Boeing 727-212
Service difficulty reports · 405
Newest first. 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' WHERE aircraft_model_key = '727212' 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 aircraft_model_key = '727212' 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 2011FA0000026Stringer · corrodedSTRINGER 30R CCORRODED ON LOWER SIDE AT BS 1013.SDR 2011FA0000025Shear Tie · corrodedSHEAR TIE CORRODED AT STA 420 BETWEEN STR 28L AND 28R.SDR 2010FA0000187Battery Pack · inoperativeCENTER CABIN EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK.SDR FY4Y197M20100129Spar · corrodedTHE ACFT INPUT FOR 6C CHECK ON DEC 10, 2009. DURING CPCP INSP, THE INSPECTOR PERFORMED VISUAL INSP AND FOUND LEVEL 2 CORROSION ON RT WING FRONT SPAR LOWER CHORD AT WS 727.5. THE CHORD THICKNESS OF ORIGINAL IS 0.103". THE THICKNESS OF CORROSION REMOVED IS 0SDR FY4Y197M20100201Spar · crackedACFT INPUT FOR 6C CHK ON DEC 10, 2009. DURING CPCP INSP, THE INSPECTOR PERFORMED VISUAL INSP AND FOUND LEVEL 2 CORROSION ON LT WING FRONT SPAR WEB BETWEEN WS 508 AND WS 517; LENGTH:3.75"; WIDTH:2.5"; THICKNESS OF ORIGINAL: 0.370"; THICKNESS OF CORROSION REMSDR 2010FA0000078Spar · corrodedTHE ACFT INPUT FOR 6C CHK ON DEC 10, 2009. DURING VISUAL INSP BY INSPECTOR, THE LEVEL 2 CORROSION WAS FOUND ON RT WING FRONT SPAR LOWER CHORD AT WS 727.5. THE CHORD THICKNESS OF ORIGINAL IS 0.103". THE CHORD THICKNESS OF CORROSION REMOVED IS 0.040". PHOTO SDR 2010F00009Spar · corrodedTHE ACFT INPUT FOR 6C CHK ON DEC 10, 2009. DURING CPCP, THE INSPECTOR PERFORMED VISUAL INSP AND FOUND LEVEL 2 CORROSION ON LT WING FRONT SPAR WEB BETWEEN WS 508 AND WS 517; LENGTH:3.75"; WIDTH:2.5"; THICKNESS OF ORIGINAL:0.370"; THICKNESS OF CORROSION REMOVEDSDR 2010F00008Skin · corrodedDURING CPCP, THE INSPECTOR PERFORMED VISUAL INSPECTION AND FOUND LEVEL 2 CORROSION ON SKIN OF FWD CARGO DOOR CUTOUT AFT LOWER CORNER STA: BS620 S26R. AFTER APA (OWNER) VERIFY AS A MAJOR REPAIR ON JAN 29, 2010, THE SKIN CORROSION HAS BEEN REPAIRED IAW DER APPRSDR 2010F00007Skin · corrodedDURING CPCP, THE INSPECTOR PERFORMED VISUAL INSPECTION AND FOUND LEVEL 2 CORROSION ON SKIN OF FWD CARGO DOOR CUTOUT AFT LOWER CORNER STA: BS 620 S26R. AFTER APA (OWNER) VERIFY AS A MAJOR REPAIR ON JAN 29, 2010, THE SKIN CORROSION HAS BEEN REPAIRED IAW FAA DERSDR 2010F00000Spar · corrodedDURING CPCP, THE INSPECTOR PERFORMED VISUAL INSPECTION AND FOUND CORROSION ON RT WING FRONT SPART LOWER CHORD PLATE AT WS 482. AFTER REPAIRING TO THE FRON SPAR LOWER CHORD PLATE, FORM 337 WILL BE SUBMITTED TO FAA FOR FINAL RESULT OF CORRECTIVE ACTIONS DETAIL.SDR I5PA20090719Line · crackedAFTER 30 MINUTES OUT, CREW CALLED IN DUE TO RAPID LOSS OF OIL QUANTITY ON NR 1 ENGINE. ON LANDING, OIL QUANTITY INDICATED 1.5 GALLONS. MX RAN ENGINE, FOUND LEAK IN TAIL PIPE, FOUND SCAVENGE LINE NR6 BEARING LEAKING. REMOVED AND REPLACED SCAVENGE LINE. ALSOSDR R5KB16027Floorbeam · corrodedSTA 1130, RBL 51, FLOORBEAM CHORD CORRODED.SDR R5KB16005Frame · dentedSTA. 