N255CM
Service difficulty reports · 245
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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' WHERE n_number = 'N255CM' AND registry_match = 'registration' 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' WHERE n_number = 'N255CM' AND registry_match = 'registration' 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 IXXA2022060216Stringer · corrodedSTRINGER 33R STA 1085-1101SDR IXXA2022060210Bracket · corrodedCORROSION ON BRACKET AT STA 1087SDR IXXA2022061311Web · corrodedFLOOR WEB CORRODEDSDR IXXA2022061309Stringer · corrodedSTRINGER FLANGE CORRODED STA 434SDR IXXA2022060808Shear Tie · corrodedFLC SHEAR TIE CORRODED STA 566SDR IXXA2022060205Structure · corrodedUPPER CHORD CORROSIONSDR IXXA2022060204Support Bracket · corrodedFLOOR BOARD BRACKET CORRODEDSDR IXXA2022053003Shear Tie · corrodedCORROSION FLC STA 434 SHEAR TIEBETWEEN STR 37R AND 38RSDR IXXA2022053002Shear Tie · corrodedCORROSION FLC STA 434 SHEAR TIE BETWEEN STR 39L AND 39RSDR IXXA2022051804Floor Panel · corrodedCORROSION FLC STA 588 RBL 2.5-7.5 FLOOR WEBSDR IXXA20220512101Floor Support · corrodedRT HAND SLOPE PANEL TO FLOOR SUPPORT FS1540 TO FS1409 RBL40 CORROSIONSDR IXXA20220507203Frame · corrodedCORROSION FLC STA 478 RBL 21 & RBL 28 FLOOR FRAME UPPER CHORD LWR SURFACESDR IXXA2022061310Support Bracket · corrodedCORROSION ON THE BULK CARGO CEILING SUPPORTSDR IXXA2022060803Ceiling Panel · corrodedALC CEILING PANEL SUPPORT CORRODEDSDR IXXA2022050607Beam · corrodedFWD LOWER CARGO DOOR BEAM BELOW VENT DOORS CORROSION AT 4 PLACES ON BEAMSDR IXXA2022053001Mount · crackedALC 8R PDU MOUNT CRACKEDSDR IXXA2022060206Lock Fitting · corrodedCORROSION ON LOWER SURFACE WING LOCK TRAYSDR IXXA2022060203Roller Tray · corrodedROLLER TRAY SUPPORT IS CORRODEDSDR IXXA2022051802Web · corrodedCORROSION ON LOWER SURFACE OF THE WING LOCK SUPPORT TRAY AT STA 1241 FROM LBL6 TO RBL20SDR IXXA2022051202Support Channel · corrodedTHE ROLLER TRAY SUPPORT IS CORRODED ON THE LOWER SURFACE, AT RBL20 FROM STA 1395 TO STA 1417SDR IXXA2022051203Support Channel · corrodedTHE ROLLER TRY SUPPORT IS CORRODED ON THE LOWER SURFACE AT RBL6 FROM STA 1395 TO STA 1417SDR IXXA2022050706Frame · corrodedCORROSION ON THE LOWER SURFACE OF THE UPPER FRAME CHORD, AT STA.1175 (ALC FLOOR LEVEL) FROM LBL42 TO RBL42SDR IXXA2022061314Cowling · dentedN0 1 ENGINE INBD TR UPPER SECTION AROUND BLOCKER DOOR HAS PUNCTURES AND DENTSSDR IXXA2022060811Cowling · cracked#1 ENGINE OB CORE COWL CRACKED AT LOWER CORNER OF VENT PANELSDR IXXA2022060807Stringer · corrodedCORROSION LH HORZ STAB INTERNAL 6" OB SID OF RIB 2L LWR #9 STRINGERSDR IXXA2022050901Tee Angle · corrodedCORROSION ON THE LOWER KEEL PANEL SUPPORT, CROSSMEMBER SUPPORT, AT STA.873.SDR IXXA2022040502Panel · crackedL/H FILLET PNL 195FL HAS COMPOSITE DAMAGESDR IXXA2022050608Skin · crackedW LES 948 LWR L/E CRACKEDSDR IXXA2022050606Intercostal · corrodedAFT CARGO DOOR HAS CORROSION ON #2,3,4 BEAM ASSY. FROM TOP OF DOOR AND ON INTERCOSTAL ON #4 BEAM ASSY. (INTERNAL SIDE)SDR IXXA2022040501Panel · crackedVERT STAB REMOVABLE L/E PANEL 321E MOST UPPER L/E COMPOSITE ERODED & CRACKEDSDR IXXA2022060804Shroud · corrodedCORROSION ON FIRE EXTINGUISHER SHOURDSDR