Service difficulty reports

1,771,154 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 VNAA202610060022Shear Panel · corrodedCORROSION ON SHEAR PANEL STA FS=1096 FROM LBL=28 TO RBL=28 AT AFT BAGGAGE BAY FLOOR STRUCTURE. SHEAR PANEL STA FS=1096 FROM LBL=28 TO RBL=28 AT AFT BAGGAGE BAY FLOOR STRUCTURE WAS REPAIRED PER REO 670-53-61-1080 REV - -Jul 29, 2026 · N648NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202610060019Floorbeam · corrodedCORROSION ON FITTING OF WEB END FS 349 LBL SIDE AT FLOOR STRUCTURE LEVEL ON PASSENGER CABIN. FITTING OF WEB END FS 349 LBL SIDE AT FLOOR STRUCTURE LEVEL ON PASSENGER CABIN WAS EVALUATED THEREFORE IT IS OUT LIMITS PER CRJ-900 SRM 53-21-23-101-001-A02 AND REPLAJul 29, 2026 · N648NN · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR VNAA202610060016Drip Tray · corrodedINITIAL INSPECTION: CORROSION ON DRAIN PAN STA FS=280 LBL 13 AT PASSENGER CABIN. DRIP TRAY ASSY (DRAIN PAN) FS=280 LBL 13 AT PASSENGER CABIN WAS EVALUATED THEREFORE AREA IT IS OUT OF LIMITS PER SRM 53-21-43-101-001-A03 AND REPLACED PER CRJ900 SRM 51-42-10-001Jul 29, 2026 · N648NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202610060004Channel · damagedCORROSION ON NUT CHANNEL IN THE LH/RH MLG WHEEL WELL STRUCTURE, NEXT TO THE MLG UPLOCKS. NUT CHANNEL IN THE LH/RH MLG WHEEL WELL STRUCTURE, NEXT TO THE MLG UPLOCKS WERE REPLACED PER CRJ-900 SRM 51-42-06-001-001-A01 AND CRJ-900 SRM 51-41-02-001-001-A01Jul 29, 2026 · N648NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR VNAA202610060003Flap · nickedSEVERAL NICKS BTW FLS=15.00 TO FLS=40.00 INBOARD FLAP AT RH WING. SEVERAL NICKS BTW FLS=15.00 TO FLS=40.00 ON INBOARD FLAP AT RH WING WAS REPAIRED PER CRJ-900 SRM 57-52-01-201-005-A01Jul 29, 2026 · N648NN · Cndair CL6002D24 · Trailing Edge FlapsSDR AALA202610028940Shear Tie · corrodedAIRCRAFT IN BASE MAINTENANCE: AFT CARGO, SHEAR TIE STA 747 LBL16 HAS CORROSION. REMOVED AND REPLACED IAW AARD 51-20-01-1 AND BOEING DRAWING 146A3234.Jul 29, 2026 · N904AN · Boeing 737823 · Fuselage Internal Mounting StructureSDR SIMA20260729007Shear Tie · corrodedSSI 53-23-003 AFT CARGO UNDER FLOOR SHEAR CLIP AT FR 75 BETWEEN STGR 28R/29R CORRODED. (LEVEL 2 CORROSION) REMOVED AND REPLACED AFT CARGO UNDER FLOOR SHEAR CLIP AT FR 75 BETWEEN STGR 28R/29R IAW ERJ 170 SRM 51-40-08 AND ERS-EJ-5300-5543.Jul 29, 2026 · N769KW · Emb ERJ170100LR · Fuselage Internal Mounting StructureSDR SIMA20260729005Shear Tie · corrodedSSI 53-23-003 AFT CARGO UNDER FLOOR SHEAR CLIP AT FR 81 BETWEEN STGR 27R/28R CORRODED. (MAJOR REPAIR) (LEVEL 2 CORROSION) REMOVED AND REPLACED AFT CARGO UNDER FLOOR SHEAR CLIP AT FR 81 BETWEEN STGR 27R/28R IAW ERJ 170 SRM 51-40-08.Jul 29, 2026 · N769KW · Emb ERJ170100LR · Fuselage Internal Mounting StructureSDR SIMA20260729006Shear Tie · corrodedSSI 53-23-003 AFT CARGO UNDER FLOOR SHEAR CLIP AT FR 82 BTW STGR 27R/28R CORRODED. (MAJOR REPAIR) (LEVEL 2 CORROSION) REMOVED AND REPLACED AFT CARGO UNDER FLOOR SHEAR CLIP AT FR 82 BETWEEN