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 DALA2018030401383Bearing · looseRIGHT INBD SPOILER PANEL CENTER HINGE BEARING LOOSE IN BORE. THE SPOILER PANEL WAS REPLACED.Mar 3, 2018 · N894AT · Boeing 717200 · SpoilersSDR DALA2018030301831Skin · crackedCRACKED LOWER SKIN AT RT UPPER MOVABLE VANE. RT UPPER MOVABLE VANE WAS REPAIRED PER SRM 57-53-01-2R-1 PARAGRAPH 4 FIG 201.Mar 2, 2018 · N892AT · Boeing 717200 · Trailing Edge FlapsSDR DALA2018030501385Light · brokenEMERGENCY LIGHT STRIP BROKEN AT SEAT 21B. REINSTALLED THE LIGHT STRIP. CHECKED OK.Mar 2, 2018 · N988DN · Boeing 717200 · Emergency LightingSDR DALA2018030301381Floor Support · corrodedCORROSION ON THE FLOOR SUPPORT. THE FLOOR SUPPORT WAS REPLACED IAW DWG #9957828, REV Y.Mar 2, 2018 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030301380Pan · corrodedCORROSION ON LOWER PAN OF THE LOWER DOOR FRAME IN THE AFT CARGO BAY, THE PAN WAS REPLACED IAW SRM 51-41-02-0G, 51-41-05-0G, AND SRM 53-20-15-2R-7.Mar 2, 2018 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030301379Floorbeam · corrodedCORROSION ON THE FLOORBEAM AT BS 148, BETWEEN RBL 30 AND 44. THE FLOORBEAM WAS REPLACED IAW SRM 53-10-51-01-2, FIG 1, AND 51-40-08-0G.Mar 2, 2018 · N955AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2018030301378Cusp Web · corrodedCORROSION ON CUSP WEB BS 389, RBL 54. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 224.Mar 2, 2018 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030301376Splice · corrodedCORROSION ON FUSELAGE SPLICE BETWEEN BS 579 TO 598, LONGERON 18R AND 19R. THE SPLICE WAS REPLACED IAW DWG 9910151, REV BL, AND SRM 51-41-05-0G.Mar 2, 2018 · N955AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018030301375Cusp Web · crackedCRACKED CUSP WEB BETWEEN BS 579 TO 598, RBL 54 - 60. THE CUSP WEB WAS REPLACED IAW DWG 9910151, REV BL, SRM 51-41-02-0G, 51-41-05-0G, AND 51-41-01-0G.Mar 2, 2018 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030201316Cusp Web · crackedCRACK ON THE RT CUSP WEB BS 218 TO 237, BETWEEN RBL 54 AND 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 215.Mar 1, 2018 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030101294Battery Pack · dischargedTHE EMERGENCY PATH LIGHTS WERE FOUND TO BE INOPERATIVE AT THE FWD RIGHT GALLEY OVERHEAD, THE EXIT LOCATOR IN THE CEILING AT ROW 1, AND AT THE FWD DROP DOWN CEILING NEXT TO THE LAVATORY. MAINTENANCE REPLACED THE BATTERY PACK B5-259 IAW AMM 33-51 AND THE EMERGENMar 1, 2018 · N603AT · Boeing 717200 · Emergency LightingSDR DALA2018030101315Access Panel · corrodedCORROSION ON FUEL ACCESS PANELS 520CT AND 620CT. THE ACCESS PANELS WERE REPLACED IAW SRM 57-10-01, REPAIR 2, PAR 5, CONDITION III.Feb 28, 2018 · N955AT · Boeing 717200 · Wing, Plate/SkinSDR HALA2018022800061Wire · unsecureATB, EN ROUTE TO DESTINATION, LT ENGINE SYS FAIL ALERT. FLASHING X ON TGT GAUGE. NO CURRENT FAULTS NR 1 EEC FAULT REVIEW SHOWS CODE 772103. TGT CIRCUIT FAULT CH-A/CH-B DISAGREE. REPAIRED WIRE 2A00G20 TO T1040-2 PER SWPM 20-20-01 AND SECURED WIRE CONNECTIONFeb 28, 2018 · N477HA · Boeing 717200 · Engine Indicating System WiringSDR DALA2018030101293Beam · crackedCRACK ON INNER PAN IN BEAM NR 1 STA Y=427 AT FWD CARGO COMPARTMENT DOOR (PTAS). INNER PAN IN BEAM NR 1 STA Y=427 WAS REPAIRED PER SRM 52-30-02-2R-1 FIG 201.Feb 28, 2018 · N938AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2018030101292Beam · crackedCRACK ON INNER PAN IN BEAM NR 3 STA Y=370 AT FWD CARGO