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 DALA2016101907362Cusp Web · crackedRT CUSP WEB AT BS 657 CRACKED. REPAIRED THE CUSP WEB IAW SRM 51-70-10 REP 2 & SRM 53-00-55 REP 4.Oct 18, 2016 · N987AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016101907360Skin · dentedDENT ON FUSELAGE SKIN BS 200 - 218 LONGERONS 17-18R. FOUND TO BE WITHIN LIMITS IAW SRM 53-01-01 PAR 4 B. DETAILED 10X MAGNIFIED VISUAL INSPECTION WAS PERFORMED AND ADDITIONAL DAMAGE WAS NOT FOUND IAW SRM 53-01-01 PAR. 4 (1). HFEC INSPECTION WAS ACCOMPLISHED Oct 18, 2016 · N925AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016101907359Cusp Web · corrodedCORROSION ON THE RT CUSP WEB BS 550. DAMAGED AREA WAS TRIMMED OUT IAW SRM 53-00-55. HFEC INSPECTION WAS ACCOMPLISHED AFTER TRIM OUT AND NO CRACKS WERE FOUND IAW NDT SPM 06-10-01. REPAIRED IAW SRM 53-00-55 FIG. 215, 51-10-4 PAR 15, 21, 51-41-02, AND 51-10-04 Oct 18, 2016 · N967AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017010500102Cusp Web · corrodedEXCESSIVE CORROSION ON RT CUSP WEB ON STA Y=550 IN REF CARD 00393. CRACK WAS FOUND WITH NEXT DIMENSION L=.320" DAMAGED AREA WAS TRIMMED OUT PER SRM 53-00-55. HFEC INSPECTION WAS ACCOMPLISHED ON RT CUSP WEB ON STA Y=550 AFTER TRIM OUT AND NO CRACKS WERE FOUND POct 17, 2016 · N967AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016101907365Cusp Web · crackedCUSP WEB AT BS 674 CRACKED. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55 REPAIR 4.Oct 17, 2016 · N987AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016101807332Longeron · corrodedCORROSION OUT OF LIMITS ON LONGERON 30 BTW STA Y= 974 TO 1005 AT AFT CARGO COMPARTMENT. LONGERON 30 BTW STA Y=974 TO Y=1005 WAS REPAIRED PER SRM 53-00-05 FIG 201 REPAIR 3.Oct 17, 2016 · N967AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016101807331Access Panel · corrodedEXCESSIVE CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE 620CB AND 620AT AT RT WING. PLATES 620AT AND 620CB WERE REWORKED AND WERE FOUND OUT LIMITS, THEREFORE FUEL ACCESS PLATES WERE REPLACED AND THE APPLICABILITY WAS VERIFIED PER IPC 57-22-01-01 AND 57-23-01-Oct 17, 2016 · N967AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016101807330Door Frame · crackedCRACKED RT NLG DOOR JAMB. (00434) LENGTH ORIGINAL CRACK LONG 1.300" AND WIDTH 0.750". DAMAGED AREA WAS REMOVED, CUT WAS CHECKED PER HFEC INSP, AND NO CRACKS FOUND. AREA WAS REPAIRED PER SRM 53-10-14 FIG 201 REPAIR 2.Oct 17, 2016 · N967AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016101807329Door Frame · crackedCRACKED LT NLG DOOR JAMB (00435). LENGTH ORIGINAL CRACK LONG 1.125" AND WIDTH 0.750", DAMAGED AREA WAS REMOVED, CUT WAS CHECKED PER HFEC INSP, AND NO CRACKS FOUND. AREA WAS REPAIRED PER SRM 53-10-14 FIG 201 REPAIR 2.Oct 17, 2016 · N967AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016101807328Cusp Web · crackedEXCESSIVE CORROSION ON RT CUSP WEB ON STA Y=550 IN REF CARD 00393. CRACK WAS FOUND WITH NEXT DIMENSION L=.320" DAMAGED AREA WAS TRIMMED OUT PER SRM 53-00-55. HFEC INSPECTION WAS ACCOMPLISHED ON RT CUSP WEB ON STA Y=550 AFTER TRIM OUT AND NO CRACKS WERE FOUNDOct 17, 2016 · N967AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017010500112Frame · corrodedNR13 FRAME AT STA 1022, BETWEEN STR 29L AND 29R IS CORRODED AT AFT FACE OF FRAME AND ALONG LWR LIP OF FRAME. NR13 REPAIRED FRAME PER SRM 53-20-07 REPAIR 3, AND LONG BEACH DWG 9912243.Oct 15, 2016 · N607AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016101607263Frame · corrodedFRAME AT BS 1022, BETWEEN STRINGERS 29L AND 29R IS CORRODED AT