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 DALA2017110908015Cusp Web · crackedCRACKED CUSP WEB BS 413 & 419, RBL 56. THE CRACKS WERE FOUND WHEN CORROSION WAS REMOVE. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 207. HFEC INSPECTION WAS ACCOMPLISHED. NO CRACKS WERE FOUND AFTER DAMAGE REMOVAL IAW NDT SPM 06-10-01-01.001.Nov 8, 2017 · N995AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017110908014Floor Panel · brokenBROKEN FLIGHT DECK FLOOR PANEL. THE FLOOR PANEL WAS FABRICATED, AND REPLACED IAW 2040-0024.Nov 8, 2017 · N995AT · Boeing 717200 · Fuselage Floor PanelSDR HALA2017110800271Spring · brokenDIVERSION DUE TO A LOUD NOISE FROM NOSE GEAR AFTER TAKEOFF. FOUND A BROKEN ANTI-RETRACTION SPRING ON THE LANDING GEAR HANDLE MODULE. FOUND RIGHT UPPER BANANA FAIRING RUBSTRIP PROTRUDING OUT INTO AIR STREAM. REMOVED AND REPLACED THE SPRING, SECURED THE RUBNov 8, 2017 · N487HA · Boeing 717200 · Landing Gear Retraction/Extension SystemSDR DALA2017110807999Floor Support · corrodedEXCESSIVE CORROSION ON THE FLOOR SUPPORT BS 140, RBL 44. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-05-0G AND 51-41-08-0G.Nov 7, 2017 · N995AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017110807998Vane · debondedDISBOND OF 2.300" X 3.500" AT 9.00" FROM OUTBOARD EDGE AND 9.00" FROM AFT EDGE ON THE RT AFT MOVABLE FLAP VANE, REPAIRED IAW SRM 57-53-01-2R-1.Nov 7, 2017 · N995AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2017110807997Floor Panel · brokenBROKEN FLOOR PANEL 221LF. A NEW FLOOR PANEL WAS FABRICATED, AND INSTALLED IAW SRM 53-20-50-2R, REP 3.Nov 7, 2017 · N995AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017110707996Skin · corrodedSEVERAL CORROSION POINTS ON THE SKIN BETWEEN BS 655 AND 696, LBL 44 AND LBL 60. REPAIRED IAW ER/A 562374-14 REV. ORIGINAL, AND ETI-17-17-210 REV 1.Nov 6, 2017 · N994AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017110707975Frame · crackedCRACK FOUND ON THE BS 851 FRAME LOWER CORNER. REPAIRED IAW SRM 56-20-02-2R, FIG 202, AND 51-41-02.Nov 6, 2017 · N995AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017110707974Frame · crackedCRACK ON THE BS 756 FRAME UPPER CORNER. REPAIRED IAW SRM 56-20-02-2R, FIG 202, AND 51-41-02.Nov 6, 2017 · N995AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017110707973Frame · crackedCRACK ON THE BS 617 FRAME LOWER CORNER. REPAIRED IAW SRM 56-20-02-2R, FIG 202, AND 51-41-02.Nov 6, 2017 · N995AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017110707971Housing · wornWEAR ON HOUSING OF THE HOOK AT THE L1 DOOR. A NEW HOUSING WAS FABRICATED IAW DWG 4955948, REV D, AND REPLACED IAW SRM 51-41-02.Nov 6, 2017 · N994AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2017110607952Intercostal · crackedCRACK ON INTERCOSTAL BS 617 TO 636, BL 0, Z=0 IN THE FWD CARGO BAY. THE INTERCOSTAL WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND 51-40-08-0G.Nov 6, 2017 · N994AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017110708001Clamp · looseDIVERTED THE AIRCRAFT DUE TO A CABIN ALTITUDE WARNING MESSAGE. A YELLOW EMERGENCY WAS DECLARED, THE QRH WAS COMPLIED