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 AALA202609237381Girt Bar · wornAIRCRAFT IN BASE MAINTENANCE: R1 DOOR SLIDE WEAR PAD FRAYED AT EDGE REPAIRED R1 DOOR SLIDE GIRT IAW AARD 25-66-00.Sep 16, 2026 · N810NN · Boeing 737823 · Emergency EquipmentSDR CALA2026092219681Speed Brake · faultedSPEED BRAKES DO NOT ARM LIGHT INTERMITTENT. CREW C/W DDP PULLED AND COLLARD FLIGHT CONTROL AUTO SPEED BRAKE CB. DEFERRED, CREW REJECTED TAKE OFF DUE TO AUTO SPEED BRAKE LESS THEN 10 KTS, DM, SEE FIM 27-62 TSK 802 FOR T/S ASSIST & FAULT ISOLATION. ADDED S/Sep 16, 2026 · N63820 · Boeing 737924ER · Drag Control SystemSDR DALA2026092205308Door Frame · corrodedDURING H CHECK IN MSP, MAINTENANCE WAS ACCOMPLISHING EO WORKCARD 5331-01297-02C (SB BD500-530010 ISSUE 004). DURING MODIFICATION, THE AFT CARGO DOOR SURROUND STRUCTURE C01343028- 103 LOWER SILL WAS FOUND WITH CORROSION. THE CORROSION FOUND IS ON THE OUTER SURFSep 16, 2026 · N301DU · Airbus BD5001A11 · Fuselage Main, StructureSDR DALA2026092205307Door Frame · corrodedAFT SERVICE DOOR SURROUND - FR76 DOOR FRAME HAS SEVERAL HOLES WITH CORROSION. -M- REFERENCE SSI: 53-61-24-03. NO PRESENCE OF BLUE PAINT FROM PREVIOUS REPAIR. ACCOMPLISHED TASKS FOR ER/A 636471-14 PRI REV. 0, ER/A 636471-14 PRI REV. 1, ER/A636471-14 PRI REV. 2Sep 16, 2026 · N301DU · Airbus BD5001A11 · Fuselage Main, StructureSDR DALA2026092205306Door Frame · corrodedAFT SERVICE DOOR SURROUND - FR74 DOOR FRAME HAS SEVERAL HOLES WITH CORROSION. -M- REFERENCE SSI: 53-61-24-03. NO PRESENCE OF BLUE PAINT FROM PREVIOUS REPAIR. ACCOMPLISHED TASKS FOR ER/A 636471-14 PRI REV. 0, ER/A 636471-14 PRI REV. 1, ER/A 636471-14 PRI REV. Sep 16, 2026 · N301DU · Airbus BD5001A11 · Fuselage Main, StructureSDR DALA2026092205305Skin · corrodedEVIDENCE OF CORROSION FOUND AT AFT WTB FUSELAGE SKIN, AIRCRAFT CENTERLINE. (M)(P) REF CORROSION SSI: 53-50-02-05. COMPLIED WITH ER/A 636443-14 PRI REV 0, ER/A 636443-14 PRI REV 1, ER/A 636443-14 PRI REV 2, AND FINAL ER/A 636443-14 REV ORIGINAL SECTION I. NOMSep 16, 2026 · N301DU · Airbus BD5001A11 · Fuselage Main, Plate/SkinSDR DALA2026092205304Stringer · damagedWHILE REMOVING DAMAGED SKIN IAW PRI 636395-14, STR 36L BETWEEN FR 34-35 DAMAGED BY CUTOFF WHEEL. COMPLIED WITH ER/A 636395-14 REV 0 PRI REV 0, REV 1, REV 2, REV 3, REV 4, AND FINAL ER/A 636395-14 REV ORIGINAL SECTION I. (LP# 1815437; AIRCRAFT WAS GROUNDED)Sep 16, 2026 · N301DU · Airbus BD5001A11 · Fuselage Main, Longeron/StringerSDR DALA2026092205303Skin · corrodedCORROSION FOUND ON BOTTOM SKIN AT FWD EDGE OF WTBF, BETWEEN STR36L. COMPLIED WITH ER/A 636395-14 REV 0 PRI REV 0, REV 1, REV 2, REV 3, REV 4, AND FINAL ER/A 636395-14 REV ORIGINAL SECTION I. (LP# 1815433; AIRCRAFT WAS GROUNDED)Sep 16, 2026 · N301DU · Airbus BD5001A11 · Fuselage Main, Plate/SkinSDR IPXA2026092267592Fairing · debondedDEBONDED SKIN , RT AFT WING TO BODY FAIRING LATCH PANEL 198 CR. 