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"

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SDR DALA2018032101820Gusset · crackedCRACKED GUSSET ON AFT BULKHEAD SUPPORT STA Y=1022 PROTECTION LONG 7R AT PAX CABIN. GUSSET ON AFT BULKHEAD SUPPORT STA Y=1022 PROJECTION LONG 7R WAS REPAIRED PER ETI-17-18-043 REV 1 AND ER/A 566865-14 REV ORIGINAL.Mar 20, 2018 · N925AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2018032101819Fire Bottle · unserviceableOUT OF LIMITS WEIGHT ON AFT/RT LAVATORY FIRE EXTINGUISHER CONTAINER. EXTINGUISHER ASSY WAS REMOVED AND A SERVICEABLE EXTINGUISHER ASSY WAS INSTALLED PER AMM 26-25-01.Mar 20, 2018 · N955AT · Boeing 717200 · Fire Bottle, PortableSDR HALA2018032100117Unknown · odorF/A REPORTED SMELLING SOMETHING BURNING THROUGHOUT CABIN AT FL200. ODOR DISSIPATED BY 170. POSSIBLY ELECTRICAL. OPS CHECKED PACKS OFF OF APU BLEED AIR. NO DEFECTS NOTED. OK FOR SERVICE.Mar 19, 2018 · N488HA · Boeing 717200 · Air Distribution SystemSDR DALA2018032001815Warning Light · false activationDECLARED AN EMERGENCY ON APPROACH, DUE TO THE TAIL TEMP HIGH WARNING INDICATION REPEATEDLY. FOLLOWING THE FIRST INDICATION THE CREW COMPLIED WITH THE QRH AND SECURED THE LEFT PACK AND BLEED. THE MESSAGE INITIALLY WENT OUT, BUT CAME BACK WITHIN 2 MINUTES. TMar 19, 2018 · N961AT · Boeing 717200 · Central WarningSDR DALA2018031901764Floor Panel · delaminatedDELAMINATION ON FLOOR PANELS #221AF, 221DF, 221FF, 221BF, 221CF, 221JF, 221HF, 222ANF, AND 222RF AT PAX CAB (CPAX). NRC 00560: FLOOR PANELS #221AF, 221DF, 221FF, 221BF, 221CF, 221JF, 221HF, 222ANF, AND 222RF WERE FABRICATED, REPLACED, AND IDENTIFIED PER B-717 Mar 18, 2018 · N925AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2018031901767Longeron · corrodedCORROSION OUT OF LIMITS ON LONGERON 30, BS 934 TO 1002. CORROSION OUT OF LIMITS. THE LONGERON WAS REPLACED IAW SRM 53-20-05-01-3, FIG 1.Mar 18, 2018 · N925AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018031901766Longeron · corrodedCORROSION ON LONGERON 30 BETWEEN BS 1022 - 1037. THE LONGERON SECTION WAS REPLACED IAW SRM 51-41-05-0G, AND SRM 51-41-02-0G.Mar 18, 2018 · N925AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018031901765Longeron · corrodedCORROSION ON LONGERON 27L BETWEEN BS 990 TO 1022. THE LONGERON SECTION WAS REPLACED SRM 53-20-05-01-3, FIG 1, AND 51-40-08.Mar 18, 2018 · N925AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018031801760Floor Panel · brokenBROKEN CHANNEL ON GEN FLOOR PANELS #221GF, 222AJF, AND 222EF. NRC 00536: GEN FLOOR PANELS #221GF, 222AJF, AND 222EF WERE REPAIRED PER B717 SRM 53-20-50-2R REPAIR 5 FIG. 202. (ET) HFEC INSPECTION WAS ACCOMPLISHED ON GEN FLOOR PANELS #222AJF AND 222EF AFTER STOPMar 17, 2018 · N925AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2018031801818Skin · wornWORN RT WING SLAT PANEL NR 1 LOWER SKIN STA XFS=145. WEAR ON RT WING SLAT WAS REPAIRED, AS A PERMANENT REPAIR PER ER/A 566779-14 REV ORIGINAL AND ETI-17-18-038 REV 3.Mar 17, 2018 · N955AT · Boeing 717200 · Leading Edge DevicesSDR DALA2018031801763Floorbeam · crackedCRACKED FLOORBEAM BS 645. THE FLOORBEAM WAS REPLACED IAW SRM 51-41-02, 51-41-05, AND DWG 5971111, REV F.Mar 17, 2018 · N925AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2018031801762Skin Splice · corrodedCORROSION ON SKIN SPLICE BS 898, BETWEEN LONGERONS 26L TO 30L. THE SKIN SPLICE WAS REPLACED