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 R61A2026041000010Skin · dentedDENT AND GOUGE BETWEN FR11-12 AND STGR 5L-6L. MAJOR REPAIR WAS ACCOMPLISHED TO DENT AND GOUGE BETWEEN FR11-12 5L-6L WITH DOUBLER PATCH IAW ETD 2025-170-923439 SRM 53-10-01 REPAIR 12 REF 1 VISION W/O 5689 NR0012 FOR ALL WORK ACCOMPLISHEDApr 15, 2026 · N647RW · Emb ERJ170100SE · Fuselage Main, Plate/SkinSDR AALA202604159139Floor Support · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN PASSENGER CABIN FLOOR STRUCTURE INTERCOSTAL AT STA 323 AND RBL 32. REPLACED INTERCOSTAL PER AARD 51-00-05-1.Apr 15, 2026 · N909AN · Boeing 737823 · Fuselage Miscellaneous StructureSDR AALA202604155481Hinge Arm · crackedAIRCRAFT IN BASE MAINTENANCE: 2.500 INCH CRACK, RIGHT MAIN LANDING GEAR DOOR HINGE BEAM ARM. MAINTENANCE REPLACED RIGHT MAIN LANDING GEAR DOOR HINGE BEAM ARM IAW CMM 52-81-18.Apr 15, 2026 · N713UW · Airbus A319112 · Landing Gear DoorsSDR AALA202604156515Hinge Arm · elongatedAIRCRAFT IN BASE MAINTENANCE: ALL 5 BEARING PLATE ATTACH HOLES ARE ELONGATED. MAINTENANCE REPLACED LEFT MAIN LANDING GEAR DOOR HINGE BEAM ARM IAW CMM 52-81-18.Apr 15, 2026 · N713UW · Airbus A319112 · Landing Gear DoorsSDR IXXA20260415001Skin · crackedFUSELAGE SKIN AND BEAR STRAP IS CRACKED AT L1 DOOR CUTOUT AFT LOWER CORNER STA 335Apr 15, 2026 · N227AZ · Boeing 767323 · Fuselage Main, Plate/SkinSDR YENA2026041500399Actuator · faultedFLT#324, LAX-JFK. (ETOPS) "FUEL ACT XFR FAULT ( AUTO TRANSFER SYSTEM (ACT) 1), 2) ADDITIONAL CENTER TANK(S) (ACT) ) PERFORMED TSM TASK 28-46-00-810-873A AND 28-46-00-810-874A UP TO STEP 4.(1).B. ACT AFT 1 AND ACT AFT 2, SET HIGH LEVEL SENSORS SWITCH 72QJ2 AND Apr 15, 2026 · N2165J · Airbus A321271NX · Aircraft Fuel Distribution SystemSDR YENA2026041500398Control Unit · failedFLT#2124, LAX-JFK. (ETOPS) "RADAR CONTROL PANEL HZD PUSH BUTTON ANNUNCIATOR LIGHT INOP. TURB PUSH BUTTON ANNUNCIATOR LIGHT INOP WHEN OVERHEAD ANN LT SWITCH IN DIM POSITION; REMOVED AND REPLACED WEATHER RADAR CNTL UNIT AS PER AMM 34-41-12 (3SQ) OPS CHK GOOD. NOApr 15, 2026 · N4077J · Airbus A321271NX · Weather Radar SystemSDR DALA2026041502388Battery Pack · inoperativeEMERGENCY ISLE LIGHTS ROW 28-32 NOT ILUMINATED ON SVC CK. R & R BATTERY PACK AT M2627 POWER SUPPLY PER B737 AMM 33-51. OPS CK OK. (LOG 8305422 - AIRCRAFT WAS GROUNDED).Apr 15, 2026 · N907DN · Boeing 737932ER · Emergency LightingSDR IPXA2026061700388Rod · corrodedRH HORIZONTAL STABILIZER O/B ELEVATOR PCU INPUT ROD AFT CLEVIS IS RUSTED AND HAS 1EA CORRODED NUT AND SAFETY WIRE ATA 55-10 MARKED 84-14 INSTALLED NEW RH-HORIZ-STAB-O/B-ELEVATOR-PCU-INPUT- (POGO) - ROD-ASSY. IAW AMM 27-31-05-424-067, UP TO REPLACEMENT OF 2EAApr 14, 2026 · N428UP · Boeing 75724APF · Horizontal Stabilizer Miscellaneous StructureSDR IPXA2026060499229Skin Panel · gougedVISUAL GOUGING FOUND IN (1) HOLE LOCATED AT RT WING BOTTOM SKIN ACCESS DOOR RIBS 24 TO 25. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-97614-REQ1 & VT-MAE EA 300-5720-27-A4485Apr 14, 2026 · N141UP · Airbus A300F4622R · Wing, Plate/SkinSDR IPXA2026070694500Skin · gougedRIGHT APU DOOR 316AR SKIN HAS A MULTIPLE GOUGE AT LWR/AFT CORNER APPROX BTW BS 1941 AND BS 1963.8, INSTALLED FABRICATED PLATE (REPAIR DOUBLER) AT RT APU DOOR 316AR SKIN AT LWR AFT CORNER APPROX BTW BS 1941 AND BS 1963.8 IAW B757-200PF SRM 52-40-01-2R-5 FIGUREApr 14, 2026 · N428UP · Boeing 75724APF · Auxiliary Power Unit (APU) DoorsSDR IPXA2026070694554Skin · dentedRIGHT APU DOOR 316AR SKIN HAS A MULTIPLE DENTS APPROX BTW BS 1918 AND BS 1941. INSTALLED -1,-2 & -3 REPAIR PARTS IAW SRM 52-40-01-2R-40FIG 201 AND SRM 51-20-01-0G-0 AND NO REPEAT INSPECTION REQUIRED PER SRM 52-40-01-2R-4.Apr 14, 2026 · N428UP · Boeing 75724APF · Auxiliary Power Unit (APU) DoorsSDR DALA2026061103539Skin · dentedDTE, ER/A 628059-14. FWD CARGO DOOR LOWER AFT CORNER DENT. TEMPORARY REPAIR C/O. (LP# 1544139; AIRCRAFT WAS GROUNDED)Apr 14, 2026 · N325DU · Airbus BD5001A11 · Cargo/Baggage DoorsSDR IPXA2026060902568Hinge · crackedTHE FWD PIANO HINGE FASTENER #5 ON THE FUSELAGE SIDE, HAS A CRACK IND. (1EA) AT THE 3 O'CLOCK POSITION IN THE ALU. LAYER ONLY. DISCREPANT HOLE LABELED IN BLACK.ACCOMPLISH REPAIR IN ACCORDANCE WITH EO-97613-REQ1 AND VT-MAE EA 300-5236-27-A4450, REV. -.Apr 14, 2026 · N141UP · Airbus A300F4622R · Fuselage, Door HingeSDR SIMA20260414001Retainer · gougedFWD PAX DOOR CUTOUT SEAL RETAINER FLANGE IS GOUGED. (MAJOR REPAIR) BLENDED 5EA MARKED GOUGES ON FWD PAX DOOR SEAL RETAIN IAW ERJ 170 SRM 51-10-03 AND FOUND 4EA BLENDED GOUGES TO BE WITHIN LIMITS IAW ERJ 170 SRM 53-10-21/AD01. PERFORMED PERMANENT REPAIR TO LOWEApr 14, 2026 · N745JB · Emb ERJ170100SE · Passenger/Crew DoorsSDR SWAA2026051989233Attach Angle · crackedCRACK FOUND ON LT VAPOR BARRIER ATTACH ANGLE AT BS 663, LBL 9 AND LBL 34. PERFORMED NDT INSPECTION PER NDT PART 6; 51-00-00 PROCEDURE 16 OF HOLES COMMON TO REPAIR; IN TANK HOLES AND WEB HOLES. NO DEFECTS NOTED. REMOVED AND REPLACED LT VAPOR BARRIER ATTACH AApr 14, 2026 · N8538V · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR SWAA2026051989234Attach Angle · crackedCRACK FOUND ON RT VAPOR BARRIER ATTACH ANGLE AT BS 663, RBL 9 AND RBL 34. PERFORMED NDT INSPECTION PER NDT PART 6; 51-00-00 PROCEDURE 16 OF HOLES COMMON TO REPAIR; IN TANK HOLES AND WEB HOLES. NO DEFECTS NOTED. FABRICATED REPAIR PARTS. REMOVED AND REPLACEApr 14, 2026 · N8538V · Boeing 7378H4 · Fuselage Main, Attach FittingsSDR REXA2026051500591Drag Angle · crackedINITIAL INSPECTION: CRACKED AFT DRAG ANGLE AT RH STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). AFT DRAG ANGLE AT RH STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE Apr 14, 2026 · N913XJ · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026051500590Drag Angle · crackedINITIAL INSPECTION: CRACKED AFT DRAG ANGLE AT LH STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). AFT DRAG ANGLE AT LH STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACApr 14, 2026 · N913XJ · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR 2026FA0000391Stiffener · shearedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF AND/OR CRACKED.Apr 14, 2026 · N1057R · Cessna 172S · Wing Miscellaneous StructureSDR 2026FA0000390Stiffener · shearedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF AND/OR CRACKED.Apr 14, 2026 · N2433S · Cessna 172R · Wing Miscellaneous StructureSDR SWAA2026051389817Attach Angle · crackedPOSSIBLE CRACK IN LT AC PACK BAY AFT UPPER CORNER. REPLACEMENT ATTACH ANGLE FABRICATED AND INSTALLED PER EA 26-157-01152.Apr 14, 2026 · N475WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR IPXA2026051202947Floor Panel · damagedAFT CARGO COMP, FLOOR PANEL 151KG, HONEYCOME DAMAGE IN ALL LATERAL FACES. PANEL 151KG FABRICATED IAW SREO-16407-REQ002 ((APPX C) A300 FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION (SREO)).Apr 14, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026051103069Floor Panel · damagedAFT CARGO COMP, FLOOR PANEL 152VF, HONEYCOME WITH DAMAGA ON 2 SPOTS. PANEL 152VF FABRICATED IAW SREO-16407-REQ002, APPX C. FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION, SREO.Apr 14, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026051102976Floor Panel · damagedAFT CARGO COMP, FLOOR PANEL 152RF, HONEYCOME BROKEN IN MULTIPLE SPOTS. PANEL 152RF FABRICATED IAW SREO-16407-REQ002 ((APPX C) A300 FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION (SREO)).Apr 14, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026051103074Floor Panel · damagedAFT CARGO COMP, FLOOR PANEL 151MG, HONEYCOME WITH CRACK. PANEL 151MG FABRICATED IAW SREO-16407-REQ002 ,APPX C. FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION, SREO.Apr 14, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026051103071Floor Panel · damagedAFT CARGO COMP, FLOOR PANEL 151UF, HONEYCOME DAMAGE IN ALL L/H SIDE. PANEL 151UF FABRICATED IAW SREO-16407-REQ002. APPX C FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION, SREO.Apr 14, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026051102984Floor Panel · damagedAFT CARGO COMP, FLOOR PANEL 152UF, HONEYCOME WITH CRACK ON 3 SPOTS. PANEL 152UF FABRICATED IAW SREO-16407-REQ002, APPX C. FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION SREO.Apr 14, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026051102945Floor Panel · damagedAFT CARGO COMP, FLOOR PANEL 151LG, HONEYCOME DAMAGE IN 3 SPOTS. PANEL 151LG FABRICATED IAW SREO-16407-REQ002 ((APPX C) A300 FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION.Apr 14, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026051102979Floor Panel · damagedAFT CARGO COMP, FLOOR PANEL 152QF, HONEYCOME DAMAGE ALL LATERAL FACES. PANEL 152QF FABRICATED IAW SREO-16407-REQ002, APPX C FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION, SREO.Apr 14, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026051103000Floor Panel · damagedAFT CARGO COMP, FLOOR PANEL 152TF, HONEYCOME DAMAGE ON 3 SPOTS. PANEL 152TF FABRICATED IAW SREO-16407-REQ002 ((APPX C) A300 FWD/AFT LOWER CARGO COMPARTMENT FLOOR PANEL FABRICATION (SREO))Apr 14, 2026 · N141UP · Airbus A300F4622R · Fuselage Floor PanelSDR 2026FA0000358Stiffener · shearedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF AND/OR CRACKEDApr 14, 2026 · N988BE · Cessna 172S · Trailing Edge FlapsSDR 2026FA0000355Stiffener · shearedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF AND/OR CRACKEDApr 14, 2026 · N437SP · Cessna 172S · Trailing Edge FlapsSDR 2026FA0000352Stiffener · shearedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF ON THE INBOARD RH INBOARD FLAP TRACKApr 14, 2026 · N211AV · Cessna 172N · Trailing Edge FlapsSDR SWAA2026051289401Support Angle · corrodedCORROSION ON ZEE SUPPORT ANGLE BS986.5+5 RBL36; WL208. REMOVED AND REPLACED ZEE SUPPORT ANGLE BS986.5+5 RBL36; WL208 IAW B737-800 SRM 51-40-02-0G-0 AND DWG:147A5700 ID:0121 REV: A.;Apr 14, 2026 · N8639B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026051289433Light · damagedPASSENGER CABIN SIDEWALL 232ZLW EMERGENCY EXIT LIGHT ASSEMBLY DAMAGED. INSTALLED PASSENGER CABIN SIDEWALL 232ZLW EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-01-960-802. STEP 3. C (10);[02]Apr 14, 2026 · N8639B · Boeing 7378H4 · Emergency LightingSDR FDEA202604140571Skin · crackedLH WING CENTER FLAP UPPER FLANGE FOUND 1EA CRACK AT RIB17 BETWEEN REAR SPAR AND STGR2.8 COMPLIED WITH EA 6-5750-T0387053 P1 TO REPAIR THE LH WING CENTER FLAP RIB UPPER FLANGE 1EA CRACK AT RIB17 BETWEEN REAR SPAR AND STGR2.8. TITLE: WINGS - FLIGHT SURFACEApr 14, 2026 · N669FE · Airbus A300F4605R · Trailing Edge FlapsSDR SWAA2026051189152Channel · crackedCRACK ON CHANNEL OF ACCESS PANEL 443AT. REPLACED CHANNEL LOCATED ON ACCESS PANEL 443AT IAW B737-800 SRM 51-40-02 SRM 51-10-02 ITEM 9Apr 14, 2026 · N8637A · Boeing 7378H4 · Aerodynamic FairingsSDR SWAA2026051189402Floorbeam · corrodedCORROSION ON BS 986.5 FLOORBEAM UPPER FLANGE AT NUTPLATE HOLE RBL43; WL208. REPAIRED BS 986.5 FLOORBEAM UPPER FLANGE IAW SRM 53-70-51-2R-6. REPAIR 6.Apr 14, 2026 · N8639B · Boeing 7378H4 · Fuselage Main, Floor BeamSDR IPXA2026050801614Floorbeam · corrodedAFT CARGO COMPARTMENT FLOOR STRUCTURE, LH FLOOR BEAM AT FR65 Y140 TO Y805 HAS (3EA) AREAS WITH CORROSION / EXFOLIATION. REMOVE CORROSION DAMAGE ON THE