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 DALA2016042303185Longeron · corrodedL30 CORRODED AT STA 1038. REPAIRED IAW SRM 53-20-07, REPAIR 3, DWG 9912243.Apr 22, 2016 · N921AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016042303184Frame · corrodedAFT CARGO BAY- FRAME AT BS 1028 IS CORRODED FROM L28L TO L28R. REPAIRED FRAME SECTION IAW SRM 53-20-07, REPAIR 3.Apr 22, 2016 · N921AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018060103770Floorboard · damagedFOUND AISLE FLOORBOARD SOFT AT SEAT ROW 17. REPAIRED THE FLOORBOARD IAW SRM 53-00-50, REPAIR 2. TAP TEST WAS PERFORMED AND DELAMINATION WAS FOUND IAW SRM 53-00-50 REPAIR 2. A NEW FLOORBOARD WAS FABRICATED AND REPLACED IAW SRM 53-20-50-2R, AND CARD 2040-0024Apr 21, 2016 · N921AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016043003458Door Frame · corrodedAFT CARGO DOOR JAMB HAS CORROSION AND A DENT TO FWD WEB. BLENDED CORROSION IAW SRM 53-00-00, ORIGINAL TC .050. REMOVED T .005 REMAINING R .045 USING TAG NR 3210, ALODINED, PRIMED, TOPCOATED IAW SRM 51-10-04 DENT MEASURES .045 X 2.00 USING TAG 3810.Apr 21, 2016 · N924AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016042203168Seat Track · corrodedCORROSION ON SEAT TRACK X -54.5 BETWEEN BS 1022 AND 1065,. SEAT TRACK WAS REPLACED IAW SRM 51-41-05.Apr 21, 2016 · N926AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016042203167Door Frame · corrodedCORROSION ON AFTER CARGO DOOR FRAME LOWER AREA. DOOR JAMB WAS REPAIRED IAW SRM 53-20-15, REP 7.Apr 21, 2016 · N926AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016042203166Longeron · corrodedCORROSION ON LONGERON 30 BETWEEN BS 889-908. DAMAGE WAS REPAIRED IAW SRM 53.00.05, REPAIR 3, 2.Apr 21, 2016 · N926AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016042203165Skin · corrodedAFT CARGO, SKIN SPLICE AT BS 898 IS CORRODED AT BL 0. ACCOMPLISHED REPAIR REF ER/A 545889-14, REV ORIGINAL REF LP 2454063 FOR SDR.Apr 21, 2016 · N921AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016042203164Skin · corrodedAFT CARGO, SKIN SPLICE AT BS 898 IS CORRODED AT BL 0, REF NR 00199. REPAIRED SKIN SPLICE REF ER/A 545889-14, REV ORIGINAL ASSOCIATED ER/A 14-545889 ADDED FOR AC 9577.Apr 21, 2016 · N921AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016042203163Floor Panel · damagedDISBONDED AND CRACKED CHANNEL ON FLOOR PANEL NR 222AJF7. CHANNEL ON FLOOR PANEL REPAIRED AND BONDED IAW SRM 53-20-50 FIG 202, 51-20-09, 51-30-08, AND 51-10-4 PAR 15/21.Apr 21, 2016 · N926AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016042203162Cusp Web · corrodedCORROSION ON LT CUSP WEB BS 851 TO BS 870 BETWEEN X=44 AND X=60 AT CPAX IN REF CARD 22, ZONE 000, CARD 87, ZONE 200. CORROSION ON CUSP WEB WAS ATTENDED IAW SRM 51-41-02, 51-41-03, 51-41-05, 5141-01, 51-10-04 PAR 15, 21 AND 37, AND 53-00-55, FIG 215, SHEET 1 OApr 21, 2016 · N926AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016042103126Nut Plate · wornVERTICAL STABILIZER MID SPAN PANEL HORSE COLLAR NUTPLATES WORN. REPAIRED OVERSIZE FASTENER HOLE IAW PRI 545887-14, REV 0, ER/A 545887-14, REV. O AND REPLACED NUTPLATES IAW SRM 51-41-01. REF LOG NR 2453267 FOR CORRECT MAJOR REPAIR ANNOTATION.Apr 21, 2016 · N921AT · Boeing 717200 · Vertical StabilizerSDR DALA2016042103125Seat Track · corrodedCORROSION ON RT SEAT TRACK X=54 FROM