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 DALA2025060604330Web · crackedSHIP 9572 CRACK ON MEMBRANE STA Y=813 X=45 AT LH PASSENGER CABIN (CPAX). CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55-2R-4. (0990285)SDR DALA2025060604329Spar Cap · crackedSHIP 9500 LH WING REAR SPAR LOWER CAP CRACK. REPAIRED PER ERA 623615-14AD REV 0 (0990246)SDR DALA2025060604326Support Fitting · wornSHIP 9577 WEAR ON SUPPORT FITTING AND BUSHING ALSO RUSTED HARDWERE OF SPRING RELEASE MECHANISM AT TAILCONE. REPAIRED PER B717-200 SRM 51-41-01-0G (0988292)SDR DALA2025060604325Cusp Web · crackedSHIP 9572 CRACK ON MEMBRANE STA Y=715 X=44 AT LH PASSENGER CABIN (CPAX). REPAIRED PER B717-200 SRM 53-00-55-2R-4 (09881240988124)SDR DALA2025060604323Floor Support · corrodedSHIP 9572 DUE TO CORROSION REMOVAL ON FLOOR SUPPORT STA Y=200, X=10, WAS MEASURE WITH ORIGINAL THICKNESS: 0.070IN MINIMUM REMAINING THICKNESS 0.042 IN THEREFORE IT IS AREA OUT LIMITS. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 51-41-02 (0986603)SDR DALA2025062504755Drain Valve · leakingAFT BAG BIN HAS FUEL SMELL. FOUND FUEL DRAIN FROM FUEL SHROUD DRAIN VALVE BEHIND RT WHEEL WELL. CLEANING BELOW FLOOR. CHECK GOOD (6811338)SDR DALA2025060604328Repair · damagedSHIP 9546 EXISTING REPAIR FOUND. CONTACT LIASON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT. REPAIRED PER ERA 6190064-14AD (0984966)SDR DALA2025060604324Repair · not reportedSHIP 9500 EXISTING REPAIR FOUND PER ERA 623617-14AD REV ORIG. CORRECTIVE ACTION: REPAIRED PER 623617-14AD (0986223)SDR DALA2025060604327Repair · not reportedSHIP 9584 EXISTING REPAIRS FOUND ON RH AFT REAR SPAR FC 5720-01103. REPAIRED PER ER/A 621136-14AD (7125256)SDR DALA2025060604322Frame · crackedSHIP 9577 IN REFERENCE TO NRC 00291; CRACK ON FRAME CANT "CAP" STA Y=1178 AND PROJECTION OF LONGERON 17R AT AFT ACCESSORIES COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER B-717-200 SRM 53-00-00-2R REP.1 (0983728)SDR DALA2025060604321Cargo Track · corrodedSHIP 9577 IN REFERENCE NRC 269: CORROSION OUT OF LIMITS (ORIGINAL THICKNESS 0.060 IN AND REMAINING THICKNESS 0.005 IN IN FLANGE AREA) OF AFT CARGO TIE TRACK LOCATED BETWEEN Y= 813 AND Y= 1022; L-27L L-28L. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 51-41-05-SDR DALA2025052704025Skin · damagedSHIP 9541 LEFT WING LOWER SURFACE AFT SPAR HOLES HAVE DAMAGE FROM STA XRS 111 TO XRS 137. CORRECTIVE ACTION: DAMAGE WAS REMOVED IAW DELTA ER/A 623679-14AD (0982505)SDR HALA20250525028Warning Light · false activationAIR TURN BACK; DUE TO GEAR UNSAFE INDICATION AFTER GEAR SELECTOR MOVED TO UP POSITION AFTER TAKEOFF. NOSE GEAR. OPERATED NLG 20X ALL INDICATIONS NORMAL. PSEU BITE NO FAULTS NOTED. NEAR/ FAR SENSOR READOUT OK. BUNGEE & RETRACT ACTUATOR TEMP READOUT OK. EXTENSIOSDR DALA2025052704026Spar Cap · crackedSHIP 9541 B717-200 / RH WING / REAR SPAR / LOWER CAP / XRS=164 / CRACK. CORRECTIVE ACTION: ASSOCIATED ER/A 00-623681 C/W. (0980036)SDR DALA2025052704030Web · crackedSHIP 9572 CRACK ON MEMBRANE STA