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 FDEA202602090151Skin · crackedDURING WORK CARD: EG-5710-E0376285F P12 STEP4.B(2).(B), THEN FOUND ONE CRACK ON RT UPPER WING SKIN FASTENER #6 AS MARKED. RIGHT WING UPPER SKIN NR 6 FASTENER HOLE REPAIRED IAW SRM 51-40-05-0G, FIGURE 4, TABLE C , SRM 51-40-02-0G, FIGURE 12, SRM 51-40-04-0G, SDR FDEA202602090150Skin · crackedDURING WORK CARD: EG-5710-E0376285F P11 STEP4.B(2).(B), THEN FOUND ONE CRACK ON LT UPPER WING SKIN FASTENER NR 6. THE LEFT WING UPPER SKIN #6 FASTENER HOLE CRACKED AREA REPAIRED AS PER B777 SRM 51- 20-07-0G FIGURE 2, SRM 51-50-02-0G FOGURE 1, SRM 51-40-02SDR FDEA202602090149Skin · crackedDURING WORK CARD: EG-5710-E0376285F P11 STEP3.B.(1) & 5.A.(2) THE FOUND TWO CRACKS ON LT UPPER WING SKIN FASTENER NR 5. THE LEFT WING UPPER SKIN NR 5 FASTENER HOLE CRACKED AREA REPAIRED IAW SRM 51- 20-07-0G, FIGURE 2, SRM 51-50-02-0G, FIGURE 1, SRM 51-40-02-0SDR FDEA202602090148Skin · wornRH WING, T/E MAIN FLAP, OTBD EDGE UPPER SURFACE HAS AREA THAT IS WORN INTO COMPOSITE. REPAIRED RT WING INBD MAIN FLAP OTBD EDGE UPPER SURFACE 23 INCHES FROM T/E IAW DRAWING 113T2204 AND SRM 51-70-05-0G. MAJOR REPAIR.SDR SCNA20260209063Light · inoperativeOVERHEAD PANEL EMERGENCY LIGHTS NOT ARMED, LAMP INOPERATIVE. R & R EMERGENCY LIGHTS NOT ARMED LIGHT ASSY REF AMM 33-18-00. OPS TEST GOOD.SDR SCNA20260209062Attach Fitting · looseL2 DOOR GIRT BAR CLIP LOOSE SLIDE FALLING OUT OF CLIP. ADJUSTED 2L CIRT BAR CLIPS REF. AMM 25-66-00. ITEM OKAY FOR SERVICE.SDR CALA2026092319703Stiffener · crackedLT HORIZONTAL STAB. IN-STAB, RIB HSS 92.7, 3RD STIFFENER FROM FRONT CRACKED. REPAIRED THE 3RD STIFFENER IAW SRM 55-10-09-2R-5, SRM 55-10-01-2R-11.SDR CALA2026092319701Stiffener · crackedRIGHT HORIZONTAL STAB, IN-SPAR HSS 92.7, NR 3 & 4 STIFFENERS TRANSITION RADIUS & HSS 111.10, NR 3 STIFFENER, CRACKED. REPAIR OVER 5LBS. WEIGHT AND BALANCE CHANGE FORM WAS COMPLETED. WEIGHT CHANGE IS 8.763LBS.+/-. REPAIRED THE DAMAGE IAW 55-10-09-2R-4 AND SRSDR REXA2026080301403Drain Pan · crackedCRACK AND BEND LEFT AND RIGHT DRAIN PAN AT AFT EQUIPMENT COMPARTMENT. LEFT AND RIGHT DRAIN PAN AT AFT EQUIPMENT COMPARTMENT WERE REPAIRED PER CRJ/700 SRM 51-71-59-001-001-A01 AND CRJ/700 SRM 51-25-16-001-001-A01SDR REXA2026080301402Drain Pan · crackedCRACK AND BEND LEFT AND RIGHT DRAIN PAN AT AFT EQUIPMENT COMPARTMENT. LEFT AND RIGHT DRAIN PAN AT AFT EQUIPMENT COMPARTMENT WERE REPAIRED PER CRJ/700 SRM 51-71-59-001-001-A01 AND CRJ/700 SRM 51-25-16-001-001-A01SDR REXA2026080301401Stiffener · wornINITIAL INSPECTION: WEAR ON INTERNAL SKIN AND ANGLE ON TAIL BUMPER CUTOUT AREA BTW STGR 26L TO STGR 27R AND VS67.5% APPROX AT AFT EQUIPMENT COMPARTMENT PAINT ON INTERNAL SKIN WAS REMOVED AND NOT DAMAGE WAS FOUND PER CRJ-700 SRM 51-26-01-001-001-A01 AND ANGLE OSDR YENA20260210001Skin · corrodedDURING HEAVY MAINTENANCE: RT WING TOP SKIN PANEL CORRODED /1/ - AIRBUS DOSSIER 81709907 /2/ - AIRBUS RDAF REF. & ISSUE.: 81709907/003/2025 ISSUE A /3/ - AIRBUS RI R572-44701 ISSUE B /4/ - AIRBUS RI R572-58616 ISSUE N /5/ - AIRBUS RI R572-58926 ISSUE E /6/ - ASDR