Service difficulty reports
1,771,154 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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CALA2026072617998Latch · wornFWD RT LATCH ON H/P PNUMATIC DOOR192, DOOR HAS WORN INTO PREVIOUS REPAIR AND STRIKER PLATE IS MISSING. REMOVED DAMAGED REPAIR STRAP IAW SRM 57-10-13-2R-3, CUT FILLER AND STRAP TO SHAPE FROM 0.125" IAW SRM 57-10-13-2R-3, TABLE 201, FOUND PREVIOUS REPAIR FSDR CALA2026072617996Trunnion · corrodedLEFT WING REAR SPAR LT MLG FWD TRUNNION SUPPORT FITTING UPPER OTBD BUSHING HOLE. REMOVED AND REPLACED LT MLG TRUNNION FITTING ASSY (INCLUDING BUSHINGS) IAW DWG 115A5002, SH7 AND SRM 51-40-02-0G-0.SDR VNAA2026072521202Skin · dentedEA 5321-2026-0570 (560FH PERM REPAIR - FUSELAGE SKIN DENTED. REPAIR FOR REWORKED DENT AND GOUGE DAMAGE TO FUSELAGE SKIN PANEL BETWEEN BS 295 & BS 310, STR 13 & STR 14R. REO 690-53-21-2176 INCORPORATED.SDR QMLA2026072520049Dual Tachometer · degradedNEEDLES ON DUAL TACH NOT ALIGNED WHILE RUNNING. FADEC DEGRADED/RESTART FAULT LIGHT ILLUMINATED AFTER STARTUP. REMOVED AND REPLACED DEFECTIVE DUAL TACH GAUGE.SDR YYMA2026072400600Slat System · faultedON APPROACH INTO KALN MRO FACILITY LOCATION, CREW REPORTED: DURING APPROACH SLAT FAIL INDICATION WITH SHAKER ANTICIPATED MESSAGE WITH ASSOCIATED MASTER CAUTION. LANDED WITH SLAT 0 FLAP 2. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT.SDR DALA2026072404323Flex Hose · leakingAFTER LANDING, APU STARTED & BOTH PACKS PUT ON APU. AN IMMEDIATE ELECTRICAL ODOR NOTED. APU BLEED SHUTOFF & PACKS PUT BACK ON ENG BLEED. ODOR DISSIPATED, APU CONTINUED TO OPS NORMALLY PROVIDING ELEC POWER ONLY. FOUND 2EA FWD GALLEY DRAIN LINE FLEX HOSES LEAKSDR WX0A2026072432898Battery · inoperative(AIRCRAFT NOT GROUNDED) FLASHLIGHT BATTERY IN AFT JUMPSEAT INOP OR NOT CHARGING. REPLACED BATTERY IN AFT JUMPSEAT PER AMM 25-60-02"SDR DALA2026072404318Charger · inoperativeDURING SVC CHK FOUND EMERGENCY LIGHTS INOP ROW 34 TO 44. R & R BATTERY PACK (M9009) NO HELP, SUSPECT BATTERY CHARGER INOP. (8847282) (AIRCRAFT GROUNDED)SDR UIEA2026072400647Contact · dirtyFO`S FLASHLIGHT GREEN LIGHT INOPERATIVE. CLEANED ELECTRICAL CONTACTS & OPS CHK FLASHLIGHT PRESS TO TEST, NORMAL IAW AMM 25-64-01. FLASHLIGHT TURNS ON NML</P>)SDR ABXA20260723333Iru · faultedCREW ABORTED T/O AT 5KTS DUE TO AN IRU GOING OFFLINE WHICH AFFECTED THE NAVIGATION. AFTER ABORTING T/O, THE ISSUE CLEARED. AFTER CHECKING WITH MAINTENANCE CONTROL IT WAS DETERMINED THEY COULD CONTINUE SINCE THE ISSUE CLEARED. A/C RETURNED TO SERVICE.SDR HNAA2026072400632Bleed Valve · faultedBLD VLV CLOSED MSG ON T/O. RAN QRH AND MESSAGE PERSISTED, WENT TO START APU AND APU FAILED WITH APU FAIL MSG FACT 23JUL26 18:15 PHL T/S IAW AMM FIM 36-11-00-810-807A BLOCK 8 AND PERFORMED OPS BLEED SYSTEM. OPS CHECK ISW AMM REF 36-00-00. FOUND NO DEFECTSDR FDEA202607231017Access Panel · crackedCRACKS ON ACCESS PANEL 241 WFF AT MDCC ACCESS PANEL 241 WFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R FIG 201 REP GEN SHEET 