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 DALA2016050603717Seat Track · damagedLEFT CTR SEAT TRACK, BS 148-1022, BL44.5 HAS MULTIPLE DISCREPANCIES. BLENDED MULTIPLE DISCREPANCIES ON LT CTR SEAT TRACK FROM BS 148 TO 1022 REMOVED .004" FROM TOP REMAINING .136" REMOVED .011 IN CENTER OF TRACK REMAINING .099" FOUND TO BE WITHIN LIMITS AT STApr 29, 2016 · N924AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016050203478Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTING BETWEEN ROWS 16 AND 17 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.Apr 29, 2016 · N892AT · Boeing 717200 · Emergency LightingSDR DALA2016043003459Intercostal · crackedCRACK ON INTERCOSTAL ON RT ELEVATOR HINGE FITTING AREA XE=204 ACCESS 340UB. SM, CRACK ON INTERCOSTAL ON RT ELEVATOR HINGE FITTING AREA BS XE=204 ACCESS 340UB, WAS REPAIRED IAW SRM 55-00-00, FIG 201.Apr 29, 2016 · N919AT · Boeing 717200 · Horizontal Stabilizer StructureSDR DALA2016043003457Beam · crackedLOWER BEAM CRACKED AT HINGE ATTACH POINT ON RIGHT GALLEY SERVICE DOOR. REMOVED R1 DOOR LOWER BEAM AND REPLACED IAW SRM 51-40-08, PAR 3, 51-41-02, PAR 4, 51-41-05, FIG 1, AND 51-41-01, FIG 2. TOOL TAG 6782.Apr 29, 2016 · N924AT · Boeing 717200 · Fuselage Main, StructureSDR 2016F00105Seal · damagedDURING NON SCHEDULED ROUTINE CHECK FOUND DAMAGED RT INBD SPOILER T/E SEAL.Apr 29, 2016 · N924AT · Boeing 717200 · SpoilersSDR DALA2016103107956Cusp Web · corrodedCORROSION OUT OF LIMITS ON RT CUSP WEB UPPER & LOWER SURFACE BS 447 - 452. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55 FIG. 215 AND 51-10-04 PAR 21-15 AND 37, 51-40-02.Apr 28, 2016 · N919AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016103107955Cargo Track · corrodedCORROSION ON CARGO TRACK FROM BS 994 - 1022, BETWEEN LONGERONS 27 TO 28R. THE CARGO TRACK WAS REPLACED IAW SRM 51-41-01, 51-40-08, AND 51-10-04 PAR 15 AND 21.Apr 28, 2016 · N926AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016050103470Frame · corrodedALC FRAME BS 870 AT LONGERON CORRODED. CLEAN, EVALUATED, TREAT WORK WITH ORNRC 0100-0101. REPAIRED FRAME AT FS 870 BETWEEN 29L AND 29R. REMOVED FASTENER IAW SRM 51-41-01, BLENDED AREA IAW SRM 53-00-00, FIG 103, REMOVING OUT OF LIMITS AREA IAW SRM 53-20-07, RApr 28, 2016 · N924AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016042903432Floor Panel · crackedCRACKED PASSENGER FLOOR PANEL. FLOOR PANEL FABRICATED IAW ER/A 545151-14 REV ORIGINAL.Apr 28, 2016 · N926AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016042903431Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 620GB. DUE TO EXCESSIVE CORROSION FUEL ACCESS PLATE NR 620GB WAS REPLACED IAW SRM 57-10-01 CONDITION III.Apr 28, 2016 · N926AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016042903430Cusp Web · corrodedCORROSION ON RT CUSP WEB UPPER, LOWER SURFACE BETWEEN BS 486 TO BS 501. AREA WAS REPAIRED IAW SRM 53-00-55, FIG 216 AND 51-10-04, PAR 15, 21, 37 UT WAS ACCOMPLISHED NDT SPM 04-00-07, PAR 5, FIG 3, ORIGINAL THICKNESS ON WEB IS 0.020" REMAINING IS 0.010". THERApr 28, 2016 · N919AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016042903429Floor Panel · crackedCRACKED PASSENGER FLOOR PANEL. FLOOR PANEL FABRICATED IAW ER/A 545151-14, REV. ORIGINAL.Apr 28, 2016 · N926AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016042903428Cargo Track · corrodedCORROSION ON RT CARGO TRACK FROM BS 816 TO 