Boeing 717-200
Service difficulty reports · 18,756
Newest first. General aviation reporting is voluntary.
Query with SQL
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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DALA2025041602960Pan · crackedCRACK ON INNER PAN FWD EDGE SIDE BTW BEAM #1 TO #2 AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC-00139: INNER PAN FWD EDGE SIDE BTW BEAM #1 TO #2 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ERA 623951-14 REV ORIGINAL. ASSOCIATED ER/A 14-623951 ADDED FOR AC SDR DALA2025041602959Doubler · crackedCRACK FOUND ON INTERNAL DOUBLER AT STA Y=1178 CANT LONGERON 17RH AT AFT ACCESSORIES COMPARTMENT. SUMMARY OF NRC 00686: INTERNAL CAP DOUBLER AT STA Y=1178 CANT LONGERON 17RH AT AFT ACCESSORIES COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1 RESDR DALA2025041502919Door · unsecureSHIP 9570 -ATB/DE- AIRCRAFT HAD AN UNCOMMANDED HEAVY ROLL IN FLIGHT DURING CLIMB AFTER TAKEOFF. THE CREW DECLARED AN EMERGENCY WITH ATC AND RETURNED THE AIRCRAFT BACK TO ATL, LANDING UNEVENTFULLY. CORRECTIVE ACTION: UPON ARRIVAL, MAINTENANCE FOUND THAT THE RIGSDR DALA2025041502917Not Reported · cracked-AD- DUE TO CRACK INDICATION FOUND DURING INSP, COMPLIED WITH AMDS CARD 5720-01103-01B. REQUIRES COMPLETION OF PRI 624259-14. COMPLIED WITH PRI 624259-14AD REV 0, 1, & 2. COMPARED PRI 324259-14AD REV 0, 1, & 2 WITH ERA 624259-14AD REV ORIG AND ALL ITEMS MATCH.SDR DALA2025041502916Spar Cap · cracked-AD- CRACK WAS FOUND IN LOWER SPAR CAP NEAR XRS=164 DURING INSP OF LT WING REAR SPAR INSP AMDS 5720-01103-01A. "CONTACT LIAISON ENGINEERING FOR REPAIR PRIOR TO FURTHER FLIGHT" FC 5720-01103. COMPLIED WITH PRI 624256-14AD REVS 0, 1, 2, 3, 4, & 5. COMPARED PRI 6SDR DALA2025041502918Pseu · failedSHIP 9553 -MISC/DE- THE CREW DECLARED AN EMERGENCY WITH ATC DUE TO THE "PROXIMITY SWITCH ELECTRONIC UNIT FAIL" MESSAGE ILLUMINATING. THE FLIGHT LANDED WITHOUT FURTHER ISSUE. CORRECTIVE ACTION: MAINTENANCE REPLACED THE PSEU AND THE OPERATIONAL CHECK WAS GOOD. (SDR DALA2025041202833Cargo Track · corrodedCORROSION ALONG OF LH TRACK BTW STA=1022-890, STA=898-851 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 0255: CORROSION LEVEL 2. LH TRACK BTW STA=1022-890, STA=898-851 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-40-04-0G, 51-41-01-0G, AND 51-41-05-0G.SDR DALA2025041202832Longeron · crackedCRACK WAS FOUND BTW STA Y=1178 APPROX IN LONG 17R AT AFT FUSELAGE. SUMMARY OF NRC 00660: CRACK BTW STA Y=1178 APPROX IN LONG 17R AT AFT FUSELAGE WAS REPAIRED PER ERA 625404-14 REV ORIGINAL SECTION 1: PERMANENT REPAIR. ASSOCIATED ER/A 14-625404 ADDED FOR AC 956SDR DALA2025041202831Fuel Cap · leaking-AD- WORKING PRI 621176-14AD REV "O" B717-200 LH WING REAR SPAR LOWER CAP FUEL LEAK. SUMMARY SEE NRC 004-0001:5720-01103-01A/004 00004: CMOR - COMPLIED WITH ER/A 621176-14 REV A, PRI REV "0", "1", "2", "3", "4", "5", "6", AND "7" REPAIR INSTRUCTIONAL STEPS. ENSDR DALA2025041202830Access Panel · corrodedCORROSION OUT OF LIMITS ON COUNTERSINKS OF ACCESS PANELS: 520CB (3 HOLES), 520DB (4 HOLES), 520FT (6 HOLES), 620GB (3 HOLES), 620FT (2 HOLES), AND 620DT (3 HOLES) PER B717-200 SRM 57-10-01-2R PROCEDURE 2. SUMMARY OF NRC 00631: CORROSION LEVEL 2. ACCESS PANELS:SDR DALA2025041502920Dimmer · failedSHIP 9562 -ATB/FUME/DE- THE CREW PERFORMED AN AIR TURN BACK TO PNS DUE TO STRONG ELECTRICAL FUMES IN THE COCKPIT WITH LIGHTING CONTROL ISSUES. AN EMERGENCY WAS DECLARED WITH ATC, THE LIGHT CONTROL WAS TURNED OFF, AND THE LANDING BACK AT PNS WAS UNEVENTFUL. NO SDR DALA2025041102826Battery Pack · inoperativeIN THE AFT TAIL SECTION, ALL EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE FOUND A BAD BATTERY PACK. THE BATTERY PACK WAS REPLACED IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. LOCATION B5-260. (LP #7244582)SDR DALA2025041102825Sign · inoperativeEXIT SIGN ABOVE AFT TAIL DOOR INOPERATIVE. MAINTENANCE REMOVED THE SIGN ASSEMBLY, FOUND WIRES DISCONNECTED, SECURED WIRES, AND THE LIGHT NOW OPERATIONALLY CHECKS GOOD IAW B717 AMM 33-51. (LP #7244583)SDR DALA2026012700608Support Angle · corrodedAFT SIDE OF FRAME WEB & LOWER SUPPORT ANGLE ARE CORRODED, JUST FWD OF PRESSURE DOME FWD FACE, LBL14 -RBL 14. REPLACED DOUBLER SUPPORT ANGLE BETWEEN JACK SUPPORT FITTING AND BS 1053 VERTICAL SUPPORT BULKHEAD WEB AT STRINGER 30, IAW SRM 51-40-02. (0904793)SDR DALA2026012700607Seat Track · corrodedRIGHT OTBD SEAT TRACK, FWD TIE FITTING AT FWD END OF TRACK, BS 212 CORRODED. REPLACED THE SEAT TRACK END FITTING IAW DWG 5930566. (0903766)SDR DALA2025102407791Hinge Fitting · corrodedLT FLAP I/B FWD HINGE FITTING MOUNT PINS ON REAR SPAR CORRODED 4EA. REPAIRED PER ERA 620694-14AD. (0904194)SDR DALA2025041102822Skin · leaking-AD- FUEL LEAK FOUND DURING INSPECTION OF THE LH WING AFT LOWER SKIN AT XRS=164 AA #FE5720-01103. ALL REPAIRS C/W PER ERA 622371-14AD. RII C/W [DELTA QC 5223]. (LP #0903380)SDR DALA2025041102821Access Panel · leaking-AD- FUEL LEAK FOUND DURING INSPECTION OF THE LH WING AFT LOWER SKIN DOUBLER AT XRS=164. CONTACT LIAISON ENG FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT AA #FE5720-011.03. ALL REPAIRS C/W PER ERA 622371-14AD. RII C/W [DELTA QC5223]. (LP #0903374)SDR DALA2025040902760Repair · misinstalledFASTENER DISCREPANT INSTALLATION ON PREVIOUS FUSELAGE SKIN REPAIR, ALSO THERE ARE LIGHTNING STRIKES AT TWO LOCATIONS ADJACENT TO REPAIR FASTENERS AT AFT LH ALTERNATE STATIC PORT AREA BTW STA Y=256-362 AND BTW LONG 26LH-27RH. SUMMARY OF NRC 00664: FASTENER DISCSDR DALA2025040902761Web · corrodedWEB FOUND CORRODED LHS OF Y CHORD AT STA 1053. SUMMARY SEE NRC 001-0575:5300-2013/027 01414: REPAIRED WEB REF B717 SRM 51-70-10-2R REPAIR 1. (LP #0903790)SDR DALA2025040902759Skin · crackedCRACKS ON