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 DALA2026042002473Floor Support · corrodedCORROSION FLOOR SUPPORT -Y765 LOCATED BTW FR 67 TO FR 69 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT IAW SRM 51-42-11, SRM 51-72-11, AND DRAWING D53472093 (LP: 1552628). AIRCRAFT WAS GROUNDED.Apr 19, 2026 · N336NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2026042002472Support · corrodedCORROSION LOWER SILL LOCATED AT FR 68 RH SIDE AT AFT GALLEY AREA. PERFORMED PERMANENT REPAIR ON LOWER SILL LOCATED AT LEVEL FR68 RH SIDE AFT GALLEY AREA IAW SRM 53-41-14-300-001, TOOK MEASURE OF CORROSION IS: L= 0.3895 INCH W= 0.2695 INCH, (LP: 1551682)Apr 19, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2026042002471Fitting · crackedCRACK INTERNAL STRUCTURE FITTING LOCATED BTW FR 11 TO FR 12 AND -Y765 IN COCKPIT. REPLACED FITTING LOCATED BTW FR 11 TO FR 12 AND -Y765 IN COCKPIT IAW SRM 51-42-11, SRM 51-72-11, AND DWG D53110097, (LP: 1551681). AIRCRAFT WAS GROUNDEDApr 19, 2026 · N341NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR JR2R20260419575Skin · chafedLH OVER PYLON WING LE EDGE PANEL CHAFED. REPAIREDApr 19, 2026 · N89313 · Emb ERJ170200LL · Wing, Plate/SkinSDR JR2R20260419574Skin · chafedLH OVER PYLON WING LE EDGE PANEL CHAFED. REPAIREDApr 19, 2026 · N89313 · Emb ERJ170200LL · Wing, Plate/SkinSDR IXXA20260419001Rib · crackedFOUND RT WING OTBD L/E RIB AT OSS 464.48 CRACKED. REFER TO XTREME WO 014592 NRC 842Apr 19, 2026 · N255CM · Boeing 767223 · Wing, Rib/BulkheadSDR SWIA2026041877227Skin · crackedONE-OFF CRACK TO AFT LOWER WING PLANK, DWG 601R10046, 0300 THK AT CRACK LOCATION AFT EDGE AT WS 45 CRACK IS 0600 LONG AND STARTS FROM AFT EDGE OF AFT LOWER WING PLANK AT WS 450 FLIGHT 6080 . COMPLIED WITH PERMANENT REPAIR FOR CRACK DAMAGE AT LT AFT LOWER WINApr 18, 2026 · N970SW · Cndair CL6002B19 · Wing, Plate/SkinSDR CALA2026083119110Skin · crackedCRACK FOUND AT RT HORIZONTAL STAB LOWER SKIN AT HSS 101.90, 13 INCHES FROM REAR SPAR , INBD ROW. CRACK LENGTH 1". ACCOMPLISHED REPAIR ON THE RT HORZ STAB LOWER SKIN IAW SRM 55-10-01-2R-11.Apr 18, 2026 · N24736 · Boeing 737724 · Horizontal Stabilizer, Plate/SkinSDR VNAA2026071320001Access Panel · crackedCRACK ON ACCESS PANEL 172CR AT OVER WING FAIRING. ACCESS PANEL 172CR AT OVER WING FAIRING WAS REPAIRED PER REO 679-53-82-430 REV - -, AND STIFFENER WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01.Apr 18, 2026 · N607NN · Cndair CL6002D24 · Aerodynamic FairingsSDR SWIA2026041876277Crossbeam · crackedRIGHT CROSSBEAM AT BS 280 CRACKED ON UPPER FLANGE. REPLACED RT CROSSBEAM AT BS 280 IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01, AND DWG CC670-34010, REV K.Apr 18, 2026 · N703SK · Cndair CL6002C11 · Fuselage Main, StructureSDR SIMA20260418003Crossbeam · corrodedSSI 53-23-005. CABIN FLOOR FR 84 CROSSBEAM CORRODED AT LH SIDE. (MAJOR REPAIR) (LEVEL 2 CORROSION) PERFORMED