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 DALA2016092406820Battery Pack · dischargedDURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING IN THE COCKPIT AND AT DOOR L1 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.Sep 24, 2016 · N982AT · Boeing 717200 · Emergency LightingSDR DALA2016092606812Intercostal · crackedCRACK ON INTERCOSTAL ANGLE IN CEILING IN FLC STA 636. LOCATION MARKED. REPAIRED CRACKED INTERCOSTAL IAW SRM 53-00-00, REPAIR 1, FIG 201.Sep 23, 2016 · N899AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016092306787Battery Pack · dischargedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT BOTH OF THE OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.Sep 23, 2016 · N978AT · Boeing 717200 · Emergency LightingSDR DALA2016092306786Angle · damagedDAMAGE LOWER ANGLE AT LT CUSP WEB BETWEEN STA Y=889 AND STA Y=908 AND STA X=54 AND X=60 AT PASSENGER CABIN. DUCT OF ANTI-ICE SYS WAS REMOVED IAW AMM 30-10-07, PAGE BLOCK 401. SPLICE WAS REMOVED IAW SRM 51-41-05, SPLICE WAS FABRICATED IAW SRM 53-20-01, FIG 1,Sep 23, 2016 · N970AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016092406808Skin · crackedFUSELAGE SKIN CRACKED AT UPPER FASTENER IN FORMER 1152 BETWEEN L2-L3 LT LOCATION MARKED. REMOVED DAMAGE FROM FUSELAGE SKIN CRACKED AND REPAIRED IAW ER/A 549614-14. REPAIR REQUIRES REPETITIVE INSPECTIONS EVERY 3000 FLIGHT CYCLES.Sep 22, 2016 · N968AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016092306782Frame · crackedCRACKED FRAME STA 1225 CANT AND 7 HRS POSITION AT AFT ACCESSORY COMPARTMENT, SM, SN 00519. HFEC WAS ACCOMPLISHED, 01 CRACK WERE FOUND OF 1.65" IAW MD NDT SPM 06-10-01.001. VISUAL INSPECTION WAS PERFORMED NOT DISCREPANCIES WERE FOUND HFEC INSPECTION WAS ACCOMPSep 22, 2016 · N970AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016092306780Cusp Web · crackedRIGHT OTBD CUSP WEB IS CRACKED ON INBD EDGE AT STA 579. REPAIRED RT OTBD WEB AT INBD EDGE OF STA 579R IAW SRM 53-00-55, REPAIR 4 FROM 7075-T6-020 FILLER AND 7075-T6, .032 DOUBLER FILLER AND DOUBLER ALODINED PRIMED IAW SRM 51-22-01, PAGES 2 AND 3.Sep 22, 2016 · N899AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016092306779Window Frame · crackedCRACK ON UPPER OUTER RT CUTOUT OF RT WINDSHIELD, SETTLEMENT AREA, AYP, SERIAL 00620. WINDSHIELD RETAINER WAS REPLACED IAW AMM 20-60-01 914-801, SRM 51-41-02, SRM 51-40-08, DWG 9966436, REV ORIGINAL, DWG NR 5911356, REV DJ.Sep 22, 2016 · N970AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016092406809Skin · crackedCRACKS IN FUSELAGE SKIN AROUND RIVET HEAD ABOVE RT PYLON STA 1095.868, JUST ABOVE L14 RT LOCATION MARKED. SKIN CRACKS REMOVED AND REPAIRED IAW ER/A 549613-14 REQUIRES REPETITIVE INSPECTIONS EVERY 3000 FLIGHT CYCLES AFTER REPAIR.Sep 21, 2016 · N968AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016092206771Panel · damagedRIGHT WING L/E PANEL 610RB HAS 2 EA ENLARGED SCREW HOLES WITH SURROUNDING CHAFED SURFACES AND 1 EA HOLES HAS TOOLING MARKS. FABRICATED REPAIR DOUBLER FOR 2 ENLARGE HOLES AND TOOLING MARK REPAIR IAW SRM 57-40-01, REPAIR 2.Sep 20, 2016 · N968AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016F00190Spoiler · delaminatedDURING UNSCHEDULED MAINTENANCE CHECK LT INBD SPOILER WAS FOUND DELAMINATED.Sep 20, 2016 · N910AT · Boeing 717200 · SpoilersSDR DALA2016110208152Skin · corrodedSKIN CORRODED AT BS 737-745 RBL 58. BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM ALLOWABLE DAMAGE 1. REPAIRED IAW SRA 549615-14.Sep 19, 2016 · N968AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016092006726Cusp Web · crackedUPPER CABIN RT CUSP WEB, STA 670 IS CRACKED OTBD OF BL 56R TRACK, MARKED. REMOVED DAMAGED CUSP WEB FROM STA 655-756, OTBD OF RBL 44 IAW SRM 51-41-02. INSTALLED REPLACEMENT CUSP WEB FROM STA 655-756, OTBD OF RBL 44 IAW SRM 51-41-02.Sep 19, 2016 · N968AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016092006725Frame · crackedUPPER FUSELAGE, AFT CABIN, STA 1037 FRAME 17R, CRACK, MARKED. REPAIRED CRACKED FRAME AT FS 1037 AT 17R BY REMOVED DAMAGE ON FRAME AND INSTALLING FILLERS, DOUBLERS IAW SRM 53-20-07. REPAIR 1, FIG 201, USING DOUBLERS MADE FROM 7075 T6 .063 AND FILLERS MADE FROMSep 19, 2016 · N968AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016092006724Structure · crackedCRACK ON SETTLEMENT AREA HOLES OF T/E FIXED STA XW=530 AT RT WING. T/E FIXED STA XW=530 AT RT WING WAS REPAIRED IAW ETI-17-16-122 REV 1 AND ER/A 550301-14, REV ORIGINAL, ASSOCIATED ER/A 00-550301.Sep 19, 2016 · N970AT · Boeing 717200 · Wing Miscellaneous StructureSDR DALA2016091906723Battery Pack · weakDURING LINE CHECK, MAINTENANCE FOUND TWO EMERGENCY LIGHT BATTERY PACKS WERE WEAK. MAINTENANCE REPLACED THE BATTERY PACKS AND THE OPS CHECKED GOOD.Sep 19, 2016 · N992AT · Boeing 717200 · Emergency LightingSDR DALA2016092606810Frame · corrodedCORROSION ALC STA 927 FRAME FORMER, BETWEEN STA 30 AND 29L FWD AND AFT. BLEND, CHECK LIMITS, REPAIR AS REQUIRED. BLENDED CORROSION AT STA 927, LONGERON 30-29L, LOWEST MEASURED THICKNESS WAS .038", FOUND TO BE OUT OF LIMITS. REPAIRED CORRODED FRAME FORMER IASep 18, 2016 · N968AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016092306784Floor Support · crackedCENTER FLOOR PANEL SUPPORT AT STA 636 IS CRACKED. MARKED, PULLEY CLUSTER AT STA 636 REMOVED IAW SRM 51-41-01, PG 1. INTERCOSTAL REMOVED IAW SRM 51-41-02. MATERIAL VERIFICATION IS 7075-T6 .050 IAW MFG PROPRIETARY DWG 9936580, REV B. ALODINED AND PRIMED IAW Sep 18, 2016 · N968AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016091906721Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPERATIONAL CHECK WAS GOOD.Sep 18, 2016 · N947AT · Boeing 717200 · Emergency LightingSDR DALA2016091906720Cargo Track · corrodedCORROSION ON LT CARGO TRACK BS 820 - 1022 BETWEEN LONGERONS 27 AND 28L AT AFT CARGO COMPARTMENT. THE CARGO TRACK WAS REPLACED IAW SRM 51-41-01 AND 51-41-02.Sep 18, 2016 · N970AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016091906719Skin · crackedCRACK AT FUSELAGE SKIN BS 1133 BETWEEN LONGERONS 2 AND 3R. REPAIRED IAW ETI-17-16-115 REV. 2 AND ER/A 549302-14AD REV. ORIGINAL.Sep 18, 2016 · N970AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016091906722Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTING AT SEAT 32 WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS AND THE OPS CHECKED GOOD.Sep 17, 2016 · N933AT · Boeing 717200 · Emergency LightingSDR DALA2016092406807Seat Track · corrodedRIGHT IB SEAT TRACK HAS NUMEROUS AREAS CORRODED OUT OF LIMITS STA 200-588, RBL22. REPAIRED SEAT TRACKS SECTION RBL 22 BETWEEN STA 200-STA 588 FOR OUT OF LIMITS DUE TO CORROSION BLENDING WORK ACCOMPLISHED IAW SRM 53-20-52, REPAIR 5.Sep 16, 2016 · N968AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016092606811Structure · wornTHE NR 2 ENGINE UPPER COWLING PRECOOLER