IAW SRM 53-20-01-0I-3, FIG 1. UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07, PAR 5, FIG 3, SHEETS 1 AND 2. FOUND OUT LIMITS IAW SRM 53-00-00-1A, ALLOWABLE DAMAGE PAR 4, FIMar 17, 2018 · N925AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018031901813Pan · crackedCRACK FOUND ON THE FWD EDGE OUTER PAN BELOW THE NR 2 STOP FITTING AT THE FWD CARGO DOOR. REPAIRED IAW ETI-17-18-055, REV 1, AND ER/A 566780-14, REV ORIG.Mar 16, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR HALA2018032000109Cover · detachedR1 SLIDE COVER DETACHED. REMOVED AND REPLACED R1 SLIDE ASSY IAW AMM 25-61-03. CONDITIONAL CHECKED GOOD. OK FOR SERVICE.Mar 16, 2018 · N493HA · Boeing 717200 · Escape SlideSDR DALA2018031701759Longeron Splice · corrodedCORROSION ON THE LONGERON 30 SPLICE BETWEEN BS 927 TO 946. THE LONGERON SPLICE WAS REPLACED IAW SRM 51-41-05.Mar 16, 2018 · N925AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018031701758Longeron Splice · corrodedCORROSION ON LONGERON SPLICE 27L BETWEEN BS 973 TO 994 IN THE AFT CARGO BAY. THE LONGERON SPLICE WAS REPLACED IAW SRM 51-41-05.Mar 16, 2018 · N925AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018031701757Vane · damagedDENTED AREA WAS FOUND DISBONDED. RT INBOARD FIXED FLAP VANE, LOWER SURFACE, DISBONDED AREA WAS REPAIRED IAW SRM 57-53-01-2R-1.Mar 16, 2018 · N955AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2018031701756Strap · corrodedCORROSION ON STRAP AT LONGERON 25L BETWEEN BS 1002 TO 1022. THE STRAP WAS REPLACED IAW SRM 51-41-05, AND DWG 5936021, REV EG.Mar 16, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018031701755Skin · crackedCRACKED FUSELAGE SKIN BS 1022, BETWEEN LONGERONS 14R TO 15R. THE SKIN & DOUBLER WERE REPAIRED IAW ETI-17-18-047, REV 3, AND ER/A 566828-14, REV ORIGINAL.Mar 16, 2018 · N893AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018031701754Skin · crackedCRACKED EXTERNAL FUSELAGE SKIN BS 1133 BETWEEN STRINGERS 2L AND 3L. THE SKIN WAS REPAIRED IAW ER/A 566630-14AD, REV ORIG, AND ETI-17-18-029, REV 2.Mar 16, 2018 · N955AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018031701753Frame · crackedCRACKED FRAME BS 1037 BETWEEN LONGERONS 14L. THE FRAME WAS REPAIRED IAW ER/A 566736-14, REV ORIG.Mar 16, 2018 · N955AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018031701752Frame · crackedCRACKED FRAME, BS 1037, LONGERON 13R. THE FRAME WAS REPAIRED IAW ER/A 566676-14, REV ORIG, AND ETI-17-18-034, REV 1.Mar 16, 2018 · N955AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018031701751Frame Angle · crackedCRACKED FRAME ANGLE ON THE LT AFT LAVATORY AREA BS 1052, BETWEEN LONGERONS 18L AND 19L. THE FRAME ANGLE WAS REPLACED IAW DWG 9915561, REV CG, SRM 51-41-05-0G, AND 51-41-02-0G.Mar 16, 2018 · N955AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018031701750Frame Angle · crackedCRACKED FRAME ANGLE, FWD FACE BS 1022, BETWEEN LONGERONS 7L - 8L. THE FRAME ANGLE WAS REPLACED IAW SRM 51-41-02, AND 51-41-05 AND DWG 9912243, REV JS. HFEC INSPECTION WAS ACCOMPLISHED AND A CRACK WAS CONFIRMED IAW NDT SPM 06-10-01.001.Mar 16, 2018 · N925AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018031601848Skin · damagedDUE TO WEAR FOUND ON THE RT WING SLAT PANEL NR 1, LOWER SKIN, XFS 145, REMOVED AND REPLACED THE SLAT PANEL IAW AMM 27-80-01 AND ADJUSTED IAW AMM 27-80-01-830-802. RT WING NR 1 SLAT WAS REPAIRED IAW ER/A 