SKIN AT STA Y=1087 AND LONG 14R ON AFT FUSELAGE. SUMMARY OF NRC 00013: SKIN AT STA Y=1087 AND LONG 14R ON AFT FUSELAGE WAS REPAIRED PER PRI 625399-14 REV 4 AND ERA 625399-14 REV ORIGINAL SECTION I: PERMANENT REPAIR SEC II. ACCOMPLISH SECTION II: REPESDR DALA2025040902758Longeron · corrodedCORROSION ON LONGERON 30 STA=994-946, STA=927-908 AFT CARGO COMPARTMENT. SUMMARY OF NRC 0256: CORROSION LEVEL 2. LONGERON 30 STA=994-946, STA=927-908 AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G PARAGRAPH 8 AND 51-41-02-0G PARAGRAPH 4. (LP #SDR DALA2025040902757None · noneCUT AND REMOVE LOWER STA 1053.00 ANGLE 9915561-35 AT APPROX LBL 16 FOR MTC ACCESS. SUMMARY SEE NRC 001-0575:5300-2013/018 01367: CUT, REMOVED, AND REINSTALLED ANGLE 9915561-35 REF B717-200 SRM 51-70-11-2R REPAIR 1. TYPICAL FORMED CHANNEL REPAIR AND DAC DWG 991SDR DALA2025040902756None · noneCUT AND REMOVE LOWER STA 1053.00 ANGLE 9915561-36 AT APPROX RBL 16 FOR MTC ACCESS. SUMMARY SEE NRC 001-0575:5300-2013/019 01368: CUT, REMOVED, AND REINSTALLED ANGLE 9915561-35 REF B717-200 SRM 51-70-11-2R REPAIR 1. TYPICAL FORMED CHANNEL REPAIR AND DAC DWG 991SDR DALA2025040802704Cargo Track · corrodedDUE TO CORRISION REWORK, (UT) THICKNESS MEASUREMENT WAS ACCOMPLISHED ON SIDE TIE TRACK BTW L27L TO L28L AND STA=900 LH TO STA=1022 LH AFT CARGO COMPARTMENT. WITH AN ORIGINAL THICKNESS OF 0.060IN, AND MINIMUN REMAINING THICKNESS OF 0.027IN. THE AREA REWORKED ISSDR DALA2025040802708Battery Pack · no testTHE R1 AND L1 SMALL EMERGENCY EXIT SIGNS ARE INOPERATIVE (LOWER). AFTER TROUBLESHOOTING MAINTENANCE FOUND THAT THE BATTERY PACK (B5-118) INSIDE THE OVERHEAD BIN ABOVE 2D WAS NOT CONNECTED. THE PLUG WAS RECONNECTED AND THE OPERATIONAL CHECK WAS GOOD IAW B717 AMSDR DALA2025040802705Lens · missingTHE OVERHEAD EMERGENCY LIGHT LENS AT 24L IS MISSING. MAINTENANCE REPLACED LENS IAW B717 AMM 33-51-08. (LP #6963274)SDR DALA2025040802703Skin · dentedDENTS ON SKIN BTW STA Y=493 AND STA Y=510 BTW LONG 28L AND LONG 29R AT CTR LOWER FUSELAGE. SUMMARY OF NRC 00025: DENTS ON SKIN BTW STA Y=493 AND STA Y=510 BTW LONG 28L AND LONG 29R WERE REPAIRED PER ER/A 625374-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOSDR DALA2025050603513Pin · misinstalledINSPECTION FOUND THAT THE RELEASE CAM PIN WAS INSTALLED INCORRECTLY AND THAT AN ADJUSTMENT WAS NEEDED ON THE TAIL CONE DEPLOYMENT SYSTEM. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OSDR DALA2025040902755Skin · crackedCRACK ON FUSELAGE EXTERNAL SKIN LOCATED ON STA Y=1037 APROX BTW L=13R AND L=14R. SUMMARY OF NRC 00056: CRACK ON FUSELAGE EXTERNAL SKIN LOCATED ON STA Y=1037 APROX BTW L=13R AND L=14R WAS REPAIRED PER ER/A 625068-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND SDR DALA2025040802702Frame · corrodedCORROSION ON FRAME STA Y=870 L29L TO L29R. ORIGINAL THICKNESS IS 0.063IN AND MINIMUM REMAINING THICKNESS IS 