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 SWIA2026042076861Pressure Deck · corrodedRIGHT CABIN PRESSURE DECK CORRODED AT ONE LOCATION BTWN BS 484 & 499. REMOVED CORROSION ON RT PRESSURE DECK IAW REO 601R-53-41-666, REV C. & SKYCARD 51-900-1003-SKY ORIGINAL THICKNESS 0.055" REMAINING THICKNESS OF LOWEST DEPTH 0.047" ALLOWABLE BLEND DEPTH 0.0SDR SWIA2026042076853Pressure Deck · corrodedRIGHT PRESSURE DECK CORRODED AT ONE LOCATION, BS 449.85. REPAIRED RT PRESSURE DECK IAW REO 601R-53-41-666, REV-C. COMPLETED TASK CARD 51-900-1003-SKY.SDR SWIA2026042076851Pressure Deck · corrodedLEFT CABIN PRESSURE DECK CORRODED AT TWO LOCATIONS, BS 424. REPAIRED LT CABIN PRESSURE DECK AT BS 424 IAW REO 601R-53-41-666, REV C. COMPLETED TASK CARD 51-900-1003-SKY.SDR SWIA2026042076849Pressure Deck · corrodedLEFT CABIN, PRESSURE DECK CORRODED AT ONE LOCATION BETWEEN BS 424 & 439. REMOVED CORROSION ON THE PRESSURE DECK IAW REO 601R-53-41-666, REV C, STEP 1.2. & TASK CARD 51-900-1003-SKY ORIGINAL THICKNESS 0.055" REMAINING THICKNESS OF LOWEST DEPTH 0.042" ALLOWABLESDR SWIA2026042076417Skin · crackedLEFT TRU BAY DOOR CUT-OUT, AFT LOWER CORNER POSSIBLE FUSELAGE SKIN CRACKED AT THE RADIUS. REPLACED LT HYDRAULIC BAY SKIN PANEL, JUST BELOW TRU BAY DOOR CUT OUT, REF SRM 51-42-06-001-001-A01 & SRM 51-42-13-001-001-A01 & DWG CC670-33040 REV G AND DWG CC670-320SDR SWIA2026042076415Housing · chafedSERVICE DOOR EXTERIOR HANDLE HOUSING IS CHAFFED AT THE FORWARD RADIUS. REMOVED AND REPLACED CHAFFED SERVICE DOOR EXTERIOR HANDLE HOUSING WITH NEW HOUSING USING ALL NEW HARDWARE INTO THE SERVICE DOOR IAW SRM 51-42-06-001-001-A01 AND DWG CC670-38103 REV -C. ALSDR SWIA2026042076377Skin · crackedRH TRU BAY DOOR CUT-OUT, AFT LOWER CORNER POSSIBLE FUSELAGE SKIN CRACKED AT THE RADIUS. REPLACED ADG SKIN WITH SERVICEABLE SKIN PANEL REF. DWG CC670-33040 REV-G, DWG CC670-32010 REV-F, SRM 51-42-06-001-001-A01 REV. 38, SRM 51-42-21-001-001-A01 REV. 38, SRM 5SDR IPXA2026061392868Fitting · damagedFAULT: STR - Z600 - PER ENG REQUEST FR47 RHS HOLE E MEASURES 0.595". ACCOMPLISHED REPAIR IN ACCORDANCE WITH EO-83044-REQ3 AND VT-MAE EA 300-5710-27-A4449, REV. _.SDR IPXA2026043094249Retainer · crackedNR 1 ENG OUTBD T/R LOWER CIRCUMFERENTIAL STRAP RETAINER BRACKET IS CRACKED. INSTALLED NEW BRACKET #1 ENG OUTBD T/R LOWER CIRCUMFERENTIAL STRAP.IAW A300-600 SRM 51-40-21/001.SDR IPXA2026060294870Rub Strip · gougedNR 1 ENG INBD T/R UPPER AFT METALLIC STRIP IS GOUGED. ACCOMPLISHED PERMANENT REPAIR IN ACCORDANCE WITH EO-97623-REQ1 AND VT-MAE EA 300-5430-27-A4474, REV. -.SDR SIMA20260420001Seal Depressor · bentFWD PAX DOOR CUTOUT FWD SEAL DEPRESSOR FRAME IS BENT IN 3 SPOTS. (MAJOR REPAIR) RAR FWD PAX DOOR CUTOUT FWD SEAL DEPRESSOR IAW ERJ 170 SRM 51-40-08SDR AALA202606089665Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER AT FR 59 AND S42L. REPAIRED