STRINGERS IN THE TAILCONE ASSEMBLY (P/N'S 0512001-9 AND 0512001-10) HAVE BENDS IN EXCESS OF THE 0.040" LIMIT DESCRIBED IN THE SERVICE LETTEApr 21, 2026 · N82MH · Cessna 172S · Fuselage Main, Longeron/StringerSDR SWAA2026052791636Strap · corrodedCORROSION ON STRAP LOCATED APROX OSS 60 LEADING EDGE AT LT WING. PERFORMED REPAIR ON STRAP LOCATED BTW OSS 26.92 TO OSS 109.69 LEADING EDGE AT LT WING IAW EA 26-157-01100-WIP1 AND 26-157-01100-WIP2 AND B737-800 SRM 57-20-01-2R-3 REPAIR 3.Apr 21, 2026 · N8645A · Boeing 7378H4 · Wing Miscellaneous StructureSDR IPXA2026052501937Skin · dentedR/H OUTBOARD FLAP, BOTTOM INBOARD SIDE APPROX 15IN FROM INNER SIDE HAD 6 DENTS. REPAIR DENTS ON LOWER SURFACE OF LOWER PANEL ON R/H WING OUTBD T/E FLAP NEAR OTEF STA 25 I.A.W. UPS EO-97203-REQ3 REV.1 AND EGAT EI NO. F2026A57M-1046 REV.1Apr 21, 2026 · N371UP · Boeing 767300 · Trailing Edge FlapsSDR IPXA2026042900034Latch · no testENG #2 O/B FAN COWL PRESSURE RELIEF DOOR LATCH TEST FAILED. REPLACED 1EA DOOR LATCH AT ENG. #2 O/B FAN COWL PRESURE RELIEF DOOR IAW A300-600 SRM 51-40-21-001.Apr 21, 2026 · N163UP · Airbus A300F4622R · Nacelle/Pylon, Main FrameSDR IPXA2026052101937Skin · dentedRT OUTBOARD FLAP, BOTTOM INBOARD SIDE APPROX 15IN FROM INNER SIDE HAD 6 DENTS ACCOMPLETED RII ITEM CHECK FOR STEP 10.Apr 21, 2026 · N371UP · Boeing 767300 · Trailing Edge FlapsSDR AALA202605217609Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT TRANSITION PANEL AT STA 727D PLUS 6 INCHES AND AT S24R. REPAIRED TRANSITION PANEL PER SRM 51-10-02.Apr 21, 2026 · N954NN · Boeing 737823 · Fuselage Miscellaneous StructureSDR ASAA2026042166209Transition Panel · corrodedAFT CARGO BAY, RH SIDEPLATE TRANSITION PANEL HAD SPOTS OF CORROSION BS 727C - 767. GROUNDED - YES. REMOVED AND REPLACED R/H SIDEPLATE TRANSTION PANEL USING SLPICE FROM BS 727+4 - 767 IAW SRM 53-0053-2R-5, REPAIR 5. W=.800" O=.040 R=.031 L=26" D=.009.Apr 21, 2026 · N464AS · Boeing 737990ER · Fuselage Miscellaneous StructureSDR ASAA2026042166208Transition Panel · corrodedAFT CARGO BAY, LT SIDEPLATE TRANSITION PANEL HAD SPOTS OF CORROSION BS 727+4 - 727K. GROUNDED - YES. REMOVED AND REPLACED THE AFT CARGO LT SIDEPLATE TRANSITION PANEL USING SPLICE REPAIR FROM BS 727A+4 - 847 IAW SRM 53-00-53-2R-5.Apr 21, 2026 · N464AS · Boeing 737990ER · Fuselage Miscellaneous StructureSDR SWAA2026052091503Skin · delaminatedLEFT WING OUTBOARD AFT FLAP UPPER SURFACE IS DELAMINATED AT I/B END. REMOVED LEFT WING OTBD AFT FLAP IAW AMM 27-51-22. SET INBD AND OTBD ROLLERS ON NEW LT WING OTBD AFT FLAP TO NOMINAL POSITION IAW AMM 27-51-22. INSTALLED LEFT WING OUTBOARD AFT FLAP PER AMM Apr 21, 2026 · N8538V · Boeing 7378H4 · Trailing Edge FlapsSDR HNAA2026052000420Frame · crackedCRACKED FRAME 72, BETWEEN STRINGER 17L AND 16L. R & R FRAME 72 IAW ETD-2026-145-007557 AND EO1-53-26-0206.Apr 21, 2026 · N655AE · Emb EMB145LR · Fuselage Main, FrameSDR