IXXA20210124003Not Reported · not reportedIN THE ACCOMPLISHMENT OF EO 53-767-767-7487, STRUCTURAL FINDINGS WERE NOTED. AIRCRAFT GROUNDED FOR PAINT WORK IN PROGRESS.SDR IXXA20200223002Keelbeam · corrodedDURING KEEL BEAM INSPECTION PER ATI TASK S53-052-02, EXFOLIATION CORROSION IDENTIFIED AT PANEL 149BL, SEC 45, FS 999. AIRCRAFT GROUNDED FOR REPAIR. DAMAGE MEASURED AT 1.5 X 9/16. TOTAL BLEND OUT MEASURED 2.375 (L) X 1.125 (W) AND DEEPEST BLEND POINT MEASURED SDR IXXA20180617027Connector · dirtyPREDEPARTURE CHECK: FLIGHT COMPARTMENT EMERGENCY EXIT SINGLE LIGHT INOPERATIVE. GENERAL VISUAL INSPECTION. CLEANED AND SECURED CONNECTOR. OPERATIONAL CHECK SATISFACTORY IAW B767 AMM 33-51-01. FAULT NOT DUPLICATED. NO FURTHER DEFECTS NOTED. NO PREVIOUS HISTORY SDR IXXA20180421018Autopilot Sys · malfunctionedAT FL 370, CRUISE FLIGHT AUTOPILOT EICAS OFF. RE-ENGAGED THE AUTOPILOT EICAS OFF AGAIN. TRIED LEFT AND RIGHT AUTOPILOT, AUTOPILOT OFF QUICKER. CENTER ON AGAIN STAYED ON UNTIL DESCENT, H/S USED AUTOPILOT OFF, DESCENT TO FL 280, NON RVSM HAND ROLL DIFFICUSDR IXXA20180227010Stringer · corrodedHORIZONTAL STAB CONTROL BOX INTERNAL. CORROSION ON THE OTBD SIDE OF RIB 2L LOWER LT STRINGER 11, VERTICAL LEG FWD SIDE. INSTALLED A NEW HORIZONTAL STABILIZER STRINGER IAW SRM 31-40-02 & REA 47308 AB01. AIRCRAFT GROUNDED.SDR IXXA20180301012Bushing · corrodedLEFT LANDING GEAR H BLOCK DAMAGED BUSHINGS WITH CORROSION. REPAIRED L/H LANDING GEAR "H" BLOCK IAW REA 47308REA08 TO REMOVE CORROSION.SDR IXXA20180227009Strut · corrodedLEFT WING LEADING EDGE STRUT AT INBOARD END OF THE NR 5 SLAT TAI TELESCOPING DUCT CORRODED AROUND END OF DUCT. THE STRUT WAS REMOVED AND REPLACED IAW DWG 114T2201. AIRCRAFT GROUNDED.SDR IXXA20180227008Keelbeam · corrodedLEFT KEEL LOWER FLANGE UPPER SURFACE CORRODED AT BS 999. REPAIRED LOWER INBOARD KEEL FLANGE IAW SRM 53-50-12, REPAIR 1. AIRCRAFT GROUNDED.SDR IXXA20170228155Bracket · damagedDURING COMPLIANCE OF AD 2008-06-06: DETAILED INSPECTION AND LUBRICATION FOR THE DRIVE MECHANISM OF THE HORIZONTAL STABILIZER, FOUND LEFT HORIZONTAL STAB UPPER BODY FAIRING DOOR, INCLUDING ATTACH BRACKETS, DAMAGED. LINKAGE FOR THE HORIZONTAL STABILIZER TO BODY SDR IXXA20170228154Structure · damagedFOUND THE LEFT HORIZONTAL STAB UPPER BODY FAIRING DOOR, INCLUDING ATTACH BRACKETS, DAMAGED. REPAIRED IAW EO 53-767-5811.SDR IXXA20160818045Tee Fitting · corrodedRIGHT TEE FITTING IS CORRODED AT THE AFT LOWER BOLT HOLE. MATCH DRILLED NEW TEE FITTING IAW SRM 51-10-02. INSTALLED IAW ENGINEERING DOCUMENT 47008ORD04.SDR IXXA20160818047Strap · crackedAIRCRAFT GROUNDED FOR HEAVY MAINTENANCE. RIGHT FAILSAFE STRAP LOWER HOLE HAS CRACKED AT 10:00 POSITION, VERIFIED WITH HFEC SURFACE SCAN AND ROTARY SCAN. FAILSAFE STRAP TRIM OUT AND REPAIR ACCOMPLISHED IAW EA 47008ORD04.SDR IXXA20160818046Tee Fitting · corrodedLEFT TEE FITTING IS CORRODED AT THE AFT LOWER BOLT HOLE. A NEW TEE FITTING MATCH DRILLED IAW SRM 51-40-05. THE TEE FITTING WAS INSTALLED IAW ENGINEERING DOCUMENT 47008ORD03.SDR IXXA20160817044Failsafe · crackedLEFT FAILSAFE STRAP HAS CRACK INDICATION IN LOWER BOLT HOLE OF TRIM OUT AREA. FAILSAFE STRAP TRIM OUT AND REPAIRED IAW ENGINEERING DOCUMENT 47008ORD03.
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