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 FDEA202603200359Skin · dentedRIGHT WING OTBD FLAP LOWER SURFACE FROM OB TO IB 272 INCHES CROSS TE TO LE 12 INCHES FOUND ONE DENT. REPAIRED RH WING OB FLAP LOWER SURFACE DENT AT OTEF STA 250 IAW SRM 57-53-01- 2R-2 FIGURE 201-204 AND SRM 51-70-04-2R-1 PARA 4G FIGURE 210 REV 51.0 AND ESDR KCSA202603201010Slat · damagedNR 8 SLAT, CENTER, LOWER LEADING EDGE, DAMAGED.SDR YENA2026031600314Coupler · failedFLT # 31 BOS -AMS (ETOPS). HF 1 RADIO RECEPTION AND TRANSMISSION VERY WEAK, BARELY USABLE, HIGH FREQUENCY (HF) COMMUNICATION SYSTEM (D-LRCS) HF 1 ). REMOVED AND REPLACED HF1 COUPLER I AW AMM 23-11-36. OPS CHECK GOOD.SDR F3LA202603200386Power Supply · failedREFERENCE LP702387 #2 EPSU BATTERY (10WL) FWD L FAILED TEST FAILED EPSU SYS TEST. AC WAS NOT GROUNDED AS A RESULT OF THIS SDR REPORTABLE EVENT, IT WAS A RON SCHEDULED HEAVY CHECK. REMOVED AND REPLACED EPSU BATTERY (10WL) IAW AMM 33-51-38-000/400-002-A. OPS CHSDR F3LA202603200385Power Supply · failedREFERENCE LP702387 #3 EPSU BATTERY (11WL) EMERG L FAILED TEST FAILED EPSU SYS TEST. AC WAS NOT GROUNDED AS A RESULT OF THIS SDR REPORTABLE EVENT, IT WAS A RON SCHEDULED HEAVY CHECK.
REMOVED AND REPLACED EPSU BATTERY (11WL) IAW AMM 33-51-38-000/400-002-A. OPSSDR F3LA202603200384Power Supply · failedREFERENCE LP702388 #1 EPSU BATTERY (13WL) AFT L FAILED TEST FAILED EPSU SYS TEST. AC WAS NOT GROUNDED AS A RESULT OF THIS SDR REPORTABLE EVENT, IT WAS A RON SCHEDULED HEAVY CHECK. REMOVED AND REPLACED EPSU BATTERY (13WL) IAW AMM 33-51-38-000/400-002-A. OPS CSDR 2026FA0000202Skin · corrodedLOWER TAILCONE SKIN CORROSION. COMPLIED WITH NETJETS AQRD ERO-988732 REV.IR, DATED MAR.19,2026. N611QS LOWER TAILCONE SKIN CORROSION.SDR 2026FA0000201Impulse Coupling · defectiveMAGNETO PULLED DURING ROUTINE MAINTENANCE TO CHECK FOR THE PRESENCE OF A CHAMPION MANUFACTURED IMPULSE COUPLING. ONE WAS FOUND INSTALLED AND THUS REMOVED FOR REPLACEMENT WITH A NEW ES3163 IMPULSE COUPLING. AFTER REMOVAL OF THE OLD IMPULSE COUPLING, I DISASSEMSDR SWIA2026062676323Skin · corrodedLBL 45 LT WING LOWER PLANK TRAILING EDGE AREA, CORRODED & CHAFED FROM THE WING TO BODY FAIRING. REPAIRED LBL 45 LT WING LOWER PLANK TRAILING EDGE AREA IAW GREO 601R-57-21-880, REV-D. NOTES/STEPS 1, 2, 3,5,6,7,9 AND10.,COMPLIED WITH 51-900-1003-SKY, FUEL LEAK CSDR SWIA2026062676315Skin · damagedTWO SCREW HOLES ELONGATED ON LT SIDE EXTERNAL SKIN BETWEEN BS 409+80 - 409+96, STR 18L- STR 20L. RECEIVED AND COMPLIED WITH REO 601R-53-31-1369 REV.--, COMPLIED WITH 51-900-1003-SKY, LEAK CHECK GOOD.SDR 2026FA0000442Stringer · bentAIRCRAFT FAILED THE INSPECTION CRITERIA OUTLINED IN TEXTRON SERVICE LETTER SEL-53-04, DATED JANUARY 14, 2026. BOTH UPPER STRINGERS IN THE TAILCONE ASSEMBLY (P/N'S 0512001-9 AND 0512001-10) HAVE BENDS IN EXCESS OF THE 0.040" LIMIT DESCRIBED IN THE SERVICE LETTESDR REXA2026050700537Fitting · corrodedCORROSION ON ATTACHMENT FITTING OF GALLEY 1 WAS FOUND. FITTING OF GALLEY 1 WAS