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 DALA2016080905885Floor Panel · damagedCRACKED CHANNEL ON FLOOR PANEL. FLOOR PANEL REPAIRED PER SRM 53-20-50 FIG. 201.Aug 8, 2016 · N959AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016080905884Cusp Web · corrodedCORROSION ON RT CUSP WEB REPAIR DOUBLER LOWER SKIN BS 446 - 465, X 56 - X 60. REPAIRED PER SRM 53-05-55 FIG. 216, 51-41-02, 51-40-8 PAR. 3, AND 51-10-04 PAR 21-15 AND 37, 51-41-05.Aug 8, 2016 · N959AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016080905883Cusp Web · corrodedCORROSION ON RT CUSP WEB BETWEEN BS 484 - 503. REPAIRED IAW SRM 51-41-02, 53-00-55. FIG.215 AND 51-41-05.Aug 8, 2016 · N959AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016080805823Seat Track · corrodedCORROSION ON LT SEAT TRACK, X=44.5 BETWEEN STA 957-STA 960, ON REF CARD 23, ZONE 200. CUT OUT IN TRACK WAS ACCOMPLISHED IAW SRM 53-20-52, FIG 201, ON STA 957-STA 960, X=44.5 NDT INSPECTION ON AREA NO CRACKS WERE FOUND AROUND CUTOUT, IAW NDT SPM 06-10-01-001, Aug 7, 2016 · N959AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016080805822Fitting · crackedCRACKED RT CLIP FRAME ON CANTED KEELBEAM STA 681 AND 696, CARD 17, ZONE 140. FRAME CLIPS ON STA 681 AND STA 696 WERE REPAIRED IAW SRM 51-70-11, FIG 201.Aug 7, 2016 · N959AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016080805821Fitting · crackedCRACKED LT CLIP FRAME ON CANTED KEELBEAM, STA 681 AND STA 696, CARD 16, ZONE 140. FRAME CLIPS ON STA Y=681 AND Y=696 WERE REPAIRED IAW SRM 51-70-11, FIG 201.Aug 7, 2016 · N959AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016080805824Power Supply · inoperativeDURING LINE CHECK, MAINTENANCE FOUND THAT SEVERAL OVERHEAD EMERGENCY PATHWAY LIGHTING IN THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY PACK 3D AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.Aug 6, 2016 · N946AT · Boeing 717200 · Emergency LightingSDR DALA2016080905882Cusp Web · crackedLEFT CUSP WEB CRACKED AT BS 222 LBL 44.5. REPAIRED IAW SRM 53-00-55 REPAIR 4.Aug 5, 2016 · N906AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016080605820Cusp Web · corrodedEXCESSIVE CORROSION ON LT CUSP MEMBRANE BETWEEN STA 756-775 IN REF CARD 62, ZONE 200. WB, CARD 104, ZONE 200. DUE TO CUSP WEB MEASURE OUT OF LIMITS .028" OF .040", REPAIR WAS ACCOMPLISHED IAW SRM 53-00-55, FIG 215. RII COMPLETED.Aug 5, 2016 · N959AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016110208145Access Panel · corrodedCORROSION ON ACCESS PANEL 370KR VOR / LOCALIZER ANTENNA PANEL.. UPPER RT VOR / LOCALIZER ANTENNA WAS REPLACED IAW AMM 34-32-03 AND TEST WAS PERFORMED IAW AMM 34-35-01 TEST OK.Aug 4, 2016 · N959AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016110208144Access Panel · corrodedCORROSION ON ACCESS PANEL 370JL VOR / LOCALIZER ANTENNA PANEL. UPPER LT VOR / LOCALIZER ANTENNA PANEL WAS REPLACED IAW AMM 34-32-03 AND TEST WAS PERFORMED IAW AMM 34-35-01. TEST OK.Aug 4, 2016 · N959AT · Boeing 717200 · Visual Omnirange (VOR) SystemSDR DALA2016110208143Access Panel · corrodedCORROSION ON ACCESS PANEL 370DL VOR/LOCALIZER ANTENNA PANEL. LOWER LT