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 DALA2019081204730Skin · delaminatedDELAMINATED AREA WAS FOUND ON LOWER SKIN DENTED. DELAMINATED AREA (0.875 IN X 0.625) ON LOWER SKIN AT RT UPPER MOVABLE VANE WAS REPAIRED IAW ETI-17-19-143 REV. 2 AND ER/A 580374-14 REV. ORIG, SECTION I, PERMANENT REPAIR.Aug 10, 2019 · N945AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2019082005180Skin · corrodedFUSELAGE / SKIN / DOUBLER / STA Y=1022.091 AND L29R / ARE CORRODED. ASSOCIATED ER/A 00-580391 ADDED FOR AC 9505. (LP #1214643)Aug 9, 2019 · N945AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2019081204729Door · damagedELONGATED SCREW HOLES ON LH AFT OVERWING EMERGENCY EXIT DOOR FROM PASSENGER CABIN. LT AFT OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER ETI-17-19-135 REV 1 AND ER/A 580351-14 REV ORIGINAL SECTION I PERMANENT REPAIR.Aug 9, 2019 · N945AT · Boeing 717200 · Emergency ExitsSDR DALA2019081204728Door · damagedELONGATED SCREW HOLES ON RH FWD OVERWING EMERGENCY EXIT DOOR FROM PASSENGER CABIN. RH FWD OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER ETI-17-19-137 REV ORIGINAL AND ER/A 580352-14 REV ORIGINAL SECTION I PERMANENT REPAIR.Aug 9, 2019 · N945AT · Boeing 717200 · Emergency ExitsSDR DALA2019081204727Door · damagedELONGATED SCREW HOLES ON THE RT AFT OVERWING EMERGENCY EXIT DOOR FROM PASSENGER CABIN. RT AFT OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER ETI-17-19-138 REV ORIGINAL AND ER/A 580353-14 REV ORIGINAL SECTION I, PERMANENT REPAIR.Aug 9, 2019 · N945AT · Boeing 717200 · Emergency ExitsSDR DALA2019081204726Cargo Track · corrodedCORROSION ON LH TIE TRACK BTW STA Y=899 TO Y=1022 AT AFT CARGO COMPARTMENT. CORROSION WAS REMOVED IAW SRM 51-10-04-0G PAR 26. MAXIMUM REMAINING THICKNESS IS 0.038 AND THEREFORE IT IS OUT OF LIMITS IAW SRM 53-20-52-1A-2 FIG 101. LT TIE TRACK WAS REPLACED IAWAug 9, 2019 · N945AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2019080904674Battery Pack · inoperativeLT AND RT LWR AFT EMER LIGHTS INOP. REMOVED AND REPLACED EMER LIGHT BATTERY PACK AT STA. 850R. OPS CHECK GOOD. (LP5743702)Aug 8, 2019 · N992AT · Boeing 717200 · Emergency LightingSDR DALA2019080904673Frame · crackedAWR HIDDEN CRACK: AFTER REMOVAL OF LONGERON IN REFERENCE NRC 00484 CRACK ON FRAME WAS FOUND STA Y 1037 AND LONG 17 LH. AREA WAS REPAIRED PER B717-200 SRM 53-20-07-2R-4 (ET) HFEC INSPECTION WAS PERFORMED ON FRAME STA Y 1037 AND LONG 17LH. NO CRACKS WERE FOUND AAug 8, 2019 · N945AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019080904672Power Supply · inoperativeDURING CHECK OF CONDITION OF THE LIGHTED EXIT SIGN LOCATED ABOVE VENTRAL DOOR THE LIGHT DID NOT WORK.. REF CARD 1130-2002 STEP 28. EMERGENCY LIGHTS POWER SUPPLY WAS REMOVED AND A SERVISEABLE EMERGENCY LIGHTS POWER SUPPLY WAS INSTALLED IAW AMM 33-51-03-400-802,Aug 8, 2019 · N944AT · Boeing 717200 · Emergency LightingSDR DALA2019080804651Door Frame · crackedCRACK ON LH DOOR JAM STA 46 APROX AT NLG WHEEL WELL (FYT). NRC 00402: CRACK ON LH DOOR JAM STA 46 APROX AT NLG WHEEL WELL WAS REPAIRED PER B717-200 SRM 53-10-14-2R-2 FIG 201. (LP #1211495)Aug 8, 2019 · N945AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019080804650Door Frame · crackedCRACK ON RH DOOR JAM STA 46 APROX AT NLG WHEEL WELL (FYT). NRC 00404: CRACK ON RH DOOR JAM STA 46 APROX AT NLG WHEEL WELL WAS REPAIRED PER B717-200 SRM 53-10-14-2R-2 FIG 201. (LP #1211487)Aug 8, 2019 · N945AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2019080804649Access Panel · corrodedCORROSION ON FUEL ACCESS PANELS (620CB & 620GB) ON COUNTERSINK AND SETTLEMENT AREA. (FUS). NRC 00619: LEVEL CORROSION 2, FUEL ACCESS PANELS #620CB & 620GB ARE OUT OF LIMITS AND WERE REPLACED. EFFECTIVITY WAS VERIFIED PER B717-200 IPC 57-23-01- 01 AND MUST BE IAug 7, 2019 · N945AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2019080804647Gusset · crackedCRACK GUSSET BTW STRGR 7R STA 1022 AFT FACE OF BULKHEAD (CPAX). NRC 00530: CRACK GUSSET BTW STRGR 7R STA 1022 AFT FACE OF BULKHEAD WAS REPAIRED PER ETI-17-19-126 REV 1 AND ER /A 580279-14 REV ORIG. SECTION I : PERMANENT REPAIR. ASSOCIATED ER/A 14-580279 ADDED Aug 7, 2019 · N945AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2019102890013Arm · wornPD:TIME / WEAR / CORROSION / OS&US DIAMETERS,NEEDS ERA REPAIR. CA:OVERHAULED. THE WORK SPECIFIED IN BLOCK(S) 11/12 ACCOMPLISHED WITHREFERENCE TO OEM CMM 32-14-1, REV. 060 11/01/2018 WITH APPLICABLEDELTA SAug 5, 2019 · Boeing 717200 · Main Landing GearSDR DALA2019080654584Cover · disengagedTHE TAIL CONE SLIDE COVER WAS FOUND TO BE DISENGAGED. THE SLIDE ASSEMBLY, SN 1571RP, WAS INSPECTED AND THE COVER WAS CLEARED TO BE RE-INSTALLED. INSTALLED SLIDE PER B717 WORKCARD 2561- 9006, STEPS 6-10. ALL RII COMPONENTS WERE SATISFIED AND THE AIRCRAFT WAS REAug 5, 2019 · N949AT · Boeing 717200 · Escape SlideSDR DALA2019080604583Threshold · corrodedNUMEROUS AREAS OF CORROSION WAS FOUND AT THE AFT CARGO THRESHOLD. REPLACED AFT CARGO DOOR THRESHOLD REF B717 SRM 53-20-15-2R.Aug 5, 2019 · N991AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019080504574Bushing · damagedHALF BUSHING GROOVED AT 4TH FROM O/B GEARED TAB HINGE, I/B LEG. REPLACED THE BUSHINGS.Aug 4, 2019 · N991AT · Boeing 717200 · Elevator, Tab StructureSDR DALA2019080504585Housing · looseTHE CREW DIVERTED THE FLIGHT DUE TO THE AIRCRAFT DEVELOPING A FUEL LEAK WHILE ENROUTE. MAINTENANCE FOUND THE FUEL FILTER HOUSING COVER ATTACHMENT LOOSE DUE TO A MIGRATED INSERT. THE FUEL FILTER HOUSING WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.Aug 3, 2019 · N989AT · Boeing 717200 · Engine Fuel DistributionSDR DALA2019080504575Packing · damagedAPPROX 40 MINUTES AFTER TAKEOFF, THE LAT FUEL UNBAL MESSAGE ANNUNCIATED. REBALANCED FUEL TRANSFER AND DIAGNOSED LEFT FUEL SYSTEM WAS LOSING FUEL. MAINTENANCE FOUND FUEL LEAKING FROM LOW PRESS FUEL FILTER CAP AND FROM BYPASS VENT VALVE ON THE NR 1 ENGINE. REPLAAug 3, 2019 · N989AT · Boeing 717200 · Fuel StorageSDR DALA2019080544573Longeron · crackedCRACKED LONGERON 6R, BS 1022, AFT FACE OF BULKHEAD. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2.Aug 3, 2019 · N945AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019080544572Longeron · crackedCRACKED LONGERON 4R, BS 1022 AFT FACE OF BULKHEAD. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2.Aug 3, 2019 · N945AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019080544571Longeron · crackedCRACKED LONGERON 7L, BS 1022 AFT FACE OF BULKHEAD. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2.Aug 3, 2019 · N945AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019080544570Longeron · crackedCRACKED LONGERON 5R, BS 1022 AFT FACE OF BULKHEAD. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2.Aug 3, 2019 · N945AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019080544569Longeron · crackedCRACK ON LONGERON 17L, BS 1022 AFT FACE OF BULKHEAD. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R-2.Aug 3, 2019 · N945AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2019080544568Cusp Web · crackedTWO CRACKS AT THE RT PREVIOUS REPAIR CUSP WEB BETWEEN BS 794 TO 813 AND -44 TO -54. THE CUSP WEB WAS REPLACED IAW SRM 51-41-02-0G, 51-41-01, AND DWG 9910151-150 REV CH.Aug 3, 2019 · N945AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019080904677Skin · damagedCOMPOSITE EXPOSED ON LEFT ELEVATOR ANTI-FLOAT TAB. REMOVED LT ELEVATOR GEARED TAB REF B717 AMM 27-31-05 TAB ASSY, GEARE OFF 92-5522-9-0007 00010. INSTALLED LT ELEVATOR GEARED TAB REF B717 AMM 27-31-05. NRC 132. TAB ASSY, GEAR ON 92-5522-9-0007 00129. (LP120205Aug 2, 2019 · N991AT · Boeing 717200 · Elevator, Tab StructureSDR DALA2019080904676Skin · damagedCOMPOSITE EXPOSED ON LEFT ELEVATOR CONTROL TAB. REMOVE LT ELEVATOR CONTROL TAB, ROUTED TO SHOP FOR REPAIR REF B717 AMM 27-31-04 TAB ASSY, CONTR OFF 95-5525-9-0003 09529. INSTALLED L/H ELEVATOR CONTROL TAB. REF B-717 AMM 27-31-04 TAB ASSY, ON 95-5525-9-0003 551Aug 2, 2019 · N991AT · Boeing 717200 · Elevator, Tab StructureSDR DALA2019080904675Skin · damagedCOMPOSITE EXPOSED ON RIGHT ELEVATOR CONTROL TAB. REMOVED RT ELEVATOR CONTROL TAB REF B717 AMM 27-31-04 TAB ASSY, CONTR OFF 95-5525-9-0002 09529. INSTALLED R/H ELEVATOR CONTROL TAB. REF B-717 AMM 27-31-04 TAB ASSY, CONTR ON 95-5525-9-0002 00268. (LP1202039)Aug 2, 2019 · N991AT · Boeing 717200 · Elevator, Tab StructureSDR DALA2019080204536Frame · crackedCRACK ON LOWER FWD CORNER OF LH RING PAN BTW STA Y=889 TO 908 AT PASSENGER CABIN (CPAX). NRC 00636: CRACK ON LOWER FWD CORNER OF LH RING PAN BTW STA Y=889 TO 908 AT PASSENGER CABIN DAMAGE AREA WAS REMOVED PER B717-200 SRM 56-20-02-2R-1 FIG. 202. REPAIR ANGLE WAug 1, 2019 · N945AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019080204535Frame · crackedCRACKED RINGPAN WINDOW BTW STA 851 TO STA 870 AT AFT UPPER CORNER SIDE (CPAX). NRC 00453: CRACKED RING PAN WINDOW DAMAGED AREA WAS REMOVED PER B717-200 SRM 56-20-02-2R-1 FIG. 202. REPAIR ANGLE WAS FABRICATED AND INSTALLED PER B717-200 SRM 56-20-02-2R-1 FIG. 20Aug 1, 2019 · N945AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019080204534Frame · crackedCRACKED RINGPAN WINDOW BTW STA 832 TO STA 851 AT AFT UPPER CORNER SIDE (CPAX). NRC 00454: DAMAGED AREA WAS REMOVED PER B717-200 SRM 56-20-02-2R-1 FIG. 202. REPAIR ANGLE WAS FABRICATED AND INSTALLED PER B717-200 SRM 56-20-02-2R-1 FIG. 202, 51-41-02-0G, AND 51-4Aug 1, 2019 · N945AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019080204533Window