Service difficulty reports

1,770,704 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 REXA2026102201983Bracket · crackedCRACK ON BRACKET BTW STA FS=1144.00 TO FS=1162.00 STGR 9L AT AFT EQUIPMENT COMPARMENT. SUMMARY: BRACKET BTW STA FS=1144.00 TO FS=1162.00 STGR 9L AT AFT EQUIPMENT COMPARMENT. WAS REPLACE PER CRJ-900 SRM 51-42-06-001-001-A01Sep 12, 2026 · N482PX · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026102201980Panel · crackedCRACKS ON DOOR STAIR AFT SIDE PANEL ON TOP STEP, UPPER MID STEP, LOWER MID STEP AND LOWER STEP AT PASSENGER DOOR. AFT SIDE PANEL AT PASSENGER DOOR WAS REPLACED PER CRJ-900 SRM 51-42-06-001-001 A01 AND SRM 51-42-10-001-001-A01Sep 12, 2026 · N482PX · Cndair CL6002D24 · Passenger/Crew DoorsSDR SWAA2026102100595Tie Clip · crackedCRACK TIE CLIP, BS 500H, STRINGER 26L IN THE FWD CARGO BAY. REPLACED THE TIE CLIP & FASTENERS IAW SRM 51-40-02, & DWG 143A1233, SHT 29, REV -.Sep 12, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026102142780Stub Frame · crackedCRACK INDICATION ON STUB FRAME BTWN BS 294.5 & 296.5, STRINGER 8R & 9R ON THE FWD GALLEY DOOR AREA . REPLACED THE STUB FRAME IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, DWG 141A8370, SHT 10, REV -, & DWG 141A8380, SHT 21, REV -.Sep 12, 2026 · N8658A · Boeing 7378H4 · Fuselage Main, FrameSDR SWAA2026102193815Web · corrodedCORROSION SHIELD WEB LOCATED BTWN BS 767 - 794.3, WL 156, RBL 22 IN THE AFT CARGO BAY. REPLACED THE SHIELD WEB IAW SRM 51-10-02, ITEM 9, & DWG 146A0081, REV A,Sep 12, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026102141257Cover · crackedCRACKED COVER ON AFT SERVICE DOOR NEXT TO THE INTERNAL HANDLE. REPLACED THE COVER IAW AMM 52-41-31-401. THE INSTALLATION ACCOMPLISH ON TTG8Q01DTL16.Sep 12, 2026 · N8658A · Boeing 7378H4 · Galley DoorsSDR SWAA2026102191104Crossbeam · crackedCRACKED CROSSBEAM, BS 540, LBL 24.75 - 44.5. REPLACED THE CROSSBEAM IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 143A5240, SHT 12, REV-.Sep 12, 2026 · N8658A · Boeing 7378H4 · Fuselage Main, StructureSDR SWAA2026102153730Support Angle · crackedCRACKED SUPPORT ANGLE, BS 500H, STRINGER 26R. REPLACED THE SUPPORT ANGLE, & FASTENERS IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHT 152, REV -.Sep 12, 2026 · N8658A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026102180435Crossbeam · crackedCRACKED CROSSBEAM, BS 540, BL 0 - LBL 24.75. REPLACED THE CROSSBEAM IAW SRM 51-10-02, ITEM 9, & DWG 143A0060, REV-. SSep 12, 2026 · N8658A · Boeing 7378H4 · Fuselage Main, StructureSDR IPXA2026101915093Fitting · crackedLEFT KEEL BEAM AT THE LEVEL OF CONNECTING FITTING BETWEEN FR13A AND 14 IN NOSE LANDING GEAR FIGURE 3, VIEW B AND C. FOUND CRACK ON FORWARD LOWER HOLE 4 O`CLOCK POSITION FACING OUTBOARD. ACCOMPLISH THE REPAIR PER EO-98843 AND STE PNA EA 300-5312-27-A4650, REV-.Sep 12, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, KeelSDR IPXA2026100619943Floor Panel · damagedMAIN DECK FLOOR PANEL 231NJ HAS AN INSERT DAMAGED, DOT 78-13. FLOOR PANEL 231NJ IS FABRICATED IAW SREO-16407-REQ001.Sep 12, 2026 · N146UP · Airbus A300F4622R · Fuselage Floor PanelSDR 3EJA202101962200Actuator · frozenDESCENDING THROUGH 43,000’ WE GOT A YELLOW TRIM MISCOMPARE ANNUNCIATION ON BOTH PFD’S FOLLOWED BY A RED TRIM MISCOMPARE ON BOTH PFD’S. I WAS PF AND DISCONNECTED THE AUTOPILOT. THE AIRPLANE JUMPED NOSE UP. I CAUGHT IT AND BROUGHT IT BACK TO A STABILIZED DESCENTSep 12, 2026 · N752JS · Cessna 525B · Elevator Tab Control SystemSDR IPXA2026101619802Seat Track · corrodedMDC RH SIDE, SEAT TRACK AT FR30 BETWEEN CROSSBEAM -Y2462 WITH CORROSION. VERIFIED ACCOMPLISHED SEAT TRACK SPLICE REPAIR AT FR27 TO FR33 -Y2462 IAW SRM 53-10-16-201, PARAGRAPH 4.C. <BR>FROM STEP 1 TO STEP 5, FIGURE 201, SRM 51-27-11-001 AND SRM 51-40-21-001.Sep 12, 2026 · N146UP · Airbus A300F4622R · Fuselage, Seat/Cargo Attach FittingsSDR IPXA2026101316528Floor Support · dentedFWD CARGO COMP FLOOR SUPPORT LBL 2.90 AT STA. 662 HAS A DENT AT UPPER SURFACE. 83-043. ATA 53-30. INSTALLED NEW FLOOR SUPPORT ON FWD CARGO AT STA. 662 LBL 7.25 IAW B757-200PF SRM 51-40-02-0G-0 REV. 125 20 MAY 2026, AUDITEDSep 12, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR SWAA2026101493719Support Bracket · crackedCRACKED SUPPORT BRACKET, BS 540, RBL 6 IN THE AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET IAW SRM 51-10-02.Sep 12, 2026 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026101492487Support Bracket · crackedCRACKED SUPPORT BRACKET, BS 540, LBL 6. REPLACED SUPPORT BRACKET IAW SRM 51-10-02.Sep 12, 2026 · N8656B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR IPXA2026101215031Keelbeam · crackedRIGHT KEEL BEAM AT THE LEVEL OF CONNECTING FITTING BETWEEN FR13A AND 14 IN NOSE LANDING GEAR FIGURE 3, VIEW B AND C. FOUND CRACK ON FORWARD LOWER HOLE 4&9 O`CLOCK POSITION FACING OUTBOARD. REMOVED WEB BETWEEN FR 13A AND 14 R/H SIDE OF NOSE LANDING GEAR BOX IN Sep 12, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, KeelSDR SWAA2026100762037Access Panel · crackedCRACKED BLADE ASSY ON THE LT HORIZONTAL STAB ACCESS PANEL 333AT. REPLACED THE BLADE ASSY FOR ACCESS PANEL 333AT IAW SRM 51-10-02, ITEM 9, AND SRM 51-40-02.Sep 12, 2026 · N208WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2026100706824Scuff Plate · crackedCRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT. REPAIRED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW SRM 53-30-15-2R-1 REPAIR 1. AND BAC 5975.Sep 12, 2026 · N208WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026100721741Support Angle · crackedCRACKED SUPPORT ANGLE LOC BS 694 AND WL 204 RBL 24.75. REPLACED SUPPORT ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, & DWG 273A9110, SHEET 6, REV A.Sep 12, 2026 · N208WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026100721589Support Angle · crackedCRACKED SUPPORT ANGLE, BS 694, WL 204, BL 0. REPLACED THE SUPPORT ANGLE & FASTENERS IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, & DWG 273A9110, SHEET 6, REV A.Sep 12, 2026 · N208WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2026100721166Scuff Plate · crackedCRACKED AFT CORNER OF SCUFF PLATE IN THE AFT CARGO BAY. REPAIRED AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1.Sep 12, 2026 · N208WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR AALA202610074881Bottle · leakingAIRCRAFT IN BASE MAINTENANCE: LOW PRESSURE OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER ON PASSENGER CREW DOOR 831. MAINTENANCE REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PART NUMBER OFF FE240-006, SERIAL/NUMBER OFF RFM25115, PART NUMBER ON FSep 12, 2026 · N117AN · Airbus A321231 · Passenger/Crew DoorsSDR VNAA202610060036Attach Bracket · corrodedCORROSION ON SUPPORTS (2EAS) THROUGHT ACCESS PANELS 542AZ/642AZ ON WS 29 AT LH/RH W/W MLG BAY. SUPPORTS (2EAS) THROUGHT ACCESS PANELS 542AZ/642AZ ON WS 29 AT LH/RH W/W MLG BAY WERE REPLACED PER SRM 51-42-06-001-001-A01Sep 12, 2026 · N648NN · Cndair CL6002D24 · Fuselage Main, Attach FittingsSDR VNAA202610060035Attach Bracket · corrodedCORROSION ON CLIPS (2EAS) THROUGHT ACCESS PANELS 542AZ/642AZ ON WS 48 AT LH/RH MLG W/W BAY. CLIPS (2EAS) THROUGHT ACCESS PANELS 542AZ/642AZ ON WS 48 AT LH/RH MLG W/W BAY WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01Sep 12, 2026 · N648NN · Cndair CL6002D24 · Fuselage Main, Attach FittingsSDR SWIA2026091277520Shear Tie · corrodedFRAME 27 SHEAR CLIP BETWEEN STRINGERS 28R AND 28L IS CORRODED C-CHECK RO 10062026REMOVED AND REPLACED FRAME 27 SHEAR CLIP BETWEEN STRINGERS 28R AND 28L, REF SRM 51-40-08 NO CHANGE TO WEIGHT AND BALANCE SEE CONTINUATION CARD FOR WORK ACCOMPLISHEDSep 12, 2026 · N185SY · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR SWAA2026100550157Blade · crackedCRACKED ACCESS PANEL 333AB BLADE ASSY AT LT HORIZONTAL STAB. REPLACED THE BLADE ASSY ON ACCESS PANEL 333AB IAW SRM 51-40-02, & SRM 51-10-02, ITEM 9.Sep 12, 2026 · N8309C · Boeing 7378H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2026100539644Fastener · pulledNR 1 ENGINE INLET COWL HAS MULTIPLE FASTENERS PULLING THROUGH BETWEEN 11 O'CLOCK AND 1 O'CLOCK POSITIONS. REMOVED AND REPLACED THE NR 1 ENGINE INLET COWL IAW SOPM 20-50-01.Sep 12, 2026 · N8305E · Boeing 7378H4 · Engine Air Intake SystemSDR SWAA2026100524039Vapor Barrier · crackedCRACK FOUND AT THE VAPOR BARRIER, BS 663, WL 165, LBL 25. REPAIRED IAW AMM 51-21-99-300-802.Sep 12, 2026 · N8305E · Boeing 7378H4 · Fuselage Main, BulkheadSDR AALA202610018737Strap · tornAIRCRAFT