BS 256 TO BS 340 IN REF CARD 14, ZONE 200. CARD 88 ZONE 200. SEAT TRACK WAS REPAIRED IAW SRM 53-20-52, FIG 201, REPAIR 5 CONFIGURATION -7005.Apr 20, 2016 · N926AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA201604200103Skin · delaminatedDURING NON-ROUTINE LINE UNSCHEDULED CHEK, RT INBD SPOILER FOUND DELAMINATED.Apr 20, 2016 · N895AT · Boeing 717200 · SpoilersSDR DALA2016102807825Pan · corrodedAFT CARGO DOOR LOWER FRAME PAN HAS CORROSION. BLENDED CORROSION AND FOUND OUT OF LIMITS, REPLACED THE PAN IAW SRM 53-00-00 FIG. 103.Apr 19, 2016 · N921AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016050103468Angle · corrodedUPPER CABIN FLOOR CUSP ANGLE AT BS 220, RBL 60 IS CORRODED AT UPPER SURFACE BLEND, CHECK LIMITS REF OR NRC 66531-0200-0115. BLENDED NOTED AREA IAW SRM 51-10-04, SECTION 26, FOUND TO BE IN LIMITS IAW SRM 53-00-00, FIG 103. REMOVED .013 FROM ORIGINAL .071 DEPTApr 19, 2016 · N924AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016042103127Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE AFT CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.Apr 19, 2016 · N943AT · Boeing 717200 · Emergency LightingSDR DALA2016042003046Floor Panel · crackedCRACKED PASSENGER FLOOR PANEL. FLOOR PANEL FABRICATED IAW SRM 53-20-50.Apr 19, 2016 · N926AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016042003045Beam · crackedGALLEY DOOR BEAM IS CRACKED AT THE LOWER HINGE MOUNTING FLANGE, MARKED. REPLACED GALLEY DOOR BEAM AT THE LOWER HINGE MOUNTING FLANGE IAW SRM 51-41-00.Apr 19, 2016 · N956AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016042003044Fitting · crackedCRACKED FWD INNER FITTINGS ON BEAM NR 1 AT AFT CARGO DOOR. FITTING WAS REPLACED IAW SRM 51-41-05, 51-40-08, 51-10-04, PAR 15/21.Apr 19, 2016 · N926AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016042003043Structure · damagedVERTICAL STABILIZER MID SPAN PANEL FRAME LOWER FASTENER HOLES ELONGATED. REPAIRED IAW REPAIR DWG SG95550001 AND SRM 55-30-01, REPAIR 7.Apr 19, 2016 · N921AT · Boeing 717200 · Vertical StabilizerSDR DALA2016041903023Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE MAIN CABIN DOOR EMERGENCY EXIT SIGN WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECKED GOOD.Apr 19, 2016 · N946AT · Boeing 717200 · Emergency LightingSDR DALA2016041903022Battery Pack · inoperativeDURING 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.Apr 19, 2016 · N608AT · Boeing 717200 · Emergency LightingSDR DALA2016041903021Beam · crackedL1 DOOR NR 1 BEAM CRACKED AT AFT END IN RADIUS. L1 INT NR 1 BEAM AT AFT END REPAIRED IAW SRM 52-10-02, REPAIR 7.Apr 18, 2016 · N921AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016041903020Beam · crackedL1 DOOR NR 1 BEAM CRACKED AT FWD END IN RADIUS. L1 INT NR 1 BEAM AT FWD END REPAIRED IAW SRM 52-10-02, REPAIR 7.Apr 18, 2016 · N921AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016041903019Seat Track · corrodedCORROSION ON SPLICE OF SEAT TRACK X=-56, BS 218. SEAT TRACK SPLICE, X=-56, BS 218 WAS REPLACED IAW SRM 51-40-08 AND DWG 5953059, REV H, SRM 51-40-01.Apr 18, 2016 · N926AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016041903018Frame · crackedCRACKED FRAME BS 694, LONGERON 26 LT AT KEELBEAM AREA. SM, CARD 24, ZONE 140. FRAME WAS REPAIRED IAW SRM 51-70-11, FIG 201, 51-41-02 AND 51-41-05 CRACK LENGTH 