STGR 27R/28R IAW ERJ 170 SRM 51-40-08.Jul 29, 2026 · N769KW · Emb ERJ170100LR · Fuselage Internal Mounting StructureSDR REXA2026091001788Support · crackedCRACK AT CORNERS SUPPORT OF THE JB 6 MODULE AT FWD EQUIPMENT COMPARTMENT. SUPPORT OF THE JB 6 MODULE AT FWD EQUIPMENT COMPARTMENT WAS REPLACED PER CRJ900 SRM 51-42-06-001-001-A01Jul 29, 2026 · N478PX · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR REXA2026091001786Drag Angle · crackedCRACK ON RH AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67.5% REAR SPAR DATUM. RH AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01Jul 29, 2026 · N478PX · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR REXA2026091001785Drag Angle · crackedCRACK ON LH AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67.5% REAR SPAR DATUM. LH AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01Jul 29, 2026 · N478PX · Cndair CL6002D24 · Fuselage, Stabilizer Attach FittingsSDR SIMA20260729004Shear Tie · corrodedSSI 53-23-003 AFT CARGO UNDER FLOOR SHEAR CLIP AT FR 76 BTW STGR 28R/29R CORRODED. (LEVEL 2 CORROSION) REMOVED AND REPLACED AFT CARGO UNDER FLOOR SHEAR CLIP AT FR 76 BETWEEN STGR 28R/29R IAW ERJ 170 SRM 51-40-08.Jul 29, 2026 · N769KW · Emb ERJ170100LR · Fuselage Internal Mounting StructureSDR SWAA2026090844421Support Angle · crackedCRACKED SUPPORT ANGLE, BODY FAIRING, BS 500I STR 19L. REPLACED SUPPORT ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, & DWG 116A3010, SHEET 59, REV A, DWG 116A3110, SHEET 8, REV -, & DWG 149A7101, SHEET 11, REV -.Jul 29, 2026 · N8652B · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026090835904Access Panel · damagedELONGATED HOLE ACCESS PANEL 561CB AT LT WING. REPAIRED ACCESS PANEL 561CB AT LT WING IAW SRM 51-70-04-2R-9, REPAIR 9.Jul 29, 2026 · N8652B · Boeing 7378H4 · Wing, Plate/SkinSDR SWAA2026090816333Access Panel · damagedELONGATED HOLE ACCESS PANEL 661AB AT RT WING. REPAIRED ACCESS PANEL 661AB AT RT WING IAW SRM 51-70-04-2R-9 REPAIR 9.Jul 29, 2026 · N8652B · Boeing 7378H4 · Wing, Plate/SkinSDR SIMA20260729002Plate · corrodedLEVEL 2 CORROSION AFT CARGO DOOR INTERNAL CUTOUT STRUCTURE LOWER HORIZONTAL BEAM SPLICE HAS CORROSION. BLENDED AREA ON FWD SPLICE PER: EMB 175 SRM 51-10-03 AND ETN-EJ-51-009. AREA MEASURES L=1.00" X W=.050" X D=.039" AND IS FOUND TO BE OUT OF LIMITS PER: EMB 1Jul 29, 2026 · N212NN · Emb ERJ170200LR · Fuselage Main, StructureSDR SIMA20260729003Shear Tie · corrodedAFT CARGO UNDER SHEAR CLIP AT FR 74 BTW STGR 28R/29R CORRODED. (LEVEL 2 CORROSION). REMOVED AND REPLACED AFT CARGO UNDER SHEAR CLIP AT FR 74 BETWEEN STGR 28R/29R IAW SRM 51-40-08.Jul 29, 2026 · N769KW · Emb ERJ170100LR · Fuselage Internal Mounting StructureSDR SIMA20260729001Shear Tie · corrodedLEVEL 2 CORROSION CORROSION AT FWD CARGO FLOOR STRUCTURE FR 26, STR 28L-28R. (MAJOR REPAIR) BLENDED ON FWD CARGO FLOOR SHEAR CLIP AT FR 26, STR 28L-28R PER SRM 51-10-03. BLENDED AREA MEASURES L=2.8" W=1.0" D=.007". ORIGINAL MATERIAL THICKNESS IS .050" PER DWJul 