OUTLET INTERNAL CONTACT SURFACE IS WORN. BLEND, CHECK LIMITS. BLENDED WORN AREA IAW SRM 54-20-00 FIG 101, .038 REMAINING FROM ORIGINAL .050, FOUND TO BE OUT OF LIMITS IAW SRM 54-20-00, FIG 101, GAUGE 6784. REPAIRED ARSep 15, 2016 · N968AT · Boeing 717200 · Nacelle/Pylon Miscellaneous StructureSDR DALA2016092306781Cusp Web · crackedLEFT CUSP WEB OTBD LIGHTNING HOLE IS CRACKED AT STA 360. REMOVED LT OTBD SEAT TRACK FROM STA 200 TO STA 445. REPAIRED CUSP WEB IAW SRM 53-00-55, REPAIR 4 AND REINSTALLED SEAT TRACK IAW SRM 51-41-01, PAR 6.Sep 15, 2016 · N968AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016091606669Channel · crackedCRACKED FWD CHANNEL ON RIGHT MLG WW CUTOUT DOOR AREA. REPLACED THE CHANNEL IAW SRM 51-41-01, 51-41-02, 51-41-05, 51-40-08, 51-10-04 PARAGRAPH 15, 21, AND AMM 20-50-02-917-801.Sep 15, 2016 · N970AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016091606668Pan · corrodedMULTIPLE SPOTS OF CORROSION ON FORWARD CARGO DOOR PAN. CLEANED UP CORROSION IAW SRM 53-00-00 FIG 103. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 FIG 103). REPLACED THE PAN IAW SRM 51-41-02 SEC 4 AND 51-41-09.Sep 15, 2016 · N968AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016091606718Floor Panel · damagedUPPER CABIN FLOOR PANEL 221CF AT BS 465, LBL 22 HAS DAMAGE ON UPPER SURFACE. FABRICATED A NEW FLOOR PANEL IAW SRM 53-20-50 REPAIR 3 AND INSTALLED.Sep 14, 2016 · N968AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016091606717Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 222GF DELAMINATING. FABRICATED FLOOR PANEL IAW SRM 53-20-50 3 AND INSTALLED.Sep 14, 2016 · N968AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016091606716Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 222DF DELAMINATING. FABRICATED A NEW FLOOR PANEL IAW SRM 53-20-50 REPAIR 3 AND INSTALLED.Sep 14, 2016 · N968AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016091606715Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 223FF IS DELAMINATING. FABRICATED A NEW FLOOR PANEL IAW SRM 53-20-50, AND INSTALLED.Sep 14, 2016 · N968AT · Boeing 717200 · Fuselage Floor PanelSDR HALA2016091400355Warning Light · false activationAFT BULKHEAD DOOR ALERT ILLUMINATED CLIMBING THROUGH APPROX 2,000 FT. ,AFT BULKHEAD DOOR VERIFIED CLOSED NO DEFECTS NOTED. INTERMITTENT INDICATION WARNING MAY OCCUR. OK FOR SVC.Sep 14, 2016 · N488HA · Boeing 717200 · Door Warning SystemSDR DALA2016091506637Tab · damagedLIGHTNING STRIKE AT RT GEARED ELEVATOR TAB (BROKEN FIBERS). REPAIRED IAW SRM 51-70-09 REP 5, REMOVED AND INSTALLED IAW AMM 27-31-05.Sep 14, 2016 · N970AT · Boeing 717200 · Elevator StructureSDR DALA2016091506635Channel · crackedCRACKED RT CHANNEL BS 47 AT NLG DOOR CUTOUT. THE CHANNEL WAS REPAIRED IAW SRM 53-10-14 FIG 201.Sep 14, 2016 · N970AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016091506634Door Frame · crackedCRACKED LEFT CHANNEL BS 47 AT NLG DOOR CUTOUT. THE DOOR FRAME WAS REPAIRED IAW SRM 53-10-14 FIG 201.Sep 14, 2016 · N970AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016091506633Shear Tie · crackedSHEAR TIE CRACKED AT BS 1022 LONGERON 6R. REPLACED THE SHEAR TIE IAW SRM 53-20-07 AND DWG 9912243 AND SRM 51-41-05 PG 1.Sep 14, 2016 · N968AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2016091506632Floor Panel · corrodedCORROSION, CRACKED, LOOSE FASTENERS ON FLOOR PANEL. CORROSION REMOVED IAW SRM 51-10-04 PAR 26Sep 14, 