Boeing 717-200
Service difficulty reports · 18,771
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 = '717200' 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 = '717200' 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 DALA2017100807369Cusp Web · corrodedCORROSION ON THE LOWER & UPPER SURFACES OF THE CUSP WEB BS 489. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 216.SDR DALA2017100807368Cusp Web · corrodedEXCESIVE CORROSION ON THE CUSP WEB RT LOWER & UPPER SURFACES BS 517, RBL 54 TO 60. REPAIRED IAW SRM 53-00-55-2R-4, FIG 216.SDR DALA2017100807367Seat Track · corrodedCORROSION ON THE SEAT TRACK RBL 22 AND SETTLEMENT AREA FROM BS 200 - 256. THE SEAT TRACK WAS REPLACED IAW SRM 51-41-01-0G.SDR DALA2017100807366Skin · crackedCRACKED SKIN AT BS 1022, LONGERON 14L. THE SKIN WAS REPAIRED IAW ER/A 560943-14, REV ORIGINAL, AND ETI-17-17-172, REV 2.SDR DALA2017100807365Skin · crackedCRACKED FUSELAGE SKIN AT BS 1037 LONGERON 14L. THE SKIN WAS REPAIRED IAW ER/A 560943-14, REV ORIG, AND ETI-17-17-178, REV 2.SDR DALA2017100807364Frame · crackedCRACKED FRAME CAP BS 1022, LONGERON 7L. THE DAMAGE FRAME CAP WAS REPAIRED IAW ER/A 560900-14, REV ORIGINAL AND ETI-17-17-176, REV ORIGINAL.SDR DALA2017100807363Skin · puncturedPUNCTURE IN THE LOWER SKIN ON THE AFT MOVABLE VANE OF THE RT WING TE FLAP. THE SKIN WAS REPAIRED IAW SRM 57-53-01-2R-1, PAR 4.SDR DALA2017100707362Skin · dentedDENT ON THE LT SIDE NEAR THE T/E OF THE RUDDER. THE RUDDER WAS REPAIRED IAW SRM 51-70-13-2R-1 PAR 4B.SDR DALA2017100707361Door Frame · crackedCRACKED RT NLG DOOR FRAME AT BS 47, LONGERON 27R. THE DOOR FRAME WAS REPAIRED IAW SRM 53-10-14-2R-2, 51-20-09-0G, 51-32-01-0G, SRM 51-41-02-0G, AND SRM 51-41-05-0G.SDR DALA2017100707360Door Frame · crackedCRACKED LEFT DOOR FRAME AT BS 47, LONGERON 27L OF NLG. THE LT NLG DOOR FRAME WAS REPAIRED IAW SRM 53-10-14-2R-2, 51-20-09-0G, 51-32-01-0G, SRM 51-41-02-0G, AND SRM 51-41-05-0G.SDR DALA2017100707359Floor Support · corrodedCORROSION ON FLOOR SUPPORT FROM BS 1025 - 1060, RBL 16. THE FLOOR SUPPORT WAS REPLACED IAW DWG 9936656-67, REV AM.SDR DALA2017100707356Cusp Web · corrodedCORROSION OUT OF LIMITS BS 541 - 560, LBL 44.5 AND LBL 60 ON THE CUSP WEB. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 215. HFEC INSPECTION WAS ACCOMPLISHED, NO CRACKS WERE FOUND AFTER TRIM OUT IAW NDT SPM 06-10-01.001.SDR DALA2017100707355Stop Fitting · crackedCRACKED STOP FITTINGS, LT LOWER AND MID POSITION, RT SIDE MID POSITION AT AFT EMERGENCY EXIT DOOR FRAME AREA BS 1053. HFEC INSPECTION WAS ACCOMPLISHED ON THE FITTING RT SIDE MID POSITION AND NO CRACKS WERE FOUND IAW NDT SPM, PART 6, 06-10-01.001. STOP FISDR DALA2017100607324Floor Support · corrodedCORROSION ON FLOOR SUPPORT BS 167, RBL 11. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-05, AND SRM 51-40-08.SDR DALA2017100607323Longeron · crackedCRACKED LONGERON 2L, BS 1133. THE LONGERON WAS REPAIRED IAW SRM 53-00-05 2R-2.SDR DALA2017100507322Support · corrodedCORROSION ON SLIDE LATCH SUPPORTS BS 160 TO 200, RBL 54 AT R1 FLOOR PANEL. THE LATCH SUPPORTS WERE REPLACED IAW SRM 51-40-08-0G, PAR 3.SDR HALA2017100400250O-Ring · leakingATB, RIGHT HYDRAULIC QUANTITY LEAK. REPLACED LT BUNGEE CYLINDER ACTUATOR O-RING.SDR DALA2017100507287Floorbeam · corrodedCORROSION ON FLOOR SUPPORTS STA Y=180 X=38 TO X=13 AND X=-9 TO -43 (2EA). CORROSION LEVEL 2. FLOOR SUPPORTS STA Y=180 X=38 TO X=13 AND X=-9 TO -43 WERE REPLACED PER SRM 51-40-08-0G AND 51-41-02-0G.SDR DALA2017100507286Cusp Web · crackedCRACKED CUSP WEB ON STA Y=662 AND X=-54 AT PAX CABIN REF NRC 00349 (CPAX). CUSP WEB WAS REPAIRED PER SRM 53-00-55-2R-4 FIG 206 AND SRM 51-41-02-0G AND 51-41-05-0G.SDR DALA2017100507285Support · corrodedCORROSION ON LOWER EPC SUPPORT STA Y=-160X=14 TO X=54. CORROSION LEVEL 2 LOWER EPC SUPPORT STA Y=-160 X=14 TO X=54. WAS REPLACED PER SRM 51-41-02-0G AND 51-41-01-0G AND DWG 9955780 REV LA.SDR DALA2017100507284Pan · crackedCRACK ON INNER PAN BETWEEN THE NR 1 BEAM AND FWD UPPER CORNER AT L1 DOOR. THE PAN WAS REPAIRED IAW SRM 52-10-02-2R-3 FIG.201.SDR DALA2017100507283Floorbeam · crackedCRACKED FLOORBEAM BS 737, RBL 54. THE FLOORBEAM WAS REPLACED IAW SRM 51-41-05-0G.SDR DALA2017100507282Beam · crackedCRACK ON THE NR 1 BEAM AFT EDGE AT THE L1 DOOR. THE BEAM WAS REPAIRED IAW SRM 52-10-02-2R, PROCEDURE 7, FIG 20.SDR DALA2017100507281Shear Tie · crackedCRACKED SHEAR TIE BS 1022, LONGERONS 6R TO 7R. THE SHEAR TIE WAS REPLACED SRM 51-41-02-0G, SRM 51-20-09-0G, SRM 51-41-05-0G, AND DWG 9912243, REV HF.SDR DALA2017100507280Shear Tie · crackedCRACKED SHEAR TIE BS 1022, LONGERONS 13 TO 14L AND RT. THE SHEAR TIE WAS REPLACED IAW DWG 9912243, REV JB, SRM 51-20-09-0G, 51-41-02-0G, AND 51-41-05-0G.SDR DALA2017100407278Floor Support · corrodedCORROSION ON FLOOR SUPPORT BS BS 200 LBL 14. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-08-0G, AND 53-10-51-0I-2, FIG 1.SDR DALA2017100407277Floor Support · corrodedCORROSION ON FLOOR SUPPORT BTW BS 147 - 200, RBL 7. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-40-08-0G, 51 41-01, AND 51-10-04-0G. PAR 26, 15, AND 21.SDR DALA2017100407255Seat Track · corrodedCORROSION ON RT SEAT TRACK X=-44.5 FROM STA Y=200 TO Y=237 REF NRC S/N 130 (W1). LEVEL CORROSION 2, SEAT TRACK WAS REPAIRED PER SRM 53-20-52-2R-5 FIG 201.SDR DALA2017100407254Floor Support · corrodedCORROSION ON FLOOR SUPPORTS STA Y=195-200 X=54, X=14 (2EA) 5300-2010)(W1). LEVEL CORROSION 2. SUPPORT WAS REPLACED PER SRM 51-40-08-0G.SDR DALA2017100407253Tab · scratchedSCRATCHES ON RUDDER CONTROL TAB RT SIDE. RUDDER CONTROL TAB WAS REPAIRED PER SRM 51-70-02-2R PROCEDURE 1 AND CARD 2000-8149-01.SDR DALA2017100307226Former · crackedCRACKED FORMER ON BS 715 AT KEELBEAM. THE FORMER WAS REPAIRED IAW SRM 53-00-00-2R-1- AND 51-41-02.SDR DALA2017100307225Former · crackedCRACKED FORMER BS 737 AT THE KEEL BEAM AREA. THE FORMER WAS REPAIRED IAW SRM 53-00-00-2R-1, AND 51-41-02.SDR DALA2017100307224Former · crackedCRACKED FORMER AT BS 694 KEEL BEAM AREA. THE FORMER WAS REPAIRED IAW SRM 