Boeing 717-200

Service difficulty reports · 18,771

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  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 DALA2016103007943Cusp Web · crackedBS 717 LBL 45 CUSP WEB CRACKED. REPAIRED THE CUSP WEB IAW SRM 53-00-55 REPAIR 4.Oct 29, 2016 · N922AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016110308233Shear Tie · crackedCRACK IN A SHEAR TIE AT BS 1022 FWD SIDE OF THE BULKHEAD AT LONGERON 14L. REPLACED THE SHEAR TIE IAW SRM 51-41-05.Oct 28, 2016 · N922AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2016103107951Sign · crackedTHE PILOT REPORTED THAT THE CENTER ISLE EXIT SIGN AT THE OVERWING EXIT HATCH IS CRACKED AND HANGING DOWN. MAINTENANCE ADJUSTED THE CORNER OF THE EXIT SIGN AND RETURNED THE EMERGENCY LIGHTS TO SERVICEABLE CONDITION.Oct 28, 2016 · N924AT · Boeing 717200 · Emergency LightingSDR DALA2016102907942Cusp Web · crackedCRACKED RT CUSP WEB BELOW SEAT TRACK X 44 BS 219. DAMAGE AREA WAS REPAIRED IAW SRM 53-00-55 FIG 219 AND 51-41-02.Oct 28, 2016 · N969AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016102907941Stop Fitting · crackedCRACKED STOP FITTINGS ON FWD EDGE OF AFT CARGO DOOR. THE STOP FITTINGS WERE REPLACED IAW SRM 51-41-01 AND 51-41-05.Oct 28, 2016 · N969AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016102807811Door Frame · crackedCRACKED UPPER AREA OF AFT VENTRAL DOOR FRAME. THE DOOR FRAME WAS REPAIRED IAW SRM 51-41-02 PAR. 7.C. (1), 51-41-05 PAR 10 FIG. 19, AND SRM 53-00-00 REPAIR 1, FIGURE 201, 51-41-02 AND 51-41-05.Oct 27, 2016 · N969AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016102807810Cusp Web · corrodedRIGHT CUSP WEB HAS CORROSION BETWEEN BS 1002-1022. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-20-51 FIG 1 ITEM 2. REPAIRED THE CUSP WEB IAW SRM 53-00-55 REPAIR 4.Oct 27, 2016 · N987AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016102807809Seat Track · corrodedSEAT TRACK FOUND TO BE CORRODED BEYOND LIMITS, AT RBL 56 IN MULTIPLE AREAS BS 200-590. REPLACED THE SEAT TRACK IAW SRM 53-20-52 REPAIR 5 AND 51-41-01.Oct 27, 2016 · N987AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016102807806Frame · corrodedFRAME AT BS 908 HAS CORROSION ON UPPER AND LOWER AREAS ON LOWER FLANGE BETWEEN STRINTERS 29 AND 30L. BLEND CORRODED AREA IAW SRM 53-00-00 FIG 103, AND FOUND TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-00 FIG 103. REPAIRED IAW SRM 53-20-07 REPAIR 3.Oct 27, 2016 · N987AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016102807805Cusp Web · crackedCRACK ON RT CUSP WEB BS 617 - 636. DAMAGE WAS REMOVED IAW SRM 53-00-00 FIG 101. HFEC INSPECTION WAS ACCOMPLISHED AFTER DAMAGE REMOVED AND NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001.Oct 27, 2016 · N969AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016102807804Cusp Web · crackedCRACK ON LT CUSP WEB BS 623 BETWEEN X 54 - X 60. THE DAMAGE WAS REMOVED IAW SRM 53-00-00 FIG 101.Oct 27, 2016 · N969AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016102707767Lens · detachedDURING LINE CHECK, MAINTENANCE FOUND THAT THE CATWALK EMERGENCY EXIT LIGHT LOST IT`S LENS. MAINTENANCE REPLACED THE LENS AND THE OPS CHECKED GOOD.Oct 27, 2016 · N607AT · Boeing 717200 · Emergency LightingSDR DALA2017010500110Skin · corrodedCORR SKIN AT STA 1002 STR 28R-25R. BLENDED CORROSION ON INTERNAL DOUBLER "SKIN" AT STA 1002 L25R-L28R FOUND TO BE