2016 · N970AT · Boeing 717200 · Fuselage Floor PanelSDR HALA2016091400352Battery · dischargedEMERGENCY LIGHT IN COCKPIT DOES NOT ILLUMINATE WHEN ON POSITION. R & R BATTERY AT B5-123 IAW WDM 33-51-12. OPS CHECK GOOD. OK FOR SERVICE.Sep 14, 2016 · N480HA · Boeing 717200 · Emergency LightingSDR DALA2016092306785Panel · crackedELEVATOR LOWER SURFACE RT PANEL 340 KB IS CRACKED. THE PANEL IS ON THE UPPER TAIL DOCK. FABRICATED NEW PANEL 340KB IAW SRM 51-20-09 AND DWG NR 5910412, REV 05. PANEL 340KB TO BE INSTALLED ON JC 2040-0030.Sep 13, 2016 · N968AT · Boeing 717200 · Elevator, Plate/SkinSDR DALA2016091506638Seat Track · damagedUPPER CABIN SEAT TRACK LBL 22, BS 520 - 598 HAS TWO AREAS OF EXPOSED METAL. REPLACED THE SECTION OF SEAT TRACK IAW SRM 53-20-52 REPAIR 5. FABRICATED THE NEW SECTION IAW SRM 53-20-05 REPAIR 5.Sep 13, 2016 · N968AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016091506631Bulkhead · crackedENGINE PYLON SUPPORT BULKHEAD ON THE RIGHT SIDE AT LONGERON 7R IS CRACKED. REPAIRED BULKHEAD IAW SRM 53-20-07 REPAIR 1.Sep 13, 2016 · N968AT · Boeing 717200 · Fuselage Main, BulkheadSDR DALA2016091406630Access Panel · crackedLEFT WING ACCESS PANEL 520GB CRACKED. REPLACED THE ACCESS PANEL IAW AMM 28-00-00-410.Sep 13, 2016 · N968AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016091406629Floorbeam · corrodedFLOORBEAM BS 135 R RBL 40 - 50 CORRODED. REPLACED THE FLOORBEAM IAW DWN S00074 AND SRM 51-41-02.Sep 13, 2016 · N968AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2016091406628Seat Track · corrodedSEAT TRACK CORRODED. FOUND BEYOND LIMITS IAW SRM 53-00-00. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-01 PAR 6.Sep 13, 2016 · N968AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016091406589Access Panel · corrodedCORROSION ON COUNTERSINK ON FUEL ACCESS PLATE 620CB, NRC 00624. CORROSION WAS REMOVED IAW SRM 51-10-04, PAR 26. COUNTERSINK AREAS WERE MEASURED MAXIMUM COUNTERSINK DIAMETER, ALLOWABLE DOOR, PN ARB0975, IS 0.532" MAXIMUM DIAMETER MEASURED IS 0.610. THEREFORESep 13, 2016 · N970AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016091406588Longeron · corrodedCORROSION ON LONGERON 30 BETWEEN STA Y=994 AND Y=905 AT AFT CARGO COMPARTMENT. LONGERON 30, FRAME CLIPS, AND SPLICES BETWEEN STA Y=897 AND Y=1012 WERE REMOVED IAW SRM 51-41-05, 51-41-02, AND 53-20-05, REPAIR 1, FIG 201. NEW LONGERON 30 BETWEEN STA Y=897 AND Sep 13, 2016 · N970AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016091106509Support · crackedCRACKED RT NLG DOOR SUPPORT STA 64, SM, SN 00590. SUPPORT WAS REPLACED IAW SRM 51-41-05 AND DWG 9910088, REV LP 2675427.Sep 10, 2016 · N970AT · Boeing 717200 · Fuselage, Door HingeSDR DALA2016091206510Battery · dischargedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 24 IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECK WAS GOOD.Sep 9, 2016 · N936AT · Boeing 717200 · Emergency LightingSDR DALA2016090906508Battery · dischargedDURING LINE CHECK, MAINTENANCE FOUND THAT A SECTION OF THE EMERGENCY ESCAPE PATH LIGHTING WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. OPS CHECK WAS GOOD.Sep 9, 2016 · N987AT · Boeing 717200 · Emergency LightingSDR DALA2016091506636Access Panel · crackedLEFT WING ACCESS PANEL 520DB CRACKED. REPLACED THE ACCESS PANEL IAW AMM 28-00-00 410.Sep 8, 2016 · N968AT · Boeing 717200 · Wing, Plate/Skin
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