AFT FACE OF FRAME AND ALONG LWR LIP. REPAIRED THE FRAME IAW SRM 53-20-07 REPAIR 3, AND DWG 9912243.Oct 15, 2016 · N607AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016101607262Cusp Web · crackedCRACK ON CUSP WEB BS 663 BTW LBL 54 TO 60. HFEC WAS ACCOMPLISHED AND A CRACK WAS CONFIRMED OF 1.900" LENGTH IAW NDT SPM 06-10-01 .001: THE CRACK WAS STOPPED DRILL IAW SRM 51-00-07 PAR 5. HFEC WAS ACCOMPLISHED IAW NDT SPM 06-10-01 .001 AND NO CRACKS WERE FOUNDOct 15, 2016 · N967AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016101607261Frame · crackedCRACKED FRAME 907 BETWEEN LONGERONS 26-28R, REPAIRED IAW SRM 51-41-02 AND 51-41-05.Oct 15, 2016 · N967AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016101607260Channel · crackedCRACKED RT MLG DOOR FRAME CHANNEL AT BS 757. THE CHANNEL WAS REPLACED IAW SRM 51-41-02 AND 51-41-05.Oct 15, 2016 · N967AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017010500108Longeron Splice · corrodedLONGERON SPLICE BETWEEN STA 954-974 IS CORRODED. REINSTALLED SKIN CLIPS AND COMPLETED REPAIR PER SRM 53-00-05 REPAIR 2.Oct 14, 2016 · N607AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017010500107Longeron Splice · corrodedLONGERON 30 SPLICE BETWEEN STA 927 AND 946 IS CORRODED. REINSTALLED SKIN CLIPS AND COMPLETED REPAIR PER SRM 53-00-05 REPAIR 2.Oct 14, 2016 · N607AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017010500106Stringer · corrodedCORROSION ON STR30 AT STA 974, 994, AND 1005. REINSTALLED SKIN CLIPS AND COMPLETED REPAIR PER B717 SRM 53-00-05 REPAIR 2.Oct 14, 2016 · N607AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017010500105Frame · corrodedFRAME AT STA 1022, BETWEEN STR 29L AND 29R IS CORRODED AT AFT FACE OF FRAME AND ALONG LWR LIP OF FRAME. REPAIRED FRAME PER SRM 53-20-07, AND DWG 9912243.Oct 14, 2016 · N607AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017010500104Frame · corrodedFOUND FRAME CORRODED ON LOWER SURFACE AT FS 974 LONGERON 30. SEE NR FOR ADDITIONAL INFORMATION 001-0002:2000-2002/014 00014. REPAIR FRAME PER SRM 53-20-07 REPAIR 3.Oct 14, 2016 · N607AT · Boeing 717200 · Fuselage Main, FrameSDR HALA2016101400369Unknown · odorELECTRIC TYPE BURNING ODOR IN AFT GALLEY AREA. NO ELECRICAL BURNING ODOR PRESENT IN AFT GALLEY AREA. ACFT OK FOR SERVICE.Oct 14, 2016 · N483HA · Boeing 717200 · Air Distribution SystemSDR HALA2016101140368Latch · out of adjustOPEN: ATB, RT GEAR UNSAFE LIGHT AFTER TO. MX NEEDS TO ADJUST THE RT MLG UPLOCK LATCH AND OPS CHK. MX IS REPLACING THE DOWN LOCK ELEC CONDUIT.Oct 14, 2016 · N480HA · Boeing 717200 · Landing Gear Retraction/Extension SystemSDR DALA2016101907367Seat Track · corrodedRIGHT INBD SEAT TRACK BS 200-256, FOUND THREE SPOTS OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-05 PG 1.Oct 13, 2016 · N987AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016101907361Frame · crackedBS 1022 FRAME ABOVE LONGERON 14R WAS FOUND CRACKED. REPLACED THE FRAME IAW SRM 51-41-02 PG 1-4, & 51-41-05 PG 1.Oct 13, 2016 · N987AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016101407266Cusp Web · crackedCRACK FOUND ON THE RT CUSP WEB BS 365 X45. HFEC INSPECTION WAS ACCOMPLISHED ON THE CUSP WEB AND A CRACK WAS CONFIRMED IAW NDT SPM 06-10-01 .001. THE DAMAGE WAS REMOVED PER B-717 SRM 55-00-55 REPAIR 4 AND ANOTHER HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKOct 13, 2016 · N967AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016101407230Angle · crackedCRACK ON BULKHEAD ANGLE BS 1022 BETWEEN LONGERONS 13-14R. A NEW ANGLE WAS MANUFACTURED IAW DRAWING 9912243-198 AND SRM 51-20-09, TREATED