0.650".Apr 18, 2016 · N926AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016041903017Frame · crackedCRACKED FRAME BS 679, LONGERON 25 LT AT KEEL BEAM AREA. FRAME WAS REPAIRED IAW 51-70-11, FIG 201. CRACK LENGTH 0.500".Apr 18, 2016 · N926AT · Boeing 717200 · Fuselage Main, FrameSDR HALA2016041700113Pitot Head · obstructedON TAKEOFF ROLL AT 80 KTS F/O'S AIRSPEED INDICATOR STARTED DROPPING OFF DUE TO A BEE IN F/O'S PITOT TUBE. CONFIRMED BEE STUCK TO F/O'S PITOT PROBE, CLEARED LINE IAW AMM 34-11-00-171-801, LEAK CHECK OK IAW AMM 34-11-00-790-801. NO BRAKE OVERHEAT NOTED DURING Apr 17, 2016 · N492HA · Boeing 717200 · Pitot/Static SystemSDR DALA2016041702961Seat Track · corrodedCORROSION ON RT SEAT TRACK BS 952-988, SEAT TRACK WAS REPLACED IAW SRM 53-20-52, FIG 201, REPAIR 5 AND 51-41-01.Apr 16, 2016 · N926AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016041702960Frame · gougedWHEN REMOVING PANEL FOR ACCESS, FOUND FRAME GOUGED AT BS 1146 ALSO 2 FWD BRACKETS CRACKED AT APPROXIMATELY 1106 IN WALKWAY. REPAIR IAW SRM. REPAIRED DAMAGED FRAME IAW ER/A 545664-14, REV O. ASSOCIATED ER/A 00-545664, ADDED FOR AC 9515.Apr 16, 2016 · N956AT · Boeing 717200 · Fuselage Main, FrameSDR HALA2016041500112Display · abnormalMCDU NR 2 BLANK. REPLACED NR 2 MCDU. GROUND OPS CHECK OK, AMM 31-65-01.Apr 15, 2016 · N493HA · Boeing 717200 · Central DisplaySDR DALA2016041602959Skin · crackedFUSELAGE SKIN CRACKED, BS 1133 OTBD OF STR 2L AT SHEAR TIE FASTENER, HFEC VERIFIED. REPAIRED SKIN CRACK AT BS Y1133 OTBD OF STR SL IAW ER/A 544353-14AD. SEE NON-ROUTINE/ AMDS CONTINUATION SHEETS FOR WORK ACCOMPLISHED. ASSOCIATED ER/A 00-544353 ADDED FOR AC 9Apr 15, 2016 · N956AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016041602958Skin · crackedFUSELAGE SKIN CRACKED, BS 1133, OTBD OF STR 2R AT SHEAR TIE FASTENER, HFEC VERIFIED. REPAIRED SKIN CRACK AT BS 1133 OTBD OF STR 2R IAW ER/A 544354-14AD, REV A. NON-ROUTINE/AMDS CONTINUATION FORMS FOR WORK ACCOMPLISHED. ASSOCIATED ER/A 00-544354 ADDED FOR AC Apr 15, 2016 · N956AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016041602957Stringer · crackedTHREE STRINGERS ARE CRACKED AT THE OTBD ENDS INTERNAL OF THE CANTED KEEL. RT BS 675, AND LT BS 675 AND 696. MARKED EXTERNALLY. REMOVED AND REINSTALLED WING TO BODY FAIRING SUPPORT IAW SRM 51-41-05. REMOVED AND REINSTALLED NOSE STEERING, SLAT EXTEND AND RETApr 15, 2016 · N956AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016041602956Frame · corrodedFRAME CORRODED IN ALC BS 927, BL0. REPLACED FORMER SECTION OF FRAME IN AFT CARGO STA 927 BL0 IAW B717 SRM 53-00-06 REPAIR 2. FORMER WAS FABBED IAW B717 PL 9915524 AND HEAT TREATED TO 7075-T6 IAW DPS 900-4-1, NR 1, PG 16 12/20/10, PG 25 1/17/12. REPAIR SPLICE Apr 15, 2016 · N956AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016041602955Frame · corrodedFRAME CORRODED IN ALC BS 908 BL0. REPLACED FORMER FRAME SECTION IN C2 AT BS 908 BL0 IAW SRM 53-00-06, REPAIR 2, FIG 201. FORMER WAS FABRICATED AND HEAT TREATED TO T6 IAW DAL PSM 900-4-1, NR 1, PG 16, 12-20-10, PG 25 1/17/12 WO 66072-0026. REPAIR SPLICE MATEApr 15, 2016 · N956AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016041602954Beam · corrodedCORROSION ON PREVIOUS REPAIR DOUBLER IN BEAM BS 427 BETWEEN LONGERONS 26-27R IN FWD CARGO COMPARTMENT. NEW REPAIR DOUBLERS WERE