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 DALA2018030901521Pan · crackedCRACKED LT RING PAN BS 617, LOWER FWD CORNER. THE RING PAN WAS REPAIRED IAW SRM 56-20-02-2R1.SDR DALA2018030901520Pan · crackedCRACKED LT RING PAN BS 636 UPPER AND LOWER FWD CORNER. THE PAN WAS REPAIRED IAW SRM 56-20-02-2R1.SDR DALA2018030901519Pan · crackedCRACK ON THE RT RING PAN BS 522 LOWER AFT CORNER. THE PAN WAS REPAIRED IAW SRM 56-20-02-2R1.SDR DALA2018030901518Floor Panel · crackedCRACKED CHANNEL OF FLOOR PANEL: THE FLOOR PANEL WAS REPAIRED IAW SRM 53-20-50-2R-5, REPAIR 5.SDR DALA2018030901517Pan · crackedCRACKED RT RING PAN BS 636 LOWER, FWD CORNER: THE PAN WAS REPAIRED IAW SRM 56-20-02-2R1.SDR DALA2018030901516Web · crackedCRACKED WEB BETWEEN BEAMS 4 & 5, THE WEB WAS REPLACED IAW SRM 51-41-02, 51-41-05, AND DWG 9955763, REV M.SDR DALA2018030801515Former · crackedCRACKED LT AND RT FORMERS AT BS 679. THE FORMERS WERE REPAIRED IAW SRM 53-00-06-2R-2.SDR HALA2018030800072Slide · partial deployPARTIAL MAIN CABIN DOOR SLIDE DEPLOYMENT AT GATE. REPLACED MAIN DOOR SLIDE IAW AMM 25-61-01, SECURITY CHECKED GOOD. OK FOR SERVICE.SDR DALA2018030801486Access Panel · corrodedCORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS PLATES 520GB. CORROSION LEVEL 2, DUE TO EXCESSIVE DAMAGE BY CORROSION ON FUEL ACCESS PLATE 520GB WAS REPLACED PER SRM 57-10-01 REPAIR 2 PAR 5 CONDITION II (A AND B) AND VERIFIED PER IPC 57-23-01SDR DALA2018030801485Cusp Web · crackedCRACK ON CUSP WEB FROM STA Y=655 TO Y=674 BTW X-54 TO X-60 RT SIDE AT PAX CABIN. CUSP WEB WAS REPAIR ON FROM STA Y=655 TO Y=674 BTW X-54 TO X-60 RT SIDE AT PAX CABIN REPAIR PER SRM 53-00-55 REPAIR 4.SDR DALA2018030801484Beam · crackedCRACKED BEAM 1 STA Y=170 AT FWD SERVICE DOOR. BEAM 1 WAS REPLACED PER SRM 51-41-02-0G AND DWG 9911579 REV L.SDR DALA2018030801483Floor Panel · damagedCRACK IN CHANNEL, ALSO BENT CHANNEL AND SKIN OF FLOOR PANEL 222AQF AND 222XF. FLOOR PANELS WERE REPAIRED (PERMANENT REPAIR) PER SRM 51-20-09-0G, SRM 53-20-50-2R-5, & SRM 51-41-02-0G.SDR DALA2018030801481Lanyard · damagedBROKEN STRANDS ON L1 AND R1 EMERGENCY SLIDE LANYARDS. LANYARDS WERE REPLACED PER AMM 25-61-01 400-801.SDR DALA2018030801480Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA Y=180 BTW X=-44 TO X=-9 5300-2010 (W1). CORROSION LEVEL 2, FLOOR SUPPORT STA Y=180 BTW X=-44 TO X=-9 WAS REPLACED PER SRM 51-41-02.SDR DALA2018030801479Support · wornWEAR ON RT SUPPORT ATTACHED TO PAN [LOWER AREA] AT AFT CABIN BULKHEAD EMERGENCY EXIT DOOR. RT SUPPORT ATTACHED TO PAN [LOWER AREA] AT AFT CABIN BULKHEAD EMERGENCY EXIT DOOR WAS REPAIRED PER SRM 52-10-02-2R REPAIR 16.SDR DALA2018030801478Former · crackedCRACKED LT AND RT FORMERS ON STA Y=715 AT KEEL BEAM AREA. LT AND RT FORMERS ON STA Y=715 AT KEEL BEAM AREA WERE REPAIRED (PERMANENT REPAIR) PER SRM 53-00-06-2R-2.SDR DALA2018030801477Access Panel · crackedCRACK ON FUEL ACCESS PLATES 520CB. FUEL ACCESS PLATE WAS REPLACE PER IPC 57-23-01-01 ITEM 442J.SDR DALA2018030801476Former · crackedCRACKED LT AND RT FORMERS ON STA Y=694 AT KEEL BEAM AREA. LT AND RT FORMERS ON STA Y=694 AT KEEL BEAM AREA WERE REPAIRED (PERMANENT REPAIR) PER SRM 53-00-06-2R-2.SDR DALA2018030801475Skin · crackedCRACKS