REPLACED PER CRJ/900 SRM 51-42-21-001-001-A01SDR REXA2026050700503Channel · damagedELONGATED HOLE ON UP CHANNEL AT LH MLG WHEEL WELL UP CHANNEL AT LH MLG WHEEL WELL WAS REPLACED PER CRJ 900 SRM 51-41-21-001-001-A01SDR SWAA2026050481577Stub Frame · crackedCRACK INDICATION ON STUB FRAME LOCATED BETWEEN BS 294.5 TO BS 296.5 AND BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 0.250 IN. REPLACED STUB FRAME LOCATED BS 294.5 AND BTW STR-6R TO STR-10R AT FWD GALLEY DOOR AREA IAW SRM 51-10-02-0G-0, ITEM 9, SRM 5SDR VNAA20260501001Bearing · excess playFREE PLAY IN THE BEARINGS (2EA) OF THE CENTRAL HINGES OF THE RUDDER. FITTING #2 WAS REPLACED PER RIL #2103 REV.B AND BEARING ON FITTING #3 WAS REPLACED PER RIL #1213 REV. A.SDR R3WA20260429001Pulley Bracket · chafedDURING SCHEDULED MAINTENANCE, A DETAILED VISUAL INSPECTION OF THE RUDDER CONTROL SYSTEM DISCOVERED A RUDDER CONTROL CABLE RUBBING AGAINST A PULLEY BRACKET WHICH WAS ALSO PART OF THE RUDDER CONTROL SYSTEM. CABLE WEAR WAS MINIMAL AND WITHIN SERVICEABLE LIMITS SPSDR SWAA2026042881418Support Angle · crackedCRACKED SUPPORT ANGLE, FWD FACE BS 695 BL 0 RT SIDE AT PASSENGER CABIN. REPLACED SUPPORT ANGLE LOCATED FWD FACE BS 695 BL 0 RT SIDE AT PASSENGER CABIN IAW SRM 51-40-02 AND DWG 273A9110 SHEET 6 REV- DWG 111A6001 SHEET 10 REV-.SDR SWAA2026042881596Access Panel · crackedCRACK SEAL - PLATE ACCESS PANEL 333AB AT LT HORIZONTAL STABILIZER. REPLACED SEAL - PLATE LOC. ON ACCESS PANEL 333AB AT LT HORIZONTAL STABILIZER IAW SRM 51-40-02-0G-0 AND MEASURES OF CRACK ARE: L:0.6250.SDR SWAA2026042881597Access Panel · crackedCRACK SEAL - PLATE ACCESS PANEL 333AT AT LT HORIZONTAL STABILIZER. REPLACED SEAL - PLATE ON ACCESS PANEL 333AT AT LT HORIZONTAL STABILIZER IAW SRM SRM-51-10-02 ITEM 9 AND SRM-51-40-02-0G-0.SDR SWAA2026042781421Cover · missingMISSING LAVATORY A EMERGENCY ENTRANCE LIGHT COVER AT FWD GALLEY AREA. INSTALLED LAVATORY A EMERGENCY ENTRANCE LIGHT COVER AT FWD GALLEY AREA IAW AMM 33-51-01-960-802.SDR AALA202604237550Anchor Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING MAIN LANDING GEAR JACK ANCHORAGE FITTING UPPER AND LOWER SURACE BETWEEN RIB 2 AND RIB 3. REPAIRED JACK ANCHORAGE FITTING PER SRM 57-26-13-300-017 AND EA 373552.SDR SWAA2026042281163Wire · cutCUT WIRE OF EMERGENCY EXIT SIGN LOCATED ON FWD WALL OF LAVATORY B. REPLACED EMERGENCY EXIT SIGN LOCATED ON FWD WALL OF LAVATORY B IAW AMM 33-51-01-960-802. OPS TEST WILL BE DOCUMENTED TTG8Q00CWNPT STEP 65.SDR SWAA2026042281589Access Panel · damagedELONGATED HOLES ON ACCESS PANEL 661AB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661AB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-70-04-2R-10.SDR SWAA2026042281591Access Panel · elongatedELONGATED HOLES ON ACCESS PANEL 661BB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661BB IAW SRM 51-70-04-2R-10 REPAIR 10.SDR AALA202604212747Access Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING FUEL TANK ACCESS PANEL 640NB COUNTERSINK HOLE. MAINENANCE REPLACED