29, 2026 · N212NN · Emb ERJ170200LR · Fuselage Internal Mounting StructureSDR AALA202609058025Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME UPPER DOUBLE JOGGLE AREA AT FR 16 BETWEEN S4R AND S14R - REPLACED FRAME PER EA 377945Jul 29, 2026 · N654AW · Airbus A320232 · Fuselage Main, FrameSDR AALA202609058236Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME UPPER DOUBLE JOGGLE AREA AT FR 16 BETWEEN S4L AND S14L - REPLACED FRAME PER EA 377920Jul 29, 2026 · N654AW · Airbus A320232 · Fuselage Main, FrameSDR ASAA2026072968496Floorbeam · corrodedAFT WET AREA FLOOR BEAM STA 987 RBL 4 TO RBL 50 CORRODED. GROUNDED - YES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW B737-800 SRM 53-70-51-1A-1, REPAIRED FLOOR BEAM 986 IAW B737-800 SRM 53-70-51-2R-4.Jul 29, 2026 · N569AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2026072968477Web · corrodedAFT WET AREA WEB STA 987 RBL 50 CORRODED. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS IAW 737-800 SRM 53-70-15-1A-1, REMOVED AND REPLACED SHEAR WEB IAW B737-800 SRM 51-40-02Jul 29, 2026 · N569AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026072968473Sill Drain · corrodedAFT WET AREA L/H MOPSILL STA 947 TO STA 987 CORRODED. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED MOPSIL IAW 737-800 SRM 51-40-02-0G-0 W= 1" O= .080" R= .070" L= 2" D= .010".Jul 29, 2026 · N569AS · Boeing 737890 · Fuselage Main, StructureSDR ASAA2026072968465Crossbeam · crackedPANEL BREAK AT STA 540 BL 0 TO LBL 24 CRACKED. GROUNDED - YES. REMOVED AND REPLACED PANEL BREAK IAW B737-800 SRM 51-40-02-0G-0.Jul 29, 2026 · N569AS · Boeing 737890 · Fuselage Main, StructureSDR REXA2026090401771Frame · corrodedFRAME BS 379 REQUIRES REMOVAL BETWEEN S20-S25R TO ACCESS CORROSION. UPON ADDITIONAL EVALUATION BS 379 BETWEEN S20 - 25R HAS EXFOLIATE CORROSION FOUND 100 PERCENT MATERIAL LOSS, OUT LIMITS IAW SRM 53-21-23-101-003-A02. INSTALLED NEW FRAME BS 379 BTWN S20 - 2Jul 29, 2026 · N810SK · Cndair CL6002D24 · Fuselage Main, FrameSDR ASAA2026072968480Floor Support · corrodedAFT WET AREA INTERCOSTAL STA 947 TO STA 967 LBL 50 CORRODED. GROUNDED - YES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-1A-1, REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0 AND AMM 20-50-11-910-801.Jul 29, 2026 · N569AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026072968479Floorbeam · corrodedAFT WET AREA FLOORBEAM STA 947 LBL 50 CORRODED. GROUNDED - YES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-1A- 1, REPAIRED FLOORBEAM IAW SRM 53-70-51-2R-5 W: 2" O: .180 R: .048" L: 2" D: .132.Jul 29, 2026 · N569AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2026072968478Floorbeam · corrodedAFT WET AREA FLOORBEAM STA 967 RBL 20 TO LBL 6 CORRODED. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT OF LIMIT IAW SRM 53-70-51-1A-1 AND REPAIRED FLOORBEAM IAW SRM 53-00-51-2R-1.Jul 29, 2026 · N569AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2026072968476Sill Drain · corrodedAFT WET AREA R/H MOPSILL STA 997 TO STA 947 CORRODED. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS IAW 53-70-15-1A-1, REMOVED AND REPLACED MOP SILL IAW B737-800 SRM 51-40-02-0G-0 W: 2" O: .080 R: .066 L: 2" D: .014.Jul 29, 2026 · N569AS · Boeing 737890 · Fuselage Main, StructureSDR ASAA2026072968475Support Angle · corrodedAFT WET AREA L/H WEB ANGLE SUPPORT STA 997 CORRODED. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED SUPPORT ANGLE IAW B737-800 SRM 51-40-02-0G-0. W= .5" O= .05" R= .043" L= 2" D= .007".Jul 29, 2026 · N569AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026072968474Floorbeam · corrodedAFT WET AREA FLOORBEAM STA 987 LBL 26 TO LBL 50 CORRODED. GROUNDED - YES. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-1A-1, REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-4.Jul 29, 2026 · N569AS · Boeing 737890 · Fuselage Main, Floor BeamSDR ASAA2026072968472Support Angle · corrodedAFT WET AREA L/H WEB SUPPORT ANGLE STA 1016 TO STA 987 CORRODED. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED SUPPORT ANGLE IAW B737-800 SRM 51-40-02-0.Jul 29, 2026 · N569AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2026072968467Web · corrodedAFT WET AREA WEB AT STA 987 LBL 50 CORRODED. GROUNDED - YES. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS, REMVOED AND REPLACED IAW B737-800 SRM 51-40-02-0G-0.Jul 29, 2026 · N569AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR SWAA2026090268410Plate · crackedCRACKED CORRUGATED PLATE ON TRAILING EDGE, BTWN ORSS 291 - ORSS 297, RT WING. REPLACED THE CORRUGATED PLATE IAW SRM 51-40-02-0G-0, & SRM 51-10-02-0G-0, STEP 9.Jul 29, 2026 · N8648A · Boeing 7378H4 · Wing Main, Frame StructureSDR SWAA2026090268219Access Panel · damagedELONGATED HOLES ON RT WING ACCESS PANEL 642BB. REPAIRED ACCESS PANEL 642BB IAW SRM 57-53-70-2R-4, REPAIR 4.Jul 29, 2026 · N8648A · Boeing 7378H4 · Wing, Plate/SkinSDR SWAA2026090280547Tie Clip · crackedCRACKED TIE CLIP, BS 277 STR 10R IN PAX CABIN. REPLACED TIE CLIP IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9, & DWG 141A1110, SHT 54, REV -.Jul 29, 2026 · N8648A · Boeing 7378H4 · Fuselage Miscellaneous StructureSDR SWAA2026090244558Plate · crackedCRACK CORRUGATED PLATE ON TRAILING EDGE LOCATED AT IRSS214 APPROX. RT WING. REPLACED CORRUGATED PLATE ON TRAILING EDGE LOCATED AT IRSS214 APPROX. RT WING IAW SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 115A2001 SHEET 78, REV A.Jul 29, 2026 · N8648A · Boeing 7378H4 · Wing Main, Frame StructureSDR SWAA2026083125153Floorbeam · corrodedCORROSION FLOORBEAM LOCATED ON BS 947 AT LEVEL LBL 25 AND WL 208.1 AT AFT GALLEY AREA 2026-456140 PERFORMED PERMANENT REPAIR LOCATED FLOOR BEAM 947.5 BTW LBL 0 TO LBL 50. I.A.W. B737-8 SRM 53-70-51-2R-5 REPAIR 5.Jul 29, 2026 · N8713M · Boeing 7378 · Fuselage Main, Floor BeamSDR SWAA2026083127160Stiffener · corrodedCORROSION FLOOR STRUCTURE STIFFENER ON BS 947 AT LEVEL LBL 52 AND WL 208.1 AT AFT GALLEY AREA 2026-456142 REPLACED STIFFENER (INTERCOSTAL) AND