PERMANENT REPAIR TO CABIN FLOOR FR 84 CROSSBEAM AT LH SIDE IAW ERS-EJ-53MR-5443Apr 18, 2026 · N745JB · Emb ERJ170100SE · Fuselage Main, StructureSDR VNAA202606060003Skin · damagedNICKS & DENTS ON LOWER SKIN OF LT INBD FLAP BTW FLS 15.00 TO FLS 75.6. NICKS ON LOWER SKIN OF LT INBD FLAP BTW FLS 48.00 TO FLS 75.60 WAS BLEND OUT IAW SRM 51-12-00-001-001-A01 & EVALUATED WITHIN OF LIMITS PER SRM 57-52-01-201-005-A01 AND LOWER SKIN OF LT INApr 18, 2026 · N606NN · Cndair CL6002D24 · Trailing Edge FlapsSDR VNAA202606060002Striker · dented1605FH PERM REPAIR - REPAIR TO PAX DOOR SEAL STRIKER - EXTENSION TO SRM 53-21-23-201-004-A01. PAX DOOR SEAL STRIKER WAS REPAIRED PER SRM 53-21-23-201-006-A01.Apr 18, 2026 · N606NN · Cndair CL6002D24 · Fuselage Main, StructureSDR VNAA202606060001Skin · damagedLIGHTNING STRIKE DAMAGE TO FUSELAGE SKINS BETWEEN FS234.00 - FS364.00 AND BETWEEN STR 20L - STR24L. REPAIRED PER REO 690-53-00-656 REV -A AND REO 690-53-21-2139 REV -.Apr 18, 2026 · N606NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR SIMA20260418002Seat Track · corrodedSSI 53-21-005: RH CENTER SEAT TRACK HAS AREA OF CORROSION BTWN FR 30-31. (MAJOR REPAIR) (LEVEL 2 CORROSION) PERFORMED PERMANENT REPAIR TO RH CENTER SEAT TRACK BTW FR 30-31 IAW ERJ 170 SRM 53-00-10/REPAIR 02P.Apr 18, 2026 · N745JB · Emb ERJ170100SE · Fuselage, Seat/Cargo Attach FittingsSDR AALA202606033294Door Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FASTENER HOLE AT FR 16 RIGHT AND #7 DOORSTOP FITTING. REPAIRED FRAME PER EA 374446.Apr 18, 2026 · N9013A · Airbus A319115 · Fuselage Main, StructureSDR IPXA2026042970084Profile · crackedM.C.DECK LH FR#79 Z-PROFILE CRACKED DOT#58-07. REMOVED CRACKED Z-PROFILE BTW C77 TO C79 LH SIDE MAIN DECK IAW A300-600 SRM 51-40-21-001. INSTALLED NEW Z-PROFILE AT M.C. DECK LH FR#79 IAW A300-600 SRM 51-40-21.Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026051567724Structure · corrodedAFT CARGO-FRAME 58 CEILING STRUCTURE FROM LH TO RH SIDE HAS CORROSION AROUND MULTIPLE HOLES. SH 91148554. REMOVED (07 EA) RECEPTACLES FROM ANGLE SUPPORT, CEILING ESTRUCTRURE BETWEEN Y450 AND Y2462 ,FOR ACCESS IAW A300-600 SRM 51-40-21-001. REMOVED DAMAGE (07 Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Main, StructureSDR SIMA20260418001Floorbeam · corrodedFWD GALLEY LH CENTER FLOOR BEAM HAS AREA OF CORROSION AT FR 19. (MAJOR REPAIR LEVEL 2 CORROSION) PERFORMED PERMANENT REPAIR TO FWD GALLEY LH CENTER FLOOR BEAM AREA OF CORROSION AT FR 19 IAW ERS-EJ-53MR-5432.Apr 18, 2026 · N745JB · Emb ERJ170100SE · Fuselage Main, Floor BeamSDR IPXA2026050267681Profile · corrodedAFT CARGO-FRAME 57 CEILING STRUCTURE FROM LH TO RH SIDE HAS CORROSION AROUND MULTIPLE HOLES. SH 91148554. REMOVED DAMAGE (02 EA) ON ANGLE SUPPORT, CEILING STRUCTRURE FR-57, BETWEEN Y1959 AND Y450 IAW A300-600 SRM 51-74-10-201. INSTALLED NEW PROFILE (CEILING