Y=645 X=-45 AND Y=653 X=-56 AT RH PASSENGER CABIN (CPAX). CORRECTIVE ACTION: MEMBRANE STA Y=645 X=-45 AND Y=653 X=-56 AT RH PASSENGER CABIN (CPAX) WAS REPAIRED PER B717-200 SRM 53-00 -55-2R PROCEDURE 4 REP.4. (0980496)SDR DALA2025100807323Fitting · corrodedCORROSION ON COUNTERWEIGHT FITTING OF ELEVATOR LH. COUNTERWEIGHT FITTING OF ELEVATOR LT WAS REPAIRED PER ERA 592404-14TR REV ORIGINAL SECTION I. (0977129)SDR DALA2025052704024Inspection · noneSHIP 9509 COMPLY WITH ERA 623616-14AD RH WING/ REAR SPAR/ LOWER CAP CRACK. CORRECTIVE ACTION: COMPLIED WITH ERA 623616-14AD (0978229)SDR DALA2025052704023Web · crackedSHIP 9572 INITIAL INSPECTION:CRACK ON MEMBRANE STA Y =692 X=-44 AT RH PASSENGER CABIN (CPAX). CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-55. (0976468)SDR DALA2025052203939Torque Tube · corrodedSHIP 9572 ON REF AMDS 2027-2004 CORROSION ON SPLINE AND BORE OF RUDDER DRIVE TORQUE TUBE P/N 5912802-13, ALSO CORROSION ON WASHER LOWER BRG P/N 2913035-1 OF RUDDER CONTROL AFT FUSELAGE // EMPENNAGE. CORRECTIVE ACTION: RUDDER TORQUE TUBE WAS REPLACED BY SERVICESDR DALA2025052704029Generator · failedABORTED TAKE-OFF DUE TO A LEFT ENGINE GENERATOR FAILURE MESSAGE: REPLACED GROND RELAY AND AUX POWER RELAY. TEST GOOD.SDR DALA2025052704028Door Frame · crackedSHIP 9577 CRACKED LOWER RH AND LH JAMB REPAIR REINFORCEMENTS AT NLG WHEEL WELL. CORRECTIVE ACTION: LOWER RH AND LH JAMB REPAIR REINFORCEMENTS AT NLG WHEEL WELL PER ER/A 495600-14MA (0973673)SDR DALA2025052203938Fastener · looseSHIP 9577 AFTER INSPECTION ON PREVIOUS REPAIR DOUBLER ON FUSELAGE SKIN STA Y= 1037 BTW LONG 13 RH TO LONG 14RH WERE FOUND LOOSE FASTENERS ON REPAIR DOUBLER AND NEAR TO REAPOIR DOUBLER. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER ER/A 14-568647 (0975044)SDR DALA2025052203941Hinge Fitting · corrodedSHIP 9577 AFTER SEALANT REMOVAL CORROSION WAS FOUND ON ( OTBD LOWER ATTACHING BOLT ) MID FLAP HINGE FITTING STA XW= 251.6 AT RH WING. CORRECTIVE ACTION: STUDS WERE REPLACED AND CENTER WING FLAP HINGE WAS REPLACED BY SERVICEABLE CENTER WING FLAP HINGE PER B717 SDR DALA2025052704022None · noneSHIP 9509 INSTALL LH INBOARD AND CENTER BUTE DOORS. CORRECTIVE ACTION: C/W ER/A 623425-14AD (0972844)SDR DALA2025052704021Structure · wornSHIP 9509 LT WING OUTBD-AIRFRAME-HINGE BOLT HOLE IS WORN. CORRECTIVE ACTION: ALL WORK C/W ON ERA 625207 -14 REV ORG. (0973047)SDR DALA2025052203935Floor Support · corrodedSHIP 9577 AFTER REMOVED CORROSION, GALLEY FLOOR SUPPORT FITTING STA Y=218 - 200 AND STA X= -11 WAS MEASURED AND EVALUATED AND WAS FOUND OUT OF LIMITS. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER CORROSION LEVEL 2, SUPPORT FITTING ON STA Y=218 - 200 STA X= -11SDR DALA2025052203940Wire · brokenSHIP 9555-SMKE/FUME- CREW REPORTED ON FINAL THE FWD F/A SMELLED SMOKE FROM FWD LAV AND REPORTED SPARKS. CORRECTIVE ACTION: MAINTENANCE REPAIRED A BROKEN WIRE AT THE TERMINAL BLOCK.SDR DALA2025052203937Hinge Fitting · wornSHIP 9577 ELONGATED BORE OF INB LUG AND WEAR ON BUSHINGS AND HARDWARE OF OUTBD FLAP HINGE FITTING STA XRS 383 AT RH WING. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER ERA 625998-14 REV ORIGINAL AND PRI 625998-14 REV 2. (0969698)SDR DALA2025052203934None · noneSHIP 9518 ACCOMPLISH ERA 624994-14 KA1717 STRUCTURAL SHIMMING FOR HUGHES WIFI INSTALLATION, CORRECTIVE ACTION: COMPLIED WITH ERA 624994-14 REV. (0969673)SDR DALA2025052203933Frame · corrodedSHIP 9577 IN REFERENCE TO NRC 00217: OUT OF LIMITS AFTER BLENDED OUT FRAME STA Y=889 BTWEN L29L TO L29R. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 REPAIR 3. (0969661)SDR DALA2025052203932Seat Track · corrodedSHIP 9577 CORROSION OUT OF LIMITS PASSENGER CABIN SEAT TRACK (X=- 44; Y= 200 - 256). CROWN WITH ORIGINAL THICKNESS IS 0.115IN. REMAINING THICKNESS IS 0.070IN. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER B-717-200 SRM 53-20-52 (0969326)SDR DALA2025052203931Window Frame · crackedSHIP 9577 CRACKS 3 EA AROUND FASTENER HOLE OF THE LH COCKPIT WINDOW RETAINER STA Y=148. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER ER/A 626178 -14 REV ORIGINAL (0968634)SDR DALA2025052704027Skin · damagedSHIP 9569 FUSELAGE SCRAPE AND GOUGE JUST BELOW L1 DOOR AREA. CORRECTIVE ACTION: REPAIRED PER ERA 6264451-14. (0967283)SDR DALA2025052203936Skin · crackedSHIP 9574 CRACK INDICATION ABOVE THE L/H PYLON IN THE FUSELAGE SKIN. CORRECTIVE ACTION: DOUBLER REPAIR ON A CRACK DAMAGE ON FUSELAGE SKIN P/N 5936436- 101, STA 1022 ABOVE STRINGER 14L. (0969252)SDR DALA2025052203930Seat Track · corrodedSHIP 9577 IN REFERENCE TO NRC 385 WIP 4 CORROSION ON SEAT TRACK X=-22 BTW STA Y=200 TO STA Y=200 TO STA Y=256 ,STA Y=275, AT PASSENGER CABIN, ORIGINAL THICKNESS ON CROWN IS 0.115IN AND THE MINIMUN REMAINING THICKNESS IS 0.046IN; AND WITH ORIGINAL THICKNESS ON SDR DALA2025051903829Longeron · crackedSHIP 9568 INITIAL INSPECTION: CRACK ON LONG 2 LH STA Y=1133 AT AFT ACC COMPARTMENT. CORRECTIVE ACTION: REPAIRED PER B717-200 SRM 53-00-05-2R REPAIR 2 (0967936)SDR DALA2025051903831Tab · damagedSHIP 9552 RT AILERON CONTROL TAB HAS DAMAGE. CORRECTIVE ACTION: RMEOVED RT AILERON CONTROL TAB PER B717 AMM 27-10 WIP 374716. (0967220)SDR DALA2025051503782Power Supply · inoperativeFOUND EMERGENCY LIGHTS TO BE INOPERATIVE FOR THE TAILCONE HANDLE RELEASE AND WALKWAY. MAINTENANCE REPLACED B5-260 EMERGENCY LIGHTS BATTERY POWER SUPPLY AND BATTERY IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7027929)SDR DALA2025051503781Cusp Web · crackedCUSP WEB LOCATED BETWEEN Y=237 AND Y=256; X=-44 AND X=-58 WAS FOUND CRACKED. SUMMARY OF NRC 00817: CUSP WEB LOCATED BETWEEN Y=237 AND Y=256; X=-44 AND X=-58 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4, REPAIR 4, FIGURE 215. (LP #0966489)SDR DALA2025051403732Battery Pack · inoperativeEMERGENCY LIGHTS OVERWING EXIT AND CEILING LIGHT ARE ALL INOPERATIVE. MAINTENANCE FOUND B5-230 BATTERY PACK NOT WORKING. THE BATTERY PACK B5-230 WAS REPLACED PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7173480)SDR DALA2025051403730Skin · crackedCRACK ON FUSELAGE SKIN ON STA Y=1152 BTW LONG 4L AND LONG 5L AT AFT FUSELAGE. SUMMARY OF NRC 00056: FUSELAGE SKIN ON STA Y=1152 BTW LONG 4L AND LONG 5L AT AFT FUSELAGE WAS REPAIRED PER PRI 626216-14 REV 1 AND ER/A 626216-14 REV ORIGINAL SECTION I: PERMANENT RESDR DALA2025051403729Seat Track · corrodedCORROSION ON SEAT TRACK X=22 Y=200 TO Y= 210 (ON SEAT TRACK LOWER FLANGES). ORIGINAL THICKNESS BOTTOM IS 0.100 IN AND MINIMUM REMAINING THICKNESS IS 0.030 IN THEREFORE AREA IS OUT OF LIMITS PER B717 SRM 53-20-52-1A PROCEDURE 1 PAR 4 FIG 101. AND DC-MD/BOEING NSDR DALA2025051403728Structure · corroded-AD- CORROSION WAS FOUND ON BORES 31, 33, ALSO ON HOLE #10 (VERTICAL AND TRANSVERSAL). SUMMARY OF NRC 667: CORROSION LEVEL 2. BORES 10, 31, AND 33 OF HORIZONTAL STABILIZER BARREL NUTS WERE REPAIRED PER PRI 625941-14 REV 1 & ER/A 625941-14AD REV ORIG. SECTION ISDR DALA2025051303689Longeron · corrodedCORROSION OUT OF LIMIT ON LONGERON 26L BTW STA Y=962/967 AND BTW STA Y=974/988 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00792: CORROSION LEVEL 2. LONGERON 26L BTW STA Y= 962/967 AND BTW STA Y=974/988 WAS REPAIRED PER B717-200 SRM 53-00-05-2R REPAIR 3 PAR 4 A (SDR DALA2025051303688Skin · crackedCRACKS ON FUSELAGE SKIN ON STA Y=1087 AND LONG 14L AT AFT FUSELAGE. SUMMARY OF NRC 00047: FUSELAGE SKIN ON STA Y=1087 AND LONG 14L AT AFT FUSELAGE WAS REPAIRED PER ERA 626154-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 626154-14 REV 3. SEC II ACCOMPLISSDR DALA2025051303687Cusp Web · crackedCUSP WEB LOCATED BETWEEN Y=218 AND Y=237; X=-44 AND X=-58 WAS FOUND CRACKED. SUMMARY OF NRC 00816: CUSP WEB BETWEEN STA Y=218 AND Y=237; STA X=-44 AND X=-58, WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 PAR 5 FIGURE 21. (LP #0963051)SDR DALA2025051303686Cusp Web · corrodedCORROSION OUT LIMITS ON PASSENGER CABIN CUSP WEB LOCATED Y=427 - 446; X=-56. SUMMARY OF NRC 00769: CORROSION LEVEL 2. PASSENGER CABIN CUSP WEB LOCATED Y=427 - 446; X=-56 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REP 4 FIG 211 CONFIG. 7017. (LP #096SDR DALA2025051203681Skin · crackedCRACKS ON FUSELAGE SKIN AT STA Y=1087 AND LONG 14R ON AFT FUSELAGE. SUMMARY OF NRC 00048: FUSELAGE SKIN AT STA Y=1087 AND LONG 14R ON AFT FUSELAGE WAS REPAIRED PER ERA 626165-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 626165-14 REV 3. ASSOCIATED ER/A SDR DALA2025051203680Hinge Fitting · corrodedFRETTING CORROSION (UT) THICKNESS MEASUREMENT WAS ACCOMPLISHED PLATE RH OUTBD ON VERTICAL STABILIZER SPAR HINGE. FITTINGS WITH ORIGINAL THICKNESS =0.250" AND MINIMUM REMAINING THICKNESS IS 0.212" THEREFORE IT IS OUT LIMITS. SUMMARY OF NRC 00820: CORROSION LEVESDR DALA2025051403727Spar Cap · crackedDUE TO CRACK IN RH WING REAR AFT SPAR LOWER CAP, COMPLY WITH PRI 621388-14. CRACKED SPAR CAP REPLACED ON PRI 621388-14 REVS 0 THRU 22. COMPARED PRI 621388-14 REVS 0 THRU 22 AND ERA 621388-14 REV ORIG. ALL ITEMS MATCH. COMPLIED WITH ERA 621388-14 REV ORIG. ALL
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