ON REMOVABLE LEADING EDGE SKIN, STA ZFS=53 AT VERTICAL STABILIZER (EHV). REMOVABLE LEADING EDGE SKIN, STA ZFS=53 WAS REPAIRED PER SRM 55-30-01-2R-8.SDR DALA2018030801474Floor Support · corrodedCORROSION ON FLOOR SUPPORT FROM STA Y=1043 TO Y=1053 X=54. LEVEL CORROSION 2, SUPPORT WAS REPLACED PER SRM 51-41-02-0G AND 51-41-05-0G.SDR DALA2018030801473Access Panel · corrodedCORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS PLATES 520CB. CORROSION LEVEL 2, DUE TO EXCESSIVE DAMAGE BY CORROSION FUEL ACCESS PLATE 520CB WAS REPLACED AND VERIFIED PER IPC 57-23-01-01 ITEM 465J.SDR DALA2018030801472Longeron · crackedCRACK ON LONG 8 RT STA Y=1022 AT CPAX. LONGERON 8R WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-00-05-2R, 51-41-02-0G, & 51-41-05-0G.SDR DALA2018030701457Access Panel · crackedA CRACK WAS CONFIRMED IAW NDTSPM PART 6, 06-10-01.001 ON ACCESS PANEL 620EB, RT WING. THE ACCESS PANEL WAS REPLACED IAW AMM 28-00-00. A LEAK CHECK WAS PERFORMED IAW AMM 28-00-00. NO LEAKS FOUND.SDR DALA2018030701456Frame · crackedCRACKED FRAME, BS 1225, BETWEEN 6 AND 7 HRS. THE FRAME WAS REPLACED IAW SRM 51-41-02 AND 51-40-08.SDR DALA2018030701455Skin · crackedCRACKED SKIN, BS 1087, BETWEEN LONGERONS 13 AND 14R. REPAIRED THE SKIN IAW ER/A 566384-14, REV ORIGINAL, AND ETI-17-014, REV 1.SDR DALA2018030701454Longeron · crackedCRACKED LONGERON 5L, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.SDR DALA2018030701453Longeron · crackedCRACKED LONGERON 8L, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.SDR DALA2018030701451Fitting · crackedCRACKED FITTING BETWEEN BEAMS 4 & 5, AFT EDGE AT AFT CARGO DOOR. THE FITTING WAS REPLACED IAW SRM 51-41-01-0G, AND 51-41-05-0G.SDR DALA2018030601405Channel · crackedCRACKED CHANNELS OF FLOOR PANEL 222AFF AND FLOOR PANEL P/N 9952521U187. PERMANENT REPAIR. FLOOR PANEL 222AFF AND FLOOR PANEL P/N 9952521U187 WERE REPAIRED PER SRM 53-20-50-2R FIG 102. INSPECTION WAS ACCOMPLISHED ON FLOORS PANELS 222AFF AND P/N 9952521U187. NO SDR DALA2018030601404Frame · gougedGOUGE ON THE UPPER SURFACE OF THE AFT HORIZONTAL LEG OF CANTED FRAME STA 1145 RT SIDE APPROX RBL 4-6. NRC 001-0253:5300-2004/005 00214: 566363-14 REV 1 AND ER/A 566363-14 REV O MATCH WORK COMPLIED WITH PER ER/A 566363-14 REV O.SDR DALA2018030601403Frame · gougedGOUGE ON THE UPPER SURFACE OF THE AFT HORIZONTAL LEG OF CANTED FRAME STA 1145 LT SIDE APPROX LBL 4-7. NRC 001-0253:5300-2004/004 00213: PRI 566363-14 REV 1 AND ER/A 566363-14 REV O MATCH. WORK WAS PERFORMED PER ER/A 566363-14 REV O.SDR DALA2018030601402Pan · crackedCRACK UPPER PAN, MID SECTION ON FWD CARGO COMPARTMENT DOOR. UPPER PAN ON MID SECTION WAS REPAIRED PER SRM 52-30-02-2R.SDR DALA2018030601401Cusp Web · crackedCRACK WAS FOUND ON CUSP WEB HOLE STA Y=480 BTW X=-54/-60 DURING CORROSION REMOVAL AT CAB PAX. CRACK WAS BLENDED OUT PER SRM 53-00-00-1A FIG. 101 (ET) HFEC INSPECTION WAS PERFORMED ON CUSP WEB HOLE STA Y=480 BTW X=-54/-60 AT CAB PAX ON BLEND OUT. NO CRACKS WERESDR DALA2018030601400Frame · crackedCRACK ON FRAME STA Y=1022 LONG 7R AT PASSENGER CABIN. DAMAGE AREA WAS REPAIRED PER ER/A 566385-14 REV ORIGINAL AND ETI-17-18-015 REV ORIGINAL. HFEC INSPECTION WAS ACCOMPLISHED ON FRAME STA