STApr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR SWAA2026052090782Pressure Deck · crackedCRACK INDICATION FOUND ON THE HORIZONTAL PRESSURE DECK WEB, RBL 42, BS 663 - 675. PERFORMED PERMANENT REPAIR ON HORIZONTAL PRESSURE DECK, BS 663 - 675, RBL 30 - 60 IAW SRM 53-40-51-2R-2,. REPAIR 2.Apr 18, 2026 · N250WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2026052090784Stiffener · crackedCRACKED STIFFENER FRONT SPAR LOCATED BS 540, LBL 24.75 AT CENTER SECTION. REPLACED STIFFENER FRONT SPAR, IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, DWG 111A6000, SHEET 245, REV-, AND DWG 111A2001, SHEET 77, REV-.Apr 18, 2026 · N250WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026052090779Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661BB AT RT WING. REPAIRED ACCESS PANEL 661BB IAW SRM 51-70-04-2R-10, REPAIR 10.Apr 18, 2026 · N250WN · Boeing 7377H4 · Wing, Plate/SkinSDR IPXA2026051567636Profile · corrodedAFT CARGO-FRAME 54-54.2 CEILING STRUCTURE RUNNING FWD AND AFT, LH AND RH STRUCTURE HAS CORROSION AROUND MULTIPLE HOLES. REMOVED DAMAGE (01 EA) ON ANGLE SUPPORT, CEILING ESTRUCTRURE BETWEEN CROSS BEAM 54 TO 54.2 , Y-450. IAW SRM 51-74-10-201. INSTALLED NEW PLApr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR HNAA2026052000417Door Frame · damagedMAIN DOOR LOWER FRAME AFT NUTPLATE HOLE DOUBLER HAS NO DTA INFORMATION. REPAIR WAS ACCOMPLISHED IAW ETN-EM-52-041. RE-ACCOMPLISHED DOUBLER FOR REPAIR OF MAIN DOOR LOWER FRAME AT AFT NUT-PLATE HOLE IAW SRM 52-10-04RE, ITEM 3, FIG 201, SHEET 3 AND EO1-52-26-019Apr 18, 2026 · N655AE · Emb EMB145LR · Fuselage Main, StructureSDR SWAA2026051990471Support Angle · crackedPANEL 661AB TRAILING EDGE SUPPORT BRACKET CRACKED. REMOVED AND REPLACED SUPPORT ANGLE PER SRM 51-10-02 AND SRM 51-40-02. REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-10-02 AND SRM 51-40-02.Apr 18, 2026 · N8538V · Boeing 7378H4 · Wing Miscellaneous StructureSDR SWAA2026051190768Skin · crackedCRACK FOUND ON LT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 18 INCHES FROM FRONT SPAR INB SIDE OF RIB LENGTH APPROX= 0.750 INCHES. REPAIRED LOWER SKIN LOCATED AT LH HORIZONTAL STABILIZER LOWER SKIN BTW STA 203.10 TO STA 184.70. IAW SRM 55-10Apr 18, 2026 · N479WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR IPXA2026051167251Cover · brokenFWD CREW DOOR HAS BROKEN SLIDE ARM/DISARM COVER. REMOVED SLIDE ARM/DISARM COVER IAW AMM 52-10-13/401. INSTALLED SLIDE ARM/DISARM COVER IAW 52-10-13/401.Apr 18, 2026 · N163UP · Airbus A300F4622R · Escape SlideSDR QXEA2026051100106Seat Track · damagedRIGHT HAND LATERAL SEAT TRACK AT FRAME 73-75 HAS TOOLING MARKS DAMAGE FROM PREVIOUS WORK PERFORMED. BLENDED AREA BUT OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM 51-40-08.Apr 18, 2026 · N635QX · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026042968001Bracket · crackedAFT CARGO- FRAME 54 RH SIDEWALL BRACKET IS CRACKED. INSTALLED BRACKET AT FRAME 54 RH SIDEWALL, IAW A300-600- SRM 51-40-21-001. NEW PART NUMBER A53410765218PNSU, IAW GMM 09.08.01.04.Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR SWAA2026050690771Angle · crackedCRACK ANGLE LOCATED BS 695 RBL1 AT CENTER WING BOX . REPLACED ANGLE AND FASTENERS LOCATED BS 695 RBL1 AT CENTER WING BOX IAW SRM 51-10-02 ITEM 9, SRM 51-40-02 AND DWG 273A9110; SHEET 6, REV A.Apr 18, 2026 · N467WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR IPXA2026050170017Web · crackedMAIN CARGO DECK RT FR 77 OTBD OF SIDEWALL LOWER WEB HAS A CRACK. REMOVED CRACKED WEB BTW C76 TO C77 RT SIDE MAIN DECK IAW SRM 51-40-21-001. INSTALLED NEW WEB 2 ANGLES AND 1 PROFILE ON MAIN CABIN BETWEEN C76 TO C77 SIDEWALL LOWER I.A.W AIRBUS SRM 51-40-21.Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026050267675Crossbeam · corrodedAFT CARGO-FRAME 54.2 CEILING STRUCTURE FROM LT TO RT SIDE HAS CORROSION AROUND MULTIPLE HOLES. INTALLED NEW PROFILE-CROSS FRAME 54.2 STA Y-450 TO Y450 AND Y-450 TO Y-1959 IAW SRM 51-40-21-001.Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Main, StructureSDR IPXA2026042968063Bracket · crackedAFT CARGO- FRAME 54 LT SIDEWALL BRACKET IS CRACKED. INSTALLED BRACKET AT FRAME 54 LH SIDEWALL, IAW SRM 51-40-21-001.Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026050262860Hinge Fitting · crackedCRACKED FITTING, RT WING NR 10 SPOILER SUPPORT FITTING WS 638. REPLACED IAW AMM 27-61-01-424-019, REV 147, STEP 3A, TO 3H (11) INSTALLED NR 10 SPOILER.Apr 18, 2026 · N320UP · Boeing 76734AF · SpoilersSDR IPXA2026042969269Attach Bracket · brokenLOWER HALF FUSL TAIL SECTION JACK SUPPORT AREA ATTACH BRACKETS BROKEN 2EA. REMOVED 2(EA) BRACKETS L/H & R/H SIDE AT LWR HALF FUSE TAIL SECTION JACK SUPPORT AREA IAW SRM 51-40-21-001. INSTALLED 2 (E/A) ANGLE IAW SRM 51-40-21.Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Main, Attach FittingsSDR IPXA2026042870068Profile · crackedMAIN CARGO DECK RH FR 74 Z PROFILE CRACKED. REMOVED CRACKED Z-PROFILE BTW C73 TO C76 RH SIDE MAIN DECK IAW SRM 51-40-21-001. INSTALLED NEW Z-PROFILE TRAVELER NUMBER:T26/1862656 BTW C73 TO C76 RH SIDE MAIN DECK IAW SRM 51-40-21-001. OK TO TOP COAT HEAD OF FASTApr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026042870092Profile · crackedMAIN CARGO DECK LT FR 74 Z-PROFILE CRACKED. REMOVED CRACKED Z-PROFILE BTW C73 TO C76 LH SIDE MAIN DECK IAW SRM 51-40-21-001. INSTALLED NEW Z-PROFILE AT MAIN CABIN L/H C73 TO C76 IAW SRM 51-40-21-001.Apr 18, 2026 · N163UP · Airbus A300F4622R · Fuselage Miscellaneous StructureSDR IPXA2026043063775Skin · crackedDURING PERFORM J/C : MXP-57-117-00-1-JIC, FOUND LEFT WING LOWER SKIN NEAR RIB 32, WSTA 1018.2 SKIN CRACKED. ACCOMPLISHED JOB I.A.W UPS EO-97334-REQ1 REV1 2.Apr 18, 2026 · N320UP · Boeing 76734AF · Wing, Plate/SkinSDR SWAA2026042990731Panel · delaminatedPANEL 191D HAS DELAMINATION