WITH, AND A FLIGHT IDLE, SPOILER DEPLOYED DESCENT TO 11,000 FEET WAS ACCOMPLISHED. MAINTENANCE FOUND THAT THE GROUND AIR CONNECTION DUCT CLAMP Nov 5, 2017 · N608AT · Boeing 717200 · Cabin Pressure Control SystemSDR DALA2017110607950Cusp Web · crackedCRACKED RT CUSP WEB BETWEEN BS 218 TO 237. THE CUSP WEB WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.Nov 5, 2017 · N994AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017110607949Shear Tie · crackedCRACKED SHEAR TIE BS 1022 BETWEEN LONGERONS 12L TO 17L. THE SHEAR TIE WAS REPLACED IAW SRM 51-20-09-0G, 54-41-05-0G, AND DWG 9912243, REV J.Nov 5, 2017 · N994AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2017110507947Rub Strip · corrodedCORROSION ON THE RT WING ACCESS PANEL RUBSTRIP 620D. THE RUBSTRIP #620DT WAS REPLACED IAW SRM 57-10-01, REP 3.Nov 5, 2017 · N995AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2017110507945Beam · crackedCRACKED LEFT BEAM AT NLG DOOR FRAME BS 46. THE BEAM WAS REPAIRED IAW SRM 53-10-14-2R-2, FIG 201, SHEET 1.Nov 5, 2017 · N994AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017110507944Door Frame · crackedCRACK ON NLG LT DOOR FRAME AT BS 46. REPAIRED IAW SRM 53-10-14-2R. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND AFT STOP DRILL IAW NDT SPM PART 6, 06-10-01.001.Nov 5, 2017 · N995AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017110507943Door Frame · crackedCRACK ON NLG RT DOOR FRAME AT BS 46. CRACK ON NLG RH DOOR JAMB AT STA 46 APPROX WAS REPAIRED IAW SRM 53-10-14-2R. NO CRACKS WERE FOUND AFT STOP DRILL IAW NDT SPM PART 6, 06-10-01.Nov 5, 2017 · N995AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017110507948Rub Strip · corrodedCORROSION POINTS ON THE RIGHT WING FUEL ACCESS PANEL RUB STRIP 620CT. THE RUBSTRIP WAS REPLACED IAW SRM 57-10-01, REP 3.Nov 4, 2017 · N995AT · Boeing 717200 · Wing Main, Frame StructureSDR DALA2017110507942Web · crackedCRACKED WEB AT NLG DOOR FRAME STATION 46, REPAIRED IAW SRM 53-10-14-2R-2, FIG 201, SHEET 1.Nov 4, 2017 · N994AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017110507941Retainer · corrodedCORROSION ON THE R1 DOOR SEAL RETAINER. THE RETAINER WAS REPLACED IAW SRM 51-41-01 AND DWG 5910084, REV EP.Nov 4, 2017 · N995AT · Boeing 717200 · Service DoorsSDR DALA2017110507940Tab · delaminatedDELAMINATED RUDDER TRIM TAB. THE TRIM TAB WAS REPAIRED IAW SRM 51-70-02-2R, PROCEDURE 7, PARAGRAPH 4 B.Nov 4, 2017 · N995AT · Boeing 717200 · Rudder, Tab StructureSDR DALA2017110507939Former · crackedCRACKED FORMER BS 694. THE FORMER WAS REPAIRED IAW SRM 51-70-11-2R-1, 51-41-02-0G, AND 51-41-05-0G.Nov 4, 2017 · N994AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017110407938Skin · damagedVERTICAL STAB LOWER LE SKIN AT ZFS 52 WORN AND CHAFED. SKIN SPLICE ON INNER SURFACE 15 INCHES ALONG LEADING EDGE. REPAIRED IAW PRI 562910-14AD REV. 0, REV 1, AND REV. 2 AND ER/A 562910-14AD REV. ORIGINAL.Nov 3, 2017 · N946AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2017110407937Skin · damagedVERTICAL STABILIZER LEADING EDGE HAD SIGNS OF DISTRESS TO COUNTERSINKS, ALL FASTENERS ARE LOOSE. REPAIRED IAW PRI 