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 DALA2018031201623Access Panel · corrodedCORROSION OUT OF LIMITS ON ACCESS PANEL 620AT. THE ACCES PANEL WAS REPLACED IAW SRM 57-10-01-2R-2, PAR 5.SDR DALA2018031201622Door Frame · crackedCRACKED NLG DOOR FRAME, RT SIDE. THE DOOR FRAME WAS REPAIRED IAW SRM 53-10-14-2R-2. HFEC WAS ACCOMPLISHED, NO CRACKS WERE FOUND AT THE TRIMMED OUT AREA IAW NDT SPM PART 6, 06-10-01.SDR DALA2018031201621Door Frame · crackedCRACKED DOOR FRAME AT THE NLG LT SIDE. THE DOOR FRAME WAS REPAIRED IAW SRM 53-10-14-2R-2. HFEC WAS ACCOMPLISHED, AND NO CRACKS WERE FOUND AT THE TRIMMED OUT AREA IAW NDT SPM PART 6, 06-10-01.SDR DALA2018031201619Web · crackedCRACKED WEB BS 208, LONGERON 15L. THE WEB WAS REPAIRED IAW SRM 53-10-15-2R, PR 4. HFEC INSPECTION PERFORMED AND NO CRACKS WERE FOUND AT THE TRIMMED OUT AREA IAW NDT SPM 06-10-01.001.SDR DALA2018031201618Cusp Web · crackedCRACKED CUSP WEB BS 219, LBL 54. THE CUSP WEB WAS REPAIRED IAW SRM 51-70-10-2R. HFEC INSPECTION WAS PERFORMED AT THE TRIMMED OUT AREA. NO CRACKS WERE FOUND IAW NDT SPM PART 6 06-10-01.001.SDR DALA2018031201617Angle · crackedCRACKED ANGLE AT THE RT FWD EMERGENCY EXIT DOOR UPPER BEAM FWD EDGE. THE ANGLE WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND DWG 9957735, REV G.SDR DALA2018031201616Angle · crackedCRACKED ANGLE AT THE FWD CARGO DOOR BETWEEN THE UPPER EDGE AND BEAM 1 AND NEXT TO AFT HINGE. THE ANGLE WAS REPLACED SRM 51-41-02, 51-41-05, AND DWG 9957664, REV N.SDR DALA2018031201615Cusp Web · corrodedCORROSION ON THE RT CUSP WEB BS 389, RBL 54. THE CUSP WEB WAS REPAIRED IAW SRM 51-70-10-2R -2, FIG 201. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND ON TRIMMED OUT AREA IAW NDT SPM 06-10-01.SDR DALA2018031201614Floor Support · corrodedCORROSION ON THE FLOOR SUPPORT BETWEEN BS 120 TO 148, RBL 50 IN THE COCKPIT. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-08, AND DWG 9936533, REV CM.SDR DALA2018031201613Door Frame · crackedCRACKED RT NLG DOOR FRAME BEAM BS 40. THE RT NLG DOOR FRAME WAS REPAIRED IAW SRM 53-10-14-2R-2, FIG 201. HFEC INSPECTION WAS ACCOMPLISHED AFTER THE DAMAGE WAS REMOVED. NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001.SDR DALA2018031101608Floor Panel · delaminatedDELAMINATION ON FLOOR PANELS #211ANF, 221WF, 222GF, 222TF, 222AAF, 222AMF, 222AEF, 222AHF, 222AVF, 222ATF, AND 222DF AT PAX CABIN. NRC 00508: FLOOR PANELS #222AAF, 221WF, 222GF, 211ANF, 222AHF, 222AEF, 222AVF, AND 222ATF WERE FABRICATED, REPLACED, AND IDENTIFISDR DALA2018031101605Floor Panel · crackedCRACKS ON FLOOR PANELS #221CF, 221BF, 222ARF, 222AMF, 223JF, AND FLOOR PANEL P/N SP95530011-3 AT PAX CAB (CPAX). NRC 00506: FLOOR PANELS #221CF, 221BF, 22AMF, 223JF, AND SP95530011-3 WERE FABRICATED, REPLACED, AND IDENTIFIED PER B-717 SRM 53-20-50-2R FLOOR PANSDR DALA2018031301629Battery Pack · inoperativeBOTH THE AFT OVERWING EXIT HATCH LOCATION LIGHTS ARE INOPERATIVE. MAINTENANCE FOUND THE BATTERY PACK B5-230 INOPERATIVE. THE BATTERY PACK WAS REPLACED IAW AMM 33-51. OPS CHECKED NORMAL. THE AIRCRAFT RETURNED TO SERVICE.SDR DALA2018031101612Rub Strip · corrodedCORROSION ON RUBSTRIPS OF THE FUEL ACCESS PANELS 520GB AND 520MB ON THE LT WING THE RUBSTRIPS WERE REPLACED IAW SRM 57-10-01-2R, REP 3, PAR 6.SDR DALA2018031101611Skin · puncturedPUNCTURE ON AFT EDGE INTERNAL SKIN OF LT MLG DOOR. THE DOOR SKIN WAS REPAIRED IAW SRM 52-82-02-2R-1, FIG 201, SHEET 5.SDR DALA2018031101610Frame Angle · crackedCRACKED FRAME ANGLE AFT FACE, BS 1022 BETWEEN LONGERONS 16 - 17R. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-02, 51-41-05, AND DRAWING 9912243, REV JS.SDR DALA2018031101609Frame Angle · crackedCRACKED FRAME ANGLE, FWD FACE BS 1022 BETWEEN LONGERONS 16 - 17R. THE FRAME ANGLE WAS REPLACED IAW DWG 9912243, REV JS, AND SRM 51-20-09.SDR DALA2018031101607Angle · crackedCRACKED ANGLE AT THE RT AFT EMERGENCY EXIT DOOR UPPER BEAM AFT EDGE. THE ANGLE WAS REPLACED IAW SRM 51-41-02, AND 51-41-05.SDR DALA2018031101606Longeron · crackedCRACKED LONGERON 8L AT BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R, REP 2.SDR DALA2018031101604Pan · crackedCRACKS ON THE LT FWD OVERWING EMERGENCY EXIT DOOR FRAME PAN UPPER AREA. THE PAN WAS REPIARED IAW SRM 53-20-15-2R-8.SDR DALA2018031001707Access Panel · damagedCORROSION OUT OF LIMITS ON COUNTERSINK FUEL ACCESS PLATE #620CB, 620AT, AND 620DT AT RH WING IN REFERENCE NRC 00548. NRC 00600: COROSION LEVEL II, ACCESS PLATE #620CB AND 620DT WERE REWORKED PER B717 SRM 57-10-01-2R-2-PAR. 5 CONDITION II AND ACCESS PLATE #620ASDR DALA2022030901529None · nonePERMANENT REPAIR WAS PERFORMED ON EXTERNAL SKIN PER B-717 SRM 53-02-01-2R-1 FIG. 202 SHEET 1. VISUAL INSPECTION WAS PERFORMED PER B717 SRM 53-02-01-2R PROCEDURE 1 PAR. 6A AND NO FUTHER DAMAGE FOUND. REPETITIVE 8000 CYCLES INSPECTION PER B717 SRM 53-02-01-2R-1 SDR DALA2018031301682Slide · damagedTHE OUT OF PLACE INFLATION CABLE PIN WAS ALSO MISSING VALVE LOCK PIN ON L1 DOOR SLIDE. THE DOOR SLIDE WAS REMOVED AND REPLACED IAW AMM 25-61-01.SDR HALA2018031200089Via · malfunctionedFMS SUDDENLY WENT TO STANDBY MODE MID FLIGHT. RETURNED TO DEPARTURE. REPLACED THE NR 1 VIA IAW AMM 31-43-01. OK FOR SERVICE.SDR DALA2018031001603Angle · crackedCRACKED ANGLE AT UPPER BEAM AFT EDGE OF THE FWD LT EMERGENCY EXIT DOOR. THE ANGLE WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, & DWG 9957735, REV G.SDR DALA2018031001602Skin · crackedCRACKED FUSELAGE SKIN, BS 1189.604 LONGERON L22R. THE SKIN WAS REPAIRED IAW SRM 53-00-00-2R-1, FIGURE 201.SDR DALA2018031001601Door Frame · crackedCRACKS ON THE RT FWD OVERWING EMERGENCY EXIT DOOR FRAME PAN UPPER AREA. REPAIRED IAW SRM 53-20-15-2R-8.SDR DALA2018031001600Fitting · crackedCRACKED AFT VENTRAL DOOR FRAME LT FITTING BS 1064, LBL 14.5, Z=37. THE FITTING WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.SDR DALA2018031001599Fitting · crackedCRACKED FITTING BS 665, LONGERON 24 OF AFT BULKHEAD IN THE FWD CARGO BAY. THE FITTING WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.SDR DALA2018031001598Fastener · shearedSHEARED FASTENER ON LONGERON 2L, BS 1153 AT AFT ACCESSORY. REPAIRED IAW ER/A 566637-14, REV ORIGINAL, AND ETI-17-18-044 REV 1.SDR DALA2018031001597Vane · debondedDISBONDED AREA OF 2"X2" ON RT AFT MOVEABLE VANE LOWER SURFACE. THE VANE LOWER SURFACE