VOR/LOCALIZER ANTENNA PANEL WAS REPLACED IAW AMM 34-32-03 AND TEST WAS PERFORMED IAW AMM 34-35-01. TEST OK.Aug 4, 2016 · N959AT · Boeing 717200 · Visual Omnirange (VOR) SystemSDR DALA2016110108052Access Panel · corrodedCORROSION ON ACCESS PANEL 370GR VOR/LOCALIZER ANTENNA PANEL. LOWER RT VOR/LOCALIZER ANTENNA PANEL WAS REPLACED IAW AMM 34-32-03 AND TEST WAS PERFORMED IAW AMM 34-35-01. TEST OK.Aug 4, 2016 · N959AT · Boeing 717200 · Glide Slope SystemSDR HALA2016080400317Apu · failedWHILE ON THE GROUND AND BOARDING FOR NEXT FLIGHT, SMELLED ELECTRICAL SMOKE & HEARD 2 LOUD BANGS, AIRPLANE WENT DARK WHEN THE APU SHUTDOWN. VISUAL FLAMES NOTED FROM LINE SERVICE. REMOVED & REPLACED APU ASSEMBLY.Aug 4, 2016 · N487HA · Boeing 717200 · APU Core EngineSDR DALA2016080505781Seat Track · corrodedLEFT CENTER SEAT TRACK, LBL 44.5, BS 986 - 1053 CORRODED. SEAT TRACK BLENDED AND FOUND TO BE OUT OF LIMITS IAW SRM 40-20-50. REPLACED THE SEAT TRACK SECTIONE. FABRICATED IAW DWG 9981474 AND ER/A 547506-14-REV A.Aug 4, 2016 · N906AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2016080505780Pan · crackedCRACKED RT RING PAN FWD LWR BS 794. REPAIRED IAW SRM 56-20-02 TYPE B REPAIR FIG 202.Aug 4, 2016 · N959AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016080405761Cusp Web · corrodedCORROSION ON RT CUSP WEB REPAIR DOUBLER AND ADJACENT AREA BETWEEN STA Y=465 AND STA Y=484 UPPER LOWER SKIN FROM X=56 TO X=60 AT PASSENGER CABIN, CARD 50, ZONE 200. DUE EXCESSIVE DAMAGE, CUSP WEB WAS REPAIRED IAW SRM 53-00-55, FIG 216.Aug 3, 2016 · N959AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016080405760Pan · crackedCRACK FORWARD LOWER RING PAN STA Y=579 RT SIDE AT PASSENGER CABIN STRUCTURE. SM, CARD 3, ZONE 100. RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK LENGTH: 0.159" AND NO CRACKS WERE FOUND AFTER REMOVED DAMAGE IAW HFEC INSPECTION.Aug 3, 2016 · N959AT · Boeing 717200 · Passenger Compartment WindowsSDR DALA2016080405759Pan · crackedCRACKED AFT LOWER RING PAN STA Y=851 LT SIDE AT PASSENGER CABIN STRUCTURE, CARD 4, ZONE 100. RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK LENGTH 0.132" AND NO CRACKS WERE FOUND AFTER REMOVE DAMAGE IAW HFEC INSPECTION.Aug 3, 2016 · N959AT · Boeing 717200 · Passenger Compartment WindowsSDR DALA2016080405758Pan · crackedCRACKED AFT UPPER RING PAN STA Y=832, LT SIDE AT PASSENGER CABIN STRUCTURE, CARD 5, ZONE 100. RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK LENGTH 0.109" AND NO CRACKS WERE FOUND AFTER REMOVED DAMAGE IAW HFEC INSPECTION.Aug 3, 2016 · N959AT · Boeing 717200 · Passenger Compartment WindowsSDR DALA2016080405757Pan · crackedCRACKED AFT LOWER RING PAN STA Y=636 LT SIDE AT PASSENGER CABIN STRUCTURE, CARD 6, ZONE 100. RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK LENGTH 0.140" AND NO CRACKS WERE FOUND AFTER REMOVE DAMAGE IAW HFEC INSPECTION.Aug 3, 2016 · N959AT · Boeing 717200 · Passenger Compartment WindowsSDR DALA2016080405756Pan · crackedCRACKED AFT LOWER RING PAN, STA Y=617 LT SIDE AT PASSENGER CABIN STRUCTURE. SM, CARD 7, ZONE 100. RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK LENGTH: 0.125" AND NO