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.
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 1Q2R2026070600001Skin · crackedTEMPORARY TO PERMANENT REPAIR REQUIRED TO FUSELAGE SKIN BETWEEN FS280 AND FS310, AND STGR 12R TO 15R. PERMANENT REPAIR PERFORMED THROUGH SKIN REPLACEMENT. REPLACEMENT PERFORMED BY MHI RJ MRT (MIS-6317).SDR SWIA2026042576295Tie Bar · gougedLEFT ENGINE FAN COWL, PYLON TIE BAR HAS A GOUGE ON FWD SIDE WHERE IT ATTACHES TO THE PYLON. REPAIRED LT ENGINE FAN COWL, PYLON TIE BAR IAW REO 670-54-12-895, REV -.SDR SWIA2026042576284Tie Bar · chafedLEFT HAND FAN COWL - PYLON TIE BAR, UPPER ATTACHMENT POINT ON PYLON BRACKET CHAFED. REMOVED CHAFE FROM L/H FAN COWL PYLON TIE BAR UPPER ATTACHMENT POINT ON PYLON BRACKET PER IAW SRM 51-12-00-001-001-A01, REWORKED AREA FOUND TO BE WITHIN LIMITS IAW REO 670-54-SDR CALA2026060116719Panel · corrodedFUSELAGE LEFT SIDE FWD RAM AIR DOOR HAS SIGN S OF CORROSION ON THE INNER STIFFNER CHANNEL. ALL WORK ACCOMPLISHED ON AAR GSO NON-ROUTINE 9289072. REMOVED AND REPLACED FWD MODULATION PANEL PER AMM 21-51-23.SDR SWAA2026060192700Scuff Plate · crackedCRACKED SCUFF PLATE FWD SERVICE DOOR AT FWD GALLEY AREA. REPAIRED SCUFF PLATE FWD SERVICE DOOR AT FWD GALLEY AREA IAW SRM 53-10-15-2R-2 REPAIR 2 AND BAC 5975.SDR SCNA20260601232Skin · dentedDENT WAS FOUND ON FUSELAGE SKIN CROWN AREA AT STA 380 + 6'' AND 0.25'' ABOVE STR4R. DENT WAS EVALUATED IAW A WORK INSTRUCTION BOEING MESSAGE #XTV-SCA-26-0015-03C AND XTREME RES #014944-12-1SDR SCNA20260601231Skin · dentedDENT WAS FOUND ON FUSELAGE SKIN CROWN AREA AT STA 380 + 14'' AND 0.25'' ABOVE STR 4R. DENT WAS EVALUATED IAW A WORK INSTRUCTION, MESSAGE # XTV-SCA-26-0015-03C AND XTREME RES # 014944-12-1SDR REXA2026052900889Hinge · corrodedCORROSION ON HINGE ARMS (2E/A) OF ACCESS DOOR ON BODY FAIRING ACCESS PANEL 196DR HINGES ARMS (2EAS) OF ACCESS DOOR ON BODY FAIRING ACCESS PANEL 196DR WERE REPLACED PER SRM 51-41-02-001-001-A01 AND AMM 20-21-00.SDR REXA2026052900888Hinge · corrodedCORROSION ON HINGE ARMS (2E/A) OF ACCESS DOOR ON BODY FAIRING ACCESS PANEL 196DR HINGES ARMS (2EAS) OF ACCESS DOOR ON BODY FAIRING ACCESS PANEL 196DR WERE REPLACED PER CRJ900 SRM 51-41-02-001-001-A01 AND CRJ900 AMM 20-21-00SDR SCNA20260529227Skin · dentedFUSELAGE SKIN RT SIDE BS 500G + 8.5'' BETWEEN S7R GALLEY R2 DOOR DENT WAS FOUND. XTREME W.O 014944 - NRC053: FUSELAGE SKIN R/H SIDE STA 500G + 8.5'' BETWEEN STRG 7R DENT WAS FOUND .SDR SCNA20260529226Skin · dentedFUSELAGE SKIN DENT WAS FOUND AT STA 440 + 8'' AND 2.50'' BELLOW STR 3L. ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER AND STRUCTURAL FILLER AT FUSELAGE SKIN STA 440 + 8" AND 2.50" BELLOW STR 3L PER BOEING MESSAGE: XTV-SCA-26-0018-03B. XTREME RESSDR SCNA20260529224Skin · dentedFUSELAGE SKIN R/H SIDE STA 380 + 2'' BETWEEN STRG 6R GALLEY DOOR DENT WAS FOUND. ACCOMPLISHED PERMANET REINFORCING REPAIR DOUBLER ALUMINUM 2024TS 0.040" IN, TRIPLER REPAIR 0.063"IN, STRUCTURAL FILLER 0.080" IN, TEAR STRAP 0.050"IN AND TAPER FILLER 0.050"IN ALSDR SCNA20260529223Skin · dentedFUSELAGE SKIN, DENT WAS FOUND AT STA 500 + 0.50'' AND 0.25'' BELLOW STR 2R. ACCOMPLISHED PERMANENT REINFORCING REPAIR EXTERNAL DOUBLER ALUMINUM 2024-T3 0.040" TRIPLER REPAIR 0.063", STRUCTURAL FILLER 0.080" TEAR STRAP 0.050" AND TAPER FILLER 0.050" AND 0.250"SDR SWAA2026052792907Light · deterioratedDETERIORATED PHOTOLUMINISCENT STRIP ALONG PAX CABIN. REPLACED PHOTOLUMINISCENT STRIP ALONG PAX CABIN IAW AMM 33-51-15-400-802 THE INSTALLATION WILL BE PERFORM ON MT 753-400-00-01Y SEE TTG8R007KHSP STEP 126.SDR SWAA2026052792909Light · brokenBROKEN EMERGENCY EXIT LIGHT ON SIDEWALL PANEL POSITION 231ZKW AT PASSENGER CABIN. REPLACED EMERGENCY EXIT LIGHT ON SIDEWALL PANEL POSITION 231ZKW AT PASSENGER CABIN IAW AMM 33-51-01-960-801, OPS TESTED OK.SDR SWAA2026052792906Crossbeam · crackedCRACK BRAKE PANEL LOCATED BS 540 BTW BL 0 TO RBL 24.75 WL 208.1 AT PASSENGER CABIN . REPLACED BRAKE PANEL AND FASTENERS LOCATED BS 540 BTW BL 0 TO RBL 24.75 WL 208.1 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02-0G-0; SRM 51-10-02 PARAGRAPH 9 AND DWG 143A0060SDR SWAA2026052792916Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BS 695 BL 0 WL 208.1 AT PASSENGER CABIN RT SIDE. REPLACED SUPPORT ANGLE LOCATED BS 695 BL 0 WL 208.1 AT PASSENGER CABIN RT SIDE IAW SRM 51-40-02 AND DRAWING 273A9110 SHEET: 6 REV. A.SDR SWAA2026052792905Crossbeam · crackedCRACKED BRAKE PANEL LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN. REPLACED BRAKE PANEL AND FASTENERS LOCATED BS 540 BTW BL 0 TO LBL 24.75 WL 208.1 AT PASSENGER CABIN IAW B737-800 SRM 51-40-02-0G-0 ; SRM 51-10-02 AND DWG 143A0060 SHEET 64 SDR IPXA2026052279872Skin · crackedNR 2 PYLON, O/B SIDE, INSIDE ACCESS 424ER, AT FR 8 AFT SIDE, STRUCTURE WITH CRACK (PICTURE ATTACHED). DOT 73-184. PERFORMED WELD REPAIR PER P&W SRM 54-50-00-101-C1, FIGURE 107 ON TRAVELER T26/1865914.SDR AALA202605262328Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUTOUT LOWER SILL AT FR 66 AND S23L. REPLACED LOWER SILL PER SRM 51-72-11.SDR AALA202605263149Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL AT FR 66 AND S23R. REPLACED LOWER SILL PER SRM 51-72-11.SDR SWAA2026052292934Door · crackedCRACK ON MAIN LANDING GEAR CENTER DOOR ASSY LT. PERFORMED PERMANENT REPAIR LOC. ON MAIN LANDING GEAR CENTER DOOR ASSY LT IAW SRM 52-80-02-2R-3 REPAIR 3. AND EA 26-152-01216-WIP1 REV A.SDR IPXA2026051481074Strap · corrodedMAJOR REPAIR. APU INLET DOOR AFT STRAP AT STA 1825.00 S-3R TO S-6R HAS CORROSION INSTALLED PARTS OF REPAIR (STRAP 1, STRAP 2, FILLER 3, FILLER 4 AND OUTER STRAP) IAW SRM 51-40-02-0G-0, DETAIL I.SDR IPXA2026050381104Strap · corrodedAPU INLET