IN BASE MAINTENANCE: STRAP ON FORWARD EMERGENCY EXIT DOOR TORN OVERHEAD FLIGHT ATTENDANT REST. REMOVED AND REPLACED STRAP ON FWD EMERGENCY EXIT DOOR AT OFAR IAW SRM B787-A-51-43-07-06A-010A-A ; SRM B787-A-51-43-07-03A-010A-A AND AMM B787-A-20-11-01-00Sep 12, 2026 · N832AA · Boeing 7879 · Emergency EquipmentSDR AALA202609307795Door Latch · inoperativeAIRCRAFT IN BASE MAINTENANCE: DOOR LATCH ON EMERGENCY EXIT DOOR (AFT) IN OVERHEAD FLIGHT ATTENDANT REST HARD TO OPEN. REMOVED AND REPLACED DOOR LATCH AT EMERGENCY EXIT DOOR (AFT) IN OVERHEAD FLIGHT ATTENDANT REST IAW BOEING AMM DMC-B787-A-20-11-00-00A-030A-ASep 12, 2026 · N832AA · Boeing 7879 · Emergency ExitsSDR IPXA2026092919935Floor Panel · damagedMAIN DECK FLOOR PANEL 232NJ DAMAGED.Sep 12, 2026 · N146UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026092919943Floor Panel · damagedMAIN DECK FLOOR PANEL 231NJ HAS AN INSERT DAMAGED,Sep 12, 2026 · N146UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026092919442Floor Panel · damaged-MAIN DECK FLOOR PANEL 231KJ HAS A CORNER DAMAGED.Sep 12, 2026 · N146UP · Airbus A300F4622R · Fuselage Floor PanelSDR IPXA2026092919354Floor Panel · damagedMAIN DECK FLOOR PANEL 232SG HAS ONE CORNER DAMAGED.Sep 12, 2026 · N146UP · Airbus A300F4622R · Fuselage Floor PanelSDR J7SA2026092900523Fce · malfunctionedCREW RECEIVED GND SPOILER FAIL ON DESCENT. AIRCRAFT LANDED WITHOUT INCIDENT AT CRE. REPLACED #2 FCE IAW EMB 505 AMM 27-03-01. OPS CHECKS GOOD.Sep 12, 2026 · N391FX · Emb EMB505 · Flight Control SystemSDR IPXA2026092815031Keelbeam · crackedMAJOR REPAIR, RIGHT KEEL BEAM AT THE LEVEL OF CONNECTING FITTING BETWEEN FR13A AND 14 IN NOSE LANDING GEAR FIGURE 3, VIEW B AND C. FOUND CRACK ON FORWARD LOWER HOLE 4&9 O`CLOCK POSITION FACING OUTBOARD. AS PER REQUEST, PERFORMED EXTERNAL HFEC SURFACE INSPECTSep 12, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, KeelSDR IPXA2026092815093Keelbeam · crackedMAJOR REPAIR, LEFT KEEL BEAM AT THE LEVEL OF CONNECTING FITTING BETWEEN FR13A AND 14 IN NOSE LANDING GEAR FIGURE 3, VIEW B AND C. FOUND CRACK ON FORWARD LOWER HOLE 4 O`CLOCK POSITION FACING OUTBOARD. VERIFIED REMOVAL OF L/H NLG DOOR TORQUE TUBE I.A.W. A300-6Sep 12, 2026 · N158UP · Airbus A300F4622R · Fuselage Main, KeelSDR SWAA2026092570877Hook · looseFWD ENTRY DOOR SLIDE GIRT BAR AFT HOOK IS LOOSE AT ATTACH POINT. ATTACHED GIRT BAR AFT HOOK IAW SRM 51-40-02.Sep 12, 2026 · N8913S · Boeing 7378 · Emergency EquipmentSDR IPXA2026092217121Floor Support · corrodedMAIN DECK CABIN FLOOR STRUCTURE BTW STA 1540 TO 1580 AND LBL 45.50 STABILIZATION STRAP HAS CORROSION, FLL-042, ATA 53. REQ. NDT (HFEC) CHECK FOR CRACK ON CUT OUTSep 12, 2026 · N402UP · Boeing 75724APF · Fuselage Miscellaneous StructureSDR DALA2026092205272Slat Track · crackedCRACK ON MAIN TRACK LOCATED INBD POSITION LOWER SKIN SLAT 10 AT RT WING. PERFORMED PERMANENT REPAIR ON MAIN TRACK LOCATED INBD POSITION LOWER SKIN SLAT 10 AT RT WING IAW SRM 57-43-01 (1809827) (AIRCRAFT GROUNDED).Sep 12, 2026 · N843MH · Boeing 767432ER · Leading Edge DevicesSDR DALA2026092205271Slat Track · crackedCRACKED MAIN TRACK LOCATED OTBD POSITION LOWER SKIN SLAT 10 AT RT WING. PERFORMED PERMANENT REPAIR ON MAIN TRACK LOCATED OTBD POSITION LOWER SKIN SLAT 10 AT RT WING IAW SRM 57-43-01 (1809819) (AIRCRAFT GROUNDED)Sep 12, 2026 · N843MH · Boeing 767432ER · Leading Edge DevicesSDR DALA2026092205268Slat Track · crackedCRACK ON MAIN TRACK LOCATED IB POSITION LOWER SKIN SLAT 10 AT RT WING. PERFORMED PERMANENT REPAIR ON MAIN TRACK LOCATED I/B POSITION LOWER SKIN SLAT 10 AT RT WING IAW SRM 57-43-01 (1809730)(AIRCRAFT GROUNDED)Sep 12, 2026 · N843MH · Boeing 767432ER · Leading Edge DevicesSDR DALA2026092205267Slat Track · crackedCRACK ON MAIN TRACK LOCATED OB POSITION LOWER SKIN SLAT 10 AT RT WING. PERFORMED PERMANENT REPAIR ON MAIN TRACK LOCATED O/B POSITION LOWER SKIN SLAT 10 AT RT WING IAW SRM 57-43-01 (1809728)(AIRCRAFT GROUNDED).Sep 12, 2026 · N843MH · Boeing 767432ER · Leading Edge DevicesSDR DALA2026092205266Slat Track · crackedCRACK ON MAIN TRACK LOCATED OB POSITION LOWER SKIN SLAT 10 AT RT WING. PERFORMED PERMANENT REPAIR ON MAIN TRACK LOCATED O/B POSITION LOWER SKIN SLAT 10 AT RT WING IAW SRM 57-43-01 (1809723) (AIRCRAFT GROUNDED).Sep 12, 2026 · N195DN · Boeing 767332 · Leading Edge DevicesSDR AALA202609217300Slide Raft · wornAIRCRAFT IN BASE MAINTENANCE: MAIN PAX CABIN.R-1,DOOR EMERGENCY SLIDE GIRT SKIRT,HAS SOME WORN AREA'S. MAINTENANCE REPLACED R-1 SLIDE PACK IAW B737-MAX8 AMM 25-66-01.Sep 12, 2026 · N318SF · Boeing 7378 · Escape SlideSDR IPXA2026091811782Panel · erodedERODED SKIN, LOWER FACE L/H WING NO.5 SLAT LOWER CLOSURE PNL, NEAR INBD TRACK. REMOVE THE EROSION MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG I.A.W. 767-300F SRM 57-43-01-2R-3 REFER TO SSep 12, 2026 · N316UP · Boeing 76734AF · Wing, Plate/SkinSDR IPXA2026091811821Skin · debondedDEBONDED SKIN, INBD EDGE OF LT WING T/E OUTBD FLAP T/E SKIN, WBL 355, TOTAL: 2 AREA. REMOVE THE DISBOND MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG. I.A.W CMM 57-53-51 REV 39 INSTALL THSep 12, 2026 · N316UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA2026091512611Antenna · damagedFOUND V.S.T HF ANTENNA (321E) EROSION. REMOVE THE DAMAGED MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH FILM ADHESIVE CURED AT 260°F FOR 130 MINUTES WITH MINIMUM VACUUM OF 22 IN/HG. I.A.W. 767-300F SRM 55-30-01-2R-6 REFER TO SRM 51-70-07-0G-0 REV. 96.Sep 12, 2026 · N316UP · Boeing 76734AF · HF Communications SystemSDR AALA202609219713Hinge 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 55-16-42Sep 12, 2026 · N582UW · Airbus A321231 · Elevator Structure