STRINGER PER EA 374801.SDR VNAA202606060005Bracket · crackedCRACKED UPPER SUPPORT BRACKET OF PYLON TIE-BAR, THROUGH PYLON ACCESS PANEL 443BT AT RH PYLON. REPLACED PER SRM 51-42-06-001-001-A01.SDR AALA202606052264Stringer · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER AT FR 59 AND S43L. REPAIRED STRINGER PER EA 374801.SDR ASAA2026042066475Baffle · crackedFWD PIT RH BAFFLE BS 500K FWD AND AFT CLIPS CRACKED. GROUNDED - YES. REMOVED AND REPLACED RT BAFFLE CLIP STA 500K FWD AND AFT IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0.SDR SWAA2026060191137Battery Pack · inoperativeINOPERATIVE LOWERED CEILING PANEL BATTERY PACK AT FWD GALLEY AREA. REPLACED LOWERED CEILING PANEL BATTERY PACK AT FWD GALLEY AREA (2 EA) IAW AMM 33-51-06-960-805 TEST OK;SDR SWIA2026042076115Skin · corrodedCORROSION FOUND AROUND FASTENERS ON SKIN BETWEEN STR 23R AND 24R @ FRAME 559+96. PERFORMED BLEND REPAIR AROUND FASTENERS ON SKIN BETWEEN STR 23R AND 24R @ FRAME 559+96 IAW REO 601R-53-51-740 REV--SDR SWIA2026042076113Skin · corrodedEXTERIOR SKIN CORRODED BETWEEN FS 559+80 AND FS559+96 AT STRINGERS 21R AND 23R. COMPLIED WITH BLEND REPAIR TO EXTERIOR SKIN BETWEEN FS559+80 - FS559+96 AT STGR 21R AND 23R IAW REO 601R-53-51-740 REV--. COMPLETE TASK CARD 51-900-1003-SKY.SDR ASAA2026042066369Transition Panel · corrodedFWD PIT LH SIDEPLATE TRANSITION PANEL STA 500C - 500L IS CORRODED IN MULTIPLE SPOTS. GROUNDED - YES. REMOVED QAND REPLACED L/H SIDEPLATE TRANSITION PANEL STA 400-500L I.A.W. BOEING 737-900CR SRM 53--00-53-22-6.SDR REXA2026052800867Floorbeam · corrodedR/H FS 280 CORRODED ON BOTTOM CORNER EDGE OF THE BEAM. REMOVED DAMAGED RH FS 280.00 CROSSBEAM IAW CRJ900 SRM 51-42-06-001-001-A01. CRJ900 SRM 51-42-13-001-001-A01. AND CRJ900 SRM 51-42-22-001-001-A01. LOCATED AND DRILLED NEW RH FS 280.00 CROSSBEAM P/N:CC670-3SDR REXA2026052800866Floorbeam · corrodedL/H FS 280 CROSSBEAM HAS CORRODED PIT ON TOP CORNER EDGE OF THE BEAM. REMOVED FS 280 SACRIFICIAL TITANIUM PLATE FOR ACCESS IAW CRJ-900 SRM 51-42-13-001-001-A01. REMOVED DAMAGED LH FS 280.00 CROSSBEAM IAW CRJ900 SRM 51-42-06-001-001-A01. CRJ900 SRM 51-42-13-00SDR AALA202605218276Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION TO FUSELAGE SKIN AT STA 892 AND S27R. ACCOMPLISHED DOUBLER REPAIR PER SRM 51-40-02.SDR AALA202605217573Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER FUSELAGE SKIN AROUND DRAIN HOLE AT BS 727E AND BL 0. ACCOMPLISHED DOUBLER REPAIR PER SRM 53-60-01-2R-4.SDR ASAA2026042066215Baffle · crackedLEFT BAFFLE FOUND TO BE CRACKED AT BS 400 - 420. GROUNDED - YES. REMOVED AND REPLACED LT BAFFLE AT BS 400 - 420 IAW SRM 51-40-02, STEP 7.0.1-2.SDR ASAA2026042066213Baffle · crackedFWD CARGO BAY, LT BAFFLE IS CRACKED BS 500F - 500G. GROUNDED - YES. REMOVED AND REPLACED LT BAFFLE BS 500F-500G IAW SRM 51-40-05-0G-0, & 51-40-02-0G-0.SDR