REPLACED IAW SRM 53-20-15, REA 6, 51-41-02, 51-10-04 PAR 15 AND 21, AND 51-20-09.Apr 15, 2016 · N926AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016102807824Floor Panel · corrodedRANDOM CORROSION ALONG EDGE OF FLOOR PANEL & UNDER PLASTIC FLOOR WRAP. CLEANED AND EVALUATED CORROSION IAW SRM 53-00-00 FIG 1. REPLACED IAW DRAWING 9957828.Apr 14, 2016 · N921AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016041502927Skin · damagedVERTICAL STABILIZER L/E ZFS 52.267, NUMEROUS FASTENERS LOOSE, SEVERAL FASTENERS PULLED THROUGH AND PARTIALLY PULLED THROUGH. REPAIRED VERTICAL STABILIZER L/W FASTENERS HOLES IAW SERVICE DWG SG 95550001, REPAIRED CRACK ON VERTICAL STABILIZER. FOUND DURING OPApr 14, 2016 · N956AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2016041502925Cusp Web · damagedDAMAGE OUT OF LIMITS CUSP WEB, BS 551 X=56 - 60 AT LT AREA OF CABIN PAX. DAMAGE WAS REMOVED IAW IAW SRM 53-00-55, FIG 125. REPAIR WAS ACCOMPLISHED IAW SRM 53-00-55, FIG 125.Apr 14, 2016 · N926AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016041402892Seat Track · corrodedCORROSION ON SEAT TRACK X=44.5 BETWEEN BS 1022 AND BS 1065. SEAT TRACK WAS REPLACED IAW SRM 53-20-50, FIG 1, 51-41-05, 51-40-08, AND 51-10-04, PAR 15/21.Apr 13, 2016 · N926AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016041402891Seat Track · not reportedLT SEAT TRACK X=56 FROM BS 817 TO 818 AND 868 TO 870 OUT OF LIMITS. SEAT TRACK WAS REPAIRED IAW SRM 53-20-52, FIG 201.Apr 13, 2016 · N926AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016041402890Seat Track · not reportedSEAT TRACK X=56 AND BS 578 OUT OF LIMITS. SEAT TRACK WAS REPAIRED IAW SRM 53-20-52, FIG 201.Apr 13, 2016 · N926AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016041402889Beam · crackedCRACK ON BEAM AFT EDGE AND FWD EDGE AT L1 DOOR. THE BEAM WAS REPAIRED IAW SRM 52-10-02, FIG 201 AND 202, 51-40-02, 51-40-05, AND 51-10-04. PAR 15 AND 21.Apr 13, 2016 · N926AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2016102807823Shear Tie · corrodedAFT CARGO BAY SHEAR TIE AT BS 954 IS CORRODED BETWEEN LONERONS 29 AND 30L. REPAIRED IAW SRM 53-00-06 REPAIR 2.Apr 12, 2016 · N921AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2016041302859Angle · crackedMAINTENANCE DISCOVERED THAT THE RT FORWARD EMERGENCY ESCAPE DOOR HAD A CRACKED CLIP BEHIND THE DOOR STOP. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE DOOR CLIP WAS REPLACED IAW SRM 51-41-05 ANApr 12, 2016 · N926AT · Boeing 717200 · Emergency ExitsSDR DALA2016041202795Battery Pack · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTING AT BOTH FORWARD DOORS, L1 & R1, AND THE COCKPIT WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.Apr 11, 2016 · N936AT · Boeing 717200 · Emergency LightingSDR DALA2016041202794Cusp Web · crackedCRACK ON LT CUSP WEB BS 665, BETWEEN X=44 AND X=56 AT CABIN FLOOR STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 226, 51-41-02, 51-10-4 PAR 15, 21 AND 37.Apr 11, 2016 · N926AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016041202793Cusp Web · crackedCRACK ON RT CUSP WEB BS 256, X=-49 AT FLOOR STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 53-00-55, 51-41-02, FIG 203, REPAIR 4.Apr 11, 2016 · N926AT · Boeing 717200 · Fuselage Miscellaneous Structure
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