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. BOND THE FOIL WITH RESIN CURED AT 200°F FOR 220 MINUTES Sep 16, 2026 · N355UP · Boeing 76734AF · Aerodynamic FairingsSDR CALA2026092219640Battery Pack · no testEMERGENCY LIGHT BATTERY PACK M1670 FAILED AN OPS CHECK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT M1670 IAW AMM 33-51-06-960-805. OPS CHKD GOOD.Sep 16, 2026 · N73299 · Boeing 737824 · Emergency LightingSDR DALA2026092205279Switch · unsecureSLIDE INDICATOR LIGHT INOP OR DAMAGED. RESECURED SWITCH AND TESTED PER B767-400 AMM 52-73-00. OPS GOOD. (1816663)(AIRCRAFT GROUNDED)Sep 16, 2026 · N839MH · Boeing 767432ER · Door Warning SystemSDR SWAA2026092146823Fastener · missingLEFT ELEVATOR OTBD BALANCE WEIGHT INNER MOST TRIM WEIGHT MISSING INBD ATTACH HARDWARE. INSTALLED FASTENER IAW SRM 51-61-04, AND SRM 51-40-02-0G-0-B00387.Sep 16, 2026 · N8670A · Boeing 7378H4 · Elevator Miscellaneous StructureSDR SWAA2026092111953Bulb · inoperativeAFT ENTRY EXTERNAL SLIDE/OVERWING EMERGENCY LIGHT INOP. REPLACED THE BULB IAW AMM 33-51-04. OPS CHKD GOOD.Sep 16, 2026 · N279WN · Boeing 7377H4 · Emergency LightingSDR SWAA2026092161145Battery Pack · no testRT EMERGENCY PACK M1669 FAILED CAPACITY CHECK. R&R CABIN EMERGENCY BATTERY PACK PER AMM 33-51-06Sep 16, 2026 · N7820L · Boeing 73779P · Emergency LightingSDR SWAA2026092180897Power Supply · inoperativeR1 DOOR SLIDE EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FORWARD GALLEY EMERGENCY LIGHT POWER SUPPLY PER AMM 33-51-06.Sep 16, 2026 · N7847A · Boeing 737752 · Emergency LightingSDR SWAA2026092126472Battery Pack · no testAFT RT EMERGENCY BATTERY PACK M1672 FAILED CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06Sep 16, 2026 · N7820L · Boeing 73779P · Emergency LightingSDR SWAA2026092107806Fitting · looseFED AFT GIRT BAR FITTING LOOSE. TIGHTENED LOOSE SCREWS COMMON TO FED AFT GIRT BAR FITTING IAW AMM 25-66-02-400-801.Sep 16, 2026 · N8535S · Boeing 7378H4 · Emergency EquipmentSDR SWAA2026092171894Rub Strip · missingAFT SERVICE DOOR EMERGENCY SLIDE COVER RUB STRIP END CAP MISSING INSTALLED AFT SERVICE DOOR EMERGENCY SLIDE COVER RUB STRIP END CAP IN REF WITH AMM 25-66-01.Sep 16, 2026 · N491WN · Boeing 7377H4 · Emergency EquipmentSDR KY7A20260916001Shutoff Valve · faultedLANDING GEAR DID NOT EXTEND NORMALLY. EMERGENCY GEAR EXTENSION WAS NECESSARY. INSTALLED RT HYDRAULIC SHUTOFF VALVE. IAW MM 29-10-30. PERFORMED OPS CHECK, OPS CHECK GOOD AND NO DEFECTS NOTED.Sep 16, 2026 · N889DC · Frchld SA227DC · Hydraulic System, MainSDR IPXA2026092166138Skin · puncturedSKIN, RT MLG W/W DOOR MID PUNCTURED. PERFORMED NDT/UT FOR THE REWORKED AREA AND PLUS 6 INCHES AROUND HEATED AREA, IAW NDT MANUAL PART 1, 51-01-01, REV 144. REMOVE THE DELAMINATION MATERIALS AND CLEAN. BOND THE REPAIR PLIES WITH RESIN CURED AT 200°F FOR 220 Sep 16, 2026 · N355UP · Boeing 76734AF · Landing Gear DoorsSDR