566779-14, REV. ORIGINAL.Mar 15, 2018 · N955AT · Boeing 717200 · Leading Edge DevicesSDR DALA2018032001814Seat Track · corrodedSEAT TRACK CORRODED. SPLICED IN A NEW SECTION OF SEAT TRACK IAW SRM 53-20-52-2R, PRO 5.Mar 15, 2018 · N943AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2018031501737Charger · inoperativeFOUND THE EMERGENCY EXIT SIGN ABOVE THE L1 FLIGHT ATTENDANT SEAT INOPERATIVE. TROUBLESHOT IAW ASM 33-51-0. REPLACED THE CHARGER AND BATTERY PACK IAW AMM 33-51. OPS CHECKED GOOD.Mar 15, 2018 · N951AT · Boeing 717200 · Emergency LightingSDR DALA2018031601736Cargo Track · corrodedCORROSION ON THE LT & RT CARGO TRACK BS 889 TO 1022. THE CARGO TRACKS WERE REPLACED IAW SRM 51-41-01-0G, AND 51-41-05-0G.Mar 15, 2018 · N955AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2018031501735Attach Fitting · corrodedTHE FWD GIRT BAR ATTACH PLATE FOR THE R1 DOOR HAS CORROSION. REPLACED THE ATTACH PLATE FITTING DWG 3936190.Mar 15, 2018 · N943AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2018031501734Attach Fitting · corrodedTHE AFT GIRT BAR ATTACH PLATE FOR THE R1 DOOR HAS CORROSION. REPLACED THE ATTACH PLATE IAW DWG 3936190.Mar 15, 2018 · N943AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2018031501733Frame · corrodedCORROSION ON FRAME, BS 954, BETWEEN LONGERONS 25 AND 28. THE FRAME WAS REPAIRED IAW SRM 51-41-05-0G, AND 53-20-07-2R-3-.Mar 14, 2018 · N955AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018031501732Channel · corrodedWEAR ON THE CORNERS OF THE FWD CARGO DOOR BARRIER. LOWER FORWARD AND LOWER AFTER CORNERS OF DOOR BARRIER CHANNEL WERE BLENDED AND UT WAS ACCOMPLISHED IAW NDT SPM 04-00-07, PAR 5, FIG 3, SHEET 1, AND 2. FOUND OUT OF LIMITS AND LOWER AFTER EDGE OF DOOR BARRIERMar 14, 2018 · N893AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2018031501713Membrane · corrodedCORROSION ON MEMBRANE STA Y=200 X=-54 5300-2010. CORROSION LEVEL 2, MEMBRANE WAS REPAIRED PER SRM 51-70-10-2R. (ET) HFEC INSPECTION WAS ACCOMPLISHED ON MEMBRANE STA Y=200 X=-54, NO CRACKS WERE FOUND AFTER CUT OUT PER NDTSPM 06-10-01.001.Mar 14, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018031501712Skin · dentedDENT ON RT FLAP LOWER MOVEABLE VANE LOWER SKIN -5" FROM OUT EDGE. RT FLAP LOWER MOVEABLE VANE LOWER SKIN WAS REPAIRED PER SRM 57-53-01-2R PROCEDURE 1 PAR 4 AND SRM 51-70-02.Mar 14, 2018 · N893AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2018031501711Skin · crackedAD 2016-09-05, AA 5530-01048: CRACKS ON REMOVABLE LEADING EDGE SKIN, STA ZFS=53 AT VERTICAL STABILIZER. REMOVABLE LEADING EDGE SKIN, STA ZFS=53 WAS REPAIRED PER SRM 55-30-01-2R-8.Mar 14, 2018 · N955AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2018031501710Door Frame · corrodedCORROSION ON L1 DOOR JAMB WEB BTW STA Y=200-207 BTW LONG 17L TO 18L AT CPAX. CORROSION LEVEL 2, L1 DOOR JAMB WEB BTW STA Y=200-207 BTW LONG 17L TO 18L AT CPAX WAS REPAIRED PER ER/A 566681-14 REV ORIGINAL AND ETI-17-18-035 REV 1.Mar 14, 2018 · N955AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018031501709Floor Support · corrodedCORROSION ON FLOOR SUPPORTS STA Y=200, X=-7, AND X=-44 REF 5300-2010 CPAX. CORROSION LEVEL 2, FLOOR SUPPORTS STA Y=200, X=-7, AND X=-44 WERE REPLACED PER SRM 51-41-02.Mar 14, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018031501708Floor Support · corrodedCORROSION ON FLOOR SUPPORTS STA Y=200 X=-10 TO X=-44, X=-44 TO X=-54, AND