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 COEA2026072219803Floorbeam · corrodedFLOORBEAM UPPER FLANGE ON R/H FRAME 25 HAS LEVEL 2 CORROSION. CORRECTIVE ACTION: REPAIRED PER U.S. TECHNICAL EO-26165-53-001 REV. NC 6/5/2026.Mar 3, 2026 · N803FX · Aerosp ATR72212 · Fuselage Main, Floor BeamSDR COEA2026070717803Door Frame · crackedDURING HEAVY CHECK, FWD CARGO DOOR FRAME AT BS 7065 WAS CRACKED, SKIN ATTACH FLANGE UPPER END. REPAIRED IAW SRM 523100-300-811-A01 REV. 122.Mar 3, 2026 · N803FX · Aerosp ATR72212 · Fuselage Main, StructureSDR COEA2026070712803Frame · damagedDURING HEAVY CHECK, INTERNAL FUSELAGE FRAME 21 HAD TWO FLAWED HOLES, INBD & OTBD OF STRINGER 5L. REPLACED IAW SRM 51-25-01, 51-25-02 AND 51-25-04 REV. 122.Mar 3, 2026 · N803FX · Aerosp ATR72212 · Fuselage Main, FrameSDR COEA2026062504803Stringer · crackedINTERNAL FUSELAGE, STRINGER 11R FRAMES 23-23D FLAW INDICATIONS FOUND TO BE CRACKS. REPAIRED PER ATR72 SRM 530000-300-826-A01 REV. 122.Mar 3, 2026 · N803FX · Aerosp ATR72212 · Fuselage Main, Longeron/StringerSDR 2026FA0000476Strut · fracturedPIPER PA-18 EXPERIENCED RIGHT HAND LANDING GEAR COLLAPSE AFTER LANDING ROLLOUT CAUSING DAMAGE TO MAIN LANDING GEAR AND RIGHT WING ASSEMBLY. DETAIL INSPECTION FOUND 2 EACH FRACTURES ON RIGHT HAND LANDING GEAR ASSEMBLY. RIGHT SHOCK STRUT HYDRASORB (PN 487 558) FMar 3, 2026 · N1532V · Piper PA18 · Main Landing Gear Strut/Axle/TruckSDR SWIA2026030376083Stringer Splice · corrodedCORROSION FOUND ON STRINGER SPLICE AT STR25R FS333. (C-CHECK RO 05/22/2026)REPLACED STRINGER SPLICE AT STR25R FS333. REF. DWG# SH670-32420 REV: E AND CRJ900 SRM 51-42-06-001-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FORMar 3, 2026 · N899SK · Cndair CL6002D24 · Fuselage Main, Longeron/StringerSDR 3EJA868JS030326Pressure Switch · failedON THE TAKEOFF ROLL PRIOR TO 80, THE R LO FUEL PRESS ILLUMINATED FOLLOWED IMMEDIATELY BY R FUEL BOOST LIGHT.Mar 3, 2026 · N868JS · Cessna 560XL · Fuel Indicating SystemSDR AALA202604234631Attach Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD FRAMING RIGHT HAND UPPER LATERAL ATTACHMENT FITTING AT FR 4 RIGHT. REPLACED FITTING PER EA 373092.Mar 3, 2026 · N194UW · Airbus A321211 · Fuselage Main, StructureSDR AALA202604234376Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD FRAMING RIGHT HAND CONTINUITY FITTING BETWEEN FR 2 AND FR 3 AT Y0. REPLACED CONTINUITY FITTING PER EO 5319Y017-002Mar 3, 2026 · N194UW · Airbus A321211 · Fuselage Main, StructureSDR AALA202604239035Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING BETWEEN FR 2 AND FR 3 AT Y0. REPLACED CONTINUITY FITTING PER EO 5319Y017-002Mar 3, 2026 · N194UW · Airbus A321211 · Fuselage Main, StructureSDR IXX2026F00007Bracket · crackedENGINE NR 2 INBD SJIP FAIRING ACCESS PANEL, LOWER BRACKET TO SIDEWALL MOUNT CRACKED. REF TO XTREME AVIATION NRC 738Mar 3, 2026 · N255CM · Boeing 767223 · Nacelle/Pylon Miscellaneous StructureSDR SWAA2026041676455Scuff Plate · corrodedCORRODED SCUFF PLATES (2) FWD AND AFT SIDE AT AFT CARGO BAY. REPLACED THE SCUFF PLATES IAW SRM 51-40-02.Mar 3, 2026 · N8630B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR IXXA202604130001Cover · wornUPPER INBD FASTENER HAS WORN THROUGH THE AFT SIDE OF THE THROTTLE STRUT CONTROL BOX ON