FASTENERS LOCATED BTW BS 947 TO BS967 AT LEVEL LBL 52 AND WL 208.1 AT AFT GALLEY AREA IAW B737-8 SRM-51-40-02 AND DWGJul 29, 2026 · N8713M · Boeing 7378 · Fuselage Miscellaneous StructureSDR AALA202608279231Shear Tie · corrodedAIRCRAFT IN BASE MAINTENANCE: GALVANIC CORROSION ON SHEAR TIE AT STA 867, LBL 8. MAINTENANCE REPLACED SHEAR TIEAT STA 867, LBL 8 IAW AARD 51-00-05-1.Jul 29, 2026 · N904AN · Boeing 737823 · Fuselage Internal Mounting StructureSDR NI6R202608260068Strut · wornRIGHT MLG SHOCK STRUT HAS DAMAGE FROM UPLOCK SWITCH, CHROME CHIPPED OFF TO BARE METAL. CHROME ON MLG STRUT ASSEMBLY HAS A DIVOT AT THE LOCATION WHERE UPLOCK PUSH BUTTON APPLIES FORCE TO PLUNGE THE BUTTON FOR GEAR UPLOCK NOTIFICATION. DIVOT BEYOND LIMITS PER CJul 29, 2026 · N115Z · Beech B200GT · Main Landing Gear Strut/Axle/TruckSDR NI6R202608260067Autothrottle Sys · disconnectedL1 AUTO THROTTLE INOP. LT CONTROL ROD FOUND NOT CONNECTED. HARDWARE DISCOVERED LOOSE AND SITTING AT LOW POINT OF BAY USING A BORESCOPE AND RETRIEVAL SUCCESSFUL USING MECHANICAL FINGERS. UNIT ORIGINALLY INSTALLED BY TEXTRON BY STC SA00400B0Jul 29, 2026 · N115Z · Beech B200GT · Auto Throttle SystemSDR HNAA2026082600795Strip · corrodedTAIL BOOM STRIP CORRODED. R & R STRIPS IAW AMM20-10-01 AND SB 145-55-0030Jul 29, 2026 · N925AE · Emb EMB145LR · Horizontal Stabilizer Miscellaneous StructureSDR ASAA2026072968163Shield · corrodedAFT PIT SHIELD FWD OF DOOR HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED AFT PIT SHIELD FWD OF DOOR, IAW B737-800 SRM 51-40-02-0G-0, STEP: 4.B & 5.B. (W: 1" / O: .050" / R: .040 / L: 2" / D: .010" ).Jul 29, 2026 · N531AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR R61A2026082400244Rib · crackedDURING HEAVY CHECK CRACK FOUND ON LT HORIZONEAL STAB RIB 14. REMOVED AND REPLACED RIB 14 IAW SRM 51-41-02Jul 29, 2026 · N213JQ · Emb ERJ170100LR · Fuselage Miscellaneous StructureSDR R61A2026082400243Floor Support · crackedDURING HEAVY CHECK AFT WET AREA FLOOR STRUCTURE, FR 85 RBL 28AND FR 86 LBL 28 THREE FLOOR SUPPORT FOUND CRACKED. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-41-01.Jul 29, 2026 · N213JQ · Emb ERJ170100LR · Fuselage Miscellaneous StructureSDR R61A2026082400242Bracket · crackedDURING HEAVY CHECK CF III INTERNAL RT OUTBOARD SEAT TRACK TO FRAME 84 BRACKET. REMOVED AND REPLACED R/H O/B SEAT TRACK IAW EMB 170/175 SRM 51-43-03 AND 51-41-01Jul 29, 2026 · N213JQ · Emb ERJ170100LR · Fuselage Main, Attach FittingsSDR R61A2026082400241Bracket · crackedDURING HEAVY CHECK CF III INTERNAL LT OUTBOARD SEAT TRACK TO FRAME 84 BRACKETS CRACKED. REMOVED AND REPLACED LT OTBD SEAT TRACK IAW SRM 51-43-03 AND 51-41-01.Jul 29, 2026 · N213JQ · Emb ERJ170100LR · Fuselage Miscellaneous StructureSDR R61A2026082400240Gusset · corrodedDURING HEAVY CHECK AFT WET AREA FLOOR STRUCTURE FR 91 RBL 25 GUSSET PLATE FOUND WITH CORROSION. REMOVED AND REPLACED GUSSET PLATE IAW EMB 170/175 SRM 51-41-02.Jul 29, 2026 · N213JQ · Emb ERJ170100LR · Fuselage Miscellaneous Structure