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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DALA2017061204633Access Panel · corrodedCORROSION ON AREA COUNTERSINK ON FUEL TANKS ACCESS PANEL 520CB. THE ACCESS PANEL WAS REPLACED IAW SRM 57-10-01.Jun 10, 2017 · N997AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017061104631Access Panel · corrodedCORROSION ON SETTLEMENT AREA AND COUNTERSINK OF FUEL ACCESS DOOR 520CT AND 620CT. THE ACCESS PANELS WERE REPLACED IAW SRM 57-10-01, REPAIR 2.Jun 10, 2017 · N717JL · Boeing 717200 · Wing, Plate/SkinSDR DALA2017061204635Channel · crackedCRACKED CHANNEL AFT INBD SIDE ON THE LT MLG INBD DOOR. REPAIRED IAW ER/A 558127-14, REV ORIGINAL, AND ETI-17-17-063, REV ORIGINAL.Jun 9, 2017 · N997AT · Boeing 717200 · Landing Gear DoorsSDR DALA2017061004630Pan · crackedCRACKED AFT UPPER CORNER ON RING PAN BTW BS 813 - 832 IN PASSENGER CABIN. THE RING PAN WAS REPAIRED IAW SRM 56-20-02.Jun 9, 2017 · N717JL · Boeing 717200 · Fuselage Main, StructureSDR DALA2017060904567Skin · damagedVERTICAL STAB LEADING EDGE BELOW ZFS 52, HAS 53 ELONGATED FASTENER HOLES. COMPLIED WITH PRI 559269-14 REV 0 AND ER/A 559269-14AD REV ORIGINAL.Jun 9, 2017 · N949AT · Boeing 717200 · Horizontal Stabilizer, Plate/SkinSDR DALA2017061204636Brace · corrodedCORROSION ON DRAG BRACE ASSEMBLY AT NLG. THE DRAG BRACE WAS REMOVED AND REPLACED IAW AMM 32-22-05 000-801, AMM 32-22-05 400-802 AND 32-22-05 400-801.Jun 8, 2017 · N997AT · Boeing 717200 · Main Landing Gear Strut/Axle/TruckSDR DALA2017060804555Power Supply · inoperativeAFT EMERGENCY EXIT DOOR OVERWING LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY. OPS OK IAW AMM 33-51.Jun 8, 2017 · N920AT · Boeing 717200 · Emergency LightingSDR DALA2017060804557Sign · inoperativeEMERGENCY EXIT SIGNS INOPERATIVE. LENS COVER IS MISSING. INSTALLED SIGN. OPERATIONAL CHECKED NORMAL.Jun 7, 2017 · N921AT · Boeing 717200 · Emergency LightingSDR DALA2017060704556Shaft · brokenDURING A CHECK OF TAILCONE RELEASE MECHANISM, MAINTENANCE FOUND THAT THE RELEASE SHAFT WAS BROKEN. MAINTENANCE REPLACED THE CAM LATCH/LOCK ASSEMBLY. THE TAILCONE WAS ADJUSTED AND RIGGED AFTER INSTALLATION AND FOUND OPERATIONAL. THE RII WAS COMPLETED FOLLOWING Jun 6, 2017 · N893AT · Boeing 717200 · Aerodynamic FairingsSDR DALA2017060604517Screw · looseVERTICAL STAB LEADING EDGE APPROX STA ZFS 52, FOUR ROWS SPLICE 40 SCREWS LOOSE. SEE NR FOR ADDITIONAL INFORMATION 001-0235:5530-2005/003 00123 REPAIR PER SRM55-30-01-2R-6. FPI PER PS 900-6-3 NR 02.Jun 5, 2017 · N949AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2017060604516Longeron · crackedCRACK ON LONG 8L AND STA Y=1022. DAMAGED LONGERON WAS REPLACED PER SRM 53-00-05-2R, 51-41-02, AND 51-41-05.Jun 5, 2017 · N997AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017060604515Frame · crackedCRACK ON FRAME AT STA Y=1037 BTW LONG'S 16R AND 18R. FRAME AT STA Y=1037 BTW LONG 16R AND 18R WAS REPAIRED PER SRM 53-20-07-2R REP 4.Jun 5, 2017 · N997AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017060504514Frame · crackedFRAME 1225 CRACKED AT TAIL CONE ALIGNMENT PIN 7 O'CLOCK POSITION. REMOVED DAMAGED AREA REF 497316-14MA. MANUFACTURED DOUBLER AND DRILLED REF 497316-14MA. INSTALLED REPAIR PER RI 559273-14.Jun 4, 2017 · N989DN · Boeing 717200 · Fuselage Main, FrameSDR DALA2017060404461Power Supply · inoperativeFORWARD CABIN NR 2 POWER SUPPLY FOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY POWER SUPPLY IAW AMM 33-51. AIRCRAFT IS OK FOR SERVICE.Jun 4, 2017 · N989AT · Boeing 717200 · Emergency LightingSDR DALA2017060404459Frame · crackedCRACK ON FRAME AT STA Y=1037 BTW LONG 16L AND 18L. FRAME WAS REPAIRED PER SRM 53-20-07-2R REP 4.Jun 4, 2017 · N997AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017060404458Fitting · crackedCRACKED FRAME CLIP BELOW LONG 16R AND STA Y=1022 (CPAX). FRAME CLIP WERE REPLACED PER DGW 9912243 REV JS AND SRM 51-41-05.Jun 4, 2017 · N997AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017070405176Beam · crackedCRACK ON THE RT NLG DOOR FRAME BEAM RBL 46 AT NLG W/W. REPAIRED IAW SRM 53-10-14, REP 2.Jun 3, 2017 · N982AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017060304457Battery · dischargedAFT OVERWING EMER EXIT DOOR LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHTS BATTERY B5-230 REF AMM 33-51. OPERATIONAL CHECK WAS GOOD.Jun 3, 2017 · N953AT · Boeing 717200 · Emergency LightingSDR DALA2017060304456Access Panel · damagedELONGATE HOLES ON FUEL TANKS ACCESS PLATES 520LB, 141AL, AND 141AR. ACCESS PLATES WERE REWORKED AND FOUND 6 HOLES OUT OF LIMITS PER SRM 57-10-01-2R B CONDITION II. FABRICATED BUSHINGS PER SRM 57-10-01-2R B CONDITION II(1), (3) (D) FOR 520 LB, AND SRM 57-10-01-Jun 2, 2017 · N997AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017060304455Frame · crackedCRACKED FRAMES IN STA Y=693 AND Y=678 LT AND RT SIDE AT UNDER WING CANTED KEEL. FRAMES (4EA) WERE REPAIRED PER SRM 51-70-11 REPAIR 1.Jun 2, 2017 · N997AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017060204460Unknown · burnedFLIGHT ATTENDANTS REPORT ODOR NEAR ROW 23 TWO DIFFERENT TIMES. BOTH TIMES IT WENT AWAY. NO VISIBLE SMOKE OBSERVED. DROPPED CEILING PANELS ON 19CDE, 23 CDE REMOVED COVER FOR EMER LITE BATTERY PACK AT 20CD. RAN UPPER BEACON & EMER LIGHTS - NO UNUSUAL SMELL. INSPJun 1, 2017 · N991AT · Boeing 717200 · AC Power Distribution SystemSDR DALA2017060204454Access Panel · corrodedCORROSION ON SETTLEMENT AREA OF FUEL ACCESS 620CT AND 520CT. BLEND OUT REPAIR IS NOT PERMITTED ON THE UPPER WING ACCESS DOOR DUE TO THE REDUCED AREA OF THE CONDUCTIVE INTERFACE THEREFORE FUEL ACCESS PLATES WERE REPLACED PER SRM 57-10-01 AND PART NUMBER WAS VERJun 1, 2017 · N997AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017060104403Cusp Web · corrodedCORROSION ON RT CUSP WEB STA Y=493 IN REF NRC 00388 5300-2020. REPAIR WAS ACCOMPLISHED PER SRM 53-00-55-2R-4.Jun 1, 2017 · N997AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017060104402Cusp Web · crackedCRACK ON RT CUSP MEMBRANE FROM STA Y=894 TO Y=896, BTW X=58-60 REF CARD 385. REPAIR WAS PERFORMED PER SRM 53-00-55-2R. HFEC INSPECTION WAS ACCOMPLISHED AFTER DAMAGE REMOVED AND NO CRACKS WERE FOUND PER NDT SPM 06-10-01.001. SPLICE WAS REMOVED AND INSTALLED PERMay 31, 2017 · N997AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017060104401Skin · dentedDENT ON LT WING AFT MOVABLE VANE LOWER SURFACE 8" FROM INBD AND 5" FROM T/E. DENT ON LT WING AFT MOVABLE VANE LOWER SURFACE AT 8" FROM INBD AND 5" FROM T/E WAS REPAIRED PER SRM 57-53-01-2R-1 AND OPN 1031, CARD 2000-8149-01.May 31, 2017 · N997AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2017060104400Longeron · crackedCRACK