X=7 TO X=-7 REF AMDS 5300-2010 CPAX. CORROSION LEVEL 2, FLOOR SUPPORTS STA Y=200 X=-10 TO X=-44, X=-44 TO X=-54, AND X=7 TO X=-7 WERE REPLACED PER SRM 51-41-02.Mar 14, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2022030901528None · 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 566676-14. DISPLACED LAV TO GAIN ACCESS TO INSPECTION AREA. PERFORMED VISUAL REPETITIVE INSPEMar 13, 2018 · N955AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018031401687Seat Track · corrodedCORROSION ON THE SEAT TRACK LBL 54, BETWEEN BS 240 TO 247. THE SEAT TRACK WAS REPAIRED IAW SRM 53-20-52-2R-5.Mar 13, 2018 · N925AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2018031401686Frame Angle · corrodedCORROSION ON THE FRAME ANGLE, BS 908, BETWEEN LONGERONS 29 AND 30R, THE FRAME ANGLE WAS REPAIRED IAW SRM 53-00-06-2R-2, REPAIR 2, 51-41-02-0G, AND 51-41-05-0G.Mar 13, 2018 · N955AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018031401685Stiffener · crackedCRACKED VERTICAL STIFFENER BS 813 TO 816, BL 0, FWD BULKHEAD AFT FACE. THE STIFFENER WAS REPAIRED IAW SRM 53-00-00-2R, FIG-201, SHEET 1.Mar 13, 2018 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018031401684Cusp Web · corrodedCORROSION ON THE CUSP WEB, BS 902 TO 904, LBL 54 TO RBL 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 215.Mar 13, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018031301683Cusp Web · crackedCRACK ON THE RT CUSP WEB, BS 674, RBL 46: THE CUSP WEB WAS REPAIRED IAW SRM 51-70-10-2R-2. HFEC WAS ACCOMPLISHED ON EDGES OF TRIMMED AREA, NO CRACKS FOUND IAW NDT SPM PART 6, 06-10-01.001,Mar 13, 2018 · N925AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018031301628Access Panel · crackedCRACKED RT WING LOWER ACCESS PANEL AT THE TRAILING EDGE AREA XRS 150. THE ACCESS PANEL WAS REPAIRED SRM 57-50-01-2R, 51-41-01 0G, AND 51-41-05-0G.Mar 13, 2018 · N955AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018031301626None · noneEXCESSIVE CORROSION ON FUEL ACCSESS PLATE #620CT, 520CT, AND 520DT AT SETTLEMENT AND COUNTERSINK AREA RH/LH WING IN REFERENCE NRCS 00549, 00553, AND 00554. NRC 00603: CORROSION LEVEL 2, FUEL ACCESS PLATES #520CT AND 620CT WERE REPLACED DUE TO BLEND OUT REPAIR Mar 12, 2018 · N925AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018031401714Battery Pack · dischargedEMERGENCY EXIT SIGN AT DOOR AND 1ST CLASS FLICKERS (ON AND OFF). MAINTENANCE REPLACED THE CABIN EMERGENCY LIGHT BATTERY PACK AND BATTERY OPERATION IS NOW NORMAL PER AMM 33-51.Mar 12, 2018 · N989AT · Boeing 717200 · Emergency LightingSDR DALA2018031301627Cap · crackedCRACKED CAP BS 1022, LONGERON 7R AND 7L. THE CAP WAS REPAIRED IAW ETI 17-18-026, REV 1, AND ER/A 566634-14, REV ORIGINAL.Mar 12, 2018 · N955AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018031301625Floor Panel · corrodedCORRODED FLOOR PANEL. A NEW FLOOR PANEL WAS FABRICATED, AND REPLACED IAW DWG 9957828, REV AB.Mar 12, 2018 · N925AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2018031201620Floor Panel · crackedCRACKS ON FLOOR PANELS #221EF, 211ANF, AND 223GF AT PAX CAB (CPAX). NRC 00556: FLOOR PANELS #221EF, 211ANF, AND 223GF WERE FABRICATED, REPLACED, AND IDENTIFIED PER B-717 SRM 53-20-50. FLOOR PANELS WERE INTALLED WITH JIC CARD 2040-0024. (LP #0460121)Mar 11, 2018 · N925AT · Boeing 717200 · Fuselage Floor Panel
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