WITHIN LIMITS IAW SRM 53-20-15 NOMINAL .071 .040. REMAINING REPAIRED OUT OF LIMITS AREA IAW ER/A 549633-14.Oct 26, 2016 · N987AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR HALA2016102600377Warning System · activated OPEN - ATO - TANK L AFT PUMP LO LIGHT ILLUMINATED ON THROTTLE ADV FOR T/O, MAIN TANK FUEL AC BOOST PUMPS. DEFERRED USING MEL 28-22-01.Oct 26, 2016 · N484HA · Boeing 717200 · Fuel Indicating SystemSDR DALA2016102707764Floor Panel · delaminatedDELAMINATED FLOOR PANEL 221PF IN THE PAX CABIN. THE FLOOR PANEL WAS REPAIRED IAW SRM 53-20-50 AND AMM 20-60-10 340-801 SUBTASK 390-002.Oct 26, 2016 · N969AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016102607650Stringer · corrodedSTRINGER 30 CORRODED AT BS 908. BLENDED CORROSION 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 53-20-05 REPAIR 1, AND SRM 53-20-05 103.Oct 25, 2016 · N987AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016102607645Intercostal · crackedINTERCOSTAL AT BS 665 UNDER LEFT INBOARD SEAT TRACK CRACKED. REPLACED IAW DWG 9911751 REV Z.Oct 25, 2016 · N987AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016102507500Lens · missingDURING LINE CHECK, MAINTENANCE FOUND THAT THE AFT CABIN DOOR EMERGENCY EXIT SIGN LOST THE LENS/COVER. MAINTENANCE REPLACED THE LENS/COVER AND THE OPERATIONAL CHECK WAS GOOD.Oct 25, 2016 · N974AT · Boeing 717200 · Emergency LightingSDR DALA2016102807808Seat Track · damagedRIGHT OTBD SEAT TRACK RBL 56 IS GOUGED AND CORRODED IN SEVERAL AREAS FROM BS 813 - 908. BLENDED, AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-01.Oct 24, 2016 · N987AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016102707765Seat Track · damagedRIGHT OUTBOARD SEAT TRACK HAS KNICKS AND CORROSION BS 500 - 600. BLENDED AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-41-01 AND SRM 53-20-52 REPAIR 5.Oct 24, 2016 · N987AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016102607649Intercostal · crackedINTERCOSTAL AT BS 665 UNDER THE RIGHT INBOARD SEAT TRACK CRACKED. REPLACED THE INTERCOSTAL IAW DWG 9911751 REV 2.Oct 24, 2016 · N987AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016102507499Pan · crackedCRACKED RING PAN ON AFT LOWER CORNER STA Y=578, FWD UPPER AND LOWER CORNER STA Y=795, AND FWD LOWER CORNER STA Y=890 AT PAX CABIN RT SIDE. REPAIRED RING PAN ON AFT LOWER CORNER STA Y=578, FWD UPPER AND LOWER CORNER STA Y=795, AND FWD LOWER CORNER STA Y=890 RTOct 24, 2016 · N969AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016102507498Pan · crackedCRACKED RING PAN ON FWD UPPER AND LOWER CORNER STA Y=637, FWD UPPER CORNER STA Y=656, AFT LOWER CORNER STA Y=713, AFT UPPER CORNER STA Y=869 AT PAX CABIN LT SIDE. RING PAN ON FWD UPPER AND LOWER CORNER STA Y=637, FWD UPPER CORNER STA Y=656, AFT LOWER CORNER SOct 24, 2016 · N969AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016102707766Cusp Web · crackedCUSP WEB AT BS 218 WAS FOUND CRACKED. REMOVED AND REPLACED THE CUSP WEB BS 218-236 IAW SRM 51-41-00 ITEM 1, SRM 51-40-08, SRM 51-41-02, AND 51-41-05.Oct 23, 2016 · N987AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016102607647Frame · corrodedNR 2 RT AIR GRILL FRAME IS CORRODED. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00 A.D. GENERAL FIG 103. INSTALLED REPAIR DOUBLERS IAW SRM 51-70-11-B1.Oct 23, 2016 · N987AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016102607646Cusp Web · corrodedCORROSION ON CUSP WEB AT BS 218. RBL 56. CUT OUT CORROSION DAMAGE AND INSTALLED A REPAIR DOUBLER IAW SRM 51-70-10 REPAIR 2, AMM 51-10-00 370-803, AND SRM 51-41-08.Oct 23, 2016 · N987AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016102407497Skin · crackedCRACKED FUSELAGE SKIN Y=1076 LONG 14 RT. REPAIR WAS ACCOMPLISHED PER ETI-17-16-123 REV 1 & ER/A 550326-14 REV ORIGINAL. LEAK TEST OF AIR CONDITION PNEUMATIC DUCT WAS ACCOMPLISHED PER AMM 21-00-00 790-801 AND NO LEAKS WERE FOUND. ACCOMPLISH SECTION II REPETIOct 23, 2016 · N967AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016102407460Pylon · crackedNUMBER 1 PYLON UPPER AND LOWER AFT COWL ATTACH POINTS HAVE CRACKS IN CUTOUTS ON SKIRT FAIRING. REMOVED BRACKETS, FITTINGS, GUSSETS, AND SHIMS. BLENDED OUT CRACKS IN RADIUS. PERFORMED PENETRANT INSPECTION OF CUTOUT LOCATIONS IAW ER/A 552108-14 REV. A SECTION 1 Oct 23, 2016 · N892AT · Boeing 717200 · Nacelle/Pylon, Main FrameSDR DALA2016102807807Longeron · corrodedCORROSION LONGERON 25R BS 1002. BLENDED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-00 FIG 103. REPLACED THE LONGERON IAW SRM 51-41-02 PAGE 1-4.Oct 22, 2016 · N987AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016102607648Cusp Web · crackedCUSP WEB AT BS 655 CRACKED. REPLACED THE CUSP WEB IAW SRM 51-41-02 AND 51-41-05.Oct 22, 2016 · N987AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR HALA2016102100375Eec · malfunctionedCREW REPORTED THAT AFTER TAKEOFF, THE RT ENGINE COMPRESSOR STALLED AT 1000 FT, ALERT WENT AWAY AFTER FIVE SECONDS. ENGINE NORMAL INDICATIONS. NO LIMITATIONS EXCEEDED. ACFT RETURNED TO DEPARTURE. ACCOMPLISHED FIM TASK 72-00TASK 801, NO DEFECTS NOTED. LPC Oct 22, 2016 · N477HA · Boeing 717200 · Turbine Engine Compressor SectionSDR DALA2016102407461Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING FOR THE TAIL COMPARTMENT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS AND THE OPS CHECKED GOOD.Oct 22, 2016 · N949AT · Boeing 717200 · Emergency LightingSDR DALA2016102307459Pylon · crackedLEFT ENGINE PYLON APRON FOUND TO BE CRACKED IN FOUR LOCATIONS. REPAIRED IAW ER/A 552108-14.Oct 22, 2016 · N892AT · Boeing 717200 · Nacelle/Pylon, Main FrameSDR DALA2016102307458Skin · damagedDISTRESS AT VERTICAL STABILIZER LEADING EDGE STRUCTURE SPLICE. BHEC INSPECTION WAS ACCOMPLISHED, NO CRACKS WERE FOUND IAW DWG SG 95550001 REV.B, BUSHINGS WERE FABRICATED AND INSTALLED IAW DPS 4.710-3 AND DWG SG95550001 REV. B.Oct 22, 2016 · N967AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2016102307457Skin · damagedVERTICAL STAB LEADING EDGE AT VSS ZFS 52.267 SPLICE HAS NUMEROUS LOOSE SCREWS & SCREWS PULLING INTO SKIN & ELONGATED HOLES. REPAIRED THE VERTICAL STAB LEADING EDGE SKIN IAW DWG SR95550001 AND JC 5530-01048-03. FABRICATED NEW SPLICE BAN IAW ER/A 549632-14 ROct 22, 2016 · N987AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2016102307456Skin · crackedCRACKED SLAT PANEL NR 2 INBD FACE XOS 238 RT WING. THE SLAT PANEL WAS REMOVED IAW AMM 27-80-01 000-806, HFEC INSPECTION WAS ACCOMPLISHED AND ONE CRACK WAS FOUND IAW NDT SPM 06-10-01. THE SLAT PANEL WAS REPAIRED IAW SRM 57-00-00 FIG. 201 AND INSTALLED IAW AMMOct 22, 2016 · N967AT · Boeing 717200 · Leading Edge DevicesSDR DALA2016102407463Handle · damagedEXTERNAL TAIL CONE JETTISON HANDLE ANGLE MISSING ALONG WITH INSTALL HARDWARE. REPLACED THE MISSING ANGLE AND HARDWARE IAW