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.
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 AALA202609050869Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HORIZONTAL STABILIZER ELEVATOR POSITION 2 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42SDR AALA202609052214Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 4 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42SDR AALA202609050268Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 1 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42SDR AALA202609055255Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 1 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42SDR AALA202609053606Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 4 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42SDR AALA202609054428Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 3 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42SDR AALA202609050132Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 6 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42SDR AALA202609053017Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND HORIZONTAL STABILIZER ELEVATOR POSITION 6 HINGE ARM END FITTING HAS EXCESSIVE PLAY -MAINTENANCE REPLACED HINGE ARM END FITTING PER AMM 55-16-42SDR IPXA2026090492079Hinge · crackedPIANO HINGE FITTING OF MDC DOOR HOLE 22F HAS INDICATIONS AT 9 O, CLOCK. ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-98430-REQ1 AND 300-5236-27-A4604, REV -. ACCOMPLISHED REPAIR IAW EA 300-5236-27-A4604, REV -.SDR SWAA2026090222369Plate · crackedFWD CARGO, FWD CORNER PLATE IS CRACKED. FWD CARGO FWD CORNER PLATE IS CRACKED. INSTALLED A NEW FWD CARGO FWD LOWER CORNER PLATE ASSY IAW AMM 53-11-02.SDR IPXA2026090191812Hinge · damagedPIANO HINGE FITTING OF MDC DOOR HOLE NR 16F HAD TWO INDICATIONS AT 6 & 4 O`CLOCK. ACCOMPLISHED THE REPAIR IAW EO-98430-REQ1, & EA 300-5236-27-A4604, REV -.SDR AALA202608314819Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER CREW DOOR CUTOUT LOWER CENTER SHAPE FITTING AT FR 67 AND S23R - MAINTENANCE REPLACED CENTER SHAPE FITTING PER SRM 51-72-11SDR AALA202608286516Gusset · crackedAIRCRAFT IN BASE MAINTENANCE: FRAME INNER CAP JOINT TO GUSSET PLATE AT FR 16 AND S16R BOTTOM HOLE CRACKED - REPLACED GUSSET PER SRM 51-42-11SDR AALA202608285499Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER CREW DOOR CUTOUT LOWER SILL CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23L - REPLACED CENTER SHAPE FITTING PER SRM 51-42-11SDR 2026FA0000674Actuator · failedAS THE PILOT AND COPILOT WERE COMING IN TO LAND, LANDING GEAR WAS LOWERED AND NOTICED THAT THE FRONT (NOSE) WHEEL LANDING GEAR INDICATION WAS RED. CREW DECIDED TO PERFROM LOW APPROACH OVER