DISCREPANT CROSSBEAM PER A300-600F IAW SRM 51-74-10. CROSS BEAM 1EA, SPLICES 2EA UPLN9496-310-12, SPLICE 1EAUApr 14, 2026 · N141UP · Airbus A300F4622R · Fuselage Main, Floor BeamSDR 2026FA0000339Stiffener · shearedFLAP TRACK SRIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF ON THE INBOARD RH INBOARD FLAP TRACKApr 14, 2026 · N211AV · Cessna 172N · Trailing Edge FlapsSDR IPXA2026050501913Floor Panel · damagedMAJOR REPAIR. MAIN CARGO DECK RH FLOOR BOARD #232XCF STA#480 CORNER DAMAGED. NEW FLOOR PANEL XCF WAS FABRICATED IAW SREO-9692-REQ0001 STEPS 1-6Apr 14, 2026 · N421UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2026042901438Floor Panel · damagedMAJOR REPAIR, MAIN CARGO COMPT. STA.879 LEFT FLOOR PANEL 231XTF DAMAGED ON END. FLOOR PANEL 231XTF FABRICATION IS COMPLETE IAW EO NO:B757-5320-9692-K / SREO-16407-REQ001Apr 14, 2026 · N421UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2026042901327Floor Panel · damagedMAJOR REPAIR, MAIN CARGO COMPT BS 900 LEFT FLOOR PANEL 231XYF HAS RIPPED OUT SCREW RETAINER HOLE FLOOR PANEL 231XYF FABRICATION IS COMPLETE IAW EO NO:B757-5320-9692-K / SREO-16407-REQ001Apr 14, 2026 · N421UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2026050401890Floorboard · damagedMAJOR REPAIR, MAIN CARGO DECK FLOOR BOARD 222XAF STA.440 CORNER DAMAGED, FABRICATED A NEW FLOOR PANEL 222XAF IAW SREO-6962-REQ001 STEPS 1-6Apr 14, 2026 · N421UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2026042901347Floor Panel · damagedMAIN CARGO COMPT. BS 900 LOWER LEFT FLOOR PANEL 231XWF HAS DAMAGED HONEYCOMB. FLOOR PANEL 231XWF FABRICATION IS COMPLETED IAW EO NO:B757-5320-9692-K / SREO-16407-REQ001. INSERTS INSTALLED IAW SREO-16407-REQ001. I.A.W. UPS GMM (RII) 04.02 STEP 1,2,3,4,AND 5Apr 14, 2026 · N421UP · Boeing 75724APF · Fuselage Floor PanelSDR IPXA2026050482714Bracket · damagedLT MLG STRUT DOOR BOTTOM INNER SKIN HAS COMPOSITE DAMAGE (2 LOCATIONS). INSTALLED LOWER LH MLG STRUT DOOR BRACKET IAW B757 AMM 32-12-04-404-012Apr 14, 2026 · N421UP · Boeing 75724APF · Landing Gear DoorsSDR IPXA2026042300388Clevis · corrodedRIGHT HORIZONTAL STAB OTBD ELEVATOR PCU INPUT ROD AFT CLEVIS IS RUSTED AND HAS ONE CORRODED NUT & SAFETY WIRE.Apr 14, 2026 · N428UP · Boeing 75724APF · Elevator StructureSDR FDEA202604140438Rib · crackedLH WING CENTER FLAP RIB UPPER FLANGE FOUND 1EA CRACK AT RIB27 BETWEEN REAR SPAR AND STGR2.8 COMPLIED WITH EA 6-5750-T0387053 P1 REPAIRED THE LH WING CENTER FLAP RIB27 UPPER CRACKED FLANGE BETWEEN REAR SPAR AND STGR2.8. CAT A REPAIR. MAJOR REPAIR IAW GMM 6Apr 14, 2026 · N669FE · Airbus A300F4605R · Trailing Edge FlapsSDR AALA202604307050Hinge Arm · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR #5 HINGE ARM HAS EXCESSIVE PLAY. REPLACED HINGE ARM PER AMM 55-16-42.Apr 14, 2026 · N105NN · Airbus A321231 · Elevator Structure