HNAA2026052000419Stringer Splice · chafedSTRINGER 19R (INTERIOR STRINGER) STRINGER SPLICE BETWEEN FR 52/53 CHAFED. REMOVED AND REPLACED STGR 19R SPLICE BTW FR 52-53 IAW EMB 145 SRM 51-40-02.Apr 21, 2026 · N655AE · Emb EMB145LR · Fuselage Main, Longeron/StringerSDR HNAA2026052000406Structure · corrodedGALLEY FLOOR, FWD DIGITAL BETWEEN FR 16-17, STGR 18L-19L AROUND NUT PLATE HOLE HAS CORROSION. PERFORMED DOUBLER ON GALLEY FLOOR FWD DIGITAL BETWEEN FR 16-17, STGR 18L-19L IAW EMB 145 SRM 53-21-10RE ITEM 2 FIG. 201 SHEET 5 DETAIL C AND EO1-05-26-0232.Apr 21, 2026 · N655AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SWAA2026051991430Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS. FLOOR PANEL 231XF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL IAW SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.Apr 21, 2026 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026051991431Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATION OF NEW 241AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.Apr 21, 2026 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026051991428Floor Panel · pulledFLOOR PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATION OF NEW 242AF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.Apr 21, 2026 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026051991429Floor Panel · pulledFLOOR PANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATION OF A NEW 241EF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.Apr 21, 2026 · N258WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026051991737Seat Track · corrodedCORROSION ON SEAT TRACK LBL 45 AT BS480+17; BS500+8; BS500A+7; BS500A+18; BS500B+19; BS500D+9. SEAT TRACK WILL BE REPLACED ON FAULT# TTG8Q01BUUY6. REMOVED DAMAGE ON TOP SURFACE OF SEAT TRACK AT DISCREPANCY AREA; REWORKED AREA: L= 1.5'; W= 0.6'; MAX. MATERIAApr 21, 2026 · N258WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2026051991730Seat Track · corrodedCORROSION ON SEAT TRACK LBL 25 AT BS480+17; BS500+8; BS500A+7; BS500A+18; BS500B+19; BS500D+9. SEAT TRACK WILL BE REPLACED ON FAULT# TTG8Q01BUUYA. REMOVED DAMAGE ON TOP SURFACE OF SEAT TRACK AT DISCREPANCY AREA; REWORKED AREA: L= 1.5'; W= 0.6'; MAX. MATERIApr 21, 2026 · N258WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2026042166183Skate Angle · crackedAFT TOP SIDE OF ECS BAY AT BS 661.95 SKATE ANGLE IS CRACKED AT RIVETS ON LEFT SIDE OF THE KEEL BEAM STREAMERS ARE BELOW THE CRACKS. GROUNDED - YES. REPAIRED SKATE ANGLE AT STA 661.95 LBL9 IAW B737-900ER SRM 57-10-10-2R-5. ACCOMPLISHED LEAK CHECK OF REPAIR IAW Apr 21, 2026 · N275AK · Boeing 737990ER · Fuselage Miscellaneous StructureSDR SWAA2026051391619Lens · missingFOUND MISSING LENSE ON OVERHEAD STOWAGE BIN EMERGENCY LIGHT AT LT ROW 4. INSTALLED NEW LENS ON OVERHEAD STOWAGE BIN EMERGENCY LIGHT AT SEAT ROW 4ABC IAW AMM 33-51-03-960-801, STEP D.