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 DALA2017062604994Cusp Web · corrodedCORROSION ON CUSP WEB UPPER & LOWER SURFACES BETWEEN RBL 54 TO 60, BS 622 TO 624 AND BS 629 TO 630. THE DAMAGE WAS REMOVED IAW SRM 53-00-55-2R, FIG 216. HFEC INSPECTION WAS ACCOMPLISHED AND NO CRACKS WERE FOUND AFTER THE DAMAGED WAS REMOVED IAW NDT SPM 06-10Jun 25, 2017 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017062604954Channel · crackedCRACKS ON CHANNEL OF PAX CABIN FLOOR PANEL 222ADF. THE CHANNEL WAS REPLACED IAW SRM 51-41-01-0G.Jun 25, 2017 · N980AT · Boeing 717200 · Fuselage Floor PanelSDR DALA2017062604953Spar Cap · crackedVERTICAL STABILIZER FRONT SPAR CAP LT SIDE, FORWARD FLANGE HAS CRACK INDICATION AT SEVENTH HOLE BELOW ZFS=52.267. COMPLIED WITH PRI 559725-14 REV 0 AND REV 1. REPAIRED IAW ER/A 559725-14 REV ORIG.Jun 25, 2017 · N948AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2017062604952Skin · crackedVERTICAL STABILIZER RT SIDE, HAS CRACK INDICATION AT SEVENTH HOLE BELOW ZFS=52.267 IN SKIN. REPAIRED IAW PRI 559738-14 REV. 0 AND 1 AND COMPLIED WITH ER/A 559738-14 REVISION ORIGINAL.Jun 25, 2017 · N948AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2017062604951Spar Cap · crackedVERTICAL STABILIZER FRONT SPAR CAP LT SIDE, FORWARD FLANGE HAS CRACK INDICATION AT THIRD HOLE BELOW ZFS=52.267. COMPLIED WITH PRI 559725-14 REV 0 AND REV 1. REPAIRED IAW ER/A 559725-14 REV ORIG.Jun 25, 2017 · N948AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2017062604950Spar Cap · crackedVERTICAL STABILIZER FRONT SPAR CAP RT SIDE, FORWARD FLANGE HAS CRACK INDICATION AT FOURTH HOLE BELOW ZFS=52.267. REPAIRED IAW PRI 559738-14 REV. 0 AND 1 AND COMPLIED WITH ER/A 559738-14 REVISION ORIGINAL.Jun 25, 2017 · N948AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2017062604949Spar Cap · crackedVERTICAL STABILIZER FRONT SPAR CAP LT SIDE, FORWARD FLANGE HAS CRACK INDICATION AT SECOND HOLE BELOW ZFS=52.267. COMPLIED WITH PRI 559725-14 REV 0 AND REV 1. REPAIRED IAW ER/A 559725-14 REV ORIG.Jun 25, 2017 · N948AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2017062604948Spar Cap · crackedVERTICAL STABILIZER FRONT SPAR CAP RT SIDE, FORWARD FLANGE HAS CRACK INDICATION AT SECOND HOLE BELOW ZFS=52.267. REPAIRED IAW PRI 559738-14 REV. 0 AND 1 AND COMPLIED WITH ER/A 559738-14 REVISION ORIGINAL.Jun 25, 2017 · N948AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2017062604947Spar Cap · crackedVERTICAL STABILIZER FRONT SPAR CAP LT SIDE, FORWARD FLANGE HAS A CRACK INDICATION AT FIRST HOLE BELOW ZFS=52.267. COMPLIED WITH PRI 559725-14 REV 0 AND REV 1. REPAIRED IAW ER/A 559725-14, REV ORIG.Jun 25, 2017 · N948AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2017062504946Tee Fitting · crackedCRACKED TEE FITTING ON THE AFT LOWER STOP OF THE FWD CARGO DOOR. THE FITTING WAS REPLACED IAW SRM 51-41-01-0G, 51-41-02-0G, 51-41-05-0G, AND DRAWING 3926046, REV. B.Jun 24, 2017 · N980AT · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2017062504945Membrane · corrodedCORROSION ON MEMBRANE BS 200 BETWEEN LONGERONS 17 &18L. THE MEMBRANE WAS REPAIRED IAW SRM 51-70-10-2R, FIG 201.Jun 24, 2017 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017062404944Cusp Web · corrodedCORROSION ON CUSP WEB BETWEEN RBL 54 TO 60 OUT OF LIMITS AT BS 655 - 663. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R.Jun 23, 2017 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017062404943Cusp Web · corrodedCORROSION ON LT CUSP WEB BETWEEN BS 602 - 603, LBL 54 TO 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG. 216.Jun 23, 2017 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017062404942Cusp Web · corrodedCORROSION ON CUSP WEB RBL 54 TO 60, BS 487 TO 490. THE DAMAGE WAS REMOVED IAW SRM 53-00-55 2R, REPAIR 4, FIG 215. HFEC INSPECTION WAS ACCOMPLISHED AFTER DAMAGE REMOVED AND NO CRACK INDICATIONS WERE FOUND IAW NDT SPM 06-10-01.001. THE REPAIR WAS FABRICATED IAJun 23, 2017 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017062404941Beam · crackedCRACK ON BELOW DOOR STOP PAN AFT EDGE BEAM 3 OF FWD CARGO DOORWAY. REPAIRED IAW SRM 52-30-02, REPAIR 3.Jun 23, 2017 · N980AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2017062304896Battery · dischargedEMERGENCY CEILING LIGHTS FROM ROWS 15 THRU 19 AND EMERGENCY CEILING EXIT SIGN INOP. MAINTENANCE REPLACED EMERGENCY LIGHTS BATTERY POWER SUPPLY B5-120 PER AMM 33-51-03, OPS CK GOOD.Jun 23, 2017 · N946AT · Boeing 717200 · Emergency LightingSDR DALA2017062304940Floor Support · corrodedCORROSION ON FLOOR SUPPORT BS 157 TO 190, LBL 58. THE FLOOR SUPPORT WAS REPLACED IAW DWG 9910078, REV JC, SRM 51-41-02 AND 51-41-05.Jun 22, 2017 · N717JL · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017062304895Seat Track · corrodedCORROSION ON SEAT TRACK X=-44.5 STA Y=429-430 AT CAB PAX. SEAT TRACK X=-44.5 STA Y=429-430 AT CAB PAX WAS REPAIR PER SRM 53-20-52-2R REPAIR 1.Jun 22, 2017 · N980AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017062304894Retaining Clip · wornWORN ON LOWER LT DOUBLER RETAINER CLIP AT AFT CABIN BULKHEAD DOOR (DOORS). LT LOWER DOUBLER RETAINER CLIP WAS REPLACED PER SRM 51-41-01 AND 51-41-02.Jun 22, 2017 · N980AT · Boeing 717200 · Passenger/Crew DoorsSDR DALA2017062304893Cusp Web · corrodedCORROSION ON CUSP WEB BTW STA Y=544 TO Y=555 X54 TO X60 AT PAX CABIN IN REF NRC 195. DAMAGE WAS REMOVED PER SRM 53-00-55-2R-4 FIG 216 HFEC INSPECTION WAS ACCOMPLISHED ON CUSP WEB BTW STA Y=544 TO Y=555 X54 TO X60 AT PAX CABIN NO CRACKS WERE FOUND AFTER DAMAGE Jun 22, 2017 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017062304892Frame · crackedCRACKED RT OVERWING FRAME STA Y=674 PROJECTION LONG 18R CPAX. RT OVERWING FRAME STA Y=674 WAS REPLACED WITH TASK CARD NUMBER:107-0002:5310-01436-03B.Jun 22, 2017 · N717JL · Boeing 717200 · Fuselage Main, FrameSDR DALA2017062304891Floor Support · corrodedCORROSION ON FLOOR SUPPORT BTW STA Y=148 TO Y=168 AND X=-6 AT COCKPIT. FLOOR SUPPORT BTW STA Y=148 TO Y=168 AND X=-6 AT COCKPIT WAS REPLACED PER SRM 51-40-08-0G AND 51-41-01.Jun 22, 2017 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017062304890Cusp Web · corrodedCORROSION ON LT CUSP WEB STA Y-855 BTW X54 TO X60 AT PAX CABIN IN REF NRC 198. REPAIR PART WAS FABRICATED AND INSTALLED PER SRM 53-00-55-2R FIG 215 AND 51-41-02. CIC WAS APPLIED PER SRM 51-10-04 PAR 37.Jun 22, 2017 · N980AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017062304889Door Frame · corrodedCORROSION ON LWR DOOR JAMB BTW STA Y=954 TO Y=994 ON AFT CARGO COMPARTMENT IN REF AMDS 5300-2007)(SM)(C2). PERMANENT REPAIR ON LOWER DOOR JAMB WAS ACCOMPLISHED PER SRM 53-20-15-2R, 51-10-04 PAR 15, 21, 37, AND 51-41-01, 51-41-02, 51-41-05.Jun 22, 2017 · N717JL · Boeing 717200 · Fuselage Main, StructureSDR DALA2017062204887Sign · missingEXIT SIGN MISSING IN MID-CABIN. INSTALLED EXIT SIGN LENS. OK FOR SERVICE.Jun 21, 2017 · N940AT · Boeing 717200 · Emergency LightingSDR DALA2017062204886Cargo Track · crackedCRACKED CARGO TRACK AT BS 937 IN THE AFT CARGO BAY. THE CARGO TRACK WAS REPLACED IAW SRM 53-20-51-0I. FIG.1, 51-41-01, 51-41-02 ,51-41-05, AND 51-10-04, PAR 15, AND 21.Jun 21, 2017 · N717JL · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017062204885Floorbeam · corrodedCORROSION ON FLOOR BEAM BS 200 BETWEEN RBL 54 TO 44 IN THE PAX CABIN. THE FLOORBEAM WAS REPLACED SRM 51-41-02, 51-10-4, PAR 26, AND 51-40-08.Jun 21, 2017 · N980AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2017062204884Floor Panel · delaminatedDELAMINATED FLOOR PANEL. THE FLOOR PANEL WAS REPAIRD IAW SRM 53-20-50, REP 3.Jun 21, 2017 · N717JL · Boeing 717200 · Fuselage Floor PanelSDR DALA2017062004838Pan · crackedCRACKED RING PAN ON STA Y=832 AND Y=870 AFT UPPER CORNER ALSO ON STA Y=579 LOWER FWD CORNER AT PAX CABIN LT SIDE. RING PAN WERE REPAIRED PER SRM 56-20-02-2R FIG 202 TYPE B.Jun 19, 2017 · N980AT · Boeing 717200 · Passenger Compartment WindowsSDR DALA2017062004835Pan · crackedCRACKED RING PAN ON STA Y=908 AFT LOWER CORNER AT PAX CABIN RT SIDE. RING PAN WERE REPAIRED PER SRM 56-20-02-2R FIG 202 TYPE B.Jun 19, 2017 · N980AT · Boeing 717200 · Passenger Compartment WindowsSDR DALA2017062004834Beam · crackedCRACK ON RIGHT DOOR JAMB BEAM STA Y=46 APPROX AT NOSE GEAR WHEEL WELL. CRACK ON RIGHT DOOR JAMB BEAM STA Y=46 WAS REPAIRED PER SRM 53-10-14-2R-2.Jun 19, 2017 · N717JL · Boeing 717200 · Fuselage Main, StructureSDR DALA2017061904804Intercostal · crackedCRACK ON INTERCOSTAL BS 636 Z=-3 X=0 FWD CARGO COMPARMENT. THE INTERCOSTAL WAS REPAIRED IAW SRM 53-00-00-2R, FIG 201.Jun 18, 2017 · N717JL · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017061904803Floorbeam · corrodedCORROSION ON FLOORBEAM BS 200 LBL 6 TO RBL 6. THE FLOORBEAM WAS REPLACED IAW SRM 51-41-02.Jun 18, 2017 · N980AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2017061704779Pan · crackedCRACKED INNER PAN ON FWD EDGE AND BEAM NR 1 BS 370 AT FWD CARGO DOOR. REPAIRED IAW SRM 52-30-02 -2R, PROCEDURE 1, REPAIR 1, TABLE 201.Jun 16, 2017 · N717JL · Boeing 717200 · Cargo/Baggage DoorsSDR HALA2017061600158Compressor · failedRIGHT ENG COMPRESSOR STALLED IN CRUISE AT 18000FT, ROLLED BACK TO ZERO THRUST, COMPLIED WITH QRH, THE ENGINE WAS SHUTDOWN FOLLOWED BY A RT ENGINE SYS FAIL.. BORESCOPE FOUND COMPRESSOR DAMAGE. ENGINE CHANGED.Jun 15, 2017 · N495HA · Boeing 717200 · Turbine Engine Compressor SectionSDR DALA2017061604742Longeron · crackedCRACKED LONGERON 2L, BS 1133 IN THE AFT ACCESORY COMPARTMENT. THE LONGERON WAS REPAIRED IAW SRM 53-00-05.Jun 15, 2017 · N717JL · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2017061504723Pan · crackedCRACK ON FWD EDGE OUTER PAN BETWEEN BEAMS 1 AND 2 IN THE AFT CARGO DOOR. FWD EDGE OUTER PAN WAS REPAIRED IAW SRM 52-30-02-2R, PROCEDURE 4, REPAIR 4.Jun 14, 2017 · N717JL · Boeing 717200 · Cargo/Baggage DoorsSDR DALA2017061504722Doubler · crackedCRACK ON PRODUCTION DOUBLER BS 1178 BETWEEN LONGERONS 19R TO 20R. REPAIRED IAW DWG 9911859, REV BU AND SRM 51-20-09.Jun 14, 2017 · N997AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017061504721Frame · crackedCRACKED FRAME BS 1225 BETWEEN 5 - 6 HRS, AND 8 - 9 HRS. FRAME WAS REPLACED IAW SRM 51-41-02.Jun 14, 2017 · N717JL · Boeing 717200 · Fuselage Main, FrameSDR DALA2017061404720Floor Support · corrodedCORROSION ON FLOOR SUPPORT BS 120 TO 148, RBL 54. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-02, 51-10-04 PAR 15 AND 16, AND DRAWING 9936533, REV CM.Jun 13, 2017 · N717JL · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017061404719Cusp Web · crackedCRACK ON RT CUSP WEB BS 600 BETWEEN RBL 54 AND 60. THE CUSP WEB WAS REPAIRED SRM 53-00-55, 51-10-04, 51-41-05, AND 51-41-02.Jun 13, 2017 · N717JL · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2017061404681Doubler · corrodedCORROSION ON PREVIOUS DOUBLER REPAIR LOWER SURFACE RT SIDE STA Y=894 TO Y=903 BTW X=-54 AND X=-60 AT PAX CABIN (CPAX). DAMAGE PRODUCTION DOUBLER LOWER SURFACE RT SIDE STA Y=894 TO Y=903 BTW X=-54 AND X=-60 WAS REPLACED PER SRM 53-20-51 AND 51-41-05.Jun 13, 2017 · N717JL · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2017061404680Seat Track · corrodedCORROSION OUT OF LIMITS ON SEAT TRACK X=-22 RT AT STA Y=427 TO Y=430. SEAT TRACK WAS REPAIRED PER SRM 53-20-52-2R-1, 51-10-04 PAR. 21, 15, 51-41-01.Jun 13, 2017 · N717JL · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017061404679Access Door · corrodedCORROSION ON COUNTERSINK OF FUEL ACCESS DOOR 141AR. ACCESS PLATE 141AR WAS MEASURED COUNTERSINK 0.745" AND HOLE 0.315" THEREFORE OUT OF LIMITS THEREFORE FUEL ACCESS WAS REPLACED PER SRM 57-10-01-2R-2 CONDITION I 1(A) AND PART NUMBER WAS VERIFIED PER IPC 57-22-Jun 13, 2017 · N717JL · Boeing 717200 · Wing, Plate/SkinSDR DALA2017061304678Cusp Web · crackedCRACK ON RT CUSP WEB STA Y=715 BTW X=- 44 AND X=-54 AT PAX CABIN. CUSP WEB WAS REPAIRED PER SRM 53-00-55, 51-10-04, AND 51-41-02.Jun 12, 2017 · N717JL · Boeing 717200 · Fuselage Miscellaneous StructureSDR HALA2017061300153Warning Light · false activationAFTER LANDING, EMERGENCY POWER ACTIVATED FOR ABOUT 10 SECONDS, RETURNED TO NORMAL, THEN FLT REC FAIL AND VIA FAIL LIGHTS ILLUMINATED AND REMAINED ON. RESET BOTH VIA 1 & 2. ACCOMPLISHED RTS TEST BOTH VIA'S. NO DEFECTS NOTED. VIA 1 & 2 TEST PASSED. ACFT OK TO CJun 12, 2017 · N488HA · Boeing 717200 · Central WarningSDR DALA2017061304656Cusp Web · crackedCRACK ON CUSP WEB BS 250 RBL 58. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, FIG 215, SRM 51-41-02, AND SRM 51-10-04 PAR 15, 21, 38.Jun 12, 2017 · N717JL · Boeing 717200 · Fuselage Miscellaneous StructureSDR HALA2017061200150Handset · overheatedF/A HANDSET HOT, BURNING ODOR. REMOVED AND REPLACED THE HANDSET IAW AMM 23-41-07, AND OPS CK OKAY IAW AMM 23-41-07.Jun 11, 2017 · N483HA · Boeing 717200 · Interphone/Passenger Announcement (PA) SystemSDR DALA2017061204632Cargo Track · corrodedCORROSION ON LEFT CARGO TRACK FROM BS 813 TO 1028. THE CARGO TRACK WAS REPLACED IAW SRM 51-41-01 AND 51-41-02.Jun 11, 2017 · N997AT · Boeing 717200 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2017061204634Support · corrodedCORROSION ON PAX CABIN GALLEY SUPPORT AT BS 217, RBL 11. THE SUPPORT WAS REPLACED IAW SRM 51-40-08, 51-41-01, 51-41-02, AND 51-41-05.Jun 10, 2017 · N717JL · Boeing 717200 · Fuselage Miscellaneous Structure
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