WAS REPAIRED IAW SRM 57-53-01-2R, PROCEDURE 1, REPAIR 1, PARAGRAPH 4, FIGURE 201.SDR DALA2018031001596Skin · debondedDISBONDED AREA OF 1.5"X 1.5" ON RH INBD SPOILER LWR SURFACE. THE SPOILER LOWER SURFACE WAS REPAIRED IAW SRM 51-70-02-2R-3.SDR DALA2018031001595Frame · crackedCRACKED FRAME BS 660. REPAIRED IAW SRM 51-70-11-2R.SDR DALA2018031001594Frame · crackedCRACKED FRAME BS 675. REPAIRED IAW SRM 51-70-11-2R.SDR DALA2018031001593Frame · crackedCRACKED FRAME BS 675. REPAIRED IAW SRM 51-70-11-2R.SDR DALA2018031001592Frame · crackedCRACKED FRAME BS 660. REPAIRED IAW SRM 51-70-11-2R.SDR DALA2018031001591Skin · dentedDENT ON FUSELAGE SKIN BETWEEN BS 275 - 294, LONGERON 18L TO 19L. REPAIRED IAW SRM 53-20-01-2R, PROCEDURE 5, FIG 202,SDR DALA2018031001590Structure · dentedDENT ON THE AFT CARGO DOOR. REPAIRED IAW SRM 53-02-01-2R-1, FIG 202, SHEET 1, AND SRM 51-41-02.SDR DALA2018030901588Latch · damagedTAIL CONE SLIDE COVER WAS FOUND NOT SECURE. REPLACED A DAMAGED LATCH ON THE SLIDE COVER IAW AMM 25-61-02 AND RIG SLIDE IAW TASK CARD 2561-9006.SDR DALA2018030901526Access Panel · corrodedCORROSION ON FUEL ACCESS PLATES #620EB, 620CB, 620DT, AND 620AT. (AD) (PTAS). NRC 00491: DUE TO EXCESSIVE DAMAGE BY CORROSION 2, FUEL ACCESS PLATES #620AT, 620EB, AND 620DT WERE REPLACED PER B-717 SRM 57-10-01 REPAIR 2 AND FUEL ACCESS PLATE #620CB WAS REPLACEDSDR DALA2018030801487Floor Support · crackedCRACK ON FLOOR SUPPORTS STA Y=674 X=-22, Y=715 X=44/-44, AND Y=737 X=44/-44 AT WING BOX (CPAX). NRC 00260: FLOOR SUPPORTS STA Y=674 X=-22, Y=715 X=44/-44, AND Y=737 X=44/-44 AT WING BOX WERE REPLACED PER B717 SRM 51-41-02-0G , 51-41-05-0G , 51-40-08-0G. (LP #0SDR DALA2022030201331None · noneFAA STAGE III APPROVAL REQUIRES INITIAL AND RECURRING GENERAL VISUAL INSPECTIONS THAT BEGIN AND ARE REPEATED EVERY C-CHECK OR 24 MONTHS WHICHEVER OCCURS FIRST PER ERA 566546-14 AFTER ACCOMPLISHMENT OF SECTION I PERMANENT REPAIR ASSOCIATED ER/A 95-566546 ADDED SDR DALA2018030901832Tab · dentedTHE RUDER CONTROL TAB WAS DENTED ON TRAILING EDGE UPPER SECTION. THE RUDDER CONTROL TAB TRAILING EDGE UPPER SECTION WAS REPAIRED PER SRM 51-70-02-0G.SDR DALA2018030901589Bulkhead · corrodedSEVERAL CORROSION POINTS ON FWD BULKHEAD. THE BULKHEAD WAS REPAIRED IAW ER/A 566355-14, REV ORIGINAL, AND ETI-17-18-027 REV 1.SDR DALA2018030901528Access Panel · crackedCRACKED FUEL ACCESS PANLE. THE ACCESS PANEL WAS REPLACED.SDR DALA2018030901527Access Panel · crackedCRACKED FUEL ACCESS PANEL. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01, REPAIR 2.SDR DALA2018030901525Skin · crackedCRACKED SKIN, BS 1076, BETWEEN LONGERONS 13L TO 14L. THE SKIN WAS REPAIRED IAW ER/A 566546-14, REV ORIGINAL, AND ETI-17-18-022, REV 2.SDR DALA2018030901524Pan · crackedCRACKED RT RING PAN BS 889, UPPER FWD CORNER. THE RING PAN WAS REPAIRED IAW SRM 56-20-02-2R1.SDR DALA2018030901523Pan · crackedCRACKED LT RING PAN BS 870, UPPER AFT CORNER. THE RING PAN WAS REPAIRED IAW SRM 56-20-02-2R1.SDR DALA2018030901522Pan · crackedCRACKED RT RING PAN BS 870, UPPER AFT CORNER. THE RING PAN WAS REPAIRED IAW SRM 56-20-02-2R1.
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