(3)(C).Apr 21, 2026 · N475WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026051391299Angle · crackedFWD ENTRY DOOR; DOOR TARGET ANGLE CRACK. REMOVED AND REPLACED FWD ENTRY DOOR; DOOR TARGET ANGLE IAW SRM 51-40-02 AND IPC 52-11-00-02B. REMOVED AND REPLACED FWD ENTRY DOOR TARGET ANGLE IAW SRM 51-40-02 AND IPC 52-11-00-02B.Apr 21, 2026 · N475WN · Boeing 7377H4 · Passenger/Crew DoorsSDR AALA202605126316Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN WING CENTER SECTION REAR SPAR VAPOR BARRIER LOWER ATTACH ANGLE LOCATED STA 663 AND LBL 12. ACCOMPLISHED SPLICE REPAIR PER SRM 57-10-10-2R-5.Apr 21, 2026 · N956NN · Boeing 737823 · Fuselage Miscellaneous StructureSDR SWAA2026051191624Plate · crackedCRACK ON CORRUGATED PLATE LOCATED TRAILING EDGE IRSS216 AT LT WING. REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE IRSS216 AT LT WING IAW SRM 51-10-02 SRM 51-40-02 AND DWG 115A2001 SHEET 30 REV A.Apr 21, 2026 · N479WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2026051191623Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED TRAILING EDGE ORSS273 AT LT WING. REPLACED SUPPORT BRACKET LOCATED TRAILING EDGE ORSS273 AT LT WING IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02.Apr 21, 2026 · N479WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2026051191626Bracket · crackedCRACK ON BRACKET LOCATED TRAILING EDGE ORSS 273 AT LT WING. REPLACED BRACKET LOCATED TRAILING EDGE ORSS 273 AT LT WING IAW SRM 51-10-02-0G-0 ITEM 9 SRM 51-40-02-0G-0Apr 21, 2026 · N479WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2026050691337Lens · brokenBROKEN EMERGENCY EXIT LIGHT LENS ON SIDEWALL PANEL 232YHW AT PASSENGER CABIN. REPLACED EMERGENCY EXIT LIGHT LENS ON SIDEWALL PANEL 232YHW AT PASSENGER CABIN IAW AMM 33-51-01-960-801 STEPS 2C.(1)(A)(4) AND 2C.(4).Apr 21, 2026 · N467WN · Boeing 7377H4 · Emergency LightingSDR ASAA2026042165876Mount · corrodedPASSENGER CABIN STA 916.5 LBL 51.55 DUAL FLOOR MOUNT ATTACHING INTERCOSTAL HAS CORROSION AROUND MOUNT. GROUNDED - YES. REMOVED AND REPLACED 147A5690-8 INTERCOSTAL IAW BAC DWG 147A5680 REV - AND B737-800 SRM 51-40-02. ALLOWABLE LIMITS IN SRM FOUND DEEMED OUT OFApr 21, 2026 · N597AS · Boeing 737890 · Fuselage, Equipment Attach FittingsSDR REXA2026050500454Floorbeam · corrodedR/H FS 280 CROSSBEAM IS CORRODED ON CORNER EDGES OF THE BEAM R/H FS 280 CROSSBEAM HAS MULTIPLE CORROSION PITS ON CORNER EDGE OF BEAM. NO LIMITS NOTED IN SRM REQUIRES REPLACEMENT CORRECTIVE ACTION: LOCATED AND DRILLED NEW SERVICEABLE R/H FS 280 CROSSBEAM PN CC6Apr 21, 2026 · N604LR · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR J7SA2026050400480Fce · faultedDURING CRUISE, CREW RECEIVED GND SPLR FAIL CAS. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED AND RIGGED FCE2. OPS CHECK GOOD. WORK PERFORMED IAW AMM 27-03-01.Apr 21, 2026 · N347FX · Emb EMB505 · Flight Management Computing Hardware System