IPXA2026092172110Bracket · crackedCRACKED BRACKET, LT WING INBD SLAT TORQUE TUBE SUPPORT AT INBD L/E CAVITY AT ISS 285.233. REMOVED DAMAGE BRACKET I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW BRACKET I.A.W SRM 51-40-02-0G REV. 96 AND BOEING DWG NO. 114T1240 SH. 6 REV. -.Sep 16, 2026 · N355UP · Boeing 76734AF · Wing, Attach FittingsSDR IPXA2026092172477Angle · crackedCRACKED ANGLE, NR 1 PYLON AFT BULKHEAD REAR LT ANGLE. REMOVED DAMAGE ANGLE I.A.W SRM 51-40-02-0G REV. 96. INSTALLED NEW ANGLE I.A.W SRM 51-40-02-0G REV. 96 AND DWG 313T2303 SH. 141 REV. A AND BOEING DWG NO. 313T2303 SH. 146 REV. -.Sep 16, 2026 · N355UP · Boeing 76734AF · Nacelle/Pylon Miscellaneous StructureSDR CALA2026092119586Access Panel · crackedRIGHT WING LOWER ACCESS PANEL 643BB HAS CRACK INDICATION IN HOLE NR 2 AT 5 O'CLOCK. INSTALLED FREEZE PLUG COMMON TO HOLE NR 2 AT RT WING LWR ACCESS PANEL 6 43BB, SKIN LOCATION IAW EA 757-5720-13-A4608, STEP 14. FABRICATION ACCOMPLISHED VIA T26/1876293 WC 61Sep 16, 2026 · N18112 · Boeing 757224 · Wing, Plate/SkinSDR CALA2026092119584Access Panel · crackedRIGHT WING LOWER ACCESS PANEL 643BB HAS CRACK INDICATION IN HOLE NR 5 AT 7 O'CLOCK. INSTALLED FREEZE PLUG HOLE NR 5 IAW EA 757-5720-13-A4608, REV-, STEP 14. VIA T26/1876292. FABRICATION ACCOMPLISHED T26/1876292 ON WC 6100815272/18159. COMPLIED WITH ECRA 5720Sep 16, 2026 · N18112 · Boeing 757224 · Wing, Plate/SkinSDR CALA2026092119582Access Panel · crackedRIGHT WING LOWER ACCESS PANEL 643BB HAS MULTIPLE CRACK INDICATIONS IN HOLE NR 19 AT 2 TO 3 O'CLOCK. INSTALLED FREEZE PLUG IN HOLE NR 19 IAW EA 757-5720-13-A4608 REV -, STEP 14. FABRICATION ACCOMPLISHED VIA T26/1876293 ON WC 6100815 272/18159. COMPLIED WITH ECSep 16, 2026 · N18112 · Boeing 757224 · Wing, Plate/SkinSDR CALA2026092119580Access Panel · crackedRIGHT WING LOWER ACCESS PANEL 643BB HAS CRACK INDICATION IN HOLE NR 27 AT 1 O'CLOCK. INSTALLED FREEZE PLUG AT HOLE NR 27 IAW EA 757-5720-13-A4608 REV - STEP 14, FABRICATION ACCOMPLISHED VIA T26/1876293 /6100815272/18 159. COMPLIED WITH ECRA 5720-03683.Sep 16, 2026 · N18112 · Boeing 757224 · Wing, Plate/SkinSDR CALA2026092119578Battery Pack · no testEMERGENCY LIGHT BATTERY PACK M1671 FAILS OPERATIONAL CHECK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT M1671 IAW AMM 33-51-06-960-805 OPS CHECK GOOD.Sep 16, 2026 · N73299 · Boeing 737824 · Emergency LightingSDR CALA2026092119576Access Panel · crackedLEFT WING LOWER ACCESS PANEL 543BB HAS CRACK INDICATION IN HOLE NR 27 AT 11 O'CLOCK. INSTALLED FREEZE PLUG AT HOLE 27 IAW EA 757-5720-13-A4607 STEP 14 VIA T26/1876291 PER WC 6100815268/18155. COMPLIED WITH ECRA 5720-03682.Sep 16, 2026 · N18112 · Boeing 757224 · Wing, Plate/SkinSDR CALA2026092119574Access Panel · crackedLEFT WING LOWER ACCESS PANEL 543BB HAS 2EA CRACK INDICATIONS IN HOLE NR 28 AT 12 AND 2 O'CLOCK. INSTALLED FREEZE PLUG IN HOLE NR 28 IAW EA 757-5720-13-A4607 REV- STEP 