Boeing 717-200

Service difficulty reports · 18,771

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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.

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.Mar 11, 2018 · N925AT · Boeing 717200 · Wing, Plate/SkinSDR 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.Mar 11, 2018 · N925AT · Boeing 717200 · Fuselage Main, StructureSDR 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.Mar 11, 2018 · N925AT · Boeing 717200 · Fuselage Main, StructureSDR 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.Mar 11, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR 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.Mar 11, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR 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.Mar 11, 2018 · N925AT · Boeing 717200 · Emergency ExitsSDR 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.Mar 11, 2018 · N925AT · Boeing 717200 · Cargo/Baggage DoorsSDR 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.Mar 11, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR 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.Mar 11, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR 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.Mar 11, 2018 · N893AT · Boeing 717200 · Fuselage Main, StructureSDR 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 IDENTIFIMar 10, 2018 · N955AT · Boeing 717200 · Fuselage Floor PanelSDR 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 PANMar 10, 2018 · N955AT · Boeing 717200 · Fuselage Floor PanelSDR 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.Mar 10, 2018 · N950AT · Boeing 717200 · Emergency LightingSDR 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.Mar 10, 2018 · N925AT · Boeing 717200 · Wing, Plate/SkinSDR 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.Mar 10, 2018 · N925AT · Boeing 717200 · Landing Gear DoorsSDR 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.Mar 10, 2018 · N925AT · Boeing 717200 · Fuselage Main, FrameSDR 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.Mar 10, 2018 · N925AT · Boeing 717200 · Fuselage Main, FrameSDR 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.Mar 10, 2018 · N925AT · Boeing 717200 · Emergency ExitsSDR DALA2018031101606Longeron · crackedCRACKED LONGERON 8L AT BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R, REP 2.Mar 10, 2018 · N925AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR 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.Mar 10, 2018 · N955AT · Boeing 717200 · Fuselage Main, StructureSDR 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 #620AMar 9, 2018 · N925AT · Boeing 717200 · Wing, Plate/SkinSDR 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 Mar 9, 2018 · N955AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR 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.Mar 9, 2018 · N896AT · Boeing 717200 · Escape SlideSDR 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.Mar 9, 2018 · N491HA · Boeing 717200 · Central ComputersSDR 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.Mar 9, 2018 · N925AT · Boeing 717200 · Emergency ExitsSDR DALA2018031001602Skin · crackedCRACKED FUSELAGE SKIN, BS 1189.604 LONGERON L22R. THE SKIN WAS REPAIRED IAW SRM 53-00-00-2R-1, FIGURE 201.Mar 9, 2018 · N893AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018031001601Door Frame · crackedCRACKS ON THE RT FWD OVERWING EMERGENCY EXIT DOOR FRAME PAN UPPER AREA. REPAIRED IAW SRM 53-20-15-2R-8.Mar 9, 2018 · N955AT · Boeing 717200 · Fuselage Main, StructureSDR 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.Mar 9, 2018 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR 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.Mar 9, 2018 · N955AT · Boeing 717200 · Fuselage Main, BulkheadSDR 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.Mar 9, 2018 · N938AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR 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.Mar 9, 2018 · N896AT · Boeing 717200 · Trailing Edge FlapsSDR 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.Mar 9, 2018 · N896AT · Boeing 717200 · SpoilersSDR DALA2018031001595Frame · crackedCRACKED FRAME BS 660. REPAIRED IAW SRM 51-70-11-2R.Mar 9, 2018 · N925AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018031001594Frame · crackedCRACKED FRAME BS 675. REPAIRED IAW SRM 51-70-11-2R.Mar 9, 2018 · N925AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018031001593Frame · crackedCRACKED FRAME BS 675. REPAIRED IAW SRM 51-70-11-2R.Mar 9, 2018 · N925AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018031001592Frame · crackedCRACKED FRAME BS 660. REPAIRED IAW SRM 51-70-11-2R.Mar 9, 2018 · N925AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018031001591Skin · dentedDENT ON FUSELAGE SKIN BETWEEN BS 275 - 294, LONGERON 18L TO 19L. REPAIRED IAW SRM 53-20-01-2R, PROCEDURE 5, FIG 202,Mar 9, 2018 · N955AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018031001590Structure · dentedDENT ON THE AFT CARGO DOOR. REPAIRED IAW SRM 53-02-01-2R-1, FIG 202, SHEET 1, AND SRM 51-41-02.Mar 9, 2018 · N955AT · Boeing 717200 · Cargo/Baggage DoorsSDR 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.Mar 9, 2018 · N894AT · Boeing 717200 · Escape SlideSDR 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 REPLACEDMar 8, 2018 · N955AT · Boeing 717200 · Wing, Plate/SkinSDR 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 #0Mar 8, 2018 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR 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 Mar 8, 2018 · N955AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR 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.Mar 8, 2018 · N938AT · Boeing 717200 · Rudder, Tab StructureSDR 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.Mar 8, 2018 · N955AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2018030901528Access Panel · crackedCRACKED FUEL ACCESS PANLE. THE ACCESS PANEL WAS REPLACED.Mar 8, 2018 · N955AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018030901527Access Panel · crackedCRACKED FUEL ACCESS PANEL. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01, REPAIR 2.Mar 8, 2018 · N955AT · Boeing 717200 · Wing, Plate/SkinSDR 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.Mar 8, 2018 · N955AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018030901524Pan · crackedCRACKED RT RING PAN BS 889, UPPER FWD CORNER. THE RING PAN WAS REPAIRED IAW SRM 56-20-02-2R1.Mar 8, 2018 · N925AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018030901523Pan · crackedCRACKED LT RING PAN BS 870, UPPER AFT CORNER. THE RING PAN WAS REPAIRED IAW SRM 56-20-02-2R1.Mar 8, 2018 · N925AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018030901522Pan · crackedCRACKED RT RING PAN BS 870, UPPER AFT CORNER. THE RING PAN WAS REPAIRED IAW SRM 56-20-02-2R1.Mar 8, 2018 · N925AT · Boeing 717200 · Fuselage Main, Structure
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