RUNWAY FOR THE TOWER TO SEE IF LANDING GEAR APPEARED TO BE DOWN. TOWER SDR AALA202608288389Elec Connector · brokenAIRCRAFT IN BASE MAINTENANCE: EMERGENCY FLOOR PATH LIGHT ON SEAT 31CBA WITH MALE CONNECTOR DAMAGED. REPAIRED WIRE SPLICE CONNECTOR AT EMERGENCY FLOOR PATH LIGHT ON SEAT 31CBA IAW B737-NG-SWPM 20-30-12 AND PERFORMED SATISFACTORY OPERATIONAL CHECK OF EMERGENCY LSDR IPXA2026082792079Hinge · crackedPIANO HINGE FITTING OF MDC DOOR, HOLE 22F HAS INDICATIONS AT 9 O,CLOCK. STEP 18 OF PRELIMINARY 1, E.A 300-5236-27-A4604, COMPLETED.SDR ASAA2026081468108Skin · crackedRIGHT HORIZONTAL STABILIZER LOWER SKIN HAS CRACK INDICATION INBOARD OF STAB STA 92.70 AS MARKED. GROUNDED - YES. ACCOMPLISHED REPAIR ON R/H HORIZONTAL STAB INCORPORATED NEW DOUBLER WITH EXISTING DOUBLER FROM STA 92.70 TO STA 102.70 IAW B737-NG SRM 55-10-01-2R-SDR 2026F00185Starter · faultedELEC ENGINE STARTER R1 STATUS MSG, WAS CARRY OUT PROCEDURE VFSG WAS REPLACED IAW AMM DMC-V787-A-24-21-09-00B-520A-A/720A-ASDR AALA202608254520Transition Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO, LEFT TRANSITION PANEL HAS GALVANIC CORROSION AT STATION 500H + 6", LBL 24. MAINTENANCE REPLACED LEFT HAND TRANSITION PANEL BAC1496-444 PER SRM 53-00-53-2R-5 AND AARD 51-00-05-1SDR JJBA20260825019Panel · corrodedCORROSION WAS FOUND IN THE WASTE SERVIE PANEL RIGESTER AND ON THE AFT PANEL FRAME AND HINGE BROKEN REMOVED WAST SERVICE PANEL REGISTER AND PANEL FRAME. REMOVED CORROSION ON THE WASTE SERVICE PANEL REGISTER AND PANEL FRAME. TOO MUCH MATERAL REMOVED. PANNEL REPSDR JJBA20260825018Skin · corrodedEVIDENCE OF CORROSION ON THE OUTER SKIN OF THE APU COMPART TH LOWER PANEL CORROSION WAS REMOVED ON THE OUTER SKIN OF THE APU COMPART RH LOWER PANELSDR CALA2026082518880Oven · contaminatedSMOKE OBSERVED COMING FROM OVEN 106. SMOKE ODOR WAS NOTICEABLE TEMPORARILY. DISCONTINUED USE AND THE SMOKE AND ODOR DISSIPATED. 106 OVEN INOPERATIVE, CB SAFETY COLLARED & PLACARDED. CLEANED OVER IAW DMC-B787-A-25-32-00-12A. NO NOTABLE SMOKE ODOR AT THIS TISDR CALA2026082518874Skin · damagedAFTER PHASE II INSPECTION FOUND LIGHTNING STRIKE ON FASTENER BTW STA 380 AND 2.5" ABOVE OF S-20R. PERFORMED REPAIR LIGHTNING STRIKE ON FASTENER BTW STA 380 AND 2.5" ABOVE OF S-20R, IAW SRM 53-00-01-2R-41 THIS REPAIR IS A CATEGORY B REPAIR TABLE 203. INSPECTIOSDR MASA20260824212Floorbeam · corrodedDURING HEAVY CHECK OF CFIII, AFT WET AREA, CORRODED FLOORBEAM AT FR 86 TO FR 89 LT, RBL 11, HAS BEEN REMOVED AND REPLACED IAW SRM 51-41-01, 51-42-01, AND SRM 51-43-03. NRC# 4502709-1000-0106. REV 45, REV 50.SDR VNAA202608200025Lug · corrodedAFTER RT AILERON BUSHINGS REMOVAL WAS FOUND CORROSION ON LUG BORE R2 AT CENTER FITTING RT AILERON. LUG BORE R2 AT CENTER FITTING, RH AILERON WAS REPAIRED PER REO 670-57-61-237 REV.