53-00-00-2R-1, AND 51-41-02.SDR DALA2017100307221Beam · crackedCRACKED NR 4 BEAM ON FWD RIGHT GALLEY DOOR. THE BEAM WAS REPLACED IAW SRM 51-41-01, 51-41-02, AND 51-41-05.SDR DALA2017100207190Web · corrodedCORROSION ON WEB LOWER SURFACE FROM BS 198 TO 202, BL 0 AND RBL 26, AND RBL 44 IN THE E & E BAY. THE WEB WAS REPAIRED IAW SRM 51-70-10-2R-2, 51-41-02-0G, AND 51-41-08-0G.SDR DALA2017100207189Skin · damagedVERTICAL STAB VSS 52, UPPER ROWS EIGHT FASTENERS COUNTERSINK HOLE OVERSIZED. REPAIRED THE VERTICAL STAB SKIN IAW SRM 55-30-01-2R-6, REPAIR 6, AND DWG SG95550001, REV ORIG.SDR DALA2017100207188Vane · dentedDISBOND WAS FOUND ON DENTS AT AFT MOVABLE FLAP VANE LOWER SURFACE, ON THE LT WING. REPAIRED IAW SRM 57-53-01-2R-1.SDR DALA2017100207187Vane · debondedDISBONDING WAS FOUND ON DENTS AT THE INBD FIXED FLAP VANE LOWER SKIN XRS=137 OF THE RT WING. REPAIRED IAW SRM 57-53-01-2R-1.SDR DALA2017100207186Vane · debondedTHREE DISBONDS WERE FOUND AT OTBD FLAP FIXED VANE UPPER SURFACE OF THE LT WING. REPAIRED IAW SRM 57-53-01-2R-1, AND JIC 5552700.SDR DALA2017100207185Cusp Web · crackedCRACKED CUSP WEB, BS 440 - 601, BETWEEN RBL 54 - 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 215.SDR DALA2017100207176Skin · damagedVERTICAL STAB HAS 4 FASTENER HOLES WORN OUT OF LIMITS AT LEADING EDGE. REPAIRED IAW SRM 55-30-01-2R-6, REPAIR 6, AND DWG SG95550001, REV ORIG.SDR DALA2017100207217Web · corrodedCORROSION DIAPHRAGM FROM BS 190 TO 200, LBL 53 - 55. THE DIAPHRAGM WAS REPAIRED IAW SRM 51-70-10-2R-2, AND SRM 53-10-51-OI-2.SDR DALA2017100107184Rub Strip · crackedCRACK ON THE RT WING LEADING EDGE AILERON RUBSTRIP UPPER SURFACE XRS 410. THE RUBSTRIP WAS REPLACED IAW SRM 51-41-02-0G, AND DWG 9957571, REV Z.SDR DALA2017100107183Angle · crackedCRACK ON ANGLE BELOW THE NR 1 BEAM, AFT EDGE. R1 DOOR. THE ANGLE WAS REPLACED IAW DWG 9911579, REV L, SRM 51-41-01, AND 51-41-05.SDR DALA2017100107182Cusp Web · corrodedCORROSION ON THE RT CUSP WEB BS 923, BETWEEN LBL 54 TO 58. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, REPAIR 4, FIG 215.SDR DALA2017100107181Fitting · crackedCRACK IN UPPER PAN FITTING NEAR BS 974 AT THE AFT CARGO DOOR. THE FITTING WAS REPLACED IAW SRM 51-41-04, AND 51-41-05, PARAGRAPH 10.SDR DALA2017100207191Lens · missingCABIN STANDBY LIGHT AT SEAT 15 ABC MISSING THE LENS. REPLACED THE OVERHEAD EMERGENCY LIGHT ASSY IAW AMM 33-51. PERFORMED AN OPS TEST IAW AMM 33-51. OPS TESTED OK.SDR DALA2017093007180Pan · crackedCRACK ON THE LT UPPER, AFT CORNER OF WINDOW RING PAN BS 832 AND 870. REPAIRED IAW 56-20-02-2R.SDR DALA2017093007179Longeron · crackedCRACKED LONGERON 10R, BS 908. REPAIRED THE LONGERON IAW SRM 53-00-05-2R-2, FIG 201.SDR DALA2017100407288Drive Assy · damagedTHE CREW EXPERIENCED AN UN-COMMANDED ROLL WHEN THEY SELECTED THE SLATS TO EXTEND. MAINTENANCE FOUND THAT THE RIGHT WING INBOARD LEADING EDGE SLAT DRIVE WAS DAMAGED. THE DRIVE WAS REPLACED AND A FUNCTIONAL TEST FLIGHT WAS ACCOMPLISHED.
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