Service difficulty reports

1,771,154 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 J7SA2026081300511Acm · overtempDIVERSION DUE TO PACK TEMP HIGH CAS WITH A HIGH PITCH WHISTLE FROM THE VENTS, A LIGHT BURNING ODOR AND RISING CABIN TEMPERATURE, NOTED WHILE EXECUTING A MISSED APPROACH AT KOXC. CREW CONTINUED TO KHPN. REPLACED AIR CYCLE MACHINE IAW BD 100 AMM 21-52-13. OPS CHAug 3, 2026 · N527FX · Bombdr BD1001A10 · Cabin Cooling SystemSDR IPXA2026081391163Angle · crackedCRACK-ANGLE, BULK CGO OVERHEAD M/D FLOOR BEAM STRUCTURE ATTACHED AT STA 1580 , ADJACENT RBL 70 AREA.(REPLACE) ACCOMPLISHED JOB I.A.W UPS EO-98247-REQ1 REV 1 AND SRM 51-40-02-0G REV.55 AND BOEING DWG:657T1332 SHEET 5 REV: A.Aug 3, 2026 · N362UP · Boeing 767346 · Fuselage Miscellaneous StructureSDR IPXA2026081387667Plate · wornNR 1 STRUT AFT FAIRING,INBOARD SUPPORT STIFFENER LINK PLATE BEARING WORN , BS 376.20. (REPLACE)1 ACCOMPLISHED JOB I.A.W UPS E0-98274-REQ1 REV.1 AND EGAT EI F2026A54M-1622 REV.1 AND SRM 51-40-02-0G REV.55 AND DWG 313T2303, SH.96, REV.C AND DWG 313T2303 SH.99 RAug 3, 2026 · N362UP · Boeing 767346 · Nacelle/Pylon, Main FrameSDR CALA2026081318549Spar · corrodedFOUND CORROSION AT LEFT WING INBD FRONT SPAR BOOST PUMP UPPER SIDE. REMOVED CORROSION AT LT WING INBD FRONT SPAR BOOST PUMP UPPER SIDE , FOUND AREA TO BE WITH LIMITS IAW SRM 57-20-10-1A-3.Aug 3, 2026 · N16709 · Boeing 737724 · Wing SparSDR SWAA2026080479015Tire · blownNOSE TIRE BLOWN ON LANDING ROLL. ACCOMPLISHED CONDITIONAL INSPECTION PER AMM 05-51-54 AND 71-00-00. NO EVIDENCE OF ENGINE CORE INGESTION ON EITHER ENGINE. ACCOMPLISHED CONDITIONAL INSPECTION PER AMM 05-51-54 NO ADDITIONAL DEFECTS NOTED OTHER THAN AIR/GRND CONDAug 3, 2026 · N8653A · Boeing 7378H4 · TireSDR IPXA2026081187679Angle · crackedTHE BULK CARGO INBOARD ANGLE AT BS 1578, RBL 80 IS CRACKED. INSTALLED A NEW ANGLE IAW SRM 51-40-02-0G, REV 95 AND DWG 146T5650 SH 5 REV.C.Aug 3, 2026 · N331UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR AALA202608121997Attach Angle · crackedAIRCRAFT IN BASE MAINTENANCE: UPON REMOVAL OF RT HEAT EXCHANGER FOUND VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT IB SIDE AT STA 663, RBL5 TO RBL12.. MAINTENANCE REPAIRED RH VAPOR BARRIER ATTACH ANGLE IN RH ECS BAY AT STA 663, RBL5 TO RBL12 IAW B737 SRM 57-10Aug 3, 2026 · N352PS · Boeing 737823 · Fuselage Main, Attach FittingsSDR AALA202608128975Attach Angle · crackedAIRCRAFT IN BASE MAINTENANCE: UPON REMOVAL OF LH HEAT EXCHANGER FOUND VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT IB SIDE AT STA 663, LBL5 TO LBL 12. MAINTENANCE REPAIRED LH HEAT EXCHANGER VAPOR BARRIER UPPER ATTACH ANGLE AT IB SIDE AT STA 663, LBL5 TO LBL 12 Aug 3, 2026 · N352PS · Boeing 737823 · Fuselage Main, Attach FittingsSDR IPXA2026080892392Splice Plate · corrodedUPON REMOVAL OF RT ELEVATOR TIP TRAILING EDGE WEDGE FOUND CORROSION ON UPPER SPLICE PLATE AND UPPER CONDUCTIVE FRAME. INSTALLED ONE UPPER SPLICE PLATE AT RT ELEVATOR IAW SRM 51-40-02-0G-0, & DWG 183N2901.Aug 3, 2026 · N438UP · Boeing 75724APF · Elevator Miscellaneous StructureSDR AALA202608113266Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 6 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42Aug 3, 2026 · N9019F · Airbus A319115 · Horizontal Stabilizer StructureSDR AALA202608117276Hinge 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 3, 2026 · N9019F · Airbus A319115 · Horizontal Stabilizer StructureSDR DALA2026081104618Indicator · inoperativeFWD 1L DOOR SLIDE LIGHT INOPERATIVE. FWD TO MEL 52-11-01. (9140462) (AIRCRAFT GROUNDED).Aug 3, 2026 · N1200K · Boeing 767332 · Door Warning SystemSDR SWAA2026081014795Battery Pack · inoperativeEMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1695 ARE INOPERATIVE. REPLACED THE BATTERY PACK M1695 AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-06-960-805.Aug 3, 2026 · N8687A · Boeing 7378H4 · Emergency LightingSDR IPXA2026080987685Support · crackedNR 1 STRUT AFT FAIRING, INBD ZEE CRACK , BS 376.20. REMOVED DAMAGE ZEE INBD SEAL IAW SRM 51-40-02-0G, REV.55. INSTALLED NEW ZEE INBD SEAL IAW SRM 51-40-02-0G REV.55 AND DWG 313T2380, SH 48, REV -, DWG 313T2303, SH 92, REV: C, SH 93 REV: C, SH 98 REV B.Aug 3, 2026 · N362UP · Boeing 767346 · Nacelle/Pylon, Main FrameSDR IPXA2026080988147Former · crackedCRACKED FORMER , LT WING OTBD FXD LE NOSE SKIN SUPPORT, OSS 648.60. INSTALLED A NEW FORMER IAW SRM 51-40-02-0G REV.95 AND DWG NR 114T2163 SH 1 REV. E, AND EO SREO-50900-REQ001 REV2.Aug 3, 2026 · N331UP · Boeing 76734AF · Wing Main, Frame StructureSDR IPXA2026080889776Bracket · chafedCHAFED BRACKET , NR 1 ENG RT T/R COWL LOWER FWD CLOSURE DOOR T/E ATTACHED. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G, REV.55. INSTALLED A NEW BRACKET IAW SRM 51-40-02-0G, REV.55 AND IPC 78-32-22, REV 96.Aug 3, 2026 · N362UP · Boeing 767346 · Engine Thrust ReverserSDR IPXA2026080889497Former · crackedRIGHT WING OUTBOARD L/E NOSE FORMER CRACK , OSS 499 (NR 8 SLAT OUTBOARD SEAL DOOR UPPER AREA). REMOVED DAMAGE FORMER IAW SRM 51-40-02-0G, REV 55. INSTALLED A NEW FORMER IAW SRM 51-40-02-0G, REV 55 AND DWG 114T2161, SH 3, REV B, AND SREO-50900-REQ001, REV Aug 3, 2026 · N362UP · Boeing 767346 · Wing Main, Frame StructureSDR AALA202608103770Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 3 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42Aug 3, 2026 · N583UW · Airbus A321231 · Elevator StructureSDR AALA202608102212Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 4 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42Aug 3, 2026 · N583UW · Airbus A321231 · Elevator StructureSDR AALA202608105975Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 6 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42Aug 3, 2026 · N583UW · Airbus A321231 · Horizontal Stabilizer StructureSDR AALA202608107122Hinge 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 3, 2026 · N583UW · Airbus A321231 · Horizontal Stabilizer StructureSDR AALA202608109038Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 5 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42Aug 3, 2026 · N583UW · Airbus A321231 · Horizontal Stabilizer StructureSDR AALA202608103137Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 1 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42Aug 3, 2026 · N583UW · Airbus A321231 · Elevator StructureSDR HNAA202608100646O-Ring · leakingEXHAUST FUME SMELL IN COCKPIT. APU BLEED SYSTEM. R&R APU BLEED VALVE O-RINGS IAW AMM 36-12-03. OPS CHECKED GOOD. LEAKS CHECK GOOD.NO OTHER OR FUMES IN COCKPIT OR CABIN.OK FOR SERVICE AT THIS TIME.Aug 3, 2026 · N644AE · Emb EMB145LR · Compressor Bleed ValveSDR REXA2026081001537Battery Pack · inoperativeFOUND FWD RT EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R LIGHT BULB. OPS TEST FAILED. SUSPECT INOPERATIVE HOUSING. NO FIX. DEFERRING RT FWD EMERGENCY LIGHT IAW MEL 33-51-2A. PLACARD INSTALLED. R & R EMERGENCY LIGHT IAW AMM 33-51-15. R & R BATTERY PACK 1 &Aug 3, 2026 · N297PQ · Cndair CL6002D24 · Emergency LightingSDR SWAA2026080773268Flashlight · inoperativeFLASHLIGHT INOPERATIVE. AFT CAPT SIDE JUMPSEAT AFT CA SIDE I/B FLASHLIGHT. OK TO CONTINUE ON MEL 25-64-02A SP1B. R & R AFT CAPT SIDE I/B FLASHLIGHT PER SIP.Aug 3, 2026 · N8717M · Boeing 7378 · Emergency EquipmentSDR SWAA2026080712151Bracket · inoperativeFLIGHT DECK FIRE EXTINGUISHER BRACKET WILL NOT STAY LATCHED R&R FLT DECK FIRE EXTINGUISHER BRACKET PER AMM 26-26-01Aug 3, 2026 · N8583Z · Boeing 7378H4 · Emergency EquipmentSDR SWAA2026080706421Handle · detachedFORWARD ENTRY ASSIST HANDLE IS NOT ATTACHED, ADJUSTED HANDLE IAW SIPAug 3, 2026 · N7744A · Boeing 7377BD · Passenger/Crew DoorsSDR SWAA2026080791823Battery · inoperativeFWD MEGAPHONE GREEN LIGHT NOT TESTING RPL BATTERIES AT FWD MEGAPHONE IAW AMM 25-64-00. NEW PLACARD INSTALLED. OPS CHK GOOD.Aug 3, 2026 · N8907L · Boeing 7378 · Emergency EquipmentSDR SWAA2026080728678Sign · missingLEFT AFT GALLEY EXIT SIGN MISSING ABOVE CABINET 4B-11. REPLACED THE MISSSING LT AFT GALLEY EXIT SIGN ABOVE CABINET 4B-11 IAW THE APPLICABLE STEPS IAW AMM 33-51-01. REPLACED THE MISSSING LT AFT GALLEY EXIT SIGN COVER ABOVE CABINET 4B-11 IAW THE APPLICABLE STEAug 3, 2026 · N8921Q · Boeing 7378 · Emergency LightingSDR SWAA2026080718742Flashlight · inoperativeRIGHT FLASHLIGHT UNDER THE FWD GALLEY JUMPSEAT INOPERATIVE. REMOVED AND REPLACED CABIN FWD INBD FLASHLIGHT AND BATTERY IAW AMM 25-64-00.Aug 3, 2026 · N8869L · Boeing 7378 · Emergency EquipmentSDR SWAA2026080700310Retainer · missingL1 DOOR GIRT BAR RETAINING CLIP HAS MISSING FASTENER INSTALLED RIVET AT L1 DOOR GIRT BAR RETAINING CLIP IAW ARM 51-40-02Aug 3, 2026 · N955WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2026080780281Flashlight · inoperativeCOCKPIT EMERGENCY FLASHLIGHT INOPERATIVE. R & R COCKPIT EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-64-00, OPS CHKD GOOD.Aug 3, 2026 · N8870K · Boeing 7378 · Emergency EquipmentSDR MASA20260807198Shear Panel · corrodedDURING HEAVY INSPECTIONS OF CFIII WET AREA, CORRODED MID SHEAR PANEL AT FR 87 TO FR 88, RBL 11 TO LBL 11. REMOVED AND REPLACED IAW SRM 51-42-01. NRC 4502680-1000-0058, REV 45.Aug 3, 2026 · N85358 · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR MASA20260807197Floor Support · corrodedDURING HEAVY CHECK INSPECTIONS OF CF ILL WET AREA, CORRODED FLOOR SUPPORT PANEL, AT FR 88 TO FR 90 UH, LBL 45 REMOVED AND REPLACED IAW ERJ 175 SRM 51-41-01, SRM 51-42-01 AND'SRM 51-43-01. NRC # 4502680-1000-0057. REV 45 DATED MAY-28-2021 AND REV 46 DATED DEC-0Aug 3, 2026 · N85358 · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR MASA20260807192Gusset · corrodedDURING HEAVY CHECK, INSPECTIONS OF CFIII FLOOR STRUCTURE, CORRODED FLOOR SUPPORT GUSSET AT FR 90 R/H, RBL 11HAS BEEN REMOVED AND REPLACED IAW ERJ 175 SRM 51-41-02. NRG# 4502680-1000-0052, REV 45 MAY-28-2021.Aug 3, 2026 · N85358 · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR IPXA2026080789540Skin · debondedDISBOND - SKIN , LT WING T/E OUTBD FLAP INBD LWR. (REPAIR). IAW SRM 57-53-01-2R-1 REFER TO SRM 51-70-07-0G-0 REV.55. PERFORM REPAIR AS BELOW STEP:1.1 REMOVED THE DISBOND MATERIALS AND CLEANED. MEASURE THE DAMAGE SIZE AND LOCATION (L:4.5", W:2", 1.3" FROM AFAug 3, 2026 · N362UP · Boeing 767346 · Trailing Edge FlapsSDR IPXA2026080790105Wedge · debondedDEBONDED SKIN , LT WING NR 4 SLAT TE WEDGE INBD. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE DAMAGE AREA I.A.W. 767-300F SRM 57-43-02-2R-1. INSTALL THE REPAIR CORE PLUG, FILLER AND INTERNAL DOUBLER WITH FILM ADHESIVE AND COMPOUND I.A.W. 767-300F SRM 51-70-10-2R-Aug 3, 2026 · N331UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA2026080792047Antenna · erodedFOUND V.S.T HF ANTENNA (321E) EROSION. REMOVE THE EROSION MATERIALS AND CLEAN IAW SRM 55-30-01-2R-6 REFER TO SRM 51-70-07-0G-0 REV. 95. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260°F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG.Aug 3, 2026 · N331UP · Boeing 76734AF · HF Communications SystemSDR MASA20260807191Floor Support · corrodedDURING HEAVY CHECK INSPECTIONS FOR CFIII WER AREA, CORRODED FLOOR SUPPORT AT FR 89 R/H, RBL 11, REMOVED AND REPLACED IAW ERJ 175 SRM 51-43-03. NRC# 4502680-1000-0051, REV# 50 DATED OCT-20-2023.Aug 3, 2026 · N85358 · Emb ERJ170200LR · Fuselage Miscellaneous StructureSDR BAGA2026080700003Hydraulic Line · leakingHYD 3 LO PRESS IN FLIGHT AT FL310. ALL HYD QTY LOST. HYD SYSTEM 3 WAS SHUTOFF AS PER QRH. HYD QTY DRAINED TO 8% PRIOR TO QRH PROCEDURE AND COMPLETLY DRAINED TO 0% FOLLOWING QRH TO TURN ON HYD PUMP 3A AND 3B. REMOVED AND REPLACED HYD COIL LINE TO LOWER RUDDER PAug 3, 2026 · N245BZ · Airbus BD5001A11 · Hydraulic System, MainSDR CALA2026080718360Control Valve · faultedRIGHT PACK LIGHT ILLUMINATED. AFTER ENG SHUTDOWN AT GATE. OPENED ECS RT PACK BAY, BURNED OIL ODOR PRESENT. TROUBLESHOT DOWN TO RT PACK, WITH PACK OFF, NO ODOR PRESENT. MEL 2101B APPLIED FOR RT PACK INOP. FIM 21-00 TASK 801 FOR RT PACK WARNING LIGHT ON, AAug 3, 2026 · N86534 · Boeing 737824 · Cabin Cooling SystemSDR CALA2026080718343Attach Angle · crackedFWD CARGO COMPARTMENT INTERCOSTAL ATTACH ANGLE IS CRACKED AT BS 500H, S26R. REMOVED CRACKED ATTACH ANGLE AND BAFFLE AND REPLACED WITH NEW IAW SRM 51-40-02, 51-40-05, & DWG 143A7505 REV-.Aug 3, 2026 · N77539 · Boeing 737824 · Fuselage Main, Attach FittingsSDR AALA202608061556Pin · missingAIRCRAFT WAS GROUNDED: FA ADVISES SHORTLY AFTER TAKEOFF LOUD SQUEAL FROM L1 FORWARD ENT RY DOOR. NOICE SEEMED TO BE COMING FROM DOOR HINGE AREA. REPEAT WRITE UP. AIRCRAFT RETURNED TO ORD NO EMERGENCY DECLARED AND LANDED WITHOUT INCIDENT. MAINTENANCE WHILE INSPAug 3, 2026 · N921NN · Boeing 737823 · Passenger/Crew DoorsSDR YENA2026080600655Pump · failedFLT # 811, BOS-ORD(EMERGENCY DECLARED). HYD 1 LO QTY EICAS AT 36000. HYD 1 LO PRESS EICAS DESCENDING THROUGH 28000; FOR CORRECTIVE ACTION REFERENCE LP 4707576 ITEM 1 & 2 R/R OF PRIORITY HYD VALVE AND R/R OF ENG 1 EDP; FOUND MAJOR LEAK FROM LANDING GEAR PRIORITAug 3, 2026 · N3142J · Airbus BD5001A11 · Hydraulic Pump (Electric/Engine), MainSDR YENA2026080600654Priority Valve · failedFLT # 811, BOS-ORD(EMERGENCY DECLARED). HYD 1 LO QTY EICAS AT 36000. HYD 1 LO PRESS EICAS DESCENDING THROUGH 28000; FOR CORRECTIVE ACTION REFERENCE LP 4707576 ITEM 1 & 2 R/R OF PRIORITY HYD VALVE AND R/R OF ENG 1 EDP; FOUND MAJOR LEAK FROM LANDING GEAR PRIORITAug 3, 2026 · N3142J · Airbus BD5001A11 · Landing Gear Retraction/Extension SystemSDR DALA2026080604553Skin · punctured2 INCH PUNCTURE ON LT HORIZONTAL STAB UPPER SKIN, 13 INCHES FROM INBD EDGE AND 23 INCHES AFT OF LEADING EDGE. REPAIRED IAW SRM 51-70-10 (1736261) (AIRCRAFT GROUNDED)Aug 3, 2026 · N594NW · Boeing 757351 · Horizontal Stabilizer, Plate/SkinSDR AALA202608061557Elec Connector · not seatedAIRCRAFT IN BASE MAINTENANCE: EMERGENCY LIGHTS TEST SHOWS FAULT EMERGENCY POWER SUPPLY UNIT COMMUNICATION FORWARD LEFT - MAINTENANCE CHECKED EMERGENCY POWER SUPPLY UNIT CONNECTION AND RECONNECTED PER TSM 33-51-00-810 WHICH RESLUTED IN THE FAULT BEING CLEAREDAug 3, 2026 · N711UW · Airbus A319112 · Light System WiringSDR AALA202608066833Elec Connector · not seatedAIRCRAFT IN BASE MAINTENANCE: EMERGENCY LIGHTS TEST SHOWS FAULT EMERGENCY POWER SUPPLY UNIT INTERNAL LOAD FORWARD LEFT - MAINTENANCE CHECKED EMERGENCY POWER SUPPLY UNIT CONNECTION AND RECONNECTED PER TSM 33-51-00-810 WHICH RESLUTED IN THE FAULT BEING CLEAREDAug 3, 2026 · N711UW · Airbus A319112 · Light System WiringSDR AALA202608065063Elec Connector · not seatedAIRCRAFT IN BASE MAINTENANCE: EMERGENCY LIGHTS TEST SHOWS FAULT EMERGENCY POWER SUPPLY UNIT COMMUNICATION AFT LEFT - MAINTENANCE CHECKED EMERGENCY POWER SUPPLY UNIT CONNECTION AND RECONNECTED PER TSM 33-51-00-810 WHICH RESLUTED IN THE FAULT BEING CLEAREDAug 3, 2026 · N711UW · Airbus A319112 · Emergency Lighting