0.029IN THEREFORE AREA IS OUT OF LIMITS PER B717-200 SRM 53-00-00-1A PAR 4C (2) FIG 103. SUMMARY OF NRC 00663: CORROSION LEVEL 2. FRAME STA Y=870 L29L TSDR DALA2025040802701Fastener · looseCRACK AND LOOSE FASTENERS (HI-LOCKS) ON EXTERNAL REPAIR DOUBLER ON STA Y=1022 AND BTW LONGERONS 13R/14R AT FUSELAGE WERE FOUND DURING REPETITIVE INSPECTION PER ER/A 577210-14 REV ORIGINAL SECTION II, STEP 1. SUMMARY OF NRC 00021: SKIN ON STA Y=1022 AND BTW LONSDR DALA2025040802700Skin · corrodedCORROSION ON BARREL NUT HOLE #28 AT HORIZONTAL STABILIZER UPPER SURFACE LH SIDE (CENTER SECTION). (EHV). SUMMARY OF NRC 00383: CORROSION LEVEL 2. BARREL NUT HOLE #28 AT HORIZONTAL STABILIZER UPPER SURFACE LH SIDE WAS REPAIRED PER PRI 624982-14 REV 1 & ER/A 624SDR DALA2025100807324Lug · corrodedAFTER REMOVAL OF INBOARD AND OUTBOARD BUSHINGS OF HINGES LOCATED AT XE= 206 AND XE= 223, CORROSION WAS FOUND ON INBOARD AND OUTBOARD LUGS OF HINGE XE= 206, AND OUTBOARD LUG OF HINGE XE= 206. CORRECTIVE ACTION: CORROSION ON INBOARD AND OUTBOARD LUGS OF HINGE XESDR DALA2025040802699Vane · dentedDENTS ON AFT MOVABLE VANE (LOWER SURFACE) AT LH WING. SUMMARY OF NRC 00468: AFT MOVABLE VANE (LOWER SURFACE) AT LH WING WAS REPAIRED PER ER/A 624886-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI REV 2. ASSOCIATED ER/A 14-624886 ADDED FOR AC 9547. (LP #08SDR DALA2025040802698Pan · corrodedCORROSION AROUND DOOR JAMB PAN OF AFT CARGO COMPARMENT BTW L=25R/28R. SUMMARY OF NRC 00305: CORROSION LEVEL 2. DOOR JAMB PAN OF AFT CARGO COMPARMENT BTW L=25R/28R WAS REPLACED AND INSTALLED PER B717 SRM 53-20-15-2R-7 REPAIR 7. (LP #0896016)SDR DALA2025040802697Support · crackedCRACKED ON SUPPORT OF FWD BULKHEAD STA Y=813 LONGERON 30 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00740: SUPPORT OF FWD BULKHEAD STA Y=813 LONGERON 30 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 1 FIG 201. (LP #0895966)SDR DALA2025040402565Frame · crackedCRACK ON FRAME STA Y=465 BTW L-25R AND L-27R AT FWD CARGO COMPARTMENT. (CCD). SUMMARY OF NRC 00149: CRACK ON FRAME STA Y=465 BTW L-25R AND L-27R AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20 -07-2R PROCEDURE 3 REPAIR 3. PERFORM VISUAL INITIAL INSDR DALA2025040402564Longeron · corrodedCORROSION OUT LIMITS, IN REFERENCE TO NRC 00163: CORROSION ON LONGERON BTW STA Y=956 TO STA Y=964 L30 AT AFT CARGO COMPARTMENT WITH ORIGINAL THICKNESS IS 0.125IN AND MINIMUM REMAINING THICKNESS IS 0.055IN, THEREFORE AREA IS OUT OF LIMITS PER B717-200 SRM 53-00SDR DALA2025041102824Skin · dentedGATE AGENT REPORTS L1 DOOR NOT CLOSING AUTO LEVER NOT INSTALLED. MTC INSPECTED DOOR FOUND DENT IN BOTTOM LEFT CORNER WITH DOOR CLOSED FROM JET BRIDGE PUSHING UP ON DOOR. FOUND DAMAGE ON INNER DOOR BUSSLE AND OUTER LEFT BOTTOM CORNER (NR 592713). COLD WORKED LOSDR DALA2025040302495Angle · corrodedCORROSION ON ANGLE OF AFT CARGO DOOR JAMB