SWIA2026020876069Floor Support · corrodedLH FLOOR SILL HAS CORROSION AT FS985 - FS1000. REPAIRED LH FLOOR SILL HAS CORROSION AT FS985 - FS1000 REF CRJ900 REO 690-53-61-1740 REV --, ALL STEPS COMPLIED WITH. SEE CONTINUE CARD FOR DETIALS. COMPLIED WITH TASK CARD 51-900-1002-SKY.SDR E0YA20260430001Controller · odorL WINDSHIELD HEAT FAIL CAS MESSAGE FOLLOWED BY BURNING SMELL.SDR AALA202604283330Shear Plate · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23 R BTW FR69 AND FR70 AFT GALLEY AREA. MEASURE OF CRACK ON SHEAR PLATE IS L= 1.826 INCH.SDR SWIA2026020875878Cleat · corrodedFOUND CORROSION ON PAX DOOR FS311.75 INTERCOSTAL DD7 CLEAT. INSTALLED NEW PAX DOOR FS311.75 INTERCOSTAL DD7 CLEAT. IAW. SRM 51-42-06-00. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR SWIA2026020875868Support Angle · gougedFOUND GOUGE ON PAX DOOR FWD ANGLE SUPPORT. UNDER PULL-IN LEVER. REMOVED AND INSTALLED NEW PAX DOOR FWD ANGLE SUPPORT. IAW SRM 51-42-06-00. SRM 51-42-21-00, SRM 51-41-02. AND DWG 601R31702 REV. N. COMPLIED WITH 51-900-1003-SKY, PRESSURE LEAK CHECK WAS GOODSDR SWIA2026020875845Intercostal · corrodedFOUND CORROSION ON FWD INTERCOSTAL DD5. INSTALLED NEW PAX DOOR FWD INTERCOSTAL DD5. IAW. SRM 51-42-06-00. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY.SDR SWIA2026020875844Bracket · damagedPAX DOOR FS311.75 INTERCOSTAL DD2 BRACKET HOLES PREVIUSLY OVERSIZE. REMOVED AND INSTALLED NEW PAX DOOR FS311.75 INTERCOSTAL DD2 BRACKET. IAW. SRM 51-42-06-00 AND DWG 601R31702 REV. N. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKYSDR SWIA2026020875837Cleat · corrodedFOUND CORROSION ON PAX DOOR FS320.163 INTERCOSTAL DD6 CLEAT. PAX DOOR FS320.163 INTERCOSTAL DD6 CLEAT, ORIGINAL MATERIAL THICKNESS IS 0.050" IAW SRM 52-10-14-00 CORROSION EXIST ON 2 ELEMENT OUT OF LIMITS REPLACE CLEAT. IAW SRM 52-00-00 PERFORMED LOCATE AND DSDR SWIA2026020875828Bracket · corrodedFOUND CORROSION ON PAX DOOR FS311.75. DD5 BRACKET. INSTALLED NEW PAX DOOR FS311.75 INTERCOSTAL DD5 BRACKET. IAW SRM 51-42-06-00 AND DWG 601R31702 REV. N.COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKYSDR SWIA2026020875815Hinge Fitting · corrodedDURING REMOVAL OF BEARING ON L/H ELEVATOR I/B HINGE FITTING PN 600-24043-1, FOUND BEARING BORES TO BE CORRODED AND PITTED. I/B HINGE FITTING REQUIRES REPLACEMENT. REMOVED CORRODED L/H ELEVATOR INBD L/E HINGE FITTING ASSY. AND INSTALLED 1 EA NEW L/H ELEVATOR ISDR SWIA2026020875711Skin · chafedLOWER WING PLANK ACCESS HOLE AT 510BB, AFT LANDING CHAFED(MARKED WITH TAPE). PERFORMED A MAJOR REPAIR BY BLENDING CORROSION ON LOWER WING PLANK ACCESS HOLE AT 510BB LANDING IAW REO 601R-57-21-030 REV L DATED 2014-02-05. COMPLETED SKYWEST TASK CARD 51-900-1SDR KCSA202604041028Battery Pack · no testRIGHT UPPER DECK ESCAPE DOOR BATTERY PACK FAIL PUSH TO TEST LIGHT DURING A/C START UPSDR VNAA202603280001Web · crackedCRACK ON UPPER WEB AFT EDGE AT PASSENGER DOOR. UPPER WEB AFT EDGE AT PASSENGER DOOR WAS REPAIRED PER SRM 52-11-04-201-006-A011SDR VNAA20260328010Seat Track · corrodedCORROSION SIDE SEAT RAIL RETAINERS, LH SIDE ON FS708 AND RH SIDE FROM FS785 TO FS797 AT