AND PAINTED IAW SRM 51-10-04 PAR 21 AND 15, AND INSTALLED IAW SRM 51-41-02 AND 51-41-05.Oct 13, 2016 · N967AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016101407229Angle · crackedCRACK ON BULKHEAD ANGLE BS 1022 BETWEEN LONGERONS 16-17L. A NEW FRAME ANGLE WAS MANUFACTURED IAW DRAWING 9912243-189 AND SRM 51-20-09. TREATED AND PAINTED IAW SRM 51-10-04 PAR 15 AND 21, AND INSTALLED IAW SRM 51-41-05.Oct 13, 2016 · N967AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2016101907366Stringer · corrodedSTRINGER 29L CORRODED BETWEEN BS 908 - 927. BLENDED THE STRINGER IAW SRM 53-00-00 FIG 103. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 103. REPAIRED THE STRINGER IAW SRM 53-00-05 REPAIR 3.Oct 12, 2016 · N987AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016101307188Longeron Splice · corrodedCORROSION ON LONGERON SPLICE 18R, BS 898. THE SPLICE WAS REMOVED IAW SRM 51-41-05. SPLICE WAS FABRICATED IAW SRM 53-20-01 FIG 1 AND 51-20-09. THE SPLICE AND AREA WAS TREATED AND PAINTED IAW SRM 51-10-04 PAR. 15/21. THE SPLICE WAS INSTALLED IAW SRM 51-41-0Oct 12, 2016 · N967AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016101307187Pan · crackedCRACK ON PAN BS 427 BETWEEN BEAM 1 AND BEAM 2 AT FWD CARGO DOOR. HFEC INSPECTION WAS ACCOMPLISHED AND CRACKS WERE FOUND IAW NDT SPM 06-10-01 .001. CRACKS ON PAN WERE STOP DRILLED IAW SRM 52-30-02 FIG 201, HFEC WAS ACCOMPLISHED ON PAN AND NO CRACKS WERE FOUNOct 12, 2016 · N967AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016101307186Cusp Web · corrodedEXCESSIVE CORROSION ON RT CUSP WEB BS 455. DAMAGE WAS REMOVED, A REPAIR WAS MANUFACTURED, AND INSTALLED IAW SRM 53-00-55 REPAIR 4. HFEC WAS ACCOMPLISHED IAW NDT SPM 06-10-01.001 AND NO CRACKS WERE FOUND AFTER CUT OUT.Oct 12, 2016 · N967AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016101307185Support · crackedCRACKED SUPPORT UNDER SEAT TRACK X 44.5 ON BS 715. THE SUPPORT WAS REPLACED IAW DWG 9923417 REV. B AND SRM 51-41-05.Oct 12, 2016 · N967AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR HALA2016101100368Latch · out of adjustRIGHT GEAR UNSAFE LIGHT ILLIMINATED AFTER TAKE OFF. ACCOMPLISHED FUNCTIONAL TEST OF MAIN & NOSE GEAR IAW AMM 32-30-00-720-801. OPS CHECKED OK. FOUND MAIN GEAR RT DOOR LATCH ROLLER TO HOOK CLEARANCE OUT OF LIMITS. ADDED A SHIM BETWEEN MLG DOOR AND DOOR LATCH. Oct 11, 2016 · N480HA · Boeing 717200 · Landing Gear Position and WarningSDR DALA2016101307184Access Panel · corrodedEXCESIVE CORROSION ON COUNTERSINK OF FUEL ACCESS PANEL 520CB LT WING. THE ACCESS PANEL WAS DETERMINED TO BE OUT OF LIMITS AND WAS REPLACED IAW SRM 57-10-01 PAR. 5.Oct 11, 2016 · N967AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016101207173Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT BOTH OF THE AFT OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECKED GOOD.Oct 11, 2016 · N980AT · Boeing 717200 · Emergency LightingSDR DALA2016101207172Access Panel · damagedELONGATED HOLES ON FUEL ACCESS PANEL 141AR ON THE RT WING. THE ACCESS PANEL WAS REWORKED IAW SRM 57-10-01 CONDITION II AND FOUND TO BE OUT OF LIMITS. REPLACED IAW SRM 57-10-01.Oct 11, 2016 · N967AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016101207171Seat Track · crackedCRACKED SUPPORT UNDER SEAT TRACK X -44.5 AT BS 715. THE SUPPORT WAS REMOVED IAW SRM 51-41-05 AND 51-41-02. A NEW SUPPORT WAS DRILLED IAW DWG 9923417 REV. B AND SRM 51-40-08. TREATED AND PAINTED IAW SRM 51-10-04 PAR. 21 AND 15. AND INSTALLED IAW DWG 9923417Oct 11, 2016 · N967AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016101207170Cusp