Y=1022 LONG 7R AT PASSENGER CABIN AND 2EA CRACKS WERE DELIMITED WITH FOSDR DALA2018030601399Fitting · crackedCRACK ON SHEAR CLIP STA Y=1022 BTW LONG 13R TO 14R AT CPAX. SHEAR CLIP WAS REPLACED PER SRM 53-00-06-2R-2 AND DWG 9912243 REV JS.SDR DALA2018030601398Fitting · crackedCRACK SHEAR CLIP STA Y=1022 BTW LONG 13L TO 14L AT CPAX. SHEAR CLIP WAS REPLACED PER SRM 53-00-06-2R-2 AND DWG 9912243 REV JS.SDR DALA2018030601397Skin · corrodedCORROSION ON CENTER FUEL TANK LOWER SKIN STA Y=747 X=-23 AT RT WHEEL WELL. CORROSION LEVEL 2, CORROSION WAS REWORKED PER ER/A 566336-14AD REV ORIGINAL AND ETI-17-18-018 REV 1. PER ER/A 566336-14AD REV ORIGINAL SECTION DTE.SDR DALA2018030601396Angle · wornWEAR ON LT ANGLE ATTACHED TO PAN [LOWER AREA] AT AFT CABIN BULKHEAD EMERGENCY EXIT DOOR. ANGLE WAS REPLACE PER SRM 51-41-04-0G, 51-41-05-0G, 51-41-02-0G, AND DWG 9929480 REV BW.SDR DALA2018030601395Cusp Web · crackedA CRACK WAS FOUND ON THE CUSP WEB BTW STA Y=370 AND 389 X=-58 DURING CORROSION REMOVAL AT CAB PAX. CUSP WEB BTW STA Y=370 AND 380 X=-58 WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-00-55-2R-4., 51-41-02-0G.SDR DALA2018030501394Plate · corrodedCORROSION ON AFT LT LAVATORY FLOOR AREA STA Y=1073 X=22 Z=-1. CORROSION LEVEL 2, PLATE WAS REPLACED PER SRM 51-41-05-0G.SDR DALA2018030501393Longeron · crackedCRACK ON LONG 4 LT STA Y=1022 AT CPAX. LONG 4 LT STA Y=1022 AT CPAX WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-00-05-2R.SDR DALA2018030501392Longeron · crackedCRACK ON LONG 6 LT STA Y=1022 AT CPAX. LONG 6 LT STA Y=1022 AT CPAX WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-00-05-2R.SDR DALA2018030501391Longeron · crackedCRACK ON LONG 13 RT STA Y=1037 AT CPAX. CRACK ON LONG 13 RT STA Y=1037 AT CPAX WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-00-05-2R-2 FIG 201.SDR DALA2018030501390Cusp Web · corrodedCORROSION ON LT CUSP WEB IN STA Y=877 TO Y=889, AND X=54 TO X=60. CORROSION LEVEL 2, CUSP WEB WAS REPAIRED (PERMANENT REPAIR) PER SRM 53-00-55-2R-4 FIG 211 SHEET 1 AND FIG 215 SHEET 1.SDR DALA2018030501389Beam · crackedCRACK ON BEAM NR 4 FWD EDGE AT FWD GALLEY SERVICE DOOR. BEAM NR 4 FWD EDGE AT FWD GALLEY SERVICE DOOR WAS REPLACED PER SRM 51-41-02 AND 51-41-05.SDR DALA2018030501388Fitting · crackedCRACKED INTERNAL FITTING STA Y=994 BEAM 4, ALSO INTERNAL FITTING Y=954 BEAM 2 AT AFT CARGO COMPARTMENT DOOR. FITTINGS STA Y=994 AND Y=954 WERE REPLACED PER SRM 51-41-01-0G, 51-41-05-0G, AND DWG 9957665 REV R.SDR DALA2018030501387Beam · crackedCRACK ON BEAM NR 1 FWD EDGE AT PASSENGER ENTRANCE DOOR. CRACK ON BEAM NR 1 FWD EDGE AT PASSENGER ENTRANCE DOOR WAS REPAIRED PER SRM 52-10-02-2R-7 FIG 202.SDR DALA2018030501386Beam · crackedCRACK ON BEAM NR 1 AFT EDGE AT PASSENGER ENTRANCE DOOR. CRACK ON BEAM NR 1 AFT EDGE AT PASSENGER ENTRANCE DOOR WAS REPAIRED PER SRM 52-10-02-2R-7 FIG 201.SDR DALA2018030901587Access Panel · damagedCRACK AND DENTS ON AILERON ACCESS PANEL 530HA, LT WING. REPAIRED IAW ER/A 566323-14 REV. ORIGINAL ASSOCIATED ER/A 00-566323.SDR DALA2018030501384Beam · crackedCRACK ON BEAM NR 6 MID SECTION AT THE PASSENGER DOOR. REPAIRED IAW ER/A 559578-14MA, REV ORIGINAL.
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