ON LONG 6L AND STA Y=1022. DAMAGE SECTION WAS REPLACED PER SRM 53-00-05-2R.May 31, 2017 · N997AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017060104399Beam · crackedCRACK ON DOOR JAMB BEAM LT SIDE Y=41 APPROX AT NLG WHEEL WELL. DOOR JAMB BEAM LT SIDE WAS REPAIRED PER SRM 53-10-14 REPAIR 2 FIGURE 201.May 31, 2017 · N997AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017060104398Beam · crackedCRACK ON DOOR JAMB BEAM RT SIDE Y=41 APPROX AT NLG WHEEL WELL. DOOR JAMB BEAM RT SIDE WAS REPAIRED PER SRM 53-10-14 REPAIR 2 FIGURE 201.May 31, 2017 · N997AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017053104385Floor Panel · crackedCRACK ON FLOOR PANELS 222AFF, 222ALF, 222AJF, AND 222AF. FLOOR PANELS WERE REPAIRED PER SRM 53-20-50-2R-5. HFEC INSPECTION WAS ACCOMPLISHED ON FLOOR PANELS 222AFF, 222ALF, 222AJF, AND 222AF. NO CRACKS WERE FOUND AFTER STOP DRILLING PER SRM 53-20-50-2R-5, GENERMay 31, 2017 · N997AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017053104384Floor Panel · damagedDAMAGE ALL FLOOR PANELS OF COCKPIT. FLOOR PANELS OF COCKPIT DAMAGE WERE REPAIRED PER SRM 53-20-50-2R-3- AND FLOOR PANELS 211ALF AND 211ANF WERE FABRICATE PER SRM 53-20-50 2R-3.May 30, 2017 · N997AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017053104383Cusp Web · corrodedCORROSION ON LT CUSP WEB BTW X=54-60 STA Y=541-560 UPPER AND LOWER SURFACE AT PAX CABIN IN REF 5300-2020. DAMAGE WAS REPAIRED PER SRM 53-00-55-2R.May 30, 2017 · N997AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017053104382Cusp Web · corrodedCORROSION ON RT CUSP WEB STA Y=419 X=-56 AT PAX CABIN IN REF NRTC 00388. CUSP WEB WAS REPAIRED PER SRM 53-00-55-2R-4, 51-41-02, 51-10-04 PAR 37.May 30, 2017 · N997AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017053004316Cusp Web · corrodedCORROSION ON THE CUSP WEB BETWEEN LBL 54 - 60, BS 598 - 617 UPPER AND LOWER SURFACES. THE CUSP WEB WAS REPAIRED IAW SRM 51-41-02, 53-00-55-2R-4, AND 51-10-04, PAR 37, REPAIR 4.May 29, 2017 · N997AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017053004315Cusp Web · crackedCRACKED CUSP WEB, RBL 54 AND 60, BS 223. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 215, AND 51-41-02.May 29, 2017 · N997AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017053004331Coffeemaker · smokeDURING TAXI IN, BOTH FWD COFFEEMAKERS STARTED SMOKING, ELECTRICAL ODOR, SHUT OFF GALLEY POWER THE SMOKE STOPPED. REPLACED THE COFFEEMAKERS IAW AMM 25-33. INSPECTED COFFEEMAKER COMPARTMENT AND WIRING, NO DEFECTS FOUND.May 26, 2017 · N978AT · Boeing 717200 · Buffet/GalleysSDR DALA2017052704314Skin · damagedVERTICAL STAB LE AT ZFS 52 HAS MANY WORN FASTENER HOLES, COUNTER SINKS, AND LOOSE FASTENERS. LT & RT SIDES, ABOVE & BELOW THE SEAM. REPAIRED IAW PRI 558868-14, REV 0.May 26, 2017 · N608AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2017052704313Skin · crackedFUSELAGE SKIN HAS HAS A .750 LONG CRACK THRU FASTENER HOLE AT BS 1087, 2.5 INCHES ABOVE SKIN LWR EDGE, NEAR LONGERON 14R. HFEC IAW NDT SPM. NR 001-0229:5300-2019/010 00062. REPAIRED IAW PRI 558866-14, REVISION 0, AND ER/A 558866-14, REV ORIGINAL.May 26, 2017 · N608AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017052704312Skin · dentedDENT ON THE LT WING INBD SPOILER UPPER SURFACE. FOUND TO BE WITHIN LIMITS IAW SRM 57-70-01-1A.May 26, 2017 · N997AT · Boeing 717200 · SpoilersSDR DALA2017052704311Skin · dentedDENT ON THE LT WING INBD SPOILER UPPER SURFACE. FOUND WITHIN LIMITS IAW SRM 57-70-01-1A.May 26, 2017 · N997AT · Boeing 717200 · SpoilersSDR 2017F00109Skin · delaminatedDURING UNSCHEDULE MAINTENANCE CHECK R/H O/B SPOILER FOUND DELAMINATED.May 26, 2017 · N974AT · Boeing 717200 · SpoilersSDR 2017F00108Skin · delaminatedDURING UNSCHEDULE MAINTENANCE CHECK, THE LEFT INBD SPOILER FOUND DELAMINATED.May 26, 2017 · N942AT · Boeing 717200 · SpoilersSDR DALA2017052604240Skin · dentedDENT ON LH WING FIXED I/B VANE LOWER SURFACE BTW ATTACH POINTS 2 AND 3 (AI). NR 00014 DENT ON LH WING FIXED I/B VANE LOWER SURFACE BTW ATTACH POINTS 2 AND 3 WAS MEASURED, DENT 1 DIAMETER 0.500" AND DEPTH 0.023" THEREFORE IS WITHIN LIMITS PER B-717 SRM 57-53-01May 26, 2017 · N997AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2017052604239Skin · dentedDENT ON LH WING FIXED I/B VANE LOWER SURFACE BTW ATTACH POINTS 2 AND 3 (AI). NR 00014 DENT ON LH WING FIXED I/B VANE LOWER SURFACE BTW ATTACH POINTS 2 AND 3 WAS MEASURED, DENT 1 DIAMETER 0.500" AND DEPTH 0.023" THEREFORE IS WITHIN LIMITS PER B-717 SRM 57-53-01May 26, 2017 · N997AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2017052604238Skin · dentedDENT ON UPPER SURFACE (MID SECTION) AT FWD MOVABLE FLAP VANE, LH WING (SM)(AI). NR 00197 DENT ON UPPER SURFACE (MID SECTION) AT FWD MOVABLE FLAP VANE, LH WING WAS MEASURED, DENT 1 DIAMETER 1" AND DEPTH 0.034" THEREFORE IS WITHIN LIMITS PER B-717 SRM 57-53-01-1May 26, 2017 · N997AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2017052604237Skin · dentedDENT ON UPPER SURFACE (MID SECTION) AT FWD MOVABLE FLAP VANE , LH WING (SM)(AI). NR 00197 DENT ON UPPER SURFACE (MID SECTION) AT FWD MOVABLE FLAP VANE, LH WING WAS MEASURED, DENT 1 DIAMETER 1" AND DEPTH 0.034" THEREFORE IS WITHIN LIMITS PER B-717 SRM 57-53-01-May 26, 2017 · N997AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2017052604310Skin · corrodedCORROSION SKIN BS 629, LONGERON 28L - 30L. REPAIRED IAW SRM 51-40-08, 51-44-02 PARA 4, AND 51-41-05 PARA 8.May 25, 2017 · N965AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR HALA2017052500123Unknown · odorODOR THROUGH TAKEOFF TO 3000FT, THE ELECTRICAL BURNING ODOR EVENTUALLY WENT AWAY. CHECKED CIRCUIT BREAKERS, TURNED ON ALL FLIGHT DECK LIGHTS, CHECKED E & E BAY, RAN LEFT AND RIGHT A/C PACKS WITH APU, ALSO WITH LEFT ENGINE. NO ELECTRICAL ODOR AT ANYTIME. May 25, 2017 · N480HA · Boeing 717200 · Air Distribution SystemSDR DALA2017052604236Angle · crackedCRACKED ANGLE ON THE LT AFT EMERGENCY EXIT DOOR AT STOP FITTING 10. THE ANGLE WAS REPLACED IAW DWG #9957735, REV G, SRM 51-41-02, AND 51-41-05.May 25, 2017 · N997AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017052604235Angle · crackedCRACKED FWD ANGLE JUST ON THE NR 1 BEAM AT FWD OVWERWING EMERGENCY DOOR. THE ANGLE WAS WAS REPLACED IAW DWG 9957735, REV G, SRM 51-41-02, AND 51-41-05.May 25, 2017 · N997AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR HALA2017053000124Fan · failedAFTER TAKEOFF TO 3000 FT, HAD AN ELECTRICAL BURNING ODOR, EVENTUALLY WENT AWAY. FOUND THE NR 1 ADIRU FAN FROZEN AND BURNED. REPLACED THE FAN IAW AMM 34-43-05. OPS CHECKED OK.May 24, 2017 · N480HA · Boeing 717200 · Doppler System
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