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 DALA2026043002738Access Door · crackedL/H PYLON I/B SKIN ACCESS DOOR 436AR CUT-OUT FOUND CRACK AT 12 O'CLOCK. REPAIRED AS PER ER/A 633786-14 (1570034) (AIRCRAFT GROUNDED)SDR 2026F00091Bracket · corrodedMECHANICALLY REMOVED 8 AREAS OF CORROSION WHERE 8 LOCK FASTENERS WERE PREVIOUSLY REMOVED ON FWD BRACKET INSIDE NLG WHEEL WELL, ON FWD FACE OF UP-LOCK BRACKET IAW SRM 51-70-02. FOUND CORROSION BLENDS TO BE BEYOND LIMITS IAW SRM 51-70-02 EXCEEDING .002" OF MATESDR JR2R20260430808Floorbeam · corrodedFWD WET AREA LBL11 FR19 FLOOR BEAM CORRODED. REPAIRED.SDR JR2R20260430806Beam · corrodedFWD WET AREA LBL11 FR16 FLOOR BEAM CORRODED. REPAIRED.SDR JR2R20260430807Floorbeam · corrodedFWD WET AREA LBL11 FR17 FLOOR BEAM CORRODED. REPAIRED.SDR JR2R20260430552Skin · chafedLEFT WING FIXED LEADING EDGEO OVER PYLON HAS CHAFE MARKS. REPAIREDSDR JR2R20260430561Skin · chafedRIGHT WING FIXED LEADING EDGE OVER PYLON HAS CHAFE MARKS. REPAIREDSDR JR2R20260430816Sill Drain · corrodedAFT WET AREA FR84 RBL36 MOP SILL CORRODED. REPLACED.SDR JR2R20260430820Sill Drain · corrodedAFT WET AREA RH MOPSILL BETWEEN FR88 AND FR90 CORRODED. REPLACEDSDR JR2R20260430812Doubler · corrodedFWD WET AREA RH DOUBLER BETWEEN FR12 AND FR14 CORRODED. REPLACED.SDR 2026FA0000305Life Raft · no testG7500 8 PERSON LIFERAFT ASSY RECEIVED IN PACKED CONDITION. DURING TRIAL INFLATION, UNIT WAS FAILED DEPLOYMENT. PREPARATION FOR THE TRIAL INFLATION TEST WAS PERFORMED, INCLUDING A RESERVOIR PRESSURE CHECKED. THE RECORDED PRESSURE OF 3423 PSI MEETS THE REQUIREDSDR 2026FA0000819Drive Gear · spalledFACE GEAR DAMAGED, ENGINE HAS EXHIBITED DAMAGE TO THE ALTERNATOR DRIVE FACE GEAR (P/N 657984), WHICH DRIVES THE NO. 1 ALTERNATOR. THE DAMAGE HAS INCLUDED VARYING DEGREES OF SPALLING AND GALLING OF THE GEAR TEETH.SDR 4VAA202604290034Skin · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT WING LEADING EDGE PNL 612BR UPPER AND LOWER SURFACE AT THE FASTENER HOLES. THE PANEL WAS REPAIRED IN ACCORDANCE WITH SAAB STATEMENT 2000SDS060706.SDR SWIA2026042977015Floor Support · corrodedRBL 9 FLOOR BEAM CAP ANGLE IS CORRODED AT MULTIPLE LOCATIONS BETWEEN F.S.409+128 TO F.S.559 (C-CHECK RO 08/28/2026)CUTAWAY CORRODED FLOORBEAM CAP ANGLE AT FS409+118 & FS559.00+10 AND INSTALLED NEW FABRICATED CAP ANGLE AT SAME LOCATION IAW ALL STEPS MHIRJ REOSDR SWIA2026042977001Floorbeam · corrodedLBL 27 FLOORBEAM CAP ANGLE IS CORRODED BETWEEN FS544 AND F.S.559. CUTAWAY CORRODED FLOORBEAM CAP ANGLE AT FS544 TO FS559 AND FABRICATED AND INSTALLED NEW REPAIR PARTS IAW ALL STEPS OF MHIRJ REO 601R-53-41-3442. PERFORMED PRESSURE LEAK TEST OF REPAIRED AREAS IASDR SWIA2026042976995Floorbeam · corrodedFLOORBEAM CAP ANGLE IS CORRODED AT MULTIPLE LOCATIONS BETWEEN BS 409+128 - 559, LBL 9. CUTAWAY CORRODED FLOORBEAM AND LOCATED, DRILLED, & INSTALLED A NEW SERVICEABLE FLOORBEAM AT SAME LOCATION IAW ALL STEPS OF REO 601R-53-41-3438, REV-. PERFORMED A LEAK CHESDR REXA2026070701031Hinge · crackedCRACK ON FWD SIDE SKIN AT SETTLEMENT AREA OF ACCESS PANEL 832AT AT PASSENGER DOOR. FWD SIDE SKIN AT SETTLEMENT AREA OF ACCESS PANEL 832AT AT PASSENGER DOOR. WAS REPAIRED PER CRJ-900 SRM 52-11-04-201-004-A01SDR AALA202606221983Frame · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FRAME AT FR 16 BETWEEN S22L AND S23L. REPAIRED FRAME PER EA 375284.SDR DALA2026060903470Rib · corrodedRT WING / GEAR RIB 6 / FWD LUG CORROSION. COMPLIED WITH ERA 633182-14AD. (1568498) AIRCRAFT WAS GROUNDED.SDR VNAA202606060016Fitting · corrodedCORROSION ON FWD RT FITTING (1EA) UNDER WASTER CONTAINER AT FWD LAV. FWD RT FITTING (1EA) UNDER WASTER CONTAINER AT FWD LAV WAS REPLACED PER SAFRAN CMM 25-40-19SDR SWAA2026060293856Fitting · crackedRH PICKLEFORK FRAME FITTING AT S-18A IS CRACKED FROM FASTENER TO EDGE OF FITTING (SECOND FASTENER DOWN ON AFT SIDE OF FITTING. REMOVED AND REPLACED RT PICKLE FORK FRAME IAW SRM 51-40-02-0-G-0 AND SB 737-53-1397.SDR HNAA2026060200469Beam · corrodedCORROSION IN COCKPIT ON PILOTS INBD BEAM GUSSET. FABRICATED AND INSTALLED BOTH DOUBLERS TO REPAIR COCKPIT PILOTS INBD BEAM GUSSET. PAINTED BOTH DOUBLER ON PILOTS OUTBD AND INBOARD SEAT TRACK GUSSET IAW EMB 145 CPM 51-21-06 AND PDT BULLETIN. REPAIR OF THE COCKSDR HNAA2026060200468Beam · corrodedCORROSION IN COCKPIT ON PILOTS OTBD BEAM GUSSET. UPON FURTHER INVESTIGATION FOUND REMAINING THICKNESS AT BLENDED AREAS IN COCKPIT ON PILOTS OTBD BEAM GUSSET TO BE WITHIN NON-SIGNIFICANT DAMAGE IAW EMB 145 SRM 51-10-05.SDR SWAA2026060193942Stop Fitting · crackedCRACK ON PAD STOP FITTING AFT EMERGENCY EXIT DOOR AT PASSENGER CABIN. REPLACED PAD STOP FITTING AFT EMERGENCY EXIT DOOR LT SIDE AT PASSENGER CABIN (1 EA) IAW AMM 52-22-01-400-801.SDR SWAA2026060193943Intercostal · crackedFAULT RAISED TO CAPTURE RII LABOR OF CRACK ON WEB INTERCOSTAL LOCATED BTW BS 344 TO BS 360 LBL 10 WL 208.1 AT FWD GALLEY AREA. REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BS 344 TO BS 360 LBL 10 WL 208.1 AT FWD GALLEY AREA IAW SRM 53-10-15; SRM 51-40-02 ASDR REXA2026052900879Hinge · damagedUPPER HINGE OF TOILET SERVICE DOOR DOES NOT LATCH ON OPEN POSITION AT FWD LOWER FUSELAGE. UPPER HINGE OF TOILET SERVICE DOOR AT FWD LOWER FUSELAGE.WAS REPLACED PER SRM 51-41-02-001-001-A01.SDR REXA2026052900878Attach Angle · corrodedCORROSION ON ATTACHMENT ANGLE OF BONDING JUMPER ON TOILET SERVICE DOOR AT FWD LOWER FUSELAGE CORROSION ON ATTACHMENT ANGLE OF BONDING JUMPER ON TOILET SERVICE DOOR AT FWD LOWER FUSELAGE. WAS REMOVED AND EVALUATED OUT OF LIMITS PER CRJ900 SRM 51-21-06-001-001-SDR REXA2026052900876Gusset · crackedCRACK ON GUSET ON AFT EQUIPMENT COMPARTMENT DOOR STRUCTURE. GUSSET ON AFT EQUIPMENT COMPARTMENT DOOR STRUCTURE WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01SDR REXA2026052900875Plate · crackedCRACK ON PLATE BTW FS 1144.00 AND LBL 3 AT AFT EQUIMPMENT COMPARTMENT. CRACK ON PLATE BTW FS 1144.00 AND LBL 3 AT AFT EQUIMPMENT COMPARTMENT.WAS REMOVED AND EVALUATED WITHIN LIMITS PER CRJ900 SRM 53-00-00-101-001-A01SDR REXA2026052900873Door Sill · crackedCRACK ON FWD RT DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) FWD RH DOOR LANDING AT FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR) WAS REPLACED PER SRM 51-42-10-001-001-A01 AND SRM 51-42-06-001-001-A01SDR 2026FA0000464Stiffener · crackedR/H WING FWD LWR I/B SKIN, AFT STIFFENER CRACKED. REPLACED WITH NEWSDR SWAA2026052794062Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 BL 0 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BETWEEN BS 380 TO BS 400 BL 0 AND WL 208.1 AT FLOOR STRUCTURE OF PASSENGER CABIN AREA IAW SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51SDR SWAA2026052794060Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 10 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BETWEEN BS 380 TO BS 400 RBL 10 AND WL 208.1 AT FLOOR STRUCTURE OF PASSENGER CABIN AREA IAW B737-800 SRM 51-10-02-0G-0 PARAGRSDR SWAA2026052794063Floor Support · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 51 WL 208.1 AT PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BETWEEN BS 380 TO BS 400 LBL 51 AND WL 208.1 AT FLOOR STRUCTURE OF PASSENGER CABIN AREA IAW SRM 51-40-02-0G-0; DRAWING 143A54SDR SWAA2026052794064Floor Support · crackedCRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 41 WL 208.1 AT PASSENGER CABIN . REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BETWEEN BS 380 TO BS 400 RBL 41 AND WL 208.1 AT FLOOR STRUCTURE OF PASSENGER CABIN AREA IAW SRM 51-40-02-0G-0; DRAWING NUMBERSDR SWAA2026052793950Frame · crackedCRACK ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA. PERFORMED PERMANENT REPAIR FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA I.A.W B737-800 EA M-22-153-01244.SDR SWAA2026052693949Web · crackedCRACK ON WEB LOCATED CEILING AREA BTW BS 847 TO BS 867 LBL 22 AT AFT CARGO COMPARTMENT. TOOK MEASURE OF CRACK LOC. WEB LOCATED CEILING AREA BTW BS 847 TO BS 867 LBL 22 AT AFT CARGO COMPARTMENT IS IS L:0.250 ?INCH. REPLACED WEB LOCATED CEILING AREA BTW BS 84SDR AALA202605220849Door Sill · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL AT FR 67 PLUS 17 INCHES AND AT S23R. REPLACED LOWER SILL PER SRM 51-42-11.SDR AALA202605228204Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT AFT PASSENGER / CREW DOOR CUTOUT LOWER SILL AFT CORNER SHAPE FITTING AT FR 68 AND S23R. REPLACED AFT CORNER SHAPE FITTING PER SRM 51-42-11.SDR SWAA2026052293954Access Panel · crackedCRACK ACCESS PANEL 344PT AT RT HORIZONTAL STABILIZER. REPLACED ACCESS PANEL 344PT AT RT HORIZONTAL STABILIZER IAW SRM 51-10-02. EVALUATED AND FOUND OUT ALLOWABLE DAMAGE LIMITS AND THERE ARE NO REPAIRS FOR THIS PART IN THE STRUCTURAL REPAIR MANUAL. IAW SRM 55-SDR SWAA2026052294066Access Panel · elongatedELONGATED HOLE ON ACCESS PANEL 661AB AT RT WING. REPAIRED ACCESS PANEL 661AB AT RT WING IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10.SDR SWAA2026052294067Access Panel · elongatedELONGATED HOLE ACCESS PANEL 661BB AT RT WING. REPAIRED ACCESS PANEL 661BB AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.SDR SWAA2026052294068Access Panel · elongatedELONGATED HOLE ON ACCESS PANEL 661CB AT RT WING. REPAIRED ACCESS PANEL 661CB AT RT WING IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10.SDR SWAA2026052294069Access Panel · damagedELONGATED HOLE ACCESS PANEL 561AB AT LT WING. REPAIRED ACCESS PANEL 561AB AT LT WING IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10.SDR SWAA2026052294070Access Panel · damagedELONGATED HOLE ON ACCESS PANEL 561CB TRAILING EDGE AT LT WING . REPAIRED ACCESS PANEL 561CB TRAILING EDGE AT LT WING IAW B737-800 SRM 51-70-04-2R-10 REPAIR 10.SDR SWAA2026052294071Access Panel · damagedELONGATED HOLE ACCESS PANEL 561BB AT LT WING. REPAIRED ACCESS PANEL 561BB AT LT WING IAW SRM 51-70-04-2R-10, REPAIR 10.SDR AALA202605221601Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSOIN ON Z-ANGLE BETWEEN STA 991 AND STA 994 AT RBL 32. REPLACED ANGLE PER AARD 51-00-5-1.SDR AALA202605228418Web · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT PASSENGER CABIN FLOOR STRUCTURE WEB AT STA 1020 AND LBL 28. REPLACED WEB PER AARD 51-00-05-1.SDR AALA202605224466Angle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT ENTRY WAY LOWER SILL INNER CHORD (CREASE ANGLE) BETWEEN STA 967 AND STA 986 AT LBL 50. REPLACED CHORD PER AARD 51-00-05-1.SDR AALA202605222136Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION AT FASTENER HOLE ON FLOOR BEAM UPPER CHORD FLANGE AT STA 986 BETWEEN LBL 7 AND LBL 54. BLENDED CORROSION PER SRM 51-10-02.