CRACKS WERE FOUND AFTER REMOVE DAMAGE IAW HFEC INSPECTION.Aug 3, 2016 · N959AT · Boeing 717200 · Passenger Compartment WindowsSDR DALA2016080405755Pan · crackedCRACKED AFT LOWER RING PAN STA Y=560 LT SIDE AT PASSENGER CABIN STRUCTURE. SM, CARD 8 ZONE 100. RING PAN WAS REPAIRED IAW SRM 56-20-02, FIG 202, TYPE B. CRACK LENGTH=0.158" AND NO CRACKS WERE FOUND AFTER REMOVE DAMAGE IAW HFEC INSPECTION.Aug 3, 2016 · N959AT · Boeing 717200 · Passenger Compartment WindowsSDR DALA2016110108051Skin · corrodedFUSELAGE SKIN STA 1002 L-24R - L-25R. CORROSION REPAIRED BY ER/A 547501-14. ACCOMPLISH SECTION II INSPECTIONS EVERY 8000 CYCLES AFTER SECTION I REPAIR.Aug 2, 2016 · N910AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016080405754Skin · corrodedCORROSION ON FUSELAGE INTERIOR SKIN AND FINGER DOUBLERS FROM STA 1002 TO STA 1012 BETWEEN LONGERONS 22R AND 26R. BLENDED CORROSION ON INTERNAL SKIN. NOMINAL THICKNESS .063. REMAINING .041. FOUND TO BE OUT OF LIMITS IAW SRM 53-01-01, FIG 103, STA 1005 L25R. Aug 2, 2016 · N910AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016080305722Fitting · crackedCRACK ON STRAP BETWEEN LONGERON 13/14 RT STA 1022, REAR FACE OF BULKHEAD, CARD 23, ZONE 220. SHEAR CLIP WAS REPLACED IAW SRM 53-20-07, 51-40-02, AND 51-41-05.Aug 2, 2016 · N959AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016080305721Skin · crackedCRACKED EXTERNAL FUSELAGE SKIN BETWEEN LONG 13RT AND 14RT STA Y=1087, CARD 2, ZONE 200. EXTERNAL FUSELAGE SKIN BETWEEN LONG 13 RT AND 14 RT STA Y=1087 WAS REPAIRED IAW ER/A 547894-14, REV ORIGINAL SECTION I. ACCOMPLISH ER/A 547894-14, REV ORIGINAL SECTION IIAug 2, 2016 · N959AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016080305720Skin · crackedCRACKED EXTERNAL FUSELAGE SKIN BETWEEN LONGERON 13RT AND 14RT STA Y=1078 TO Y=1074, CARD 1 ZONE 200. EXTERNAL FUSELAGE SKIN BETWEEN LONG 13 RT AND 14 RT STA Y=1078 TO Y=1074 WAS REPAIRED IAW ER/A 547894-14, REV ORIGINAL SECTION I. ACCOMPLISH ER/A 547894-14 RAug 2, 2016 · N959AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016080205719Fitting · corrodedCORROSION ON LONGERON 25R END CAP AND POSSIBLY ON LONGERON 25R FROM STA 1002 TO STA 1022. REPLACED LONGERON 25R END FITTING AT FS 1002 IAW SRM 51-4-05. NO CORROSION NOTED ON LONGERON 25R FS 1002 TO 1022.Aug 1, 2016 · N910AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2016080205718Door Frame · corrodedFUSELAGE AFT CARGO LOWER DOOR JAMB HAS NUMEROUS AREAS OF CORROSION FROM THE AFT LOWER STOP FITTING DOWN TO AND AROUND THE FORWARD LOWER STOP FITTING. REPLACED LOWER DOOR JAMB IAW SRM 53-20-15, REPAIR 7.Aug 1, 2016 · N910AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2016080205717Skin · corrodedCORROSION ON SKIN AT STA 1212.225 L30 FOUND TO BE OUT OF LIMITS, REF ORNRC 7046-0100-0041. INSTALLED REPAIR DOUBLER IAW SRM 53-02-01, REPAIR 1, FIGURE 202 AT STA 1212.225 L30.Aug 1, 2016 · N906AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2016080105680Access Panel · corrodedCORROSION ON COUNTERSINKS AT FUEL TANK ACCESS 520 MB. CORROSION WAS REMOVED, REWORKED AREAS WERE MEASURED. IT IS OUT OF LIMITS IAW SRM 