Web · corrodedPUNCTURE ON LT CUSP WEB BS 294 BETWEEN X 44 TO 54. DAMAGE WAS REMOVED, HFEC INSPECTION ACCOMPLISHED, NO CRACKS WERE FOUND IAW NDT SPM 06-10-01 .001. DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-00-55 AND SRM 51-41-02.Oct 11, 2016 · N967AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016101207169Cusp Web · corrodedEXCESSIVE CORROSION ON LT CUSP WEB BS 856. DAMAGE WAS REMOVED, DOUBLER FABRICATED, AND INSTALLED IAW SRM 53-00-55 AND 51-41-02, HFEC INSPECTION WAS ACCOMPLISHED IAW NDT SPM 06-10-01.001.Oct 11, 2016 · N967AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016101207168Cusp Web · corrodedEXCESSIVE CORROSION ON RT CUSP WEB ON BS 513. DAMAGE ON AREA WAS TRIMMED OUT IAW SRM 53-00-55. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. REPAIR FABRICATED IAW SRM 53-00-55 REPAIR 4 FIG. 215 AND INSTALLED IAW SRM 51-4Oct 11, 2016 · N967AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016102107462Seat Track · damagedLEFT OTBD SEAT TRACK LBL 56 IS CORRODED AND GOUGED IN SEVERAL AREAS FROM BS 1020 - 1053. BLENDED THE AREAS OF CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 PG 105 FIG 103. FABRICATED A NEW SEAT TRACK IAW DWG 9981474 REV.L. AND INSTALLED THE NEW Oct 10, 2016 · N987AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016101907368Frame · crackedCRACK IN BS 1022 MAIN FRAME, AFT SIDE AT STRINGER 7R. REPAIRED THE FRAME IAW SRM 51-70-11 REPAIR 1.Oct 10, 2016 · N987AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016101907364Frame · crackedCRACK IN BS 1022 MAIN FRAME AT STRINGER 7L. THE FRAME WAS REPAIRED IAW SRM 51-70-11 REPAIR 1.Oct 10, 2016 · N987AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016101907363Bracket · crackedCRACKED BRACKET UNDER UPPER CABIN FLOOR, ABOVE CENTER WING FUEL TANK AT APPROXIMATE BS 735 RBL 48. REMOVED AND REPLACED THE BRACKET IAW SRM 51-41-05.Oct 10, 2016 · N987AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2016101107154Cusp Web · corrodedEXCESSIVE CORROSION ON RT CUSP WEB ON BS 489 IAW CARD 00393. DAMAGE WAS REMOVED IAW SRM 53-00-55 FIG. 215. HFEC INSPECTION WAS ACCOMPLISHED AFTER TRIM OUT AND NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. REPAIR FABRICATED IAW SRM 53-00-55. REPAIR INSTALLEDOct 10, 2016 · N967AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016101107153Cusp Web · crackedCRACK ON RT CUSP WEB BS 218 X=45 AT CABIN PAX RH. CRACK WAS STOP DRILL IAW SRM 53-00-55 REPAIR 4, HFEC INSPECTION WAS ACCOMPLISHED IAW NDT SPM 06-10-01.001, NO CRACKS WERE FOUND AFTER STOP DRILL. REPAIR DOUBLER WAS FABRICATED IAW SRM 53-00-55. AREA DRILLED WOct 10, 2016 · N967AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016101007121Access Panel · damagedRT WING UPPER ACCESS PANEL 620FT HAS ELONGATED HOLES. REPLACED THE ACCESS PANEL IAW AMM 28-00-00-410.Oct 10, 2016 · N987AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016101007120Access Panel · damagedRT WING UPPER ACCESS PANEL 620CT HAS ELONGATED HOLES. REPLACED THE ACCESS PANEL IAW AMM 28-00-00-410.Oct 10, 2016 · N987AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016101007119Access Panel · damagedELONGATED HOLES ON FUEL ACCESS PANEL 141AL ON THE LT WING. THE FUEL ACCESS PANEL WAS REPAIRED SRM 57-10-01 CONDITION II.Oct 9, 2016 · N967AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016101007118Frame · crackedCRACKED FRAME ANGEL BS 1116 BETWEEN LONGERONS 15 -16 BOTH SIDES. THE ANGLS WERE REPLACED IAW SRM 51-41-05.Oct 9, 2016 · N967AT · Boeing 717200 · Fuselage Main, Frame
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