DOOR FWD STRAP AT BS 1787.45 FROM S-3R TO S-6R HAS CORROSION INSTALLED NEW FWD STRAP IAW SRM 51-40-02-0G-0.SDR AALA202605210935Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT AFT PASSENGER / CREW DOOR CUT OUT LOWER SILL AFT CORNER SHAPE FITTING AT FR 68 AND S23R. REPLACED CORNER SHAPE FITTING PER SRM 51-42-11.SDR AALA202605212015Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER, CREW DOOR CUTOUT LOWER SILL FORWARD CORNER SHAPE FITTING AT FR 66 AND S23R. REPLACED CORNER SHAPE FITTING PER SRM 51-72-11.SDR SWAA2026052092892Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED BS 867, BTW S2R & S3R. REPLACED SUPPORT BRACKET LOCATED BS867 AND BTW STR2R TO STR3R AT PASSENGER CABIN IAW SRM 51-10-02, ITEM 9 AND DWG 146A7901, SHEET 66, REV A. APPLIED PROTECTIVE TREATMENT ON HOLES IAW SRM 51-20-01.SDR SWAA2026052092890Support Bracket · crackedCRACKED SUPPORT BRACKET IB FLAP INTERNAL CAVITY AT RT WING. REPLACED SUPPORT BRACKET AND FASTENERS LOC IB FLAP INTERNAL CAVITY AT RT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 113A2100, SHEET 58, REV -.SDR SWAA2026052092889Angle · crackedCRACKED ANGLE ON AUXILIARY TRACK SLAT 1 AT LT WING. REPLACED ANGLE ON AUXILIARY TRACK SLAT 1 AT LT WING IAW SOPM 20-50-01, REV 40, AND SRM 51-40-02.SDR IPXA2026050681325Angle · corrodedAPU INLET DOOR LOWER CORNER ANGLE AT STA 1787.45 S-R6 HAS EVIDENCE OF CORROSION. INSTALLED NEW LOWER CORNER ANGLE I.A.W. SRM 51-40-02-0G-0.SDR IPXA2026050681237Angle · corrodedAPU INLET DOOR UPPER CORNER ANGLE AT STA 1787.45 S-3R HAS EVIDENCE OF CORROSION. INSTALLED NEW UPPER CORNER ANGLE I.A.W. SRM 51-40-02-0G-0.SDR IPXA2026050681291Angle · corrodedAPU INLET DOOR LOWER ANGLE AT STA 1787.45 TO STA 1825.00 S6R HAS EVIDENCE OF CORROSION. INSTALLED NEW LOWER ANGLE I.A.W. SRM 51-40-02-0G-0.SDR SWAA2026051992975Support Angle · crackedECS BAY TEE SUPPORT ANGLE IS CRACKED AT BS 650, RBL 41, WL 143. REMOVED AND REPLACED TEE SUPPORT ANGLE BS 650 RBL41; WL143 IAW SRM 51-40-02 AND DWG 149A7210 REV -.SDR AALA202605198887Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION CORNER FITTING FRAME 66L AT LEVEL STR 23 AT AFT GALLEY MEASURE ARE: L=0.751 INCH, W=0.438 INCH, D=0.020 INCH. MAINTENACE REPLACED CORNER FITTING AND FASTENERS LOC FR66L AT LEVEL STR23L AFT GALLEY AREA IAW A319 SRM 51-4SDR AALA202605194754Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION CORNER FITTING FRAME 68L AT LEVEL STR 23 AT AFT GALLEY MEASURE ARE: L=0.294 INCH, W=0.138 INCH, D=0.018 INCH. MAINTENANCE REPLACED CORNER FITTING AND FASTENERS LOC. FR68L AT LEVEL STR23L AFT GALLEY AREA IAW A319 SRM 51-4SDR R61A2026051800134Floor Support · corrodedDURING HEAVY CHECK CF III RT FLOOR SILL BETWEEN FR 83 - 84 RBL 49 CORRODED. REMOVED AND REPLACED RT FLOOR SILL IAW SRM 51-41-02.SDR R61A2026051800132Plate · corrodedDURING HEAVY CHECK CF III FLOOR STRUCTURE