AREA BTW STA Y=956 AND LONGERON 27R AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00300: CORROSION LEVEL 2. ANGLE OF AFT CARGO DOOR JAMB AREA BTW STA Y=956 AND LONGERON 27R AT AFT CARGO COMPARTMENT WAS REPLACED AND INSTALLESDR DALA2025040302494Retainer · crackedCRACK WAS FOUND ON RETAINER OF LH SLIDING WINDOW CUTOUT. SUMMARY OF NRC 00878: CRACK ON RETAINER OF LH SLIDING WINDOW CUTOUT WAS REPAIRED PER ER/A 624944-14 REV ORIG SECTION I PERMANENT REPAIR. ASSOCIATED ER/A 14-624944 ADDED FOR AC 9547. (LP #0891407)SDR DALA2025040302493Strap · crackedCRACKED STRAP STA Y 1178 CANT UPPER CHORD, PROJECTION LONG 2 RH AT AFT ACCESORY COMPARTMENT. INITIAL INSPECTION: PERFORM DECAL CONDITION INSPECTION EVERY C-CHECK PER TOPP MANUAL 30-10-70 PAR I PAGE 14. LOG PAGE FOR CRACKED STRAP STA Y 1178 CANT UPPER CHORD, PRSDR DALA2025033102355Power Supply · inoperativeTHE EMERGENCY EXIT SIGN ABOVE FWD F/A SEAT IS INOPERATIVE. MAINTENANCE REPLACED THE B5-235 EMERGENCY BATTERY POWER SUPPLY/CHARGER REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7237017)SDR DALA2025040802706Defog System · faultedWHEN COCKPIT CREW TURNED ON THE WINSHIELD ANTI-FOG SWITCH, WHILE AT CRUISE, A SHOWER OF SPARKS SHOT OUT OF THE UPPER EDGE OF FIRST OFFICER'S FORWARD FACING WINDOW. THE CREW PULLED CIRCUIT BREAKER X26 10592. MAINTENANCE PERFORMED A VISUAL INSPECTION OF FIRST OFSDR DALA2025033102354Repair · crackedCRACKED PREVIOUS REPAIR DOUBLERS (2 EA) ON INTERNAL STRUCTURE OF NLG DOOR JAMB STA Y=46 X-16 RH AND X16LH. SUMMARY OF NRC 00334: PREVIOUS REPAIR DOUBLERS (2 EA) ON INTERNAL STRUCTURE OF NLG DOOR JAMB STA Y=46 X-16 RH AND X16LH, WERE REPLACED PER B717-200 SRM 5SDR DALA2025033102353Longeron · crackedCRACK LONGERON 4LH & STA Y=1152 AT AFT ACCESORY COMPARTMENT. SUMMARY OF NRC 00090: LONGERON 4LH BTW STA Y=1169 AND STA Y=1138 WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #0883561)SDR DALA2025033102352Skin · crackedCRACK ON SKIN AT STA Y=1076 AND LONG 14R ON AFT FUSELAGE. SUMMARY OF NRC 00035: CRACK ON SKIN AT STA Y=1076 AND LONG 14R ON AFT FUSELAGE WAS REPAIRED PER PRI 624820-14 REV 3 AND ER/A 624820-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. PERFORM GVI EVERY 24 MONTSDR DALA2025033102351Pan · crackedCRACKED INNER PAN OVER BEAM #4 AFT EDGE, AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00171: INNER PAN OVER BEAM #4 AFT EDGE AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 623968-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 623968-14 REV 2. ASSOCIATESDR DALA2025033102350Skin · crackedCRACK EVIDENCE ON FUSELAGE SKIN LOCATED AT Y=1087 AND L-14L. SUMMARY OF NRC 00444: CRACK EVIDENCE ON FUSELAGE SKIN LOCATED AT Y=1087 AND L-14L WAS REPAIRED PER PRI 625028-14 REV 1 AND ER/A 625028-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. PERFORM GENERAL VIS
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