2 REV 94 DEC 15/2025SDR FDEA202607231016Access Panel · crackedCRACK ON FLOOR ACCESS PANEL 241 JFF AT MDCC FLOOR PANEL 241 JFF AT MDCC WAS REPAIRED IAW B767 SRM 53-00-50-2R FIG 201 REP GEN SHEET 2 REV 94 DEC 15/2025SDR FDEA202607231015Floor Panel · puncturedA PUNCTURE ON FLOOR PANEL 251AFF OF MAIN DECK CARGO. FLOOR PANEL 251AFF OF MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR 4-B FIG. 201 SHEET 2 REV. 94 DEC 15/2025.SDR FDEA202607231014Skin · dentedDENT ON INTERNAL SURFACE OF SLAT NO. 8 AT 72.5" FROM INBOARD EDGE AND 7" FROM TRAILING EDGE, RIGHT WING. SLAT NO. 8 AT 72.5" FROM INBOARD EDGE AND 7" FROM TRAILING EDGE, RIGHT WING WAS REPAIRED IAW B767 SRM 51-70-10-2R REPAIR 4 REV. 94 DEC 15/2025SDR FDEA202607231013Beam · corrodedNOSE WHEEL WELL STRUCTURE BS 310.5 LOWER AREA INTERNAL BEAM WITH CORROSION REMOVED VERTICAL BEAM OUT OF LIMITS AT NOSE WEEL STRUCTURE BS 310.5 LBL 20.05 LOWER AREA INTERNAL IAW B757 51-40-02-0G; TRIMED LOCATED, DRILLED AND INSTALLED NEW VERTICAL BEAM REPLASDR FDEA202607231012Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 251VFF ON MAIN DECK CARGO COMPARTMENT FLOOR PANEL 251VFF ON MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025SDR FDEA202607231011Floor Panel · puncturedPUNCTURE ON FLOOR PANEL 241FFF ON MAIN DECK CARGO COMPARTMENT FLOOR PANEL 241FFF ON MAIN DECK CARGO COMPARTMENT WAS REPAIRED IAW B767 SRM 53- 00-50-2R PAR 4-B FIG 201 SHEET 2 REV 94 DEC 15/2025.SDR FDEA202607231010Floor Panel · damagedPUNCTURE ON ACCESS FLOOR PANEL 242 FFF AT MDCC. ACCESS FLOOR PANEL 242 FFF AT MDCC WAS REPAIRED I.A.W B767 SRM 53-00-50-2R PAR 4.G(2). REV 94 DATE DEC 15 2025.SDR SIMA20260723001Windshield · damagedCAPTAIN`S WINDSHIELD BIRD STRIKE AT FL220 TRANSFERRED TO NRWC 792-ORD-02395 ITEM-1. R & R CAPTAIN COCKPIT WINDSHIELD IAW AMM 56-11-00. LEAK CHECKED GOOD.SDR DALA2026072404317Skin · not reportedFUSELAGE CROWN, BS 560, S-2L - S-4L, DOUBLER NEAR STC INSTALL AREA. COMPLIED WITH ER/A 635805-14AD. (1715519) (AIRCRAFT GROUNDED).SDR SCNA20260724325Window · detachedVIEWING WINDOW OFF SLIDE 1R FELL OFF. SECURED VIEWING WINDOW ON 1R DOOR SLIDE REF AMM 25-66-00. THIS CLEARS MEL 25-10N.SDR SCNA20260724324Window · crackedFWD SLIDE L1 VIEWING WINDOW CRACKED. R & R L1 DOOR SLIDE WINDOW WITH NEW IAW AMM 25-66-00.SDR CALA2026072417985Stop Fitting · gougedFWD CARGO DOOR AFT SIDE LOWER STOP FITTI NG HAS A GOUGE ON UPPER SURFACE. REPLACED STOP FITTING IAW DWG 143A6117 REV A AND SRM 51-40-02.SDR CALA2026072417983Door Frame · scratchedFWD CARGO DOOR AFT END LOWER SIDE CORNER FRAME HAS MULTIPLE SCRATCHES. REPLACED CORNER FRAME IAW DWG 143A6110, REV A.SDR CALA2026072417981Lamp · brokenEMERGENCY ESCAPE PATH LIGHT ASSEMBLY ON SEAT 37F IS BROKEN. REMOVED AND REPLACED ESCAPE PATH LIGHT ASSEMBLY ON SEAT 37F REF AMM 33-51-10-962-104. ESCAPE PATH LIGHT SYSTEM IS GOOD FOR SERVICE.SDR CALA2026072417978Battery Pack · no testDURING EMERGENCY ESCAPE PATH LIGHT SYSTEM CHECK ON LOG PAGE 9707422 FOUND EMERGENCY CEILING LIGHTS FROM SEATS ROW 47LK TO 50LK DO NOT TURN ON. PERFORMED TROBLESHOOTING AND FOUND BATTERY PACK ON POWER SUPPLY M734 DISCHARGED. REMOVED AND REPLACED BATTERY PACK RESDR CALA2026072417976Skin · missingLEFT INBD FLAP TRAILING EDGE WEDGE LOWER SKIN COMPLETELY MISSING. MEASUREMENTS ARE 29" X 14". REMOVED FLAP WEDGE ASSEMBLY PER S.R.M. 57-53-01 PICKED UP FRAME MOUNTING HOLES AND SKIN FASTENER HOLES ON NEW WEDGE PANEL REF SRM 51-40-02. LOCATED ALL HOLES, INSSDR CALA2026072417974Battery · inoperativeONE FLASHLIGHT INOPERATIVE, FWD GALLEY. REMOVED AND REPLACED THE FLASHLIGHT BATTERY IN FWD GALLEY IAW AMM 25-64-00. OPS NORMAL.SDR CALA2026072417972Housing · brokenSEAT 8C EPL HOUSING HAS BROKEN MOUNTING TAB REPLACED SEAT 8C EPL HOUSING IN REF WITH CMM 25-22-59-3952.SDR CALA2026072417970Fuel Cap · missingDURING EXTERNAL WALKAROUND, FOUND RT UNDERWING REFUEL CAP-COUPLING MISSING. PREVIOUSLY INSTALLED REFUEL CAP-COUPLING IS PDA2 AND PART LOCATION IS UNKNOWN AT THIS TIME. INSTALLED SERVICEABLE UNDERWING REFUEL CAP-COUPLING IAW AMM 28-25-41. PART SECURED TO ACFTSDR DALA2026072404314Web · corrodedLEVEL 2 CORROSION, WEB FRAME 16 LOCATED AT LEVEL STR 23L AT FWD GALLEY AREA. REPLACED WEB LOCATED BTW FR12 TO FR16 AT LEVEL STR23L FWD GALLEY AREA IAW SRM 51-72-11, SRM 51-42-11, DWG# D53112570, AND DWG D53114392, TOOK MEASURES OF CORROSION ARE:L=0.734 IN SDR JR2R20260723433Skin · chafedRH OVER PYLON FIXED LEADING EDGE PANEL IS CHAFED. REPAIREDSDR JR2R20260723434Skin · chafedLH OVER PYLON FIXED LEADING EDGE PANEL IS CHAFED. REPAIREDSDR J7SA2026072300493Position Unit · faultedDISCOVERED AIRCRAFT SUSCEPTIBLE TO HIGH SPEED DATA BUS (HSDB) ISSUE CAUSED BY A FAILURE OF THE XM RADIO RECEIVER. THIS AIRCRAFT IS ONE OF 17 EMBRAER PHENOM 300 AIRCRAFT IN THE FLEXJET FLEET THAT IS EQUIPPED WITH XM RADIO AND AVIONICS SOFTWARE LOAD 18.10. IN THSDR J7SA2026072300492Position Unit · faultedDISCOVERED AIRCRAFT SUSCEPTIBLE TO HIGH SPEED DATA BUS (HSDB) ISSUE CAUSED BY A FAILURE OF THE XM RADIO RECEIVER. THIS AIRCRAFT IS ONE OF 17 EMBRAER PHENOM 300 AIRCRAFT IN THE FLEXJET FLEET THAT IS EQUIPPED WITH XM RADIO AND AVIONICS SOFTWARE LOAD 18.10. IN THSDR J7SA2026072300491Position Unit · faultedDISCOVERED AIRCRAFT SUSCEPTIBLE TO HIGH SPEED DATA BUS (HSDB) ISSUE CAUSED BY A FAILURE OF THE XM RADIO RECEIVER. THIS AIRCRAFT IS ONE OF 17 EMBRAER PHENOM 300 AIRCRAFT IN THE FLEXJET FLEET THAT IS EQUIPPED WITH XM RADIO AND AVIONICS SOFTWARE LOAD 18.10. IN THSDR J7SA2026072300490Position Unit · faultedDISCOVERED AIRCRAFT SUSCEPTIBLE TO HIGH SPEED DATA BUS (HSDB) ISSUE CAUSED BY A FAILURE OF THE XM RADIO RECEIVER. THIS AIRCRAFT IS ONE OF 17 EMBRAER PHENOM 300 AIRCRAFT IN THE FLEXJET FLEET THAT IS EQUIPPED WITH XM RADIO AND AVIONICS SOFTWARE LOAD 18.10. IN THSDR J7SA2026072300489Position Unit · faultedDISCOVERED AIRCRAFT SUSCEPTIBLE TO HIGH SPEED DATA BUS (HSDB) ISSUE CAUSED BY A FAILURE OF THE XM RADIO RECEIVER. THIS AIRCRAFT IS ONE OF 17 EMBRAER PHENOM 300 AIRCRAFT IN THE FLEXJET FLEET THAT IS EQUIPPED WITH XM RADIO AND AVIONICS SOFTWARE LOAD 18.10. IN TSDR J7SA2026072300488Position Unit · faultedDISCOVERED AIRCRAFT SUSCEPTIBLE TO HIGH SPEED DATA BUS (HSDB) ISSUE CAUSED BY A FAILURE OF THE XM RADIO RECEIVER. THIS AIRCRAFT IS ONE OF 17 EMBRAER PHENOM 300 AIRCRAFT IN THE FLEXJET FLEET THAT IS EQUIPPED WITH XM RADIO AND AVIONICS SOFTWARE LOAD 18.10. IN THSDR IPXA2026072316966Control Panel · inoperativeEMERGENCY DECLARED, DIVERTED. RECEIVED CABIN ALT WARNING AT 40,000 FT. AUTO 1 AND AUTO 2 NOT WORKING. WAS ABLE TO REGAIN PRESSURIZATION CONTROL IN MANUAL MODE REMOVED AND REPLACED CABIN PRESSURIZATION SELECTOR PANEL IAW AMM 21-31-01. OPS TEST GOOD REMOVED ANSDR DALA2026072304309Bridge · crackedRIGHT WING NR 3 FLAP TRACK CARRIAGE ASSY OTBD BRIDGE CRACKED. REPLACED THE RT WING NR 3 FLAP TRACK CARRIAGE ASSY OTBD BRIDGE IAW AMM 27-54-78. (1714801) AIRCRAFT WAS GROUNDED.SDR DALA2026072304305Wire · brokenEMERGENCY LIGHTS AT SEATS 14-20 INOP. FOUND BROKEN GROUND WIRE AT ROW 20. REPAIRED WIRE PER SWPM 20-10 . EMERG LIGHTS OPS CHECK GOOD PER AMM 33-51. (9599809)(AIRCRAFT GROUNDED)SDR DALA2026072304304Repair · not reportedEXISTING REPAIR WAS FOUND IN THE INSPECTION AREA (LOWER AFT CORNER OF R1 DOOR CUTOUT, FROM BS 352 TO 378, BTW S15R AND S19R. STA 352 TO STA 378, BTW S15R AND S19R).PER PRI 635771-14 REV. 1 AND ER/A 635771-14AD REV. ORIGINAL. (1714692)(AIRCRAFT GROUNDED)SDR UIEA2026072300640Apu · odorBACK TO BLOCK DUE TO EICAS MESSAGE SMOKE CREW REST AND UNUSUAL SCENT DETECTED IN UPPER DECK. PERFORM FIRE TEST, NO SMOKE PRESENT IN CABIN. OIL SCENT COMING FROM APU. SUSPECT APU BEARING OIL LEAK ENTERING CABIN. REMOVED AND REPLACED APU IAW ATLAS WORK CARD 49-SDR FDEA202607231009Landing · corrodedLEFT WING- TRAILING EDGE LOWER ACCESS PANEL 541JB CUTOUT FORWARD EDGE SUPPORT CHORD LOWER SURFACE FOUND CORROSION AT STA XW= 335. EVALUATED & FOUND EXFOLIATED OUT OF LIMITS IAW SRM 57-00-00-2R, FIGURE 202, SHEET 3. REPAIRED STA XW= 276.029 - XW= 375.50 OSDR FDEA202607231008Floor Support · corrodedMAIN DECK CARGO AFT FLOOR PANEL SUPPORT ASSEMBLY FOUND WITH CORROSION FROM STATION 1984 X= -57. EVALUATED FOUND EXFOLIATED AND EXCEEDED LIMIT IAW SRM 53-00-00-2R, FIGURE 206, REPAIR GENERAL. THE FLOOR SUPPORT WAS R & R, BS 1887 - 2007, X= - 57 IAW SRM 51-SDR FDEA202607231007Seat Track · wornMAIN DECK CARGO SEAT TRACK AT BS 889, X= 27.5" FOUND CROWN WORN. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT EXISTING SPLICES BS 869 TO 929, X = 27.5 IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA202607231006Seat Track · wornMAIN DECK CARGO SEAT TRACK AT BS 889, X= 8.5" FOUND CROWN WORN. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT BS 869 TO BS 909, X = 8.5 IAW SRM 53-00-52-2R, FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA202607231005Seat Track · wornMAIN DECK CARGO SEAT TRACK AT BS 889, X= -8.5, FOUND CROWN WORN. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT AT BS 869 TO 909, X = - 8.5, IAW SRM 53-00-52-2R, FIGURE 201, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.