COMPARTMENT DOOR (PTAS). INNER PAN IN BEAM NR 3 STA Y=370 WAS REPAIRED PER SRM 52-30-02-2R-1 FIG 201.Feb 28, 2018 · N938AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2018030101291Membrane · crackedCRACK ON MEMBRANE STA Y=674 X=-54 AT PASSENGER CABIN. DAMAGE AREA WAS REPAIRED PER SRM 53-00-55-2R FIG 223 (ET) HFEC INSPECTION WAS ACCOMPLISHED ON MEMBRANE STA Y=674 X=-54 AT PASSENGER CABIN AND NO CRACKS WERE FOUND AFTER TRIM OUT PER NDT SPM 06-10-01.001. EQFeb 28, 2018 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018030101290Tee Fitting · crackedCRACK ON INTERNAL FITTING "T" STA Y=389 (LOWER EDGE) AT FWD CARGO COMPARTMENT DOOR (PTAS). FITTING "T" STA Y=389 WAS REPLACED PER SRM 51-41-01, 51-41-02, 51-41-05, AND DWG 3926046 REV D.Feb 28, 2018 · N938AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2018030101289Beam · crackedCRACK ON INNER PAN IN BEAM NR 5 STA Y=427 AT FWD CARGO COMPARTMENT DOOR (PTAS). PAN IN BEAM NR 5 STA Y=427 WAS REPAIRED PER SRM 52-30-02-2R-1 FIG 201.Feb 28, 2018 · N938AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2018030101288Beam · crackedCRACK ON INNER PAN IN BEAM NR 5 STA Y=370 AT FWD CARGO COMPARTMENT DOOR (PTAS). PAN IN BEAM NR 5 STA Y=370 WAS REPAIRED PER SRM 52-30-02-2R-1 FIG 201.Feb 28, 2018 · N938AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2018030101287Beam · crackedCRACK ON INNER PAN IN BEAM NR 1 STA Y=370 AT FWD CARGO COMPARTMENT DOOR (PTAS). PAN IN BEAM NR 1 STA Y=370 WAS REPAIRED PER SRM 52-30-02-2R-1 FIG 201.Feb 28, 2018 · N938AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2018022801273Floor Panel · crackedCRACKED CHANNELS ON FLOOR PANELS #221XF, 221TF, 222AFF, AND 222AJF AT PAX CABIN (CPAX). NRC 00438: CRACKED CHANNELS ON FLOOR PANELS #221XF, 221TF, 222AFF AT PAX CABIN WERE REPAIRED PER B717 SRM 53-00-00-1A FIG 101. AND CRACKED CHANNEL ON FLOOR PANEL 222AJF WAFeb 27, 2018 · N938AT · Boeing 717200 · Fuselage Floor PanelSDR DALA20180301295Unknown · malfunctionedTHE FLIGHT CREW DECLARED AN EMERGENCY ON APPROACH INTO CAE AFTER THE FLAPS STOPPED EXTENDING BEYOND 18 DEGREES. MAINTENANCE FUNCTIONALLY CHECKED THE FLAP CONTROL SYSTEM, THE FLAP POSITION TRANSMITTERS, THE FLAP RATE TEST, AND THE ADJUSTMENT OF THE FLAP BUS CABFeb 27, 2018 · N988DN · Boeing 717200 · Trailing Edge Flap Control SystemSDR DALA2018022801272Pan · crackedCRACKED UPPER AFT CORNER OF THE RT WINDOW RING PAN BS 851. THE RING PAN WAS TRIMMED OUT, NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. REPAIRED IAW SRM 56-20-02-2R-1 FIG.202, SRM 51-41-02-0G, AND SRM 51-41-05-0G.Feb 27, 2018 · N955AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018022801271Pan · crackedCRACKED UPPER FWD CORNER OF THE LT WINDOW RING PAN BS 696. THE PAN WAS TRIMMED OUT, NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. REPAIRED IAW SRM 56-20-02-2R-1 FIG.202, SRM 51-41-02-0G AND SRM 51-41-05-0G.Feb 27, 2018 · N955AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018022801270Pan · crackedCRACKED LOWER FWD CORNER OF THE RT WINDOW RING PAN BS 889. THE RING PAN WAS TRIMMED OUT, NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. REPAIRED IAW SRM 56-20-02-2R-1, FIG.202, SRM 51-41-02-0G, AND SRM 51-41-05-0G.Feb 27, 2018 · N955AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018022801269Pan · crackedCRACKED AFT UPPER CORNER OF THE LT WINDOW RING PAN AT BS 889 AND 870. THE RING PAN WAS TRIMMED OUT, NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. REPAIRED IAW SRM 56-20-02-2R-1, FIG.202, SRM 51-41-02-0G, AND SRM 51-41-05-0G.Feb 27, 2018 · N955AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018022801268Pan · crackedCRACKED LOWER FWD CORNER OF THE LEFT WINDOW RING PAN BS 579 AND 908. THE WINDOW RING PAN WAS TRIMMED OUT, NO CRACKS WERE FOUND IAW NDT SPM 06-10-01.001. REPAIRED IAW SRM 56-20-02-2R-1, FIG.202, SRM 51-41-02-0G, AND SRM 51-41-05-0G.Feb 27, 2018 · N955AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018022801267Cusp Web · crackedCRACKED CUSP WEB BETWEEN BS 655 TO 674, RBL 54 - 60. THE DAMAGE WAS REMOVED IAW SRM 53-00-55-2R-4, FIG 216.Feb 27, 2018 · N955AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018022801266Door Frame · crackedA CRACK WAS FOUND ON THE AFT CARGO DOOR FRAME AFT EDGE. THE DOOR FRAME WAS REPAIRED IAW SRM 53-20-15-2R, PROCEDURE 12, PARAGRAPH 6 A.Feb 27, 2018 · N892AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018022801265Door Frame · crackedCRACK FOUND ON THE LT NLG DOOR FRAME BEAM Y=40. REPAIRED IAW SRM 53-10-14-2R, PROCEDURE 2, REPAIR 2.Feb 27, 2018 · N892AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018022801264Door Frame · crackedCRACK ON THE RT NLG DOOR FRAME BEAM Y=40. REPAIRED IAW SRM 53-10-14-2R, PROCEDURE 2, REPAIR 2.Feb 27, 2018 · N892AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018022701261Door Frame · crackedCRACK ON L1 DOOR FRAME WEB BS 207, LONGERON 11L AND 15L. THE DOOR FRAME WEB WAS REPAIRED IAW SRM 53-10-15-2R-1.Feb 27, 2018 · N955AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018022701203Battery Pack · failedFOUND WALKWAY EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE FOUND THAT THE BATTERY PACK WAS NOT CHARGING. THE BATTERY PACK WAS REPLACED AND NOW THE LIGHT OPERATE NORMALLY.Feb 27, 2018 · N988AT · Boeing 717200 · Emergency LightingSDR HALA2018022700053Apu · malfunctionedSMOKE ODOR IN THE CABIN, FOLLOWED BY APU SHUTDOWN. REMOVED AND REPLACED THE APU IAW TASK CARD E1128-717-49-006. OPS AND LEAK CHECKED GOOD. OK FOR SERVICE.Feb 26, 2018 · N493HA · Boeing 717200 · APU Core EngineSDR DALA2018022701202Cusp Web · corrodedCORROSION ON CUSP WEB BS 487 - 491, BETWEEN RBL 54 TO RBL 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, FIG 215.Feb 26, 2018 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018022701201Door Frame · crackedCRACKS FOUND ON THE LT & RT DOOR FRAME BS 46 AT NLG WHEEL WELL. THE DOOR FRAME WAS REPAIRED IAW SRM 53-10-14 R2, FIG 201. HFEC INSPECTION WAS ACCOMPLISHED, AND NO CRACKS WERE FOUND AFTER CUT OUT IAW NDT SPM 06-10-01.001.Feb 26, 2018 · N938AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018022601170Power Supply · defectiveTHE TAIL CONE EMERGENCY EXIT LIGHT ILLUMINATED ON THE GROUND UNCOMMANDED. MAINTENANCE REPLACED THE AFT CABIN EMERGENCY EXIT LIGHT POWER SUPPLY PER AMM 33-51. THE LIGHT CHECKS GOOD AT THIS TIME.Feb 26, 2018 · N922AT · Boeing 717200 · Emergency LightingSDR DALA2018022601168Floor Panel · damagedPUNCTURED AND BROKEN ON FLOOR PANELS 211AQF, 211ALF, 221AF, 221BF, 221CF, 221EF, 221JF, AND 222PF AT PAX CABIN / COCKPIT. NRC 00473: FERRULES DAMAGES ON FLOOR PANEL 221EF, 222PF, 221BF, 221AF, AND 221JF WERE REPLACED PER B-717 SRM 53-20-50-2R PROCEDURE 3. FLOOFeb 25, 2018 · N938AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2018022601169Power Supply · inoperativeTHE OVERWING EMERGENCY LIGHT DOES NOT TURN ON. TROUBLE SHOT PER 33-50-00 810-801. DURING CHECK POWER SUPPLY B5-119 REPLACEMENT BECAME REQUIRED. POWER SUPPLY WAS REPLACED PER AMM 33-51-03 AND TEST WAS PERFORMED PER AMM 33-51-00. OPERATIONAL TEST IS OK.Feb 25, 2018 · N988DN · Boeing 717200 · Emergency LightingSDR DALA2018022601167Intercostal · crackedCRACKED INTERCOSTAL IN X=O BTW STA Y=1002-1022 AT PAX CABIN. INTERCOSTAL IN X=O BTW STA Y=1002-1022 AT PAX CABIN WAS REPLACED PER SRM 51-41-02-0G AND SRM 51-41-05-0G.Feb 25, 2018 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018022601166Fitting · crackedCRACK FRAME CLIPS BTW LONG 13L AND 14L STA Y=1022 AND LONG 13R TO 14R. FRAME CLIP REPLACED PER DWG 9912243 REV HG. HFEC INSPECTION WAS ACCOMPLISHED ON FRAME CLIPS BTW LONG 13L AND 14L AND LONG 13R TO 14R STA Y=1022. CRACK OF 0.375" LENGTH ON FRAME CLIP BTW LONFeb 25, 2018 · N938AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018022601165Floor Panel · brokenBROKEN FLOOR PANEL NR 211ANF OF COCKPIT. FLOOR PANEL 211ANF WAS FABRICATED, REPLACED. AND IDENTIFIED PER SRM 53-20-50-2R PROCEDURE 3. AND WAS INSTALLED WITH THE CARD JIC 2040-0058.Feb 25, 2018 · N938AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2018022601164Access Panel · corrodedCORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS PLATES 620CT. CORROSION LEVEL 2, FUEL ACCESS PLATE 620CT WAS REPLACED AND VERIFIED PER IPC 57-22-01. INSTALLATION IS ATTENDED WITH CARD 2040-0012.Feb 25, 2018 · N938AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018022601163Access Panel · corrodedCORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS PLATES 620DT. CORROSION LEVEL 2, FUEL ACCESS PLATE 620DT WAS REPLACED AND VERIFIED PER IPC 57-23-01. INSTALLATION IS ATTENDED WITH CARD 2040-0012.Feb 25, 2018 · N938AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018022601162Access Panel · corrodedCORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS PLATES 520DT. CORROSION LEVEL 2, FUEL ACCESS PLATE 520DT WAS REPLACED AND VERIFIED PER IPC 57-23-01. INSTALLATION IS ATTENDED WITH CARD 2040-0010.Feb 25, 2018 · N938AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018022601161Access Panel · corrodedCORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS PLATES 620CB. CORROSION LEVEL 2, FUEL ACCESS PLATE 620CB WAS REPLACED AND VERIFIED PER IPC 57-23-01. INSTALLATION IS ATTENDED WITH CARD 2040-0012.Feb 25, 2018 · N938AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018022601160Access Panel · corrodedCORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS PLATES 520CT. CORROSION LEVEL 2, FUEL ACCESS PLATE 520CT WAS REPLACED AND VERIFIED PER IPC 57-22-01. INSTALLATION IS ATTENDED WITH CARD 2040-0010.Feb 25, 2018 · N938AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018022701263Access Panel · corrodedCORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS PANEL 520HB. THE ACCESS PANEL WAS REPAIRED IAW SRM 57-10-01, REPAIR 2, PAR. 5, CONDITION II.Feb 24, 2018 · N938AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018022701262Floorbeam · corrodedCORROSION ON THE FLOORBEAM ANGLE BS 200 BETWEEN RBL 22 TO 44 AND BTW RBL 44 TO 56. THE FLOORBEAM ANGLE WAS REPLACED IAW SRM 51-41-02-0G, AND 51-41-05-0G.Feb 24, 2018 · N938AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2018022501159Rib · crackedCRACK ON SLAT NR 5 CORNER EXTERNAL LOWER SIDE STA XW 536.861 APPROX AT LT WING. CRACKED RIB ON SLAT NR 5 WAS REPLACED PER SRM 51-41-02 AND 51-41-08.Feb 24, 2018 · N938AT · Boeing 717200 · Leading Edge Devices
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