FUEL TANK ACCESS PANEL PER TASK CARD 26C64057007.SDR ASAA2026031965493Floorbeam · corrodedAFT WET AREA FLOORBEAM 986.5 UPPER REPAIR T-CAP CORRODED RBL 0 TO RBL-45. GROUNDED - YES. REMOVED DAMAGE ON AFT WET AREA FLOORBEAM STA 986.5 REPAIR T-CAP MAX MAT LOSS 100% FOUND TO BE OUT LIMITS. REMOVED AND INSTALLED NEW REPAIR ON FLOORBEAM T-CAP STA 986.5 DBSDR ASAA2026031965486Intercostal · corrodedAFT WET AREA STA 967-987 RBL-16 INTERCOSTAL CORRODED ON UPPER FLANGE. GROUNDED - YES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1. REMOVED AND REPLACED INTERCOSTAL IAW B737-800 SRM 51-40-02-0G-0. W= 1.5" O= .075 R= 0.65 L= 3.0" SDR ASAA2026031965484Floor Support · corrodedAFT WET AREA FLOOR SUPPORT STA 986.5 TO 1016 RBL-32 CORRODED. GROUNDED - YES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED FLOOR SUPPORT AT RBL 32 STA 986.5 TO 1016 IAW B737-800 SRM 51-40-02-0F-0.SDR IPXA2026033051174Bracket · corrodedGOUGED BRACKET, LT WING T/E LOWER SURFACE WBL 289. ACCOMPLISHED GOUGE AND CORROSION DAMAGE REPAIR IAW EO-96933-REQ1, REV 1, & SRM 51-40-02-0G, REV 94, DWG 113T1944, SHT 2, REV A, & DWG 113T1551, SHT 1, REV E.SDR ASAA2026031965261Floorbeam · corrodedAFT WET FLOORBEAM BS 993, LBL 32 TO LBL 45 CORRODED. GROUNDED - YES. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-40-02-0G-0.SDR ASAA2026031965260Floor Support · corrodedFWD WET AREA FLOOR SUPPORT BS 294.5 - 312, LBL 12, CORRODED ON UPPER FLANGE AT LAV MOUNT. GROUNDED - YES. UPON FURTHER EVALUATION, 100% MATERIAL LOSS, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0.SDR ASAA2026031965259Floor Support · corrodedAFT WET AREA BS 967 - 987, LBL-16 FLOOR SUPPORT CORRODED ON UPPER FLANGE. GROUNDED - YES. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-1A-1. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0.SDR AALA202604020285Angle · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN FORWARD CARGO COMPARTMENT TRANSITION PANEL SUPPORT ANGLE AT BS 748 AND LBL 64. REPLACED ANGLE PER AARD 51-00-05-1.SDR IPXA2026032052387Repair · debondedMAJOR REPAIR, DEBONDED, PREVIOUS REPAIR, L/H WING NO.5 SLAT UPPER SURFACE LES 440. CUT OUT THE DAMAGE MATERIALS AND CLEAN, MEASURE THE CUTOUT SIZE (L:5.75", W:5.25", 38" FROM INBD EDGE AT AFT EDGE OF THE LT WING NR 5 SLAT UPPER SURFACE LES 440) IAW SRM 57-43SDR IPXA2026033158453Door · damagedTHE DESCENT DEVICE CONTAINER DOOR IS CRACKED. REPAIRED THE LID ASSY IAW EO-96902-REQ1, REV 2.SDR IPXA2026033156373Retainer · damagedFOUND NUTPLATE DAMAGED 1EA, PNL NO.611JB. FABRICATE RETAINER IAW DWG 114T1400, SH 3, REV F, PL REV BW, PSDL REV F AS A SAMPLE IAW GMM-MTX CH 9.08 REV 14.1 REQUIREMENT. INSTALL THE NUTPLATE TO RETAINER IAW SRM 51-40-02-0G, REV 94, & DWG 114T1400, SH 3, REV SDR SWAA2026033081537Panel · crackedLEFT WING INBD FIXED T/E LOWER PANEL CRACKED AROUND FASTNER LOCATION. REPAIRED IAW SRM 57-51-01-2R-1-D00001, REPAIR 1. WING FIXED TRAILING EDGE SKIN PANELS MADE OF COMPOSITE MATERIALS CATEGORY A REPAIR.SDR SWAA2026032781083Floor