SPLICE PLATE AT FR 90 LBL 0 FOUND CORRODED. REMOVED AND REPLACED FLOOR STRUCTURE SPLICE PLATE IAW EMB 170/175 SRM 51-43-04SDR R61A2026051800131Splice · corrodedDURING HEAVY CHECK CF III FLOOR STRUCTURE SPLICE PLATE AT FR 90 LBL 0 FOUND CORRODED. REMOVED AND REPLACED FLOOR STRUCTURE SPLICE PLATE IAW EMB 170/175 SRM 51-43-04SDR R61A2026051800130Doubler · corrodedDURING HEAVY CHECK CF III FOOR STRUCTURE CORROSION FOUND ON DOUBLER FLOOR AT FR 84 OUTBD OF R/H INBD SEAT TRACK. REMOVED AND REPLACED FLOOR STRUCTURE DOUBLER IAW EMB 170/175 SRM 51-43-04SDR R61A2026051800129Shear Panel · corrodedDURING HEAVY CHECK CF III FR 87-88 FOUND TO HAVE CORRODED L/H SHEAR PLATE. REMOVED AND REPLACED SHEAR PLATE IAW EMB 170/175 SRM 51-42-01SDR R61A2026051800128Shear Panel · corrodedDURING HEAVY CHECK CF III FR 87-88 FOUND TO HAVE CORRODED RT SHEAR PLATE. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-01.SDR AALA202605180806Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION CENTER FITTING BTW FR66 AND FR68 LH SIDE AFT GALLEY MEASURES ARE L=1.302 IN, W=0.383 IN, D=0.220 IN. MAINTENANCE REPLACED CENTER FITTING AND FASTENERS LOCATED BTW FR66 AND FR68 LH SIDE AFT GALLEY AREA I.A.W A319 SRM 5SDR SWAA2026051392862Handle · looseL1 DOOR ATTACHED ASSIST HANDLE LOOSE. ACCOMPLISHED STEP 1 IAW AMM 25-21-31-420-802. SECURED L1 ASSIST HANDLE IAW AMM 25-21-31-420-802.SDR SWAA2026051392863Handle · looseR1 DOOR ATTACHED ASSIST HANDLE LOOSE. ACCOMPLISHED STEP 1 IAW AMM 25-21-31-420-802. SECURED R1 DOOR HANDLE IAW AMM 25-21-25-420-801.SDR SWAA2026051392864Handle · looseR2 DOOR ATTACHED ASSIST HANDLE LOOSE. ACCOMPLISHED STEP 1 IAW AMM 25-21-25-420-801. SECURED R-2 DOOR HANDLE IAW AMM 25-21-25-420-801.SDR IPXA2026050572367Bracket · corrodedACCESS DOOR 313AL LT AND RT LATCH STOPS AT THE CUT-OUT 4EA BRACKETS ARE CORRODED. INSTALLED 4EA BRACKETS ND RT AND LT LATCH STOP IAW SRM 51-40-02-0G-0.SDR IPXA2026050281431Skin · crackedNR 1 ENGINE AFT STRUT FAIRING LOWER AFT EXTERIOR OTBD SHOWS EVIDENCE OF A CRACK NEAR FASTENER. INSTALLED AFT STRUT FAIRING NR 1 ENGINE IAW SRM 51-40-02-0G.SDR AALA202605052946Baffle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT BAFFLE CLIP AT STA 500H AND RBL 23. REPLACED BAFFLE CLIP PER AARD 51-00-05-1.SDR SWIA2026042575973Skin · dentedINSPECTED DENT REPORTED BY RAMP. MEASURED TO BE APPROXIMATELY 0.085" DEEP, 12" LONG AND 3.5" WIDE AND SLIGHTLY CREASED OVER FR 11 BETWEEN STGR 18L AND 19L. OUT OF LIMITS PER SRM 53-10-01. (FLIGHT 3896) COMPLIED WITH PERMANENT REPAIR ON LT FWD FUSELAGE SKIN ASDR CALA2026050415948Lamp · inoperativeSEAT 26 C BULLNOSE EMERGENCY PATHWAY LIGHT OUT NEEDS ADDITIONAL TROUBLESHOOTING SUSPECT WIRE BUNDLE W00634 BAD , RELAMPED AND REPLACED HOUSING ASSEMBLY STILL NOT WORKING REQUEST MEL 3314A FOR AREA LIGHT INOP BULLNOSE EMERGECY LIGHT MEL 3314A NOT CORRECT MEL RE