Boeing 717-200
Service difficulty reports · 18,756
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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 DALA2024120311393Cusp Web · corrodedCORROSION ON CUSP WEB BTW X=-56 TO X=-60 AND BTW STA Y=794-813 AT CPAX. SUMMARY OF NRC 00739: CORROSION LEVEL 2. CUSP WEB BTW X=-56 TO X=-60 AND BTW STA Y=794-813 AT CPAX WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR PARAGRAPH 5 B (14) FIG 216.SDR DALA2024120311396Service difficultySHIP 9501 -MISC/DE- THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC GOING INTO ATL DUE TO "PSEU FAIL" MESSAGE AND THE RESULTANT FLAPS-UP LANDING AS PER THE QRH. CORRECTIVE ACTION: MAINTENANCE FOUND THE LEFT SLAT A SENSOR WIRES TO BE SHORTED TO GROUND. THE WIRE SDR DALA2024120211375Light Sys · inoperativeDURING SERVICE NOTED THAT THE LH AND RH AFT OVERWING AND RH FWD OVERWING EMERGENCY EXIT LIGHTS WERE INOPERATIVE. REPLACED THE POWER SUPPLY B5-119 REF B717 AMM 33-51. BOTH AFT OVER WING LIGHTS WORK BUT RH FWD STILL INOPERATIVE. FOUND GROUND LOOSE FOR L2-832. RESDR DALA2024121311700Cusp Web · crackedCUSP WEB LOCATED BETWEEN Y=218 TO Y=237, BETWEEN X=-56 TO X=-44 WAS FOUND CRACKED. SUMMARY OF NRC 00647: DUE TO CRACKS, NEW CUSP WEB LOCATED AT BETWEEN Y=218 TO Y=237, BETWEEN X=-56 TO X=-44 WAS FABRICATED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIG SDR DALA2024120211377Sensor · inoperativeSHIP 9501 -MISC/DE- THE FLIGHT CREW DECLARED EMERGENCY WITH ATC INTO CHA DUE TO THE "PSEU FAIL" MESSAGE. A FLAPS-UP LANDING FOLLOWED PER THE QRH. CORRECTIVE ACTION: MAINTENANCE PERFORMED BITE OF THE PSEU WHICH RETURNED CODES 326029 (PSEU INTERNAL FAULT INTERMISDR DALA2024120211376Light · inoperativeEMERGENCY LIGHTS ABOVE ROWS 24-27 ARE INOPERATIVE. REPLACED EMERGENCY POWER SUPPLY (B5-231) AND OPERATIONAL CHECK WAS GOOD IAW B717 AMM 33-51. (LP #6585094)SDR DALA2024120211374Seat Track · corrodedCORROSION ON LH SEAT TRACK X=44 BTW STA Y=200-214 AT PASSENGER CABIN. SUMMARY OF NRC 00661: CORROSION LEVEL 2. LH SEAT TRACK X=44 STA Y=200 TO Y=304 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5 REPAIR 5. (LP #0685816)SDR DALA2024120211373Door Frame · corrodedCORROSION ON ANGLE AND WEB ON LOWER DOOR JAMB STA Y=200 AT PAX CABIN (L1). SUMMARY OF NRC 00386: CORROSION LEVEL 2. ANGLE AND WEB ON LOWER DOOR JAMB STA Y=200 AT PAX CABIN WERE REPLACED PER B717-200 SRM 51-41-01-0G, 51-41-02-0G, 51-41-05-0G, AND 51-41-08-0G. (SDR DALA2024120211372Doubler · corrodedCORROSION ON DOUBLER BELOW TEE FITTING STA 1053 LONGERON 30 AT AFT BULKHEAD. SUMMARY OF NRC 00563: CORROSION LEVEL 2. DOUBLER BELOW TEE FITTING STA 1053 LONGERON 30 AT AFT BULKHEAD WAS REPLACED PER B717 SRM 53-20-08-0I PROCEDURE 2 AND 51-41-05-0G. (LP #0684614SDR DALA2024120311397Transducer · shortedSHIP 9550 -ATB/DE- THE FLIGHT CREW RETURNED THE AIRCRAFT TO CAE AND DECLARED AN EMERGENCY DUE TO "STICK PUSHER FAIL" MESSAGE WITH AN ASSOCIATED STALL WARNING LIGHT. CORRECTIVE ACTION: MAINTENANCE FOUND THAT THE CAPTAINS CONTROL WHEEL FORCE TRANSDUCER (T2-6080)SDR DALA2024120211371Cusp Web · crackedCRACKS ON LH CUSP WEB (3 EA) STA Y=657 & X=56 AND STA Y=716 & X=44.5 AND Y=888 & X=56 AT PASSENGER CABIN. SUMMARY OF NRC 00426: FABRICATED WEB STA Y-655 TO Y-715 PER B717-200 SRM 53-20-51-01 PROCEDURE 2. REPAIRED CUSP WEB STA 888 & X 56 PER B717-200 SRM 53-00-SDR HALA202411290077Window · crackedPOSSIBLE CRACK IN LOWER PORTION OF CO PILOT WINDSHEILD APPROX 1 INCH. REMOVED RIGHT AND CENTER FAIRING COVER AND WINDSHEILD WIPER AMM 56-11-02-801 25000. REMOVED AND REPLACED RIGHT SIDE WINDSHEILD IAW AMM 56-11-02 UP TO PARA 4E (6). ACCOMPLISHED REMAINING STEPSDR DALA2024120211370Rib · elongatedELONGATED HOLE ON RIB ON COUNTERWEIGHT-TO-L.E. CONNECTION FITTING AT RIGHT ELEVATOR STA XH 217. SUMMARY OF NRC 00410: RIB ON COUNTERWEIGHT-TO-L.E. CONNECTION FITTING AT RIGHT ELEVATOR STA XH 217 WAS REPAIRED PER B717 SRM 55-00-00-2R REPAIR 2 PAR 4. THIS REPAIRSDR DALA2024112711265Door · damagedCONT OF LOG #693782 L1 DOOR FWD LOWER DOOR DAMAGED. FABRICATED REPAIR DOUBLER AND FILLER PER B717 SRM 52-10-01-2R PROC 1. COMPLETED FWD PASSANGER DOOR LOWER FWD CORNER SKIN REPAIR PER B717 SRM 52-10-01-2R PROC 1 REPAIR 1. A/C OK FOR SERVICE. (LP #0680895)SDR DALA2024112711263Skin · dentedRAMP REPORTS DENT ON L1 DOOR BOTTOM FWD CORNER. ATEMPTED TO REWORK/STRAIGHTEN DOOR EDGE PER B717 SRM 52-00-00-2R -3. FOUND CRACK APPOX 1/4" LONG 1/4" FROM BOTTOM OF DOOR. REMOVED DAMAGE AREA OF DOOR SKIN PER B717 SRM 52-10-01-2ER-PROCEDURE 1. ACCOMPLISHED DAMASDR DALA2025011500350Skin · damagedLIGHTNING STRIKE ON THE FUSELAGE AT THE RH WINDOW PANEL, STA 484 TO 503. ACCOMPLISH ER/A 622755-14 SECTION II INSPECTION WITHIN EVERY 24 MONTHS UNTIL ACCOMPLISHMENT OF SECTION III PERMANENT REPAIR NO LATER THAN 48,400 TOTAL CYCLES. ASSOCIATED ER/A 00-622755 ADSDR DALA2024112711259Skin · mechanic errorEXTERNAL SURFACE OF FUSELAGE SKIN COMMON TO VHF ANTENA MATING SURFACE WAS FOUND MISDRILLED, LOCATED Y=917 L-30/L-29L IN REF NRC 12. SUMMARY OF NRC 00169: FUSELAGE SKIN COMMON TO ANTENA MATING SURFACE WAS FOUND MISDRILLED, LOCATED Y=917 L-30/L-29L WAS REPAIRED SDR DALA2024112711258Seat Track · corrodedCORROSION ON RH SEAT TRACK X=22 BTW STA Y=200-256 IN PASSENGER CABIN. SUMMARY OF NRC 00662: CORROSION LEVEL 2. SEAT TRACK RH X=22 STA Y=200 TO Y=266 WAS REPAIRED PER B717-200 SRM 53-20-52-2R REPAIR 5, 51-41-01-0G, AND 51-41-05-0G PAR 8. (LP #0679793)SDR DALA2024112711257Spar · cracked-AD- WORKING PRI 615810-14AD REV 0. LH WING SPAR CRACK FUEL LEAK. ACCOMPLISHED PRI 615810-14AD REVISION D, REV 3. VERIFIED ERA 615810-14AD REV D SECTION VI TIME LIMITED REPAIR III MATCHES COMPLETED PRI 615810-14AD REV 0, 1, 2, AND 3. ASSOCIATED ER/A 14-615810 SDR DALA2024112611229Cable · disconnectedTHE GIRT BAR RETAINER WITH THE CABLE WAS DISCONNECTED FROM THE SLIDE BUSSLE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. *** CONTRACT MAINTENANCE EVENT - OCM: 291111 *** REATTACHED GIRT BAR RSDR DALA2024112711256Light · sparksF/O BRIEFCASE LIGHT IS SPARKING INTERNALLY. MAINTENANCE REPLACED THE F/O BRIEFCASE LIGHT IAW B717 AMM 33-16. OPERATIONAL CHECK WAS GOOD. AIRCRAFT IS OK FOR SERVICE. (LP #6723386)SDR DALA2024112611228Slide · out of positionON WAKE-UP CHECK FOUND THE AFT TAIL CONE SLIDE PACK HAD ROTATED OUT OF SECURED POSITION. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REMOVED THE TAIL SLIDE PACK REF W/C 2561-9006 SDR DALA2024112611227Cusp Web · crackedFOUND RACKS ON CUSP WEB BTW STA Y=239-258 X=44 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00737: CRACKS ON CUSP WEB BTW STA Y=239-258 X=44 AT PASSENGER CABIN WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0678225)SDR DALA2024112611226Longeron · crackedCRACKS ON LONGERONS 6R, 3L, AND 6L STA Y 1020 AT C. PAX. SUMMARY OF NRC 0486: CRACKS ON LONGERONS 6R, 3L, AND 6L STA Y 1020 AT C. PAX WERE REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #0678029)SDR DALA2024112711260Fastener · loose-AD- FOUND LOOSE FASTENERS ON RH VERTICAL STABILIZER LEADING EDGE REF AA 553001048 AND AD 2018-10-08. SUMMARY NRC 018-0001:5530-01048-02 / 002 00005: CHECK IF THE FASTENER(S) HOLE COUNTER SINK AND DIAMETER ARE WITHIN LIMITS LISTED IN SERVICE GENERAL DRAWING SGSDR DALA2024112611225Fastener · loose-AD- FOUND LOOSE FASTENERS ON LH VERTICAL STABILIZER LEADING EDGE REF AA 553001048 AND AD 2018-10-08. SUMMARY OF NRC 018-0001:5530-01048-02 /001 00004: CHECKED AND FOUND OK. SUMMARY OF NRC 018-0001:5530-01048-02/001 00004: CMOR VERIFIED LH FASTENER HOLES LIMITSDR DALA2024112511165Skin · dentedDENTS AND NICKS WERE FOUND ON THE EXTERNAL SKIN FLUSH REPAIR STA Y 237 AND BTW LONGERON 17L/18L. ALSO WRONG INSTALLED FASTENERS ON INTERNAL DOUBLERS BTW STA Y218/256 AND BTW LONGERONS 16/18 AT FUSELAGE. SUMMARY OF NRC 00343: PREVIOUS REPAIR ON STA Y 237 AND BTSDR DALA2024112511164Door Frame · corrodedCORROSION ON DOOR JAMB FWD/AFT AT REPAIR SPLICES AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00806: CORROSION LEVEL 2. AFT CARGO DOOR JAMB FWD/AFT REPAIR SPLICES WERE REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. (LP #0674286)SDR DALA2024112511163Cusp Web · crackedCRACKS ON LH CUSP WEB (2 EA) STA Y=595 & X=56 AND STA Y=907 & X=56 BELOW SEAT TRACK SPLICE IN PASSENGER CABIN. SUMMARY OF NRC 00425: CUSP WEBS BTW STA Y 579-598 AND X=54 TO X=60 AND BTW STA Y 889-908 AND X=54 TO X=60 WERE REPLACED PER B717 SRM 53-00-55-2R REPASDR DALA2024112611222Pan · crackedCRACK ON FWD INNER PAN BTW STA 954 BEAM 3 APPROX AT AFT CARGO DOOR. SUMMARY OF NRC 00086: AFT CARGO DOOR WAS REPLACED WITH A SERVICEABLE AFT CARGO DOOR AND PART NUMBER WAS VERIFIED PER B717-200 AIPC 52-33-01-01 ITEM 130J AND IS INSTALLED UNDER AMDS 5231-4004.SDR DALA2024112511166Bolt · shearedSHIP 9521 -ATB/GEAR/DE- THE FLIGHT CREW PERFORMED AN AIR TURN BACK TO CLT DUE TO A "RIGHT MAIN LANDING GEAR UNSAFE" MESSAGE WITH AN ASSOCIATED "RIGHT GEAR DOOR OPEN" MESSAGE. THE ALTERNATE GEAR EXTENSION LEVER WAS PULLED. AN EMERGENCY WAS DECLARED WITH ATC. COSDR DALA2024112211134Pan · crackedCRACK ON INNER PAN FWD EDGE IN BEAM #5 AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00325: INNER PAN FWD EDGE IN BEAM #5 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ERA 621747-14, REV ORIGINAL. ASSOCIATED ER/A 14-621747 ADDED FOR AC 9539. (LP #0671941)SDR DALA2024120911533None · none-AD- ACCOMPLISH ER/A 539703-14AD REV A SEC II. ACCOMPLISH ER/A 539703-14AD REV A SEC II FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATED. INSPECTIONS CANNOT BE PUSHED PAST 04DEC24. ASSOCIATED ER/A 14-539703 ADDED FOR AC 9501. **REDEFFESDR DALA2024120311392Bulkhead · abnormal-AD- ACCOMPLISH ER/A 558098-14AD REV A SEC II. ACCOMPLISH ER/A 558098-14AD REV A SEC II FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATED. INSPECTIONS CANNOT BE PUSHED PAST 04DEC24. ASSOCIATED ER/A 14-558098 ADDED FOR AC 9562. ACCOMPLISSDR DALA2024112511162Skin · dentedSEVERAL DENTS ON SKIN OF AFT MOVABLE FLAP VANE GUIDE AT RH WING. SUMMARY OF NRC 00196: AFT RH FLAP VANE WAS REPLACED PER AMDS 2750-4008. (LP #0670862)SDR DALA2024112211133Frame · dentedDENT ON FRAME STA Y=408 AND LONG 27LH AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 634: DENT ON FRAME STA Y=408 AND LONG 27LH AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 2, REPAIR 2, FIG. 201. (LP #0670995)SDR DALA2024112111102Hinge Fitting · crackedCRACKED OUTBOARD LOWER BORE OF FLAP HINGE FITTING #3 AT RH WING. RH OUTBOARD WING FLAP HINGE FITTING WAS REMOVED PER B717-200 AMM 57-55-25 000-803 STEP A TO STEP E (2). RH OUTBOARD WING FLAP HINGE FITTING WAS REPLACED & INSTALLED PER B717-200 AMM 57-55-25 400-SDR DALA2024112011084Seat Track · mechanic errorMISDRILLED SEAT TRACK (SETTLEMT AREA) BTW STA Y=908-927 AND X=54 LH AT PASSENGER CABIN. SUMMARY OF NRC 00751: SEAT TRACK (SETTLEMT AREA) BTW STA Y=908-927 AND X=54 LH AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-20-52-2R REPAIR 5. PERFORM DECAL CONDITIOSDR DALA2024112011083Tripler · corrodedCORROSION ON PREVIOUS REPAIR TRIPLER ON FUSELAGE UNDER FILLET FAIRINGS AREA STA Y=843-860 LONG 28L-28R. SUMMARY OF NRC 00467: CORROSION LEVEL 2. PREVIOUS REPAIR TRIPLER WAS REPLACED PER B717 SRM 53-20-70-2R REP 1. PERFORM EXTERNAL VISUAL INSPECTION EVERY 8,000SDR DALA2024111911028Cusp Web · crackedCRACK AT LH CUSP MEMBRANE AT STA 800 X=55 ON CPAX. SUMMