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 DALA2018022501158Former · crackedCRACKED FORMER LT/RT SIDE STA Y=694 AT CANTED KEEL INTERNAL STRUCTURE. FORMER LT/RT SIDE STA Y=694 AT CANTED KEEL INTERNAL STRUCTURE WAS REPAIRED PER SRM 51-70-11 REPAIR 1.Feb 24, 2018 · N938AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018022501157Former · crackedCRACKED FORMER LT/RT SIDE STA Y=679 AT CANTED KEEL INTERNAL STRUCTURE. FORMER LT/RT SIDE STA Y=679 AT CANTED KEEL INTERNAL STRUCTURE WAS REPAIRED PER SRM 51-70-11 REPAIR 1.Feb 24, 2018 · N938AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018022501156Retainer · wornWEAR ON LOWER RETAINER (FWD AND AFT SECTION) AT FWD CARGO DOOR BARRIER. LOWER RETAINER FWD AND AFT SECTION WAS REPAIRED PER ER/A NR 559579-14MA REV ORIGINAL.Feb 24, 2018 · N938AT · Boeing 717200 · Cargo CompartmentsSDR DALA2018022501155Former · crackedCRACKED FORMER RT SIDE STA Y=715 AT CANTED KEEL INTERNAL STRUCTURE. FORMER RT SIDE STA Y=715 AT CANTED KEEL INTERNAL STRUCTURE WAS REPAIRED PER SRM 51-70-11 REPAIR 1.Feb 24, 2018 · N938AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018022301098Actuator · out of rigLT GEAR UNSAFE LIGHT ILLUMINATED WITH THE LANDING GEAR RETRACTED. WHEN THE CREW LOWERED THE GEAR RECEIVED 3 DOWN AND LOCKED GREEN INDICATIONS. AN EMERGENCY WAS DECLARED FOR THE RETURN TO DEPARTURE. MAINTENANCE RIGGED BOTH OF THE MLG DOOR ACTUATORS, BOTH OF Feb 23, 2018 · N945AT · Boeing 717200 · Landing Gear ActuatorSDR DALA2018022401154Cusp Web · corrodedCORROSION ON CUSP WEB FROM STA Y=515-519 BTW X=-54 TO X=-60 AT PAX CABIN IN REF NRC 00325 (5300-2020). CORROSION LEVEL 2, CUSP WEB FROM STA Y=515-519 BTW X=-54 TO X=-60 AT PAX CABIN WAS REPAIRED PER SRM 53-00-55-2R.Feb 23, 2018 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018022401153Cusp Web · corrodedCORROSION ON CUSP WEB FROM STA Y=449-457 BTW X=-54 TO X=-60 AT PAX CABIN IN REF NRC 00324 (5300-2020). CORROSION LEVEL 2, CUSP WEB FROM STA Y=449-457 BTW X=-54 TO X=-60 AT PAX CABIN WAS REPAIRED PER SRM 53-00-55-2R.Feb 23, 2018 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018022401152Cusp Web · corrodedCORROSION ON CUSP WEB FROM STA Y=467-475 BTW X=-54 TO X=-60 AT PAX CABIN IN REF NRC 00324 (5300-2020). CORROSION LEVEL 2, CORROSION ON CUSP WEB FROM STA Y=467-475 BTW X=-54 TO X=-60 AT PAX CABIN WAS REPAIRED PER SRM 53-00-55-2R.Feb 23, 2018 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018022401151Access Panel · corrodedCORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS PLATES 520EB. CORROSION LEVEL 2, DUE TO EXCESSIVE DAMAGE BY CORROSION ON COUNTERSINK AREAS, ACCESS PLATE 520EB WAS REPAIRED PER SRM 57-10-01 REPAIR 2 PAR 5 CONDITION II.Feb 23, 2018 · N938AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018022401150Access Panel · corrodedCORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS PLATES 520DB. CORROSION LEVEL 2, FUEL ACCESS PLATE 520DB WAS REPLACED FOR NEW ACCESS PLATE PER SRM 57-10-01 REPAIR 2 PAR 5.Feb 23, 2018 · N938AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018022401149Access Panel · corrodedCORROSION ON COUNTERSINK HOLES AND SETTLEMENT AREA AT FUEL ACCESS PLATES 620AT. CORROSION LEVEL 2, FUEL ACCESS PLATE 620AT WAS REPLACED FOR NEW ACCESS PLATE PER SRM 57-10-01 REPAIR 2 PAR 5.Feb 23, 2018 · N938AT · Boeing 717200 · Wing, Plate/SkinSDR DALA2018022201830Skin · crackedCRACK WAS FOUND OF 0.250" ON R1 FWD SERVICE DOOR, BOTTOM AREA, OUTER SKIN. PERMANENT REPAIR. CRACK ON R1 FWD SERVICE DOOR BOTTOM AREA WAS REPAIRED PER SRM 51-70-01-2R. HFEC INSPECTION WAS ACCOMPLISHED ON R1 FWD SERVICE DOOR BOTTOM AREA, OUTER SKIN AFTER TRIM OFeb 22, 2018 · N988DN · Boeing 717200 · Service DoorsSDR DALA2018022301148Diaphragm · corrodedCORROSION ON DIAPHRAGM BTW STA Y=200-205 AND BTW X=-40 TO X=-50 AT PAX CABIN IN REF NRTC 00316 (5300-2010). CORROSION LEVEL 2, DIAPHRAGM BTW STA Y=200-205 AND BTW X=-40 TO X=-50 AT PAX CABIN WAS REPAIRED PER SRM 53-00-00-2R FIG 201.Feb 22, 2018 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018022301097Longeron · crackedCRACK LONGERON 6R, BS 1022. THE LONGERON WAS REPAIRED IAW SRM 53-00-05-2R.Feb 22, 2018 · N938AT · Boeing 717200 · Fuselage Main, Longeron/StringerSDR DALA2018022301096Pan · crackedCRACK RING PAN ON LWR CORNER BS 889. THE RING PAN WAS REPAIRED IAW SRM 56-20-02-2R, FIG 202.Feb 22, 2018 · N938AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018022301095Spar Cap · crackedCRACK INDICATION BELOW THE LEADING EDGE SKIN SPLICE AT ZFS=51.67, ZFS=50.17, ZFS=49.17, AND ZFS=48.17 ON THE LT VERTICAL STABILIZER FRONT SPAR CAP FORWARD FLANGE. REPAIRED IAW ETI-17-18-010, REV 1, DWG SG95550005 CONFIGURATION -7005 AND ER/A 566080-14AD REVFeb 22, 2018 · N998AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2018022301094Floorbeam · corrodedCORROSION ON FLOORBEAM BS 198 BTW X=16 TO X=44 . REPLACED PER B717 SRM 51-41-02-0G.Feb 22, 2018 · N938AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2018022301093Cusp Web · corrodedCORRODED CUSP WEB RBL 43 AND 54, BS 160 - 200. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-00-2R-2.Feb 22, 2018 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018022301092Floorbeam · corrodedCORROSION ON FLOORBEAM BS 200. LBL 14 TO 9. REPLACED IAW SRM 51-41-02-0G.Feb 22, 2018 · N938AT · Boeing 717200 · Fuselage Main, Floor BeamSDR DALA2018022301091Access Panel · damagedELONGATED HOLES ON FUEL ACCESS PANEL 520DT ON THE LT WING. THE ACCESS PANEL WAS REPAIRED IAW SRM 57-10-01-2R-2, PAR 5, CONDITION II.Feb 22, 2018 · N988DN · Boeing 717200 · Wing, Plate/SkinSDR DALA2018022301090Skin · crackedCRACK INDICATION BELOW THE LEADING EDGE SKIN SPLICE AT ZFS=51.67, ZFS=50.17, ZFS=49.17 AND ZFS=48.17 OF THE LT VERTICAL STAB FRONT SPAR CAP FORWARD FLANGE. REPAIRED IAW ETI-17-18-010, REV 1, DWG SG95550005 AND ER/A 566080-14AD, REV. ORIG.Feb 22, 2018 · N998AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2018022301089Door Frame · corrodedCORROSION WAS FOUND ON THE DOOR FRAME WEB BS 200 - 202, LONGERON 18L. REPAIRED IAW SRM 53-00-00, REP 2.Feb 22, 2018 · N938AT · Boeing 717200 · Fuselage Main, StructureSDR DALA2018022201088Skin · damagedVERTICAL STAB RIGHT SIDE AT ZFS 52.267, UPPER L/E SEGMENT LOWER ROW OF FASTENER HOLES FROM L/E AFT HAVE DEFORMED HOLES. REPAIRED IAW ER/A 565657-14AD, REV O.Feb 21, 2018 · N945AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2018022201087Skin · damagedVERTICAL STAB L/E LOWER ROW OF FASTENERS, RIGHT SIDE HAVE ELONGATED HOLES AND COUNTERSINKS, AT ZFS 52.267. REPAIRED IAW ERA 565657-14AD, REV O.Feb 21, 2018 · N945AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2018022201086Skin · damagedRIGHT SIDE OF VERTICAL STAB AT XFS 52.267, RIGHT LOWER SEGMENT LOWER ROW OF FASTENERS, ELONGATED COUNTERSINKS. REPAIRED IAW ER/A 565657-14AD, REV O.Feb 21, 2018 · N945AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2018022201085Skin · damagedRIGHT SIDE OF THE VERTICAL STAB, UPPER SEGMENT, UPPER ROW OF FASTENERS, COUNTERSINKS ELONGATED. REPAIRED IAW ERA 565657-14AD, REV O.Feb 21, 2018 · N945AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2018022201084Skin · damagedL/E OF VERTICAL STAB, RIGHT SIDE LOWER SEGMENT, UPPER ROW OF FASTENERS COUNTERSINKS ELONGATED. REPAIR IAW ER/A 565657-14AD, REV O.Feb 21, 2018 · N945AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2018022201067Power Supply · inoperativeLEFT HAND AFT EMERGENCY EXIT OVERWING IDENTIFIER IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY POWER SUPPLY IAW AMM 35-51. OPERATIONAL CHECKS NORMAL. OK FOR SERVICE.Feb 21, 2018 · N948AT · Boeing 717200 · Emergency LightingSDR DALA2018022201066Strap · corrodedCORROSION ON STRAP FRONT OF DOOR JAMB WEB STA Y=200 X=54 (5310-2005). LEVEL CORROSION 2, STRAP WAS REPLACED PER DWG 9910078 REV JC.Feb 21, 2018 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018022201065Skin Panel · crackedCRACK INDICATIONS IN L/E SKIN PANEL ATTACH HOLES BELOW SPLICE ZFS 52.267, RIGHT HAND SIDE. HOLE 6 TOP TO BOTTOM, MARKED. 5530-01048-01/010 00252: PRI 565466-14AD REV O-4 MATCHES ER/A 565466-14AD REV O STEPS 1-12. COMPLY WITH STEP 13 OF ER/A 565466-14AD REV O OFeb 21, 2018 · N945AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2018022201064Skin · damagedLEFT HAND VERTICAL STAB L/E AT ZFS 52.267: LOWER 2EA ROWS FASTENERS HAVE ELONGATED HOLES AND COUNTERSINKS. REF: AA5530-01048 AND AD 2016-09-05. NRC 018-0001:5530-01048-01/001 00200: REPAIR COMPLIED WITH ON ER/A 565657-14AD REV O. ATTACHED TO NRC 254.Feb 21, 2018 · N945AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2018022201063Spar Cap · crackedVERTICAL FWD LT SPAR CAP IS CRACKED AT APPROX AT ZFS 52.267 NRC 018-0001:5530-01048-01/011 00254: PRI 565362-14AD REV O-5 MATCHES ER/A 565362-14AD REV O STEPS 1-22 AND 24 COMPLIED WITH STEP 23 OF ER/A 565362-14AD REV O ON THIS NRC. PRI 565657-14AD REV O-4 MATCFeb 21, 2018 · N945AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2018022201061Skin · corrodedCORROSION TYPE EXFOLIATION AT CENTER WING TANK UPPER SKIN AT LT MLG WHEEL WELL AREA BELOW SLANT PRESSURE PANELS. THIS NRC WAS ATTENDED WITH ETI-17-18-009 REV 5 AND ER/A 565972-14 REV ORIG. ASSOCIATED ER/A 00-565972.Feb 21, 2018 · N998AT · Boeing 717200 · Fuel StorageSDR DALA2018022101060Floor Support · corrodedCORROSION ON FLOOR SUPPORT BTW STA Y=200-218 IN X=56 AT PAX CABIN (W1) (AMDS 5300-2010). CORROSION LEVEL 2, FLOOR SUPPORT BTW STA Y=200-218 IN X=56 WAS FABRICATED PER DWG 9936535 REV CS, AND IT WAS INSTALLED PER SRM 51-41-05 AND 51-41-08-OG.Feb 21, 2018 · N938AT · Boeing 717200 · Fuselage Miscellaneous StructureSDR DALA2018022101059Skin · crackedCRACK IN VERTICAL STAB SKIN LT SIDE AFT OF SPAR CAP. NRC 018-0001:5530-01048-01/007 00234: CRACK TO BE COMPLIED WITH ON NRC 254 AND ER/A 565362-14AD REV O.Feb 20, 2018 · N945AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2018022101058Skin Panel · crackedCRACK INDICATIONS IN L/E SKIN PANEL ATTACH HOLES BELOW SPLICE ZFS 52.267, LEFT HAND SIDE. HOLE 1, 2, 6, 7, 8, AND 9, TOP TO BOTTOM. NRC 018-0001:5530-01048-01/009 00251: CRACK TO BE COMPLIED WITH ON NRC 254 AND ER/A 565362-14AD REV O.Feb 20, 2018 · N945AT · Boeing 717200 · Vertical Stabilizer, Plate/SkinSDR DALA2018022101057Spar Cap · crackedINTERNAL WEB AT VERTICAL FWD LT SPAR CAP IS CRACKED AT APPROX. AT ZFS 52.267. NRC 018-0001:5530-01048-01/012 00255: CRACK TO BE COMPLIED WITH ON NRC 254 AND ER/A 565362-14AD REV O.Feb 20, 2018 · N945AT · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2018022001002Spar Cap · damagedVERTICAL STABILIZER LEFT FRONT SPAR CAP DAMAGED, BELOW ZFS 52.267. REPAIRED THE SPAR CAP IAW ERA 565658-14AD, REV ORIGINAL.Feb 19, 2018 · N989DN · Boeing 717200 · Vertical Stabilizer, Spar/RibSDR DALA2018021901529Lens · damagedEMERGENCY LIGHT LENS DAMAGED. REPLACED THE DAMAGED LENS.Feb 18, 2018 · N894AT · Boeing 717200 · Emergency LightingSDR HALA2018022000046Compressor · stalledENG L COMP STALL, BTB. BORESCOPED NR 1 ENG LPC MM 72-31-00-200-802, MM HPC 72-33-00-200-801, MM HPT 72-50-00-200-802 AND LPT MM 