51-10-01. FUEL ACCESS WAS REPLACED AND PN VERIFIED IAW AIPC 57-23-01-01 AND MUST BE INSTALLED WITH CARD 2040-0010, ZONE 52Jul 31, 2016 · N959AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016080105679Access Panel · corrodedCORROSION ON COUNTERSINKS AT FUEL TANK ACCESS NR 620JB, SM. CORROSION WAS REMOVED, REWORKED AREA WERE MEASURED. IT IS OUT OF LIMITS IAW SRM 51-10-01. FUEL ACCESS WAS REPLACED AND PN VERIFIED IAW AIPC 57-23-01-01 AND MUST BE INSTALLED WITH CARD 2040-0012, ZOJul 31, 2016 · N959AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016080105678Access Panel · corrodedCORROSION ON COUNTERSINKS AT FUEL TANK ACCESS 620 CB, SM. CORROSION WAS REMOVED, REWORKED AREAS WERE MEASURED. IT IS OUT OF LIMITS IAW SRM 57-10-01. FUEL ACCESS WAS REPLACED AND PN VERIFIED IAW AIPC 57-23-01-01 AND MUST BE INSTALLED WITH CARD 2040-0012, ZONJul 31, 2016 · N959AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016080105677Access Panel · corrodedCORROSION ON COUNTERSINKS AT FUEL TANK ACCESS 620DT, SM. CORROSION WAS REMOVED, REWORKED AREAS WERE MEASURED. IT IS OUT OF LIMITS IAW SRM 51-10-01. FUEL ACCESS WAS REPLACED AND PN VERIFIED IAW AIPC 57-22-01 AND MUST BE INSTALLED WITH CARD 2040-0012, ZONE 62Jul 31, 2016 · N959AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016080105676Access Panel · corrodedCORROSION ON COUNTESINKS AT FUEL TANK ACCESS NR 620 GB, SM, CARD 66, ZONE 000, CORROSION WAS REMOVED, REWORKED AREAS WERE MEASURED, IT IS OUT OF LIMITS IAW SRM 51-10-01. FUEL ACCESS WAS REPLACED AND PN VERIFIED IAW AIPC 57-23-01-01 AND MUST BE INSTALLED WITHJul 31, 2016 · N959AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016080105675Access Panel · corrodedINITIAL CORROSION ON COUNTERSINK AT FUEL TANK ACCESS NR 520, SM, CARD 69, ZONE 000. CORROSION WAS REMOVED, REWORKED AREAS WERE MEASURED. IT IS OUT OF LIMITS IAW SRM 51-10-01. FUEL ACCESS WAS REPLACED AND PN VERIFIED IAW AIPC 57-22-01-01 AND MUST BE INSTALLEDJul 31, 2016 · N959AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2016080105673Floor Support · corrodedCORROSION ON RT FLOOR SUPPORT BETWEEN STA 1053-STA 1056 X=-55, W2, SM. CARD 87, ZONE 200. DUE TO EXCESSIVE CORROSION FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-02 AND 51-41-05, ORIGINAL THICKNESS 0.080", REMAINING THICKNESS 0.053", THEREFORE IS OUT LIMITS IAW SJul 31, 2016 · N959AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016073005682Starter · smokeFLIGHT EXPERIENCED SMOKE COMING FROM THE APU COMPARTMENT AFTER ARRIVAL. THE PASSENGERS DEPLANED NORMALLY THROUGH THE L1 DOOR. MAINTENANCE FOUND THE APU STARTER SMOKING AND GLOWING. MAINTENANCE USED THE GROUND BASED FIRE EXTINGUISHER TO SECURE APU COMPARTMENT.Jul 30, 2016 · N983AT · Boeing 717200 · APU Start/Ignition SystemSDR DALA2016073105672Web · corrodedCORROSION UNDER FLOOR SUPPORT BETWEEN STA 190/205 AREA NEXT TO CUSP ANGLE. IN REF CARD 65, ZONE 200, CARD 95, ZONE 200. DUE TO EXCESSIVE CORROSION WEB WAS REPAIRED IAW SRM 51-70-10, FIG 201.Jul 30, 2016 · N959AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016073105669Floor Panel · delaminatedDELAMINATION ON FLOOR PANEL RT AFT