PAX CABIN. CORROSION ON SIDE SEAT RAIL RETAINERS, LH SIDE ON FS708 AND RH SIDE FROM FS785 TO FS797 (PAX CABIN) WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND REWORKESDR VNAA20260328009Seat Track · corrodedCORROSION ON LH SIDE SEAT RAILS; (2 SECTIONS) FROM FS379 TO FS573, (3 SECTIONS) FROM FS661 TO FS761 AND (2 SECTIONS) FROM FS785 TO FS953 AT PAX CABIN. CORROSION ON LH SIDE SEAT RAILS; (2 SECTIONS) FROM FS379 TO FS573, (3 SECTIONS) FROM FS661 TO FS761 AND (2 SDR VNAA20260328007Hinge Fitting · corrodedCORROSION IN THE INNER AREA OF THE BORE LUGS AT AILERON FITTING 1, CENTRAL FITTING (L1, L2, L3, L4, L5, L6) AND FITTING 4 (UPPER AND LOWER) OF LH WING AILERON. BORE LUGS HINGE FITTING NO. 1 & 4 (LOWER) , CENTER HINGE FITTING BORE LUGS L1, L3, L4, L6 WERE CLEASDR VNAA20260328006Fitting · corrodedWORKSHOP INTERIOR SHEET METAL: CORROSION FLOOR FITTING IN FRONT ACCESS 107 (1EA) ON GALLEY 1. FLOOR FITTING IN FRONT ACCESS 107 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-44SDR REXA2026032700269Web · crackedCRACKED FLOOR WEB RIGHT SIDE AT_ ELECTRICAL BAY (BELOW ADG SUPPORT DOUBLER) FS193.00 CRACKED DOUBLER AT FLOOR WEB RIGHT SIDE AT_ ELECTRICAL BAY (BELOW ADG SUPPORT DOUBLER) FS193.00 WAS REPLACED PER CRJ-900 SRM 53-11-43-201-001-A01, SRM 51-42-06-001-001-A01 SDR REXA2026032700268Web · crackedCRACKED FLOOR WEB LEFT SIDE AT_ ELECTRICAL BAY (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) FS193.00. FLOOR WEB LEFT SIDE AT_ ELECTRICAL BAY (BELOW BRAKE ACCUMULATOR INDICATION SUPPORT DOUBLER) FS193.00 WAS REPAIRED PER CRJ 900 SRM 53-11-43-201-001-A0SDR REXA2026032700267Skin · crackedTORN UPPER AND LOWER AFT SEAL AT RT UPPER AND LOWER THRUST REVERSE ALSO CRACK AFT SEAL PLATE AT RT LOWER THRUST REVERSE. CRACK AFT SEAL PLATE AT RT LOWER THRUST REVERSE WAS REPAIRED PER EA CRJ954-21516 REV IR AND UPPER AND LOWER AFT SEAL AT RT UPPER AND LOWERSDR REXA2026032700263Support · crackedCRACK AT CORNERS OF SUPPORT AT THE JB 6 MODULE AT FWD EQUIPMENT COMPARTMENT SUPPORT AT THE JB 6 MODULE AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01SDR REXA2026032700261Fitting · corrodedCORROSION ON FITTING (10 EACH) BTW FS280/FS379 AND LBL42/RBL42 AT FLOOR STRUCTURE. CORROSION ON FITTING (10 EAÏ¿½S) BTW FS280/FS379 AND LBL42/RBL42 AT FLOOR STRUCTURE WAS CLEANED, REMOVED, EVALUATED WHITIN LIMITS, EVALUATED DUE TO EXCESSIVE DAMAGE AND REPLACSDR REXA2026032700253Fairing · crackedCRACKED THRUST-REVERSER AFT UPPER HINGE LINE FAIRING 443BT ALSO BEND AND WEAR AFT LOWER HINGE LINE FAIRING 443BB AT RH ENGINE. THRUST-REVERSER AFT UPPER HINGE LINE FAIRING 443BT WAS REPLACED PER CRJ900 AMM 54-12-01 AND AFT LOWER HINGE LINE FAIRING 443BB AT RHSDR VNAA20260326009Seat Track · corrodedCORROSION ON RH SIDE SEAT RAIL; (4 SECTIONS) FROM FS349 TO FS661 AND (1 SECTION) FROM FS677 TO FS724 AT PAX CABIN. DUE TO EXCESSIVE DAMAGE ON RH SIDE SEAT RAIL; (4 SECTIONS) FROM FS349 TO FS661 AND (1 SECTION) FROM FS677 TO FS724 AT PAX CABIN WERE REPLACED PESDR VNAA20260326008Seat Track · corrodedCORROSION ON RH SEAT RAIL RBL9 (4 SECTIONS) FROM FS485 TO FS953. CORROSION ON RH SEAT