ASAA2026042066211Baffle · crackedFWD CARGO LT BAFFLE BS 500K FWD & AFT CLIPS ARE CRACKED. GROUNDED - YES. REMOVED AND REPLACED LT BAFFLE BS 500K IAW SRM 51-40-05-0G-0, & 51-40-02-0G-0.SDR ASAA2026042066205Angle · crackedFWD CARGO RT BAFFLE BS 500I CLIP IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED RT BAFFLE ANGLE STA 500 I I.A.W. BOEING SRM 51-40-05-0G-0, & 51-40-02-0G-0.SDR ASAA2026042066201Bulkhead · corrodedFWD PIT AFT BULKHEAD STA 500L LOWER SUPPORT IS CORRODED. GROUNDED - YES. REMOVED AND REPLACED LOWER BLEND SUPPORT ANGLE IAW SRM 51-40-02-0G-0 STEP 7.A. 1-4 W= 2.0" O= .080 R= .050 L= 3" D= .030.SDR SWAA2026052091365Stringer · crackedCRACKED STRINGER 9 INTERNAL AREA FUEL TANK UPPER POSITION, BTW RIB 21 AND RIB 22 AT LT WING. PERFORMED REPAIR ON STRINGER 9 INTERNAL LT WING FUEL TANK UPPER POSITION IAW EA- 26-157-01136-WIP1 AND EA- 26-157-01136-WIP2.SDR HNAA2026052000418Floor Support · crackedFOUND CRACKS ON LH OMEGA BEAM #2 AT FR 29. PERFORMED CUT-OUT OF DAMAGE, AND DOUBLER REPAIR TO LT OMEGA BEAM #2 AT FR 29 IAW EMB ETD2026-145-007261 AND EO1-53-26-0215.SDR SWAA2026051991424Vapor Barrier · crackedLEFT BS 663 VAPOR BARRIER IS CRACKED. REPAIRED PER SRM 51-70-04-2R-10-A00755, REPAIR 10, REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH IN SOLID LAMINATES.SDR SWAA2026051991425Vapor Barrier · crackedR/H B.S. 663 VAPOR BARRIER IS CRACKED. REPAIRED PER SRM 51-70-04-2R-10-A00755, REPAIR 10 - REPAIR OF DAMAGE THAT IS MORE THAN 0.50 INCH IN SOLID LAMINATES.SDR AALA202605183360Floorbeam · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM +Y1292 LOC. AT LEVEL FR16 AT FWD GALLEY AREA THE MEASUREMENTS ARE L=1.598 IN, W=1.117 IN, D= 0.050 IN. MAINTENANCE REPLACED FLOOR BEAM Y1292 AT LEVEL FR12 TO FR24 AT FWD GALLEY AREA I.A.W A319 SRM 51-42-11-80SDR QXEA2026051100113Not Reported · corrodedFRAME 19 LBL 11 CORROSION AT SCRFW HOLE ON BEAM. AFTER REWORK FOUND TO BE OUT OF LIMITS. REPAIRED AREA IAW ARM 53-10-10-02-01. RESTORED FINISH.SDR QXEA2026051100112Doubler · corrodedDOUBLER AT FRAME 16 LBL 11 IS CORRODED. REMOVED DAMAGED AREAS AND FOUND TO BE OUT OF LIMITS. REPAIRED PER ETD 2026-170-006563.SDR IPXA2026042090836Skin · crackedRIGHT WING, BETWEEN SLAT NR 8 & 9, FIXED LEADING EDGE SKIN CRACKED. COMPLIED WITH EO-97223-REQ1 & EA 757-5741-27-A4443, REV-.SDR CALA2026050516020Skin · crackedCRACK FOUND AT LEFT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 101.90, 19" FROM REAR SPAR , I/B ROW. CRACK LENGTH - 3/4". REPAIRED LEFT HORIZONTAL STAB LOWER SKIN AT STAB STA 101.90, 19" FROM REAR SPAR IAW SRM 55-10-01-2R-11.SDR HNAA2026050500370Floor Support · corrodedRIGHT FLOOR SILL PN 145-25800-010, ITEM 130 EMB 145 SRM 53-23-10, FROM BS 11990.0 TO BS 13804.5, HAS CORROSION. REMOVED AND REPLACED WITH NEW CENTRAL FUSELAGE III RIGHT FLOOR SILL PN 145-25800-010, ITEM 130 EMB 145 SRM 53-23-10, FROM BS 