72-50-00-200-801 FOUND NO DEFECTS NOTED. ACCOMPLISHED TEST 4- ENGINE POWER ASSURANCE CHECK ON NR 1 ENGINE PER AMM 71-00-13-710-802. Feb 18, 2018 · N490HA · Boeing 717200 · Turbine Engine Compressor SectionSDR HALA2018022000045Reservoir · contaminatedON TAXI OUT, "HYD R TEMP HI" MASTER CAUTION. BLEED RIGHT HYD RES. CYCLED ALL KNURLED KNOBS. RAN PUMPS MESSAGE DID NOT RETURN.Feb 17, 2018 · N486HA · Boeing 717200 · Hydraulic Reservoir, MainSDR DALA2018021900985Power Supply · inoperativeEMERGENCY LIGHTS AT THE MAIN CABIN AND SERVICE DOORS ARE INOPERATIVE. MAINTENANCE TROUBLESHOT IAW WDM 33-51 AND REPLACED THE BATTERY PACK AND POWER SUPPLY IAW AMM 33-51. OPS CHECKED GOOD.Feb 17, 2018 · N989AT · Boeing 717200 · Emergency LightingSDR DALA2018021800983Skin · crackedCRACK ON THE FUSELAGE SKIN, BS 1037, LONGERONS 13R AND 14R. THE SKIN WAS REPAIRED IAW ETI-17-18-003, REV 4, AND ER/A 565867-14, REV ORIGINAL.Feb 17, 2018 · N998AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018021800982Fitting · crackedCRACK ON FUSELAGE FITTING LONGERON 22R, BS 661. THE FITTING WAS REPAIRED ETI-17-18-004, REV 1, AND ER/A 565939-14, REV ORIGINAL.Feb 17, 2018 · N998AT · Boeing 717200 · Fuselage Main, Attach FittingsSDR DALA2018021800981Skin · crackedCRACK ON THE SKIN AT BS 1076 BETWEEN LONGERONS 13L AND 14L. THE SKIN WAS REPAIRED IAW ETI-17-18-002, REV 2 AND ER/A 565871-14, REV ORIGINAL. HFEC INSPECTION WAS PERFORMED THE CRACK WAS FOUND OF 0.110" OF LENGTH IAW NDT SPM 06-10-01.001.Feb 17, 2018 · N998AT · Boeing 717200 · Fuselage Main, Plate/SkinSDR DALA2018021901003Light · missingDURING A SERVICE CHECK, FOUND THE EMERGENCY LIGHT AT SEAT 19AB MISSING. INSTALLED A NEW LIGHT SECTION. CHECKED OK.Feb 16, 2018 · N961AT · Boeing 717200 · Emergency LightingSDR DALA2018021700980Frame · crackedCRACK OF 0.250 INCH IN LENGTH APROXIMATELY ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAME AT BS 696 RT. THE FRAME WAS REPLACED IAW 5310-01436-03B.Feb 16, 2018 · N998AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018021600941Frame · corrodedCORRODED FRAME BS 1037, BETWEEN LONGERONS 28L AND 28R IN THE AFT CARGO COMPARTMENT. THE FRAME WAS REPAIRED IAW SRM 53-20-07-2R, FIG 201.Feb 15, 2018 · N998AT · Boeing 717200 · Fuselage Main, FrameSDR DALA2018021600940Door · corrodedCORROSION ON LOWER INNER EDGE OF THE FWD AIR STAIRWELL DOOR. THE STAIRWELL DOOR WAS REPLACED IAW AMM 52-63-01.Feb 15, 2018 · N998AT · Boeing 717200 · DoorsSDR DALA2018021500906Lamp · inoperativeDURING A SERVICE CHECK, FOUND THE TAIL CONE EMERGENCY LIGHT INOPERATIVE. TROUBLESHOT THE EMERGENCY LIGHT IAW AMM 33-51. CLEANED AND REPLACED THE LAMPS. OPS CHECKED GOOD.Feb 15, 2018 · N892AT · Boeing 717200 · Emergency Lighting
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