-- "SDR VNAA202608200024Fitting · corrodedCORROSION ON CENTER FITTING OF LH AILERON L5 LUG BORE. REPAIRED PER REO 670-57-61-237SDR VNAA202608200023Fitting · corrodedCORRODED FLOOR FITTING IN AFT ACCESS 107 OUTSIDE (1EA) ON GALLEY 1. FLOOR FITTING IN AFT ACCESS 107 OUTSIDE (1EA) ON GALLEY WAS FABRICATED AND INSTALLED PER EA NO:2531-2026-0889 REV: - - SECTION III PERMANENT REPAIR.SDR VNAA202608200022Fitting · corrodedCORROSION FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1. FLOOR FITTING IN FWD ACCESS 107 (1EA) ON GALLEY 1 WAS REPLACED PER SAFRAN CMM 25-33-21."SDR VNAA202608200021Bearing · wornFREE PLAY ON BEARINGS OF RUDDER HINGES NR 2 AND 3 AT REAR SPAR OF VERTICAL STABILIZER. BEARINGS OF RUDDER HINGES NR 2 AND 3 AT REAR SPAR OF VERTICAL STABILIZER WERE REPLACED PER RIL #1213 REV. NC.SDR VNAA202608200020Floor Support · crackedCRACK ON FLOOR SUPPORT RBL 12, BTW BS 221.73 - 229, (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL 79.50) AT FWD FUSELAGE INTERNAL STRUCTURE. FLOOR SUPORT RBL 12.0 BTW BS 221.73 - 229 (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL 79.50) AT FWD FUSELAGE INTERNALSDR VNAA202608200019Canister · crackedCRACK ON CANISTER WELDED NO.3 IN STA WS=148 AT INTERNAL LH MAIN FUEL TANK. CRACK ON CANISTER WELDED NO.3 IN STA WS=148 AT INTERNAL LT MAIN FUEL TANK WAS REPAIRED PER REO 670-57-42-577 REV -.SDR VNAA202608200018Seat Track · corrodedWEAR RH SEAT RAIL FS 847.00 +16.00 TO 977.00 AT PAX CABIN. RT SEAT RAIL FS 847.00 +16.00 TO 977.00 AT PAX CABIN. WAS EVALUATED OUT OF LIMITS PER SRM 53-51-49-101-001-A02 AND REPLACED PER AMM 53-00-49.SDR VNAA202608200017Seat Track · corrodedCORROSION ON LT SIDE RAIL BTW FS=700 TO FS=379 AT CPAX. CORROSION ON LH SIDE RAIL BTW FS=700 TO FS=379 AT CPAX. WERE EVALUATED OUT OF LIMITS PER SRM 53-21-49-101-001-A01, SRM 53-31-49-101-001-A02 AND SRM 53-41-49-101-001-A02 REPLACED PER AMM 53-00-49.SDR VNAA202608200016Seat Track · corrodedCORROSION ON LT SIDE RAIL BTW FS=881 TO FS=785 AT CPAX. CORROSION ON LH SIDE RAIL BTW FS=881 TO FS=785 AT CPAX WAS EVALUATED OUT OF LIMITS PER SRM 53-41-49-101-001-A02 REPLACED PER AMM 53-00-49.SDR VNAA202608200015Seat Track · corrodedCORROSION ON RH SIDE RAIL BTW FS=744 TO FS=761 AT CPAX. CORROSION ON RH SIDE RAIL BTW FS=744 TO FS=761 AT CPAX. WERE EVALUATED OUT OF LIMITS PER SRM 53-41-49-101-001-A02 REPLACED PER AMM 53-00-49.SDR VNAA202608200014Seat Track · corrodedCORROSION ON RH SIDE RAIL BTW FS=421 TO 485 , FS=501 TO FS=570 , FS=610 TO FS=720 AT CPAX. RIGHT SIDE RAIL BTW FS=421 TO 485 , FS=501 TO FS=570 , FS=610 TO FS=720 AT CPAX WERE REPLACED PER CRJ900 AMM 53-00-49"SDR VNAA202608200013Seat Track · corrodedCORROSION ON SEAT RAIL LBL=26 BTW FS=486 TO FS=597 AT CPAX. CORROSION ON SEAT RAIL LBL=26 BTW FS=486 TO FS=597 AT CPAX. WAS EVALUATED OUT OF LIMITS PER CRJ-900 SRM 53-31-49-101-001-A02 AND REPLACED PER CRJ-900 AMM 53-00-49.SDR VNAA202608200012Seat Track · corrodedCORROSION ON SEAT RAIL LBL=10 BTW FS=598 TO FS=669.40 AT CPAX. CORROSION ON SEAT RAIL LBL=10 BTW FS=598 TO FS=669.40 AT CPAX. WAS EVALUATED OUT OF LIMITS PER SRM 53-31-49-101-001-A02 REPLACED PER AMM 53-00-49.SDR VNAA202608200011Seat Track · corrodedCORROSION ON SEAT RAIL RBL9.00 BTW FS=486 TO FS=597, FS=598 TO FS=669.40 AT CPAX. CORROSION ON SEAT RAIL RBL9.00 BTW FS=486 TO FS=597, FS=598 TO FS=669.40 AT CPAX WAS EVALUATED OUT OF LIMITS PER SRM 53-31-49-101-001-A02 REPLACED PER AMM 53-00-49.SDR VNAA202608200010Seat Track · corrodedCORROSION ON SEAT RAIL LBL=26 BTW FS=364 TO FS=485 AT PAX CABIN. CORROSION ON SEAT RAIL LBL=26 BTW FS=364 TO FS=485 AT CPAX WAS EVALUATED OUT OF LIMITS PER SRM 53-21-49-101-001-A02. AND SRM 53-31-49-101-001-A02 REPLACED PER AMM 53-00-49.SDR VNAA202608200009Seat Track · corrodedCORROSION ON SEAT TRACK LBL 9 BTW BS 379 - 485 AT CPAX. CORROSION ON SEAT TRACK LBL 9 BTW BS 379 - 485 AT CPAX. WAS EVALUATED OUT OF LIMITS PER SRM 53-21-49-101-001-A02 AND SRM 53-31-49-101-001-A02 REPLACED IAW AMM 53-00-49.SDR VNAA202608200008Seat Track · corrodedCORROSION ON SEAT TRACK RBL9, BTW BS 349 - 485 AT CPAX. CORROSION ON SEAT TRACK RBL9.00 BTW FS=349 TO FS=485 AT CPAX. WAS EVALUATED OUT OF LIMITS IAW SRM 53-21-49-101-001-A02 AND SRM 53-31-49-101-001-A02 REPLACED IAW AMM 53-00-49.SDR VNAA202608200007Floor Support · crackedCRACK ON COCKPIT FLOOR LONGITUDINAL BEAM (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT. CRACK ON COCKPIT FLOOR LONGITUDINAL BEAM (LBL12) TO CROSSBEAM FS 280. FLOOR STRUCTURE BELOW FLIGHT COMPARTMENT WAS REPAIRED PER REO 690-53-11-2234 SDR VNAA202608200006Rib · crackedCRACK ON RIB LEADING EDGE SS 57.16 AT RH WING. CRACK ON RIB LEADING EDGE SS 57.16 AT RH WING WAS REPAIRED PER REO 690-57-41-240 REV. -.SDR VNAA202608200005Rib · crackedCRACK ON RIB LEADING EDGE SS 57.16 AT LH WING. RIB LEADING EDGE SS 57.16 AT LH WING WAS REPAIRED PER REO 690-57-41-240 REV -.SDR VNAA202608200004Web · crackedCRACK ON ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193. ELECTRICAL BAY FLOOR WEB RIGHT SIDE WAS REPAIRED PER SRM 53-11-43-201-001-A01SDR VNAA202608200003Skin · damagedSEVERAL NICKS, EROSION AND WEAR ON LOWER SKIN OF LH INBOARD FLAP FLS 15.5 TO FLS 75.5 WAS REPAIRED PER CRJ900 SRM 57-52-01-201-005-A01SDR VNAA202608200002Tail Cone · dentedDENT IN TAILCONE WAS REPAIRED IAW REO 690-53-84-062 REV -.SDR VNAA202608200001Door · crackedDOOR WASTE ASSEMBLY WAS REPAIRED PER EA NO: 2542-2026-0913 REV. -