Frame · crackedCRACKED RINGPAN WINDOW BTW STA 908 TO STA 889 AT AFT UPPER CORNER SIDE (CPAX). NRC 00447: CRACKED RINGPAN WINDOW DAMAGED AREA WAS REMOVED PER B717-200 SRM 56-20-02-2R-1 FIG. 202. REPAIR ANGLE WAS FABRICATED AND INSTALLED PER B717-200 SRM 56-20-02-2R-1 FIG. 202Aug 1, 2019 · N945AT · Boeing 717200 · Fuselage Main, StructureSDR HALA2019080200379Apu · malfunctionedAPU AUTOMATICALLY SHUTDOWN AT GATE. TROUBLESHOT AND FOUND A FAULT ON APU, FAULT CODE 494157, STARTER MOTOR AND ALSO APU STARER CLUTCH. REMOVED AND REPLACED IAW AMM 49-44-01-400-801, AND 49-44-03. CONDITION SAME. R & R THE APU ASSY IAW E1128-717-49-006. LEAKJul 31, 2019 · N481HA · Boeing 717200 · APU Start/Ignition SystemSDR HALA2019080100377Water Separator · odorON GROUND BURNING OIL SMELL WHEN PACKS ON APU. APU BLEED AIR MODULATING VALVE. REMOVED AND REPLACED BOTH WATER SEPERATORS FOR AIR CONDITIONING. APU COMPARTMENT INSPECTED. NO OIL LEAK. REACTIVATED APU BLEED AIR VALVE AND PERFORMED APU RUN, CHECKED NO OIL SMEJul 31, 2019 · N486HA · Boeing 717200 · Humidity Control SystemSDR DALA2019080104516Access Panel · corrodedCORROSION ON FUEL ACCESS PANELS #520CT AND #620CT AT SETTLEMENT AREA. NRC #00658: CORROSION LEVEL 2, UPPER WING ACCESS DOOR #520CT AND #620CT WERE REPLACED PER B717-200 SRM 57-10-01 AND VERIFIED PER IPC 57-22-01-01 IMAGE 065. (LP #1199639)Jul 31, 2019 · N945AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2019073100000Skin Panel · delaminatedINITIAL INSPECTION, DELAMINATED AREAS ON EXTERNAL WING SPOILER PANEL, UPPER AND LOWER SURFACE.Jul 31, 2019 · N963AT · Boeing 717200 · SpoilersSDR DALA2019073104497Vane · delaminatedDELAMINATION WAS FOUND FROM STA XF 91 TO XF 99, AT LEFT INBD FLAP AFT MOVABLE VANE IN REF NRC 00337. AI. NRC 00655: REPAIR WAS PERFORMED ON DELAMINATION AREA FROM STA XF 91 TO XF 99, AT LEFT INBD FLAP AFT MOVABLE VANE PER SRM 51-70-02-0G PAR.15.A.(1) TO (15) AJul 30, 2019 · N945AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2019073004485Floor Panel · delaminatedDELAMINATED FLOOR PANELS #222DF, 222GF, 222KF, 222ACF, AND 222AAF. PAX CABIN. (CAB PAX). NRC 00605: FLOOR PANELS #222DF, 222GF, 222KF, 222ACF, AND 222AAF WERE FABRICATED, REPLACED, AND IDENTIFIED PER SRM 53-20-50-2R-3. (LP #1196723)Jul 30, 2019 · N945AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2019073004484Floor Panel · crackedCRACK AND DELAMINATION ON FLOOR PANELS #222ARF AND 223BF. PAX CABIN. (CAB. PAX). NRC 00666: FLOOR PANEL #222ARF AND 223BF WERE FABRICATED, REPLACED, AND IDENTIFIED PER SRM 53-20- 50-2R-3. (LP #1196590)Jul 29, 2019 · N945AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2019073004483Access Panel · corrodedCORROSION ON COUNTERSINK HOLES OF FUEL ACCESS PLATES #520FT, 620AT, AND 620FT WERE FOUND OUT OF LIMITS REF SRM 57-10-01-2R REPAIR 2 CORROSION LEVEL II. NRC 00801: FUEL ACCESS PLATES WERE REPLACED AND WILL BE INSTALLED ON 2040- 0012 AND AMDS 2040-0010. (LP #119Jul 29, 2019 · N944AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2019072904460Battery Pack · dischargedEMERGENCY LIGHTS #L2-873, L2-845, L2-846, L2-848, AND L2-847 WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE B5-260 BATTERY PACK AND CHARGER PER AMM 33-51-03. OPERATIONAL CHECK WAS GOOD. (LP #4621054)Jul 29, 2019 · N957AT · Boeing 717200 · Emergency LightingSDR DALA2019072904459Access Panel · damagedELONGATED HOLES IN ACCESS PLATE #520MB AND 520FT AT FUEL TANK LEFT WING (AI). NRC 00611: ELONGATED HOLES IN FUEL ACCESS PLATE #520MB WAS REPAIRED PER SRM 57-10-01-2R, REPAIR 2, CONDITION II AND FUEL ACCESS PLATE #520FT WAS REPLACED AND MUST BE INSTALLED ON 204Jul 28, 2019 · N944AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2019072904458Cusp Web · corrodedCRACK ON LT CUSP WEB BTW STA Y=218 AND X=44 (IN REF TO 5300-2020). (CPAX). NRC 369: CRACK ON LT CUSP WEB BTW STA Y=218 AND X=44 DAMAGED AREA ON LT CUSP WEB BTW STA Y=218 AND X=44 WAS TRIMED OUT PER SRM 53-00-55-2R FIGURE 212. REPAIR PARTS WERE FABRICATED AND IJul 28, 2019 · N945AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019072804457Battery Pack · dischargedTHE EMERGENCY CEILING LIGHTS AT ROW 10 THRU 13 ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-227 REF AMM 33-51. OPERATIONAL CHECK IS GOOD. (LP #6005927)Jul 28, 2019 · N927AT · Boeing 717200 · Emergency LightingSDR DALA2019072904482Channel · crackedCRACKS (2 EA.) IN CHANNEL FLOOR PANEL #222ZF. NRC 00797: CHANNEL FLOOR PANEL #222ZF WAS REPAIRED PER SRM 53-20-50-2R-5 REPAIR 5. (LP #1193258)Jul 27, 2019 · N944AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2019072804456Intercostal · corrodedCORROSION ON INTERCOSTAL FROM STA Y=946 TO Y=954 ABOVE LONG PROJECTION 29R AT AFT CARGO COMPARTMENT. NRC 00348: CORROSION LEVEL 2, INTERCOSTAL FROM STA Y=946 TO Y=954 ABOVE LONG PROJECTION 29R AT AFT CARGO COMPARTMENT WAS REPAIRED PER SRM 51-70-11-2R. (LP #119Jul 27, 2019 · N944AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019072704455Frame · corrodedEXFOLATION ON FRAME STA Y=1022 BTW LONG 28R TO 28L AT AFT CARGO COMPARTMENT. NRC 00362: CORROSION LEVEL 2, FRAME STA Y=1022 BTW LONG 28R TO 28L AT AFT CARGO COMPARTMENT WAS REPAIRED PER SRM 53-20-07-2R PROCEDURE 3, REPAIR 3 FIG 201 SHEET 4 AND 5. (LP #1191865)Jul 27, 2019 · N944AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2024052305458Web · corrodedCORROSION ON WEB AT L26 RH TO L25 RH BTW STA Y=946 TO Y=949 APROX (C2). SUMMARY: OF NRC 00664: WEB WAS REPAIRED PER B717 SRM 51-70-10-2R-1 FIG 201. (LP #0136346)Jul 26, 2019 · N951AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2019072704454Frame · corrodedCORROSION ON FRAME STA Y=927 BTW LONG 28L TO LONG 24R AT AFT CARGO COMPARTMENT. NRC 00338: CORROSION LEVEL 2, FRAME STA Y=927 BTW LONG 28L TO LONG 24R AT AFT CARGO COMPARTMENT WAS REPAIRED PER SRM 53-20-07-2R-3- FIG. 201. (LP #1191594)Jul 26, 2019 · N944AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2019072704453Skin · puncturedPUNCTURE ON FUSELAGE EXTERNAL SKIN BTW STA 160 AND 165 STRINGERS 29 AND 30 LT SIDE (SM). NRC 00126: FUSELAGE EXTERNAL SKIN BTW STA 160 AND 165 STRINGERS 29 AND 30 LT SIDE WAS REPAIRED PER ETI-17-19-115 REV: 2 AND ER/A: 579976-14 REV: ORIGINAL. ASSOCIATED ER/A Jul 26, 2019 · N944AT · Boeing 717200 · Fuselage Main, Plate/Skin
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