14. FABRICATION ACCOMPLISHED VIA WC 6100815268 / 18155 & T26/ 187691. COMPLIED WITH ECRA UASep 16, 2026 · N18112 · Boeing 757224 · Wing, Plate/SkinSDR CALA2026092119572Access Panel · crackedLEFT WING LOWER ACCESS PANEL 543BB HAS CRACK INDICATION IN HOLE NR 22 AT 12 O'CLOCK. INSTALLED FREEZE PLUG IN HOLE NR 22 IAW EA 757-5720-13-A4607, REV-, STEP 14. FABRICATION ACOMPLISHED VIA T26/1876291 WC 6100815268/18 155. COMPLIED WITH UAL ECRA 5720-0368Sep 16, 2026 · N18112 · Boeing 757224 · Wing, Plate/SkinSDR CALA2026092119570Battery Pack · faultedEMERGENCY LIGHT BATTERY PACK M1676 FAILED AN OPS CHECK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT M1676 IAW AMM 33-51-06-960-805 OPS CHECK GOOD.Sep 16, 2026 · N73299 · Boeing 737824 · Emergency LightingSDR DXTA2026092109742Relief Valve · defectiveDURING CRUISE RECEIVED AN EMER BRK LOW PRESSURE CAS. PRESSURE WAS APPROXIMATLEY 150PSI AND CONTINUED TO DROP. SOMETIME BETWEEN TOUCHDOWN AND ENGINE SHUTDOWN PRESSURE CAME BACK UP TO 2900 THEN DROPPED TO 2400PSI WITHIN 10 MINUTES. TWO MORNINGS IN A ROW AIRCRAFTSep 16, 2026 · N328QS · Emb EMB505 · Landing Gear Brake SystemSDR DXTA2026092109748Brake Sys · malfunctionedDURING TAXI IN RIGHT BRAKE HAD UNCOMMANDED ACTIVATION. WHEN RIGHT BRAKE PEDAL PRESSED THE THE BRAKES FELT LIKE THEY WERE SLIPPING CAUSING THE ENTIRE PLANE TO SHAKE. LEFT BRAKE PEDAL SIMILAR CONDITION BUT LESS PRONOUNCED. PERFORMED BRAKE CHECK. NO FAULTS FOUNDSep 16, 2026 · N444QS · Emb EMB505 · Landing Gear Brake SystemSDR DALA2026091805229Floor Support · corrodedCORROSION ON FLOOR STGRS STA 1330 LBL 10.45 AFT CARGO COMP. REPAIRED PER SRM. 53-00-53 (1816659)(AIRCRAFT GROUNDED)Sep 16, 2026 · N595NW · Boeing 757351 · Fuselage Miscellaneous StructureSDR DALA2026091805228Bearing · migratedMIGRATED BEARING ON INB TRACK OF INBOARD MAIN FLAP AT LH WING. REPAIRED PER PRI 636580-14 (1815568)(AIRCRAFT GROUNDED)Sep 16, 2026 · N595NW · Boeing 757351 · Trailing Edge FlapsSDR UATA2650916265301Skin · damagedFS 27 LOWER BEAM & LOWER SKINS DAMAGED. REMOVED F27 LOWER BEAM. PREVIOUSLY REPAIRED RT LOWER SKIN SECTION, LT & RT FS27 TO C CHANNEL BRACKETS/CVR BOX MOUNTING STRUCTURE. CUT MIDDLE/LH LOWER SKINS JUST AHEAD OF F28 FLANGE REMOVING FWD ~13" OF BOTH SKINS. FAB'D Sep 16, 2026 · N1331C · Casa C212CC · Fuselage Main, Plate/SkinSDR N6WA2026091816Frame · corrodedCORROSION BS 250 BETWEEN STRG 25L - 25R. REMOVED AND REPLACED FRAME AT BS 250 BETWEEN STRG 25L & 25R IAW SRM 51-42-06.Sep 16, 2026 · N528GJ · Cndair CL6002C11 · Fuselage Main, FrameSDR N6WA2026091815Stringer · corrodedCORROSION ON STRINGER 27 BTWN BS 250 - 265. REMOVED AND REPLACED STR 27 BTWN BS 250 - 265 IAW SRM 51-42-06.Sep 16, 2026 · N528GJ · Cndair CL6002C11 · Fuselage Main, Longeron/StringerSDR N6WA2026091814Stringer · corrodedCORROSION STRINGER 26L BETWEEN BS 250 - 280. REMOVED AND REPLACED THE STRINGER 26L BTWN BS 250 - 280 IAW SRM 