889. RT CARGO TRACK WAS REPLACED IAW SRM 51-41-01.Apr 28, 2016 · N926AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016042903427Cargo Track · corrodedCORROSION ON RT CARGO TRACK FROM BS 900 TO 954. CARGO TRACK WAS REPLACED IAW SRM 51-41-01.Apr 28, 2016 · N926AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016042903426Cargo Track · corrodedCORROSION ON LT CARGO TRACK FROM BS 816 TO 889. CARGO TRACK WAS REPLACED IAW SRM 51-40-08, 51-41-01, 51-10-4.Apr 28, 2016 · N926AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016050103467Fitting · corrodedCORROSION FOUND UNDER FLIGHT DECK FLOOR PANEL 211ANF F/O AFT OTBD SEAT TRACK FITTING. CHECK LIMITS, CLEAN, BLEND 53-00-00. BLENDED CORROSION ON SEAT TRACK. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, PG 105, FIG 103. REPLACED SEAT TRACK F/O AFT OTBD SEAT TRApr 27, 2016 · N924AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2016042803395Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN ROWS 15-18 OF THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.Apr 27, 2016 · N951AT · Boeing 717200 · Emergency LightingSDR DALA2016042803394Skin · corrodedCORROSION ON UPPER CENTER WING SKIN AFT EDGE FROM BS XCW 10 TO XCW=50 AT LT MLG WHEEL WELL FWD BULKHEAD, SM, CARD 3, ZONE 140. CORROSION WAS REMOVED, MEASURE NDT SPM 04.00.07 PAR 5, FIG 3, SH 1-2, ORIGINAL THICKNESS 0.177" REMAINING THICKNESS 0.157" WITHIN LIApr 27, 2016 · N926AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016042803393Access Panel · corrodedCORROSION ON COUNTERSINK OF FUEL ACCESS DOOR. OUT OF LIMITS FUEL ACCESS PLATE WAS REPLACED IAW SRM 57-10-01.Apr 27, 2016 · N926AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016042803392Angle · crackedCRACKED ZEE ON LOWER LT CORNER AT AFT CABIN BULKHEAD DOOR. DAMAGE ZEE WAS REPLACED FOR NEW 1 IAW SRM 51-41-02.Apr 27, 2016 · N926AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016042803391Floor Panel · crackedCRACKED PASSENGER FLOOR PANEL. FLOOR PANEL FABRICATED IAW ER/A 545151-14, REV ORIGINAL SECTION I.Apr 27, 2016 · N926AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016050603716Door Frame · corrodedFWD CARGO DOOR JAMB CORRODED IN SEVERAL PLACES AT LOWER PART OF JAMB. MARKED. REPLACED FORWARD CARGO LOWER PAN SECTION IAW SRM 53-20-15, REPAIR 6. REPLACED 2 EA LOWER SEAL DEPRESSOR SPLICES IAW SRM 51-41-02. TAG 1553387.Apr 26, 2016 · N924AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016050303562Frame · corrodedALC FRAME BS 889 CORRODED BETWEEN LONGERON 29L-29R. REPAIRED FRAME AT FS 889 BETWEEN LONGERON 29L AND 29R BY BLENDING AREA IAW SRM 53-00-00, FIG 103, REMOVED SECTION THAT WAS OUT OF LIMITS IAW SRM 53-20-07, AND INSTALLED REPAIR FILLER, CHANNELS IAW SRM 53-20-Apr 26, 2016 · N924AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016050103460Scuff Plate · crackedAFT CARGO SCUFF PLATE CRACKED AT FWD INBD END AND SAME END DOES NOT SET FLUSH WITH FLOOR PANELS. WELD REPAIR SCUFF PLATE. REF ORNRC 66531-0100-0005. AFT CARGO SCUFF PLATE FWD INBD REPAIR IAW STEPS 3 THRU 7 IAW ER/A 54149-14MA. W/O 66532-0012 FOR ALL MAINTENApr 26, 2016 · N924AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016042703390Access Panel · corrodedCORROSION OUT OF LIMITS ON FUEL ACCESS PANEL 520CT. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01 AND IPC 57-22-01-01.Apr 26, 2016 · N926AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016042703389Doubler · corrodedCORROSION AT PRODUCTION DOUBLER UNDER LONGERON 30, BS 969. REPAIRED IAW ER/A 5451-04-14, REV ORIGINAL.Apr 26, 2016 · N926AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016042703388Cusp Web · out of limitsOUT OF LIMITS LT CUSP WEB UPPER AND LOWER SURFACE BETWEEN BS 525 TO 526 AND 530 TO 531, X 60 TO X 54. REPAIRED IAW SRM 53-00-55, FIG 216 51-10-04 PAR 15, 21, AND 37.Apr 26, 2016 · N919AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016042703387Cusp Web · crackedCRACK ON RT CUSP WEB, BS 645. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 215, SRM 51-41-05, 51-41-02, SRM 53-20-51, 51-10-04, PAR 15, 21.Apr 26, 2016 · N919AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016050103471Cusp Web · crackedUPPER CABIN FLOOR CUSP WEB BS 672, LBL 42 IS CRACKED REPLACE CUSP WEB. REF ORNRC 66531-0200-0102. REPLACED CUSP WEB IN UPPER CABIN AT BS 672, LBL42 IAW SRM 51-41-02, PG 1, PARA 4 AND 51-41-08, PG 9, PARA 7.Apr 25, 2016 · N924AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR HALA2016042500122Tire · delaminatedNR 3 MLG TIRE DELAMINATED. TIRE PRESSURE AT REMOVAL 170PSI. R & R NR 3 MLG TIRE IAW AMM 32-41-01. SPIN CK OK.Apr 25, 2016 · N479HA · Boeing 717200 · TireSDR DALA2016042603271Battery Pack · dischargedDURING LINE CHECK, MAINTENANCE FOUND THAT BOTH THE L1 AND L2 MAIN CABIN DOORS, EMERGENCY LIGHT HANDLE ILLUMINATOR WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.Apr 25, 2016 · N989AT · Boeing 717200 · Emergency LightingSDR DALA2016042603270Frame · corrodedLOWER FUSELAGE, ELECTRONIC EQUIPMENT COMPARTMENT, MAIN FRAME, BS 140-L30, CORROSION FWD OF ELECTRONIC EQUIPMENT OPENING, MARKED. BLENDED NOTED AREAS IAW SRM 51-10-04, SECTION 26. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, FIG 103. REPAIRED OUT OF LIMITS ARApr 25, 2016 · N924AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016042603269Pan · crackedCRACKED UPPER PAN AT RT, FWD OVERWING EMERGENCY EXIT DOOR JAMB. CRACK WAS STOPPED IAW 53-20-15, FIG 201, REP 8. NEW DOUBLER WAS DRILLED IAW 51-40-08. NEW DOUBLER WAS INSTALLED IAW 51-40-02. LENGTH CRACK .265".Apr 25, 2016 · N926AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016042603268Longeron · corrodedCORROSION ON LONGERON 30 FROM BS 889 TO 927 AT AFT CARGO COMPARTMENT. THE LONGERON WAS REPLACED IAW SRM 53-20-05, FIG 201, 51-41-02, AND 51-41-05.Apr 25, 2016 · N926AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016042603267Longeron · corrodedCORROSION ON LONGERON 30 BETWEEN BS 927 - 1000 ON AFT CARGO COMPARTMENT. THE LONGERON WAS REPLACED IAW SRM 53-20-05, FIG 201, 51-41-02, AND 51-41-05.Apr 25, 2016 · N926AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016042503196Cusp Web · puncturedPUNCTURE ON LT CUSP WEB BS 715, BETWEEN X 54 - 44. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 219, SHEET 1 AND 51-10-04, PAR 15, 21.Apr 24, 2016 · N919AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016042503195Skin · crackedCRACK ON FUSELAGE SKIN BS 1086.5, LONGERON 14L. SKIN WAS REPAIRED IAW ETI-17-16-002, REV 2 AND ER/A 545090-14, REV ORIGINAL.Apr 24, 2016 · N926AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016042503194Frame · crackedCRACK ON FRAME BS 256 LONGERON 18L. FRAME WAS REPLACED IAW DWG 9911524, REV N AND SRM 51-40-5, 51-40-2, AND 51-10-04, PAR 15 AND 21.Apr 24, 2016 · N919AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016042503193Pan · crackedCRACK ON LWR FWRD CORNER WINDOW RING PAN BS 560 LONGERON 14 LT AT PAX CABIN. SM, CARD 21, ZONE 201. DAMAGE WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, 51-41-02, 51-41-05, 51-20-09, AND 51-10-04, PAR 15 AND 21. CRACK LENGTH: 0.093.Apr 24, 2016 · N919AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016042503192Pan · crackedCRACK ON UPPER/AFT WINDOW RING PAN STA 851. DAMAGE WAS REPAIRED IAW SRM 56-20-02. REPAIR 1, 51-41-02, 51-41-05, 51-20-09, AND 51-10-04 PAR 15 AND 21.Apr 24, 2016 · N919AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016042503191Pan · crackedCRACK ON LOWER/FWD WINDOW RING PAN BS 636. DAMAGE WAS REPAIRED IAW SRM 56-20-02, REPAIR 1, 51-41-02, 51-41-05, 51-20-09, AND 51-10-04, PAR 15 AND 21.Apr 24, 2016 · N919AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016042503198Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LOWER INTERIOR LIGHTS AT THE OVERWING HATCHES WERE INOPERATIVE IN 4 POSITIONS. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.Apr 23, 2016 · N967AT · Boeing 717200 · Emergency LightingSDR DALA2016042403190Frame · corrodedCORROSION ON FRAME BS 1022 BETWEEN LONGERON 20 RT TO 26 RT AT AFT CARGO COMPARTMENT, C2,SM, CARD 10, ZONE 180. CORROSION WAS REMOVED, REWORKED AREA WAS MEASURED, TREATED, AND PAINTED IAW SRM 51-10-04, PAR 26, 21 AND 5. ORIGINAL THICKNESS: 0.063", REMAINING THApr 23, 2016 · N926AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016042403189Skin · damagedBLEND OUT ON UPPER FUSELAGE SKIN BS 858 BETWEEN LONG 5-6R. AREA WAS REPAIRED IAW SRM 53-02-01, FIG 202, SHEET 3 AND 51-10-04, PAR 15, 21. HFEC WAS PERFORMED AND CRACKS WERE NOT FOUND. PERFORM GENERAL VISUAL INSPECTION INITIAL AND REPETITIVE EA 8,000 CYCLES IApr 23, 2016 · N919AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016042403188Frame · crackedCRACKED FRAME BS 679, LONGERONSS 25 AND 26R AT KEEL BEAM AREA. FRAME REPAIRED IAW SRM 51-70-11, REP 1.Apr 23, 2016 · N926AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016103107969Support · corrodedVERTICAL SUPPORT AT BS 1028 AFT BULKHEAD IN AFT CARGO BAY CORRODED. REPLACED THE SUPPORT IAW DRAWING 5965788-15A.Apr 22, 2016 · N921AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2016042503266Cam · dislodgedDURING A CHECK OF TAILCONE RELEASE MECHANISM, MAINTENANCE FOUND THE CAM ASSY FOR THE TAILCONE LATCH WAS DISLODGED. MAINTENANCE REINSTALLED THE CAM ASSY. THE TAILCONE WAS RIG CHECKED AFTER INSTALLATION AND FOUND OPERATIONAL. THE RII COMPLETED FOLLOWING MAINTApr 22, 2016 · N921AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2016042503197Skin · crackedAFT CARGO DOOR HAS CRACK IN INTERIOR SKIN AT LOWER FWD CORNER NEAR DOOR HOOK. REPAIRED CRACK IN INTERIOR SKIN AT LOWER FWD CORNER NEAR DOOR HOOK IAW SRM 52-30-02 REPAIR 4, FIG 201.Apr 22, 2016 · N924AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016042303187Rub Strip · brokenBROKEN RUBSTRIP ON FLOOR PANEL NR 223. NEW SECTIONS OF RUB STRIPS WERE INSTALLED IAW SRM 51-20-05, 51-10-04 PAR 15 DWG NR 9956320, REV G AND SRM 51-40-08.Apr 22, 2016 · N926AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016042303186Longeron · corrodedAFT CARGO BAY- L23R CORRODED AT BS 1008. REPAIRED IAW SRM 53-00-05, REPAIR 2.Apr 22, 2016 · N921AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
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