680, STR 23R TO 24R, FRAME DENTEDSDR R5KB16004Frame · dentedSTA 660, STRINGER 24R, FRAME DENTED.SDR R5KB15983Frame · corrodedSTA 340, RBL 19 TO RBL24, FRAME CORRODEDSDR R5KB15982Shear Tie · corrodedSHEAR TIE CORRODED STA 350 FROM RBL 19 TO RBL 24.SDR R5KB15862Structure · corrodedRBL 16, STA 350, BILGE AREA, LOWER CHORD CORRODED.SDR R5KB15798Floorbeam · corrodedUPPER FLOORBEAM CORRODED FS 1070, LBL 56.SDR R5KB15789Frame · corroded1/2 INCH CRACK IN FRAME AT STA 580 ABOVE FWD SERVICE DOOR.SDR R5KB15756Seat Track · corrodedLBL 44, SEAT TRACK CROWN CORRODED FROM STA 760 TO 848.SDR R5KB15651Frame · dentedFRAME AT STA 26 LEFT DENTED.SDR R5KB15650Frame · dentedFRAME AT STATION 950 DENTED.SDR R5KB15752Hinge · corrodedTOP OF ELEVATOR HINGE CHORD CORRODED FROM STA 70 THRU 170.SDR R5KB15652Frame · dentedFRAME AT STATION 950 DENTED.SDR R5KB15981Structure · corroded'T' CHORD AT STA 350 CORRODED.SDR R5KB15950Beam · corrodedLOWER BEAM CORRODED.SDR R5KB15945Beam · corrodedTAIL SKID TRANSVERSE BEAM FWD ATTACH ANGLE CORRODED.SDR R5KB15936Floor Support · corrodedFLOOR SUPPORT CORRODED.SDR R5KB15776Web · corrodedSUB FLOOR CORRODEDSDR R5KB15774Channel · corrodedHAT CHANNEL CORRODEDSDR R5KB15927Floorbeam · corrodedFLOOR BEAM UPPER CHORD CORRODED AT NUTPLATE.SDR R5KB15916Angle · corrodedVERTICAL ANGLE CORRODED.SDR R5KB20081220001Web · corrodedWEB CORRODED AT BS 1213 WL 177 RBL 5.SDR R5KB15914Beam · corrodedTRANSVERSE BEAM AT TAIL SKID CORRODED.SDR R5KB15838Web · crackedVERTICAL WEB CRACK AT LIGHTNING HOLE.SDR R5KB15825Seat Track · corrodedSEAT TRACK FLANGE CORRODED.SDR R5KB15808Web · corrodedUNDER FLOOR WEB CORRODED.SDR R5KB15807Web · corrodedSUBFLOOR WEB CORRODED AFT LAV.SDR R5KB15804Floor Support · corrodedFLOOR SUPPORT EXTRUSION CORRODED.SDR R5KB15803Seat Track · corrodedSEAT TRACK CORRODED.SDR R5KB15791Seat Track · corrodedSEAT TRACK CORRODED.SDR R5KB081218001Seat Track · corrodedSEAT TRACK CORRODED BS 1130.SDR R5KB15779Seat Track · corrodedSEAT TRACK CROWN CORRODED.SDR R5KB15795Seat Track · corrodedSEAT TRACK CORRODED.SDR R5KB15785Seat Track · corrodedSEAT TRACK CROWN AND FLANGE CORRODEDSDR R5KB15784Seat Track · corrodedSEAT TRACK CROWN CORRODED.SDR R5KB15781Seat Track · corrodedSEAT TRACK FLANGE CORRODED.SDR R5KB15782Seat Track · corrodedSEAT TRACK CORRODED.SDR R5KB15750Hinge Fitting · corrodedELEVATOR UPPER HINGE CORD CORRODED.SDR R5KB15678Floorbeam · damagedFLOORBEAM WEB DAMAGED BELOW UPPER CHORD, STA 460, RBL-25.
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