LAVATORY. SM, CARD 30, ZONE 000. FLOOR PANEL RT AFT LAVATORY WAS REPAIRED IAW SRM 51-70-09, REPAIR 3, PARA 6.Jul 30, 2016 · N959AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016073105668Floor Panel · damagedDAMAGE FLOOR PANEL AT LT AFT LAVATORY, N/P 9981474-71, SH-CP-SM, CARD 51, ZONE 000. FLOOR PANEL AT LT AFT LAVATORY WAS REPAIRED IAW SRM 51-70-09 REPAIR 3, PARAGRAPH 6.Jul 30, 2016 · N959AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2016073105683Connector · failedTHE PILOT REPORTED THAT THE EEPL EXIT SIGN AT THE AFT DOOR AND AT THE OVERWING EXITS IN THE CABIN WERE FLASHING ON & OFF AND WOULD NOT RESPOND TO COMMANDS DURING FLIGHT. MAINTENANCE FOUND A FAILED CONNECTOR IN THE WIRE HARNESS FOR THE OVERWING LIGHTS AND REPLJul 29, 2016 · N989DN · Boeing 717200 · Light System WiringSDR DALA2016073105681Power Supply · unknownTHE PILOT REPORTED THAT THE EEPL EXIT SIGN AT THE AFT DOOR AND AT THE OVERWING EXITS IN THE CABIN WERE FLASHING ON & OFF AND WOULD NOT RESPOND TO COMMANDS DURING FLIGHT. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY AT P1-119 AND THE FUNCTIONAL CHECK OF TJul 29, 2016 · N989DN · Boeing 717200 · Emergency LightingSDR DALA2016073005667Splice · corrodedCORROSION ON RT CUSP LOWER ANGLE SPLICE X=60 BETWEEN STA Y=579 AND Y=598 AT PASSENGER CABIN, SM, CPAX CARD 55, ZONE 200. LOWER ANGLE SPLICE WAS REPLACED IAW SRM 53-20-51, FIG 1 AND 51-41-05.Jul 29, 2016 · N959AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2016080505782Pan · crackedCRACKED INTERIOR STRUCTURE OF THE FWD CARGO DOOR, LWR FWD AREA. REPAIRED THE DOOR PAN IAW CMM 52-30-01 PG D601.1.Jul 28, 2016 · N906AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2016073105671Former · crackedLEFT CANTED KEEL FORMERS CRACKED AT STA 674 AND STA 714 ON OTBD END. REPAIR IAW ER/A 545683-14MA, REF ORNRC 69946-0100-0127. REPAIRED LT CANTED KEEL FORMERS AT STA 674, 696, & 714 ON OTBD END IAW ER/A 545683-14MA, TAG 6782.Jul 28, 2016 · N910AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2016072805625Control Unit · faultyFLIGHT CREW DIVERTED THE AIRCRAFT AFTER THE NR 1 ENGINE FIRE INDICATION ILLUMINATED, ACCOMPANIED WITH AURAL WARNINGS. THE QRH PROCEDURE WAS COMPLIED WITH AND THE NR 1 ENGINE WAS SHUTDOWN. MAINTENANCE FOUND NO EVIDENCE OF ANY ACTUAL FIRE AND REPLACED THE NR 1Jul 28, 2016 · N936AT · Boeing 717200 · Fire DetectionSDR HALA2016072800267Slat System · malfunctionedSPLIT SLAT CONDITION WITH ROLLING MOTION WHEN SLATS RETRACTED DURING CLIMBOUT. SLATS NORMAL WHEN EXTENDED. TROUBLESHOT IAW FIM 27-80 TASK 802. VISUAL INSPECTION OF SLAT CABLES AND CABLE DRUM PERFORMED, NO DEFECTS NOTED. PERFORMED FUNCTIONAL TEST OF LIFT AUGMJul 28, 2016 · N487HA · Boeing 717200 · Leading Edge Slat Control SystemSDR DALA2016073105670Longeron · corrodedCORROSION ON LONGERON 23R FROM STA 1002 TO STA 1037. MARKED CHECK LIMITS, REPLACE AS REQUIRED, REF ORNRC 69946-0100-0060. REPLACED LONGERON 23R AT FS 1002 TO FS1043 IAW SRM 51-41-02, PARA D, NOTE 3, 51-41-05, PG 17, NR 8.Jul 27, 2016 · N910AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
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