Panel · delaminatedMAIN CABIN ZONE 241 FLOOR PANEL 241UF DELAMINATED. FABRICATED NEW FLOOR PANEL 241UF IAW DWG 146A5810 REV- AND SRM 53-00-50-2R-0.SDR AALA202603269938Release Cable · disengagedAIRCRAFT IN BASE MAINTENANCE: L2 DOOR SLIDE RAFT COVER RELEASE CABLE DISENGAGED WHILE MAINTENANCE WAS TAKING THE SLIDE ASSEMBLY TO THE AIRCRAFT FOR INSTALLATION. MAINTENANCE REPLACED THE SLIDE RAFT ASSEMBLY WITH A SERVICEABLE UNIT PER TASK CARD 26C83252008.SDR IPXA2026032656802Pad · damagedDAMAGED PAD, NR 1 ENGING EXHAUST SLEEVE L/E MID LOAD SHARE BRACKET AT 09:00 O'CLOCK POS. REPLACED IAW AMM 20-51-01-912-008 REV50 REPLACED THE PAD.SDR IPXA2026032252574Repair · debondedDEBONDED PREVIOUS REPAIR, LT WING NR 5 SLAT UPPER SURFACE LES 500. INSTALL THE EXTERNAL DOUBLER WITH FILM ADHESIVE IAW SRM 51-70-10-2R-0 PARAGRAPH 10 & 18 REV. 94. ACCOMPLISH THE REPAIR PER SRM (REV 94) 57-43-02-2R-1 REPAIR 1, AND 51-70-10-2R-4 REPAIR 4.SDR IPXA2026032052772Plate · wornRIGHT BODY WHEEL WELL INBOARD DOOR, DOOR STRIKE PLATE WORN 2 EA. INSTALLED NEW PLATE IAW SRM 51-40-02-0G, REV 48, & DWG 149U1608, SHEET 2, REV -.SDR IPXA2026032052743Plate · wornWORN PLATE, LT BODY GEAR W/W INBD DOOR STOP PLATE. INSTALLED A NEW PLATE IAW SRM 51-40-02-0G, REV 48, AND DWG 149U1608, SHEET 2, REV -.SDR 2026FA0000225Stiffener · crackedLH WING TOP I/B FWD SKIN, AFT STIFFENER CRACKED. REPLACED WITH NEWSDR DALA2026032502003Pan · crackedREPAIR TO FUSELAGE AFT LAVATORY SERVICE PAN AT STA 1681-1701 AND S27R - 29R CRACKED. REQUIRES ACTIONS PER ERA 632865-14 REV ORIG. REF ERA 632865-14. (1502037)SDR AALA202603252254Engine · failedAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS NOT DECLARED DUE TO: DURING CLIMBOUT NUMBER 1 ENGINE VIBRATIONS FLUCTUATED WILDLY OSCILLATING BETWEEN 2.0 AND 3.5, ENGINE NUMBER 1 HAVING VIBRATIONS ISSUES RECENTLY. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDED SAFELY AT SDR AALA202603258015Receptacle · leakingAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED DUE TO: THROUGH 11000 FT WE GOT A CABIN ALTITUDE WARNING HORN, WE DESCENDED IMMEDIATELY BACK TO 10000 FT; RAN THE CHECKLIST AND COULD NOT GET THE AIRCRAFT TO PRESSURIZE. AIRCRAFT AIR INTERRUPTED BACK TO AND LANDSDR IPXA2026032556716Retainer · crackedFOUND RH INBD ELEVATOR LOWER SPAR RETAINER DAMAGE. (REPLACE) 1. REMOVED DAMAGE RETAINER I.A.W SRM 51-40-02-0G REV.48. INSTALLED A NEW RETANER IAW SRM 51-40-02-0G REV 48, & DWG 65B05701, SHEET 02, REV J.SDR G1IA20260319106Clevis · unserviceableWHILE PUTTING THE GEAR DOWN APPROACHING THE RUNWAY, WE DID NOT GET THREE GREEN. FAILED TO GET RIGHT MAIN DOWN INDICATION. GOT DELAYED VECTORS, RAN CHECKLISTS. DID MANUAL GEAR EXTENSION, GOT THREE GREEN AT THAT POINT. DECLARED EMERGENCY AND LANDED WITHOUT EVENSDR AALA202603246116Battery Pack · brokenAIRCRAFT IN BASE MAINTENANCE: OVERHEAD FLIGHT ATTENDANT REST AREA HAS A BROKEN FLASHLIGHT. REMOVED AND REPLACED FLASHLIGHT (AALA202603247389) AND BATTERY PACK (AALA202603246116). PER BOEING CMM 25-60-14.