DAMAGE ON OUTER SURFACE. PANEL 191D WITH DELAMINATION DAMAGE ON OUTER SURFACE WAS REPAIRED IAW SRM 51-70-05-2R-2.Apr 18, 2026 · N8865L · Boeing 7378 · Aerodynamic FairingsSDR IPXA2026042563148Seal · tornLEFT WING NR 6 SPOILER HAS A TORN SEAL LOCATED AT THE 3RD ATTACH POINT FROM INBD END. IAW AMM 20-11-00-910-802, REV 147, REPLACED THE SEAL.Apr 18, 2026 · N332UP · Boeing 76734AF · SpoilersSDR IPXA2026042563692Hinge · wornFOUND NR 8 TAI DOOR AFT HINGE WORN OUT. IAW AMM 57-41-58-434-044, ADJUSTED AND PERFORMED A BONDING TEST OF NR 8 TAI DOOR AFTER HINGE,RESULT WAS SATISFACTORY.Apr 18, 2026 · N332UP · Boeing 76734AF · Wing, Attach FittingsSDR SWAA2026042890560Web · crackedAPB APEX DOME HAS SURFACE WEB CRACK AT STR23R FROM UPPER LH RIVET GOING TO CENTER EDGE OF DOME. REPAIRED PER EA 26-153-01061 WITH AN INSPECTION THRESHOLD DEFINED IN 26-153-01061-DTI..Apr 18, 2026 · N7815L · Boeing 73776Q · Fuselage Miscellaneous StructureSDR IPXA2026042463695Bearing · migratedMIGRATED BEARING, RT WING T/E NR 7 SPOILER LOWER FITTING. IAW AMM27-61-02-424-023 REV.147 CONNECT RH WING NO.7 SPOILER PCA ROD END AND THE SPOILER TO FLAP CLEARANCE MEASURED CHECK SATISFIED.Apr 18, 2026 · N332UP · Boeing 76734AF · SpoilersSDR SWAA2026042390778Battery Pack · inoperativeFWD EMERGENCY EXIT LIGHTS (5 EACH) INOPERATIVE. REMOVED / REPLACED AND PERFORMED SUCCESSFUL OPS CHECK OF EMERGENCY LIGHTS BATTERY PACKS M1675 AND M1674 IAW B737 AMM 33-51-06.Apr 18, 2026 · N7885A · Boeing 73776N · Emergency LightingSDR SWAA2026042392140Battery Pack · inoperativeFWD EMERGENCY EXIT LIGHTS (5 EACH) INOPERATIVE. REMOVED & REPLACED, PERFORMED SUCCESSFUL OPS CHECK OF EMERGENCY LIGHTS BATTERY PACKS M1675 AND M1674 IAW B737 AMM 33-51-06.Apr 18, 2026 · N7885A · Boeing 73776N · Emergency LightingSDR IPXA2026042265192Skin · dentedDURING WALK AROUND INSPECTION FOUND DENT /HOLE IN FUSELAGE LEFT SIDE BELOW MAIN CARGO DOOR LEFT AND DOWN OF THE FORWARD STATIC PORT ABOUT STATION 478. CATEGORY B PERM SKIN REPAIR PERFORMED PER EO-97184-REQ1.Apr 18, 2026 · N387UP · Boeing 767300 · Fuselage Main, Plate/SkinSDR IPXA2026042160589Roller · wornFAULT - FOUND MAIN DECK CARGO HANDLING SHAFT OF ROLLER RAIL ASSY WORN TOTAL: 2EA AT STA 456 ~ STA 500 LBL 77.50, LBL 55.50. I.A.W AMM 25-57-05-004-001 AND AMM 25-57-05-404-006 REV.147 REPLACED ROLLER RAIL ASSY.Apr 18, 2026 · N320UP · Boeing 76734AF · Cargo CompartmentsSDR IPXA2026042162967Seat Track · wornFOUND SEAT TRACK ASSY INBOARD AFT INBD FWD OF CAPTAIN SEAT WORN . I.A.W AMM 25-11-01-822-095-001 REV.147 REPLACED SEAT TRACK ASSY.Apr 18, 2026 · N320UP · Boeing 76734AF · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026042163509Lock · wornFOUND MAIN DECK CARGO HANDLING BASE OF LOCK ASSY WORN TOTAL : 1EA AT BS 1000 LBL 11.50. REPLACED LOCK IAW AMM 25-58-01-004-001 AND AMM 25-58-01-404-005 REV.147.Apr 18, 2026 · N320UP · Boeing 76734AF · Cargo Compartments