11990.0 TO BS 13804.5 SDR ASAA2026042065823Baffle · crackedFWD PIT LH BAFFLE STA 500E - 500F IS CRACKED. GROUNDED - YES. REMOVED & REPLACED L/H BAFFLE STA 500E-500F IAW BOEING 737-900ER SRM 51-40-02-0G-0.SDR SWIA2026042075982Flap Track · wornRIGHT WING FLAP TRACK 1A HAS A THICKNESS REDUCTION OF .63MM. REMOVED AND REPLACED RT WING FLAP TRACK 1A. IAW AMM 57-54-25.SDR IPXA2026050282674Skin Panel · corrodedMAJOR REPAIR, CORROSION-FUSELAGE SKIN IMMEDIATELY SURROUNDING THE DRAIN VALVE AT STA 1410 BETWEEN S-38R AND S-39R. (REPAIR) INSTALLED BULK CARGO FLOOR PANEL IAW AMM 53-01-05-404-004 REV.1472. CONDITION CHECK NORMAL.SDR AALA202604304655Baffle · corrodedAIRCRAFT IN BASE MAINTENANCE: FORWARD CARGO BAFFLE CORRODED AT BETWEEN BS 500F AND 500G. INSTALLED NEW BAFFLE. PER SRM 53-30-53-2R-1SDR ASAA2026042065767Channel · corrodedFLOOR SIDEPLATE CHANNEL CORRODED AND PUNCTURED. OUT OF SRM 53-00-53-1A-2 LIMITS GROUNDED - YES. REMOVED AND REPLACED CHANNEL REF BOEING DWG 146A7500 ID 225 AND 228SDR SWAA2026042991178Cartridge · crackedLEFT WING OTBD AFT FLAP INBD END ROLLER CARTRIDGE CRACKED AT LOWER FWD RADIUS. LT WING OTBD AFT FLAP; CARTRIDGE WAS REMOVED AND REPLACED IAW SRM 51-40-02-0G-0. TASK COMPLETED.SDR SWIA2026042075915Skin · puncturedTRANSFER FROM EAML 1870599 : APPARENT PUNCTURE AND ABRASION DAMAGE TO SKIN ON NADER SIDE OF RIGHT SIDE HORIZONTAL STABILIZER/ ELEVATOR. (FLIGHT 6327) COMPLIED WITH RIGHT HORIZONTAL REPAIR PER ETD 206-170-00741-A, DATED APRIAL 27 2026 AND CARD 51-00-00-002 SDR IPXA2026042185805Skin · debondedDEBONDED SKIN, INBD EDGE LOWER FACE OF LT WING T/E, OTBD FLAP LOWER SKIN, WBL 355. IAW CMM 57-53-51, REV 38, AND AMM 20-11-00-910-802 REV 147 INSTALLED THE OTBD FLAP INBD UPPER AND LOWER SIDE SEAL WITH RETAINER.SDR AALA202604295341Stop Fitting · out of positionAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND AFT EMERGENCY EXIT DOOR AFT UPPER DOOR STOP PAD IS OUT OF POSITION. REPOSITIONED AFT UPPER DOOR STOP PAD, TO ITS ORIGINAL POSITION ON RIGHT HAND AFT EMERGENCY EXIT DOOR, PER B737 AMM 52-22-01-400-801. PERFORMED SATISFACSDR AALA202604298967Stop Pad · out of positionAIRCRAFT IN BASE MAINTENANCE: LEFT HAND AFT EMERGENCY EXIT DOOR AFT UPPER DOOR STOP PAD IS OUT OF POSITION. REPOSITIONED AFT UPPER DOOR STOP PAD TO ITS ORIGINAL POSITION ON LEFT HAND AFT EMERGENCY EXIT DOOR. PER B737 AMM 52-22-01-400-801. PERFORMED SATISFACTORSDR AALA202604290152Stop Pad · out of positionAIRCRAFT IN BASE MAINTENANCE: LEFT HAND FORWARD OVERWING EMERGENCY EXIT DOOR AFT UPPER DOOR STOP PAD IS OUT OF POSITION. REPOSITIONED AFT UPPER DOOR STOP PAD TO ITS ORIGINAL POSITION ON LEFT HAND FORWARD OVER WING EMERGENCY EXIT DOOR, PER B737 AMM 52-22-01-400SDR AALA202604278571Bottle · low pressureAIRCRAFT IN BASE MAINTENANCE: FORWARD PASSENGER / CREW DOOR 842 DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.