562910-14AD REV 0, REV 1. AND REV 2, ER/A 562910-14AD, REV ORIGINAL.Nov 3, 2017 · N946AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2017110407936Spar Cap · damagedRT VERTICAL STABILIZER FRONT SPAR CAP FORWARD FLANGE, FIRST HOLE BELOW LEADING EDGE SKIN SPLICE IS OUT-OF-ROUND & UNABLE TO PERFORM OPEN-HOLE HFEC INSPECTION. REPAIRED IAW PRI 561916-14AD, REV 0, & 1, AND ER/A 561916-14AD, REV ORIG.Nov 3, 2017 · N946AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2018122607396Structure · damagedDAMAGE FOUND AFT OF L1 DOOR LOWER EDGE AT STATION 227 AND 1 INCH ABOVE L-20 STRINGER. COMPLIED WITH REPAIR INSTRUCTIONS IAW ER/A 563130-14 REV ORIG. WILL REQUIRE REPEATED INSPECTION EVERY 20 DAYS AND A PERMANENT REPAIR AT OR BEFORE NEXT C-CHECK. NO CRACK INDICNov 2, 2017 · N996AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2018110606494Skin · gougedDENT AND GOUGE DAMAGE AT STA 227 ABOVE L-20L. ER/A 563130-14 REV A IS CURRENT.Nov 2, 2017 · N996AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017110307970Floor Support · corrodedCORROSION ON FLOOR SUPPORT RBL 45, BS 160 - 200. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-02-0G.Nov 2, 2017 · N994AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017110307934Threshold · corrodedCORROSION AT FWD LAVATORY ENTRY DOOR LOWER THRESHOLD. REPAIRED IAW PRI 561911-14, REV 0, AND ER/A 562911-14, REV ORIGINAL.Nov 2, 2017 · N946AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017110307933Skin · crackedCRACK ON THE FUSELAGE SKIN AROUND AFT THE HINGE OF THE NLG DOOR. THE SKIN WAS REPAIRED IAW SRM 53-10-01-2R-11, 51-41-02-0G, AND 51-41-05-0G.Nov 2, 2017 · N994AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017110307930Pan · crackedCRACK ON INNER PAN AT FWD CARGO DOOR AFT EDGE BS BS 427 BETWEEN BEAMS NR 5 AND 4. THE PAN WAS REPAIRED IAW SRM 52-30-02-2R-1, FIG 201.Nov 2, 2017 · N994AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2017110307929Skin · crackedFUSELAGE SKIN HAS A CRACK EMANATING FROM FASTENER HOLE 6 INCHES ABOVE RT PYLON, BS 1076. REPAIRED THE SKIN IAW PRI 562852-14, REV 0, REV 1, REV 2, AND ER/A 562852-14, REV ORIGINAL.Nov 2, 2017 · N946AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017110307927Skin · crackedFUSELAGE SKIN HAS A CRACK EMANATING FROM FASTENER HOLE AT BS 1095, 8 INCHES ABOVE THE LT PYLON. PERFORMED HFEC IAW AMM NDT SPM 06-10-01.001. REPAIRED THE SKIN IAW PRI 562854-14, REV 0, REV 1, AND REV 2, AND ER/A 562854-14, REV ORIGINAL.Nov 2, 2017 · N946AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017110307926Stop Fitting · corrodedCORROSION ON THE AFT CARGO DOOR STOP FITTING NR 3. THE STOP FITTING WAS REPLACED IAW SRM 51-41-01, AND 51-41-05.Nov 2, 2017 · N994AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2017111308094Cover · looseEMERGENCY EXIT SIGN COVER LOOSE. TRIM PIECE SURROUNDING EXIT SIGN AT AFT JUMP TAPED AND SECURE. REPLACED AFT EMERGENCY EXIT COVER BY REMOVING TWO SCREWS HOLDING IT IN PLACE. CHECKS GOOD. OKAY FOR SERVICE.Nov 1, 2017 · N948AT · Boeing 717200 · Emergency LightingSDR DALA2017110207914Floor Support · corrodedCORROSION ON FLOOR SUPPORT LBL 7 BETWEEN BS 148 - 200. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-01-0G, 51-41-08-0G, AND 51-10-04-0G, PAR 21, 15, 37.Nov 1, 2017 · N994AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017110207913Pan · corrodedAFT LOWER LEFT FUSELAGE, LAVATORY SERVICING PAN HAS MULTIPLE AREAS OF CORROSION. REPAIRED IAW ER/A 561915-14, REV ORIG.Nov 1, 2017 · N946AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017110207912Shear Tie · crackedCRACK ON SHEAR TIE BS 1087 BETWEEN LONGERONS 13 & 14R. THE SHEAR TIE WAS REPLACED IAW SRM 51-20-09-0G, 51-41-05-0G, AND DWG 9971140, REV F.Nov 1, 2017 · N994AT · Boeing 717200 · Fuselage Internal Mounting StructureSDR DALA2017110207911Doubler · corrodedCORROSION ON INTERNAL DOUBLER BETWEEN BS 968 TO 978 AT THE LWR CARGO DOOR FRAME. THE DOUBLER WAS REPAIRED IAW ETI 17-17-205, REV 3, AND ER/A 562358-14, REV ORIG.Nov 1, 2017 · N979AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017110107910Floor Support · corrodedCORROSION ON FLOOR SUPPORT BS 197 TO 200 LBL 57. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-20-09-0G, 51-41-05-0G, AND 51-41-02-0G.Oct 31, 2017 · N994AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017110107884Longeron · corrodedCORROSION ON CARGO BAY LONGERON 30, BS 900 - 1006. THE LONGERON WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05.Oct 31, 2017 · N979AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017110107883Door Frame · corrodedCORROSION ON THE AFT LOWER CARGO DOOR FRAME BETWEEN BS 954 AND 994. THE DOOR FRAME WAS REPAIRED IAW ER/A 562361-14, REV ORIG, AND ETI-17-17-203, REV 3.Oct 31, 2017 · N979AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017110107882Frame Angle · corrodedCORROSION ON FRAME ANGLE, BS 908 BETWEEN LONGERONS 26R TO 26L. THE FRAME ANGLE WAS REPLACED IAW SRM 53-20-07-01-3, 51-41-02 0G, AND 51-41-05 0G.Oct 31, 2017 · N979AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2017103107880Web · corrodedCORROSION ON WEB AT BS 200 BETWEEN RBL 7 AND RBL 13. REPAIRED IAW SRM 51-70-10-2R.Oct 30, 2017 · N994AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017103107878Rub Strip · corrodedCORROSION AND DISBONDED RUB STRIPS AT THE LT AND RT SIDE ON FILLET PANELS. THE RUBSTRIPS WERE REPLACED IAW SRM 53-20-70-01, AND 51-20-05-0G.Oct 30, 2017 · N979AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017103107877Seat Track · corrodedCORROSION ON COCKPIT RT SEAT TRACK BETWEEN BS 110 AND 140, RBL 44. DAMAGED AREA WAS REPAIRED IAW ER/A 562373-14, REV ORIG, AND ETI-17-17-215, REV 1.Oct 30, 2017 · N979AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017103107855Sign · missingDOOR 1L EXIT SIGN IS MISSING. MAINTENANCE INSTALLED THE EXIT SIGN AS PER AMM 33-51. OPERATIONAL CHECK WAS NORMAL.Oct 30, 2017 · N978AT · Boeing 717200 · Emergency LightingSDR DALA2017103107854Diaphragm · corrodedEXCESSIVE CORROSION ON DIAPHRAGM AT STA Y=200 BTW X=7 AND X=8 IN REF NRC 00328. LEVEL CORROSION 2. REPAIR WAS ACCOMPLISHED PER SRM 53-00-00-2R.Oct 30, 2017 · N994AT · Boeing 717200 · Fuselage Miscellaneous Structure
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