RAIL RBL9 FROM FS485 TO FS581 (1EA) AT PASSENGER CABIN FLOOR STRUCTURE WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PER CRJ-700 SRM 53-21-SDR VNAA20260326007Seat Track · corrodedCORROSION ON LH SEAT RAIL LBL9 (4 SECTIONS) FROM FS485 TO FS953. CORROSION ON LH SEAT RAIL LBL9 FROM FS485 TO FS581 (1EA) AT PASSENGER CABIN FLOOR STRUCTURE WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PER CRJ-700 SRM 53-21-SDR VNAA20260326006Seat Track · corrodedCORROSION ON LH SEAT RAIL LBL26 (1 SECTION) FROM FS364 TO FS485 AT PAX CABIN. DUE TO NOT ALLOWED DAMAGE ON SEAT RAIL LBL26 (1 SECTION) FROM FS364 TO FS485 AT PAX CABIN WAS REPLACED PER CRJ-700 SRM 53-21-49-101-001-A01 AND PER CRJ-700 AMM 53-00-49-400-801SDR SWAA2026031668956Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA. REPLACED SUPPORT ANGLE LOCATED BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA; IAW SRM 51-40-02 AND DWG 141A8310, SHEET 33, REV-.SDR SWAA2026031668954Frame · crackedCRACKED FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA. REPAIRED THE FRAME IAW EA M-22-153-01244.SDR VNAA202603140005Seat Track · corrodedCORROSION ON SIDE SEAT RAIL FROM FS 379 TO FS 669 AND STGR 15LH AND STGR 15 RH . CORROSION ON SIDE SEAT RAIL FROM FS 379 TO FS 669 AND STGR 15LH (3EAS) AND STGR 15 RH (4EAS) WAS EVALUATED OUT OF LIMITS PER CRJ900 SRM 53-21-49-101-001-A01. REPLACED PER CRJ-90SDR VNAA202603140004Seat Track · corrodedCORROSION ON SIDE SEAT TRACK FROM FS699 TO FS977 STGR 15LT AND STGR 15RT. THE SEAT TRACK EVALUATED OUT OF LIMITS IAW SRM 53-41-49-101-001-A02, SRM 53-51-49-101-001-A02, AND SRM 53-31-49-101-001-A02. REPLACED IAW AMM 53-00-49 CONFIG.A12.SDR VNAA202603140003Seat Track · corrodedCORROSION ON LH SEAT TRACK (3 EAS) BTW FS 364.0 TO FS 693.0, LBL 27 AT PASSENGER CABIN. THE LH SEAT TRACKS EVALUATED OUT OF LIMITS IAW SRM 53-21-49-101-001-A01, AND SRM 53-31-49-101-001-A02. REPLACED IAW AMM 53-00-49, CONFIG.A12.SDR VNAA202603140002Seat Track · corrodedCORROSION ON LT SEAT TRACKS BTW FS 364.0 TO FS 683.0 LBL 9 AT PASSENGER CABIN. LT SEAT TRACKS EVALUATED OUT OF LIMITS IAW SRM 53-21-49-101-001-A01, AND SRM 53-31-49-101-001-A02. REPLACED IAW AMM 53-00-49, CONFIG.A12.SDR VNAA202603140001Seat Track · corrodedCORROSION ON RT SEAT TRACKS BTW FS 349.0 TO FS 683.0, RBL 9 AT PASSENGER CABIN. THE SEAT TRACKS EVALUATED OUT OF LIMITS IAW SRM 53-31-49-101-001-A02 AND WERE REPLACED IAW AMM 53-00-49, CONFIG.A12.SDR SWAA2026031369060Access Panel · crackedCRACKED ACCESS PANEL 644BB INNER SURFACE. REPAIRED THE ACCESS PANEL 644BB IAW 26-157-00475-WIP1.SDR SWAA2026031368848Scuff Plate · crackedCRACKED SCUFF PLATE, FWD SERVICE DOOR. REPAIRED THE SCUFF PLATE IAW SRM 53-10-15-2R-2, REPAIR 2.SDR SWAA2026031368955Tie Clip · crackedCRACKED TIE CLIP, BS 277, STR 10R. REPLACED THE TIE CLIP AND FASTENERS IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, DRAWING 141A1110, SHEET 55, REV-, & DWG 141A8380, SHEET 21, REV-.SDR SWAA2026031369046Support Angle · crackedCRACK ON SUPPORT ANGLE, BS 380 - 400, LBL 13, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9, & DWG 143A5400, SHEET 184, REV-.