TOP OF #1 PYLON.Mar 3, 2026 · N227AZ · Boeing 767323 · Nacelle/Pylon Miscellaneous StructureSDR IXXA04132026CC02Cover · wornUPPER INBD FASTENER HAS WORN THROUGH THE AFT SIDE OF THE THROTTLE STRUT CONTROL BOX ON TOP OF #1 PYLON.Mar 3, 2026 · N227AZ · Boeing 767323 · Nacelle/Pylon Miscellaneous StructureSDR IXXA202604130002Cover · wornUPPER INBD FASTENER HAS WORN THROUGH THE AFT SIDE OF THE THROTTLE STRUT CONTROL BOX ON TOP OF #1 PYLON.Mar 3, 2026 · N227AZ · Boeing 767323 · Nacelle/Pylon Miscellaneous StructureSDR U2RA202604110006Web · crackedCRACK FOUND ON FORWARD FUSELAGE WEB OF THE NOSE GEAR WELL AT STRINGER 26, BS 160-180 CORRECTIVE ACTION: CAT B. REPAIR PER SRM. REINSPECT DUE AT 33,018 CYCLESMar 3, 2026 · N952CA · Boeing 747428 · Fuselage Miscellaneous StructureSDR VNAA202604110013Rib · crackedCRACKED MACHINED RIB SS 57.16 ON INBD FIXED LEADING EDGE AT RT WING. CRACKED MACHINED RIB SS 57.16 ON INBD FIXED LEADING EDGE AT RT WING WAS REPAIRED PER REO 690-57-41-240 REV - -Mar 3, 2026 · N603NN · Cndair CL6002D24 · Wing, Rib/BulkheadSDR IXXA202604060011Support Bracket · crackedSTRUT NR 1, LT AT NAC 295.09 SUPPORT BRACKET WITH CRACK. REF XTREME AVIATION NRC 732Mar 3, 2026 · N255CM · Boeing 767223 · Nacelle/Pylon, Main FrameSDR SWAA2026033176435Stringer · crackedCRACKED STRINGER 25R, BS 535, WL155. REPAIRED IAW EA 26-153-00644. THIS IS A CATEGORY A REPAIR AS DEFINED IN SRM 51-00-06.Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2026033176027Floor Panel · pulledFLOOR PANEL 232RF UPPER SKIN HAS AREAS OF PULLED STRANDS. FLOOR PANEL 232RF WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, AND DWG 144A5810, 0151, DUE TO AMOUNT OF ALL DAMAGE.Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026033176029Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS. FLOOR PANEL 241AF WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 AND DWG: 144A5810, 0127.Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026033176028Floor Panel · pulledFLOOR PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, & DRAWING 144A5810, SHEET 161.Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Floor PanelSDR IPXA2026032803895Splice Angle · corrodedBS 1992 AT THE 6 O`CLOCK POSITION HAD CORROSION BETWEEN FRAME AND SPLICE ANGLE TO INCLUDE SURROUNDING EXTERNAL SURFACES. VERIFIED STEP 10 IAW GMM. INSTALLED REPLACED SPLICE, REINSTALLED DOUBLER AT STA. 1992, 6:0 O'CLOCK PER B757-200PF SRM 51-40-02-0G-0Mar 3, 2026 · N451UP · Boeing 75724APF · APU Cowling/ContainmentSDR U2RA2026033100003Floor Support · crackedAFT CARGO INTERCOSTAL CRACK AT STA 1940 TO STA 1960, LBL77 PERFORMED REPAIR IAW SRM 51-70-13 R1Mar 3, 2026 · N952CA · Boeing 747428 · Fuselage Miscellaneous StructureSDR SWAA2026033076436Stringer · crackedCRACKED STRINGER 26R, BS 535, WL153. REPAIRED STRINGER 26R BTWN BS 500D & 540, AND APPLIED A FILLET SEAL & CIC IAW SRM 53-00-03-2R-1, REPAIR 1.Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2026033076437Stringer · crackedCRACKED STRINGER 23 LT, BS 535, WL164. REPAIRED STRINGER 23L BTWN BS 500D & 540, WL 164. APPLIED A FILLET SEAL AND CIC IAW SRM 53-00-03-2R-1, REPAIR 1.Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2026033076020Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS. FLOOR PANEL 231XF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, & DWG 144A5810, 0126.Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026033076026Floor Panel · debondedFLOOR PANEL 231ZF LOWER SKIN IS DEBONDED NEAR AFT EDGE. FLOOR PANEL 231ZF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, & DWG 144A5810, SHEET 160.Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026033076021Floor Panel · debondedFLOOR PANEL 241BF UPPER SKIN IS DEBONDED NEAR CENTER OF PANEL. FABRICATION OF A NEW FLOOR PANEL REPLACEMENT HAD BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026033076030Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAD AREAS OF PULLED STRANDS. FLOOR PANEL 241DF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, AND DWG 144A5810, 0128.Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026033076022Floor Panel · pulledFLOOR PANEL 241EF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATED A NEW FLOOR PANEL 241EF & REPLACED IAW SRM 53-00-50-2R-0.Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026033076023Floor Panel · pulledFLOOR PANEL 242AF UPPER SKIN HAD AREAS OF PULLED STRANDS. FLOOR PANEL 242AF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810, SHEET 189.Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026033076031Floor Panel · pulledFLOOR PANEL 242BF UPPER SKIN HAD AREAS OF PULLED STRANDS. FLOOR PANEL 242BF WAS REPLACED IAW SRM 53-00-50-2R-0, & DWG 144A5810, SHEET 122. ;[02] ITEM 1Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026033076025Floor Panel · pulledFLOOR PANEL 242DF UPPER SKIN HAD AREAS OF PULLED STRANDS. FLOOR PANEL 242DF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0, & DWG 144A5810, SHEET 150.Mar 3, 2026 · N249WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026033075818Pressure Blkhd · crackedAFT PRESSURE BULKHEAD HAD A CRACK INDICATION EMANATING FROM RIVET AT STRINGER 7R LOWER GROUP OF FIVE CLOSEST TO APEX. APPROX. 1/8' LONG. IAW PART 6, 51-00-00, PROCEDURE 23.Mar 3, 2026 · N486WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR IPXA2026032396237Bracket · crackedNR 1 ENG INBD SIDE, DURING ENGINE INSTALLATION FOUND SUPPORT BRACKET THAT ATTACH FUEL AND HYDRAULIC HOSES CRACKED. REMOVED THE HYDRAULIC AND FUEL JUNCTION BOX IAW AMM 70-00-00-401. INSTALLED HYDRAULIC AND FUEL JUNCTION BOX IAW AMM 70-00-00-401 AND IAW AMM 29Mar 3, 2026 · N135UP · Airbus A300F4622R · Nacelle/Pylon Miscellaneous StructureSDR SIMA20260303006Seat Track · gougedSSI 53-21-005-0090 RH LATERAL SEAT TRACK IS GOUGED ON TOP SIDE AT FR 28 (MAJOR REPAIR). BLENDED AREA ON FWD RH LATERAL SEAT TRACK AT FR 28 PER EMB 175 SRM 51-10-03. AREA MEASURES (L: 3.00? W: .50? D: .014?) AND IS FOUND TO BE OUT OF ALLOWABLE LIMITS PER EMB 17Mar 3, 2026 · N259NN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA20260303007Seat Track · gougedSSI 53-21-005-0090 LH LONGITUDINAL SEAT TRACK IS GOUGED ON TOP SIDE AT FR 23 AND Y= -29.5" (MAJOR) (REPAIR). BLENDED AREA ON FWD LH LONGITUDINAL SEAT TRACK ON TOP SIDE AT FR 23 AND Y=29.5? PER EMB 175 SRM 51-10-03. AREA MEASURES (L: .7" W: .2" D: .027") AND ISMar 3, 2026 · N259NN · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR SIMA20260303005Floorbeam · corrodedCORROSION FOUND RH BEAM AT FR 88-89, Y= +10.75 (MAJOR