AMM 53-50. OK FOR SERVICE.Oct 21, 2016 · N996AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2016102107426Battery · dischargedDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT SEAT 20BCD IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND THE OPERATIONAL CHECK WAS GOOD.Oct 20, 2016 · N961AT · Boeing 717200 · Emergency LightingSDR DALA2016102107423Cusp Web · corrodedCUSP WEB CORRODED ON FWD AND AFT SIDE OF FLOORBEAM AT FS 389 ON UNDERSIDE OF WEB. REPAIRED CORRODED CUSP WEB AT FS 389 BY REMOVING DAMAGED SECTION AND REPAIRING IAW SRM 53-00-55 REPAIR 4 FIG 224.Oct 20, 2016 · N987AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016102107422Door Frame · crackedCRACK ON DOOR JAMB STA Y=954 AT AFT CARGO COMPARTMENT C2 (SM) (S/N 00135). DOOR JAMB WAS REPLACE PER SRM 51-41-02 AND 51-41-05. PERFORM DECAL VISUAL INSPECTION EVERY C CHECK PER TOPP 30-10-70 PAR I PG 14.Oct 20, 2016 · N967AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016102107421Longeron · crackedCRACKED LONGERON 2R ON STA 1133 AT AFT ACCESSORIES AREA. LONGERON SECTION WAS REPLACED PER SRM 51-41-05, 51-40-08, 51-10-04 PAR 15 AND 21, AND SRM 51-41-01.Oct 20, 2016 · N967AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016102107420Pan · crackedCRACK ON LOWER FWD CORNER AT AFT CARGO COMPARTMENT DOOR PAN. REPAIR WAS ACCOMPLISHED PER ER/A 550336-14 REV ORIGINAL AND ETI-17-16-127 REV 3.Oct 20, 2016 · N967AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016102607654Access Panel · corrodedRT WING UPPER FUEL PANEL 620AT MATING SURFACE HAS CORROSION. REPLACED ACCESS PANEL IAW AMM 28-00-00 410.Oct 19, 2016 · N922AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016102607653Access Panel · corrodedRT WING UPPER FUEL PANEL 620DT MATING SURFACE HAS CORROSION. REPLACED THE ACCESS PANEL IAW AMM 28-00-00 410.Oct 19, 2016 · N922AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016102607652Access Panel · corrodedLT WING UPPER FUEL PANEL 520CT MATING SURFACE HAS CORROSION. REPLACED THE ACCESS PANEL IAW AMM 28-00-00 410.Oct 19, 2016 · N922AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016102607651Access Panel · corrodedLEFT WING UPPER FUEL PANEL 520DT MATING SURFACE HAS CORROSION. REPLACED THE ACCESS PANEL IAW AMM 28-00 00-410.Oct 19, 2016 · N922AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016102107425Skin · dentedDENT IN FUSELAGE AT C-1 UPPER CORNER CUTOUT. EVALUATED DENT IN FUSELAGE AT C-1 UPPER FWD CORNER CUTOUT IAW SRM 53-01-01 AD3 DENT IS OUT OF LIMITS. REPAIRED DENTED AREA AT C1 DOOR CUTOUT IAW SRM 53-20-15 REPAIR 1. REPLACED FWD HINGE BRACKET IAW SRM 51-41-05.Oct 19, 2016 · N987AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016102007386Beam · crackedCRACKED NR 1 BEAM AT THE L1 DOOR INTERNAL STRUCTURE AFT EDGE. THE BEAM WAS REPAIRED IAW SRM 52-10-02 FIG. 201.Oct 19, 2016 · N925AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016102007385Frame · crackedCRACKED FRAME ANGLE ON BULKHEAD PYLON SUPPORT AT BS 1022 LONGERON 7L. REPAIRED IAW ETI-17-16-130 REV. ORIGINAL AND ER/A 550341-14 REV. ORIGINAL.Oct 19, 2016 · N967AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016102007384Cusp Web · crackedLEFT CUSP WEB FOUND CRACKED BETWEEN BS 579 & 598. REPLACED THE CUSP WEB IAW SRM 51-41-05 PG 17 STEP 8.Oct 18, 2016 · N987AT · Boeing 717200 · Fuselage Miscellaneous Structure
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