51-42-06.Sep 16, 2026 · N528GJ · Cndair CL6002C11 · Fuselage Main, Longeron/StringerSDR N6WA2026091813Stringer · corrodedCORROSION STRINGER 26R BTWN BS 250 - 280. STARTED INSTALLING STR 26R BTWN BS 250 - 280 IAW SRM 51-42-06.Sep 16, 2026 · N528GJ · Cndair CL6002C11 · Fuselage Main, Longeron/StringerSDR N6WA2026091812Seat Track · corrodedSEAT TRACK RBL9 BETWEEN FS 830-FS969 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK RBL9 BETWEEN FS 830-FS969 IAW SRM CRJ 53-41-49.Sep 16, 2026 · N581GJ · Cndair CL6002C11 · Fuselage, Seat/Cargo Attach FittingsSDR N6WA2026091811Seat Track · corrodedSEAT TRACK AT LBL 9 BETWEEN BS 830 - 897 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK AT LBL 9 BETWEEN FS 830 - 897 IAW SRM 53-41-49.Sep 16, 2026 · N581GJ · Cndair CL6002C11 · Fuselage, Seat/Cargo Attach FittingsSDR N6WA2026091810Seat Track · corrodedSEAT TRACK RBL 9 BETWEEN FS 690 - 830 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK RAIL RBL 9 BETWEEN FS 690 - 830 IAW SRM 53-41-49.Sep 16, 2026 · N581GJ · Cndair CL6002C11 · Fuselage, Seat/Cargo Attach FittingsSDR N6WA2026091809Seat Track · corrodedSEAT TRACK LBL 9 BETWEEN FS 690 - 830 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK LBL 9 BETWEEN FS 690 - 830 IAW CRJ SRM 53-41-49.Sep 16, 2026 · N581GJ · Cndair CL6002C11 · Fuselage, Seat/Cargo Attach FittingsSDR N6WA2026091808Angle · crackedANGLE CRACKED AT BS 349 - 364 ON INTERCOSTAL BETWEEN CROSSBEAM. NEW CLIP INSTALL ON INTERCOSTAL AND CROSSBEAM IAW SRM 51-40-11 AND SRM 51-42-13.Sep 16, 2026 · N581GJ · Cndair CL6002C11 · Fuselage Miscellaneous StructureSDR N6WA2026091807Proximity Sensor · out of adjustLEFT OVERWING EMERGENCY EXIT DOOR SHOWS WRONG INDICATION WHILE OPEN. PERFORMED ADJUSTMENT OF THE LT OVERWING EMERG EXIT DOOR PROXIMITY SENSOR IAW AMM 52-70-10. OPS CHECK GOOD IAW AMM 52-21-00.Sep 16, 2026 · N536GJ · Cndair CL6002C11 · Door Warning SystemSDR N6WA2026091806Cable · frayedPAX DOOR COUNTER-BALANCE CABLES FRAYED FWD NR 1 CABLE, & AFT NR 4 CABLE. OPS CHECK AND SAFETY OF PAX DOOR COUNTER BALANCE GOOD IAW AMM 52-11-17. NO ADJUSTMENTS REQUIRED.Sep 16, 2026 · N536GJ · Cndair CL6002C11 · Passenger/Crew DoorsSDR N6WA2026091805Cover · corrodedEVALUATE POSSIBLE CRACKS ON PAX DOOR FWD & AFT UPPER COVER CORNERS. REMOVED AND REPLACED PAX DOOR FWD AND AFT UPPER COVERS IAW SRM 51-42-06.Sep 16, 2026 · N536GJ · Cndair CL6002C11 · Passenger/Crew DoorsSDR N6WA2026091804Seat Track · corrodedLEFT SEAT TRACK INBD AT FS 364 - FS 485 HAS CORROSION. REPLACED LT SEAT TRACK INBD AT FS 364 - FS 485 IAW SRM 53-00-59.Sep 16, 2026 · N526GJ · Cndair CL6002C11 · Fuselage, Seat/Cargo Attach FittingsSDR N6WA2026091803Support Frame · corrodedFRAME SUPPORT STRUCTURE RT AFT FAIRING AT FS 939 IS OUT OF LIMITS. REMOVED AND REPLACED RT FRAME SUPPORT STRUCTURE AFT FAIRING AT FS 939 IAW SRM 51-26-00.Sep 16, 2026 · N526GJ · Cndair CL6002C11 · Aerodynamic Fairings