REPAIR) (LEVEL 2 CORROSION) BLENDED AREA ON RH AFT FLOOR BEAM AT FR 88-89, Y= +10.75" PER EMB 175 SRM 51-10-03. BLENDED AREA MEASURES (L: 1.60" W: .60? D: .040".) AND IS FOUND TO BE OUT OF ALLOWABLE LIMITS Mar 3, 2026 · N259NN · Emb ERJ170200LR · Fuselage Main, Floor BeamSDR HNAA2026032600242Hinge Fitting · wornRUDDER I LOWER CENTER HINGE FITTING UPPER DOUBLE HAT BUSHING HOLE WORN. REWORKED AND ACCEPTED WORN RUDDER I LOWER CENTER HINGE FITTING UPPER DOUBLE HAT BUSHING HOLE IAW EMB 145 SRM 55-00-02 AND EMB 145 SRM 51-20-09.Mar 3, 2026 · N699AE · Emb EMB145LR · Rudder StructureSDR IPXA2026031987548Pressure Blkhd · dentedMAJOR REPAIR, THROUGH RADOME 110AL, FWD PRESSURE BULKHEAD, ABOVE LOCALIZER ANTENNA RH ATTACHMENT HAS BULGE. DOT 103-25 ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-96865-REQ1 AND VT-MAE EA 300-5311-27-A4387, REV. -.Mar 3, 2026 · N162UP · Airbus A300F4622R · Fuselage Main, BulkheadSDR SWAA2026032376434Web · corrodedCORRODED RT DOOR SUB THRESHOLD WEB, BS 767 - 787, RBL 27, WL 154. REMOVED AND REPLACED THE SUB-THRESHOLD WEB IAW SRM 51-40-02-0G-0-A00729.Mar 3, 2026 · N924WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032375867Access Panel · elongatedELONGATED HOLES ON ACCESS PANEL 561BB AT LT WING. REPAIRED THE ACCESS PANEL 561BB IAW SRM 51-70-04-2R-10 REPAIR 10.Mar 3, 2026 · N7889A · Boeing 73779L · Wing, Plate/SkinSDR SWAA2026032075976Floor Panel · pulledFLOOR PANEL 231JF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL 231JF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0 & DRAWING 146A5810, SHEET 577.Mar 3, 2026 · N924WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026032075978Floor Panel · pulledAFT FLOOR PANEL 241ZF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241ZF WAS REPAIRED IAW SRM 53-00-50-2R-1.Mar 3, 2026 · N924WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026032075980Floor Panel · pulledAFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 242VF WAS REPAIRED IAW SRM 53-00-50-2R-1.Mar 3, 2026 · N924WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026032075977Floor Panel · pulledFLOOR PANEL 232FF UPPER SKIN HAS AREAS OF PULLED STRANDS. FABRICATION OF NEW 232FF FLOOR PANEL REPLACEMENT HAS BEEN ACCOMPLISHED IAW SRM 53-00-50-2R-0.Mar 3, 2026 · N924WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026032075983Floor Panel · pulledAFT FLOOR PANEL 241ACF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241ACF WITH UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1.Mar 3, 2026 · N924WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2026032076431Sidewall Support · corrodedCORROSION ON L/H FLOOR TO SIDEWALL SUPPORT STA 727+4-847; LBL 22; WL 156 AT VARIOUS SPOTS. IN AFT CARGO COMPARTMENT. REMOVED AND REPLACED L/H FLOOR TO SIDEWALL SUPPORT (ZEE ANGLE) AT STA 727+4-847; LBL 22; WL 156. PER SRM 51-40-02-0G .Mar 3, 2026 · N924WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026032076432Sidewall Support · corrodedCORROSION ON RT FLOOR TO SIDEWALL SUPPORT BS 727+4 - 767, RBL 22, WL 156 AT VARIOUS SPOTS. AFT CARGO COMPARTMENT. REMOVED AND INSTALLED A NEW RT FLOOR TO SIDEWALL SUPPORT BS 727+4 -767, RBL 22, WL 156 IAW SRM 51-40-02-0G-0.Mar 3, 2026 · N924WN · Boeing 7377H4 · Fuselage Miscellaneous Structure