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 HNAA2026061700518Floor Support · corroded00235 OMEGA BEAM GUSSET, MID, FROM FR 53 TO FR 57 HAS CORROSION. REMOVED AND REPLACED WITH NEW AFT WET AREA OMEGA BEAM GUSSET MID FROM FR 53 TO FR 57 IAW EMB 145 SRM 51-40-02-PRMay 7, 2026 · N657AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026061700517Floor Support · corroded00234 FLOOR SILL, RH, FROM FR 53 TO FR 59 HAS CORROSION. REMOVED AND REPLACED RH FLOOR SILL FROM FR 53 TO FR 59 PER EMB 145 SRM 51-40-02 STEP 2, BMay 7, 2026 · N657AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026061700516Bracket · crackedAFT CARGO DOOR MECHANISM BOX FRAME BRACKET ON FR 61 HAS A CRACK. REMOVED AND REPLACED WITH NEW AFT CARGO DOOR MECHANISM BOX FRAME BRACKET ON FR 61 IAW EMB 145 SRM 51-40-02 STEP 2, B AND C.May 7, 2026 · N657AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026061700515Bracket · cracked00216 AFT CARGO DOOR MECHANISM BOX FRAME BRACKET ON FR 61 HAS A CRACK. REMOVED AND REPLACED WITH NEW AFT CARGO DOOR MECHANISM BOX FRAME BRACKET ON FR 61 IAW EMB 145 SRM 51-40-02 STEP 2, B AND C.May 7, 2026 · N657AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR HNAA2026061700514Bracket · gougedRUDDER 2 LOWER SECTION INTERNAL BRACKET IS GOUGED. REMOVED AND REPLACED INTERNAL BRACKET ON RUDDER 2 LOWER SECTION PER SRM 51-40-02.May 7, 2026 · N657AE · Emb EMB145LR · Rudder Miscellaneous StructureSDR 2026FA0000524Slide · fodDURING THE INSPECTION AND TESTING PHASE OF THE MAINTENANCE, A SMALL SCREWDRIVER WAS FOUND INSIDE THE SLIDE ENCLOSURE UNDERNEATH THE INFLATABLE SECTION. A FULL INSPECTION OF THE SLIDE ASSEMBLY WAS CARRIED OUT AND THE FOLLOWING DEFECTS WERE IDENTIFIED: UNIT RECMay 7, 2026 · Escape SlideSDR IPXA2026060970211Panel · delaminatedCOMPOSITE DAMAGE ON INTERIOR OF PANEL BETWEEN STA 1941 AND STA 1963.8 ACCOMPLISH REPAIR IAW SRM REV 124 CHAPTER 51-70-10-2R-4, USING SRM 51-70-10-2R-0 REPAIR GENERAL PER SRM 53-80-01-2R-0May 7, 2026 · N423UP · Boeing 75724APF · Passenger Compartment EquipmentSDR IPXA2026061069790Frame · dentedAFT CARGO COMPARTMENT FRAME UPPER FLANGE HAS A DENT APPROX AT BS 1500, STGR 26R, ACCOMPLISHED REPAIR PER EO-97485-REQ1 AND EA 757-5360-01-B0741, REV. I/R.May 7, 2026 · N417UP · Boeing 75724APF · Fuselage Main, FrameSDR IPXA2026061070206Strap · corrodedAFT CARGO COMPARTMENT CEILING STABILIZATION STRAP HAS CORROSION APPROX BTW BS 1400 AND BS 1420, RBL 24.75, INSTALLED REPAIR SECTION CEILING STRAP STA 1380-1440 RBL 24.75 I.A.W B757-200 SRM 51-40-02- OG -0May 7, 2026 · N417UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026060872812Panel · deformedTHE R/H LWR FWD TORQUE BOX PANEL HAS EXCESSIVE HAIL DAMAGE AND MULTIPLE DISBONDS / DELAMINATIONS ACROSS THE ENTIRE SURFACE OF THE PANEL FROM TOP TO BOTTOM. INSTALLED 1 EA TORQUE BOX PANEL IAW SRM 51-40-02.May 7, 2026 · N423UP · Boeing 75724APF · Vertical Stabilizer Miscellaneous StructureSDR IPXA2026060473078Panel · damagedTHE L/H LWR FWD TORQUE BOX PANEL HAS MULTIPLE DELAMINATIONS / DISBONDS (3EA TOTAL) NEAR THE TOP AND BOTTOM OF THE PANEL. ALL DAMAGE MARKED IN WHITE. INSTALLED NEW PART FWD TORQUE BOX LWR PANEL ASSEMBLY LH IAW SRM 51-40-02-0G-0.May 7, 2026 · N423UP · Boeing 75724APF · Vertical StabilizerSDR IPXA2026061069168Gusset · gougedMAJOR REPAIR NR 2 PYLON LT SIDE AFT STRUT AREA FWD FRAME SUPPORT GOUGED IN 2 PLACES AT LOWER END. ACCOMPLISHED THE PERMANENT REPAIR PER EO-97464-REQ1 AND EA 757-5410-01-B0751, REV IRMay 7, 2026 · N417UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR IPXA2026051570260Strap · corrodedAFT CARGO COMPARTMENT CEILING STABILIZATION STRAP HAS CORROSION APPROX BTW BS 1560 AND BS 1580, LBL 45.50, INSTALLED REPAIR PARTS. AT AFT  COMPARMENT CARGO CEILING STABILIZATION STRAP STA 1543, LBL 45.50 IAW SRM-51-70-11-0G-0.   STEP 8 TO 12. AND INSTALLEDMay 7, 2026 · N417UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026060970356Strap · corrodedAFT CARGO COMPARTMENT CEILING STABILIZATION STRAP HAS CORROSION APPROX AT BS 1240, LBL 45.50, INSTALLED REPAIR PARTS AT AFT CARGO COMPARMENT CEILING STABILIZATION STRAP BETWEEN  STA 1228 TO 1550 LBL 45.50  IAW SRM 51-70-11-0G-0   STEP  10,11 AND 12. AND INSTMay 7, 2026 · N417UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR IPXA2026060970215Strap · corrodedAFT CARGO COMPARTMENT CEILING STABILIZATION STRAP HAS CORROSION APPROX BTW BS 1560 AND BS 1580, LBL 24.75 INSTALLED REPAIR PARTS (2EA SECTIONS AND 2 EA SPLICES) AT AFT CARGO COMP. CEILING STABILIZATION STRAP BS 1540 TO 1611 LBL 24.75 IAW SRM 51-40-02-0G-0May 7, 2026 · N417UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR VNAA202606120022Fitting · corrodedCORROSION FLOOR FITTING IN AFT ACCESS 109 (1EA) ON GALLEY 1. FLOOR FITTING P/N CDSP2019-7C-620 IN AFT ACCESS 109 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-96May 7, 2026 · N563NN · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR SWAA2026061196057Support · corrodedFWD CARGO AFT BULKHEAD LOWER SUPPORT STRUCTURE AT BS 500I, LBL 24, HAS CORROSION. REMOVED AFT BULKHEAD LOWER SUPPORT ANGLE IAW SRM 51-40-02. LOCATED AND DRILLED NEW SUPPORT ANGLE. SRM 51-40-02. INSTALLED NEW SUPPORT ANGLE. SRM 51-21-02.May 7, 2026 · N8540V · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026061103710Seal · wornRIGHT MAIN WHEEL WELL BLADE SEALS (8) ON THE AFT SIDE ARE WORN. REMOVED AND REPLACED RT MAIN WHEEL WELL, WORN BLADE SEALS AS REQUIRED. WORK PERFORMED IAW AMM 32-12-12-401-NG.May 7, 2026 · N8540V · Boeing 7378H4 · Fuselage Main, StructureSDR ASAA2026050766649Web · corrodedFWD CARGO SILL WEB CORRODED STA 440 TO STA 492. GROUNDED - YES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-30-15-1A-1. REMOVED AND REPLACED SILL WEB IAW B737-800 SRM 51-40-02-0G-0W= 1.25 O= .045 R= .035 L= 3.75 D= .010.May 7, 2026 · N558AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026050766643Transition Panel · corrodedFWD CARGO R/H TRANSITION CORRODED FROM STA 500A TO 500E. GROUNDED - YES. REMOVED AND REPLACED DAMAGED SECTION FWD CARGO R/H TRANSITION BETWEEN STA 500A TO 500E IAW B737-800 SRM 51-40-02-0G-0W 1" O .040" R .030 L 4" D .010".May 7, 2026 · N558AS · Boeing 737890 · Fuselage Main, StructureSDR ASAA2026050766642Transition Panel · corrodedFWD CARGO R/H TRANSITION CORRODED FROM STA 500F TO 500I. GROUNDED - YES. REMOVED AND REPLACED DAMAGED SECTION FWD CARGO R/H TRANSITION BETWEEN STA 500F TO 500I IAW B737-800 SRM 51-40-02-0G-0W 1" O .040" R .030" L 4" D .010".May 7, 2026 · N558AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026050766641Transition Panel · corrodedFWD CARGO L/H TRANSITION CORRODED FROM STA 500B TO 500I. GROUNDED - YES. REMOVED AND REPALCED DAMAGED SECTION FWD CARGO L/H TRANSITION FROM STA 500B TO 500I IAW B737-800 SRM 51-40-02-0G-0W 1" O .040" R .032" L 3" D .008".May 7, 2026 · N558AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR SWAA2026061096592Vapor Barrier · crackedCRACK VAPOR VARRIER LOC BS 663 AND LBL 45.64 TO LBL 54.21 AT MAIN WHEEL WELL. REPAIRED VAPOR VARRIER BS 663, LBL 45.64 - 54.21 IN THE MAIN WHEEL WELL IAW SRM 51-70-04-2R-10, REPAIR 10.May 7, 2026 · N7749B · Boeing 7377BD · Fuselage Main, BulkheadSDR SWAA2026060896333Stiffener · crackedCRACKED STIFFENER, FWD BULKHEAD, BS 540, LBL 24.75 IN THE FWD CARGO BAY. REPLACED STIFFENER AND FASTENERS IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 111A2001, SHEET 79, REV -.May 7, 2026 · N253WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026060896527Support Angle · corrodedCORROSION ON SUPPORT ANGLE, BS 727D, STR 27L, WL 156 IN THE AFT CARGO BAY. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, & DWG 146A7810, SHEET 3, REV A.May 7, 2026 · N253WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026060896336Support Angle · crackedCRACKED SUPPORT ANGLE, BS 500D, S28L IN THE FWD CARGO BAY. INSTALLED A NEW SUPPORT ANGLE AND FASTENERS, BS 500D, S28L IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, AND DWG: 143A7902, SHEET 126, REV A.May 7, 2026 · N253WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR IPXA2026051070809Skin · dentedRH FUSELAGE HAS A DENT STA#1355 BETWEEN RBL S-13R & S-14R #58-01. DISCOVERED IN LIMIT DENT INFO DEFERRED IAW UPS EO97560-REQ1, IN LEAVE AS IS CONDITION.May 7, 2026 · N423UP · Boeing 75724APF · Fuselage Main, Plate/SkinSDR VNAA202606060015Fitting · corrodedCORROSION FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1. FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1 WAS REPLACED IAW CMM 25-33-21.May 7, 2026 · N606NN · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026060400933Fitting · corrodedCORROSION FLOOR FITTING IN AFT ACCESS 107 OUT SIDE (1EA) ON GALLEY 1 NEW FLOOR FITTING P/N: A661091-1 IN AFT ACCESS 107 OUT SIDE (1EA) ON GALLEY 1. WAS MANUFACTURED PER EA NO: CRJ953-22230 REV IR. AND REPLACED PER SAFRAN CMM 25-33-67 REV NO. 10 DATED JUN 20/May 7, 2026 · N909XJ · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026060400908Fitting · corrodedCORROSION FLOOR FITTING IN AFT ACCESS 108 (1EA) ON GALLEY 1. FLOOR FITTING IN AFT ACCESS 108 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-67 REV. 10May 7, 2026 · N909XJ · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026060400906Fitting · corrodedCORROSION FLOOR FITTING IN AFT ACCESS 108 (1EA) ON GALLEY 1. FLOOR FITTING IN AFT ACCESS 108 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-67 REV. 10May 7, 2026 · N909XJ · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR REXA2026060400905Fitting · corrodedCORROSION FLOOR FITTING IN AFT AND FWD ACCESS 205 (2EAS) ON GALLEY 2. FLOOR FITTING (PN: A391251-3) IN AFT ACCESS 205 (1 EA) ON GALLEY 2 WAS MANUFACTURED PER EA CRJ953-22214 REV IR AND INSTALLED PER CMM 25-32-84 REV NO. 9 AND FLOOR FITTING ( PN: 9861251-3 IN May 7, 2026 · N909XJ · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR HNAA2026060400483Rivet · misinstalledEXTERNAL RIVET PLUG IMPROPERLY INSTALLED AT BTW FR2-3 AND ABOVE STR14L NEAR UPPER SKIN EDGE. REPAIRED IAW ETD2026-145-008984 AND EO1-53-26-0258May 7, 2026 · N908AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR ASAA2026050766476Baffle · crackedLEFT BAFFLE AND CLIPS CRACKED AT BS 500C TO 500D. GROUNDED - YES. R & R LT BAFFLE AND CLIPS BS 500C - 500D IAW SRM 51-40-02-06-0 & SRM 51-40-05-06-0.May 7, 2026 · N464AS · Boeing 737990ER · Fuselage Miscellaneous StructureSDR SWAA2026060396526Support · corrodedCORROSION SUPPORT ZEE LOCATED BTW BS 727B TO BS 787 LBL 21 WL 156.1 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 847 LBL 21 WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9; DWG# 146A7502; SHEET 27; RMay 7, 2026 · N253WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026060396334Stringer · corrodedCORROSION STRINGER 27L LOCATED STA 540 WL 150.2 FWD CARGO COMPARTMENT. REPLACED REPAIR PARTS [7] STRINGER SECTION; [2] CHANNEL; [3] ANGLES (2EA) AND SHIM LOC. STRINGER 27L BTW BS 500D TO BS 540 FWD CARGO COMPARTMENT IAW SRM 53-00-03-2R-1 REPAIR 1; PARAGRAPH 4.May 7, 2026 · N253WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR HNAA2026060300480Rivet · looseEXTERNAL SKIN: LOOSE RIVET PLUG BTW FR1A-2, BTW STR14-15L. REPAIRED IAW ETD2026-145-008939.May 7, 2026 · N908AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR SWAA2026060296331Stringer · crackedCRACKED STRINGER 25R LOCATED BS 540 WL 156.1 AT FWD CARGO COMPARTMENT. REPAIRED STRINGER 25R LOC. BTW BS 500C TO BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1.May 7, 2026 · N253WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2026060296332Stringer · crackedCRACK STRINGER 27R LOCATED BS 540 WL 156.1 AT FWD CARGO COMPARTMENT. REPLACED REPAIR PARTS STRINGER SECTION, CHANNEL, ANGLES. STR 27R BTW BS500D TO BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; PARAGRAPH 4.K AND DWG 143A3210; SHEEMay 7, 2026 · N253WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2026060296335Stringer · crackedCRACK STRINGER 26L STA 540 FWD CARGO COMPARTMENT. REPLACED REPAIR PARTS LOC 26L STA 500D+10 - 540 FWD CARGO COMPARTMENT. REPLACEMENT STRINGER SECTION CHANNEL ANGLE IAW SRM 53-00-03-2R-1 PARAGRAPH 4.K AND DWG 143A3230; SHEET 122; REV A. REPAIRED STRINGER 26May 7, 2026 · N253WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR R61A2026060100151Support Angle · crackedDURING HEAVY CHECK LT WHEEL WELL CENTER WING BOX FR 52 LWR WING SKIN SUPPORT ANGLE CRACKED. REMOVED AND REPLACED WING SKIN SUPPORT ANGLE IAW SRM 51-41-01 51-42-01 AND 51-43-03May 7, 2026 · N212JQ · Emb ERJ170100LR · Fuselage Miscellaneous StructureSDR SWAA2026060196199Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB RBL 40 STA 663 AT PASSENGER CABIN. PERFORMED PERMANENT REPAIR ON HORIZONTAL PRESSURE DECK LOCATED BETWEEN BS 663 TO BS 675 AND BETWEEN RBL 30 TO RBL 60 IAW SRM 53-40-51-2R-2, REPAIR 2.May 7, 2026 · N477WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026060196200Pressure Deck · crackedCRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 31 STA 663 AT PASSENGER CABIN. PERFORMED PERMANENT REPAIR HORIZONTAL PRESSURE DECK WEB BETWEEN BS 663.75 AND BS 675 BTW LBL 24 TO LBL 60 IAW SRM 53-40-51-2R-2 REPAIR 2.May 7, 2026 · N477WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026060196343Rib · crackedCRACK INSPAR RIB LOCATED STAB STA 120.30 AND 28 INCH FROM FRONT SPAR AT LT HORIZONTAL STABILIZER. PERFORMED PERMANENT REPAIR ON INSPAR RIB LOCATED STAB STA 120.30 AND 28 INCH FROM FRONT SPAR AT LT HORIZONTAL STABILIZER IAW SRM 55-10-09-2R- 4 REPAIR 4.May 7, 2026 · N477WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2026060196567Access Panel · damagedELONGATED HOLE ACCESS PANEL 123YAC AT FWD CARGO COMPARTMENT. FABRICATED ACCESS PANEL 123YAC AT FWD CARGO COMPARTMENT IAW AMM 25-52-01-201-801 STEP 1 F AND DWG 453A1210 SHEET: 5 REV: AMay 7, 2026 · N477WN · Boeing 7377H4 · Fuselage Main, StructureSDR R61A2026060100150Attach Bracket · crackedDURING HEAVY CHECK CF III RT OTBD LATERAL SEAT TRACK ATTACHED BRACKET FOUND CRACKED. REMOVED AND REPLACED LATERAL SEAT TRACK IAW SRM 51-43-08May 7, 2026 · N212JQ · Emb ERJ170100LR · Fuselage, Seat/Cargo Attach FittingsSDR R61A2026060100149Attach Bracket · crackedDURING HEAVY CHECK CF III FR 84 LT OTBD LATERAL SEAT TRACK ATTACHED BRACKET FOUND CRACKED. REMOVED AND REPLACED SEAT TRACK ATTACHMENT BRACKET IAW SRM 51-43-03May 7, 2026 · N212JQ · Emb ERJ170100LR · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026052971327Shim · migratedINTERNAL NACELLE STRUT MIDSPAR FITTING AT REAR BULKHEAD OUTBD. LOWER CORNER AND FORWARD INBD. LOWER HAS SHIM MIGRATION. ACCOMPLISH REPAIR INSTRUCTIONS PER EO-97449-REQ1 AND VT-MAE 757-5451-27-A4487,May 7, 2026 · N423UP · Boeing 75724APF · Nacelle/Pylon Miscellaneous StructureSDR CALA2026060116668Power Supply · faultedIDT INSPECTION REQUIRED.REMOVED EMERGENCY LIGHT OVERHEAD INSIDE PASSENGER COMPARTMENT ABOVE ROWS 20-21 FOR SHEETMETAL ACCESS RESEARCHED ASSIGNMENT, EMERGENCY LIGHTS ARE NO LONGER IDT INSPECTION, NEED INSPECTION TO CONCUR AND REMOVE IDT. ITEM IS NOT AN IDT TRAMay 7, 2026 · N76515 · Boeing 737824 · Emergency LightingSDR SWAA2026052896337Support Angle · crackedCRACK SUPPORT ANGLE, AFT SIDE OF BS 500D, STR 28R IN THE FWD CARGO BAY. REPLACED THE SUPPORT ANGLE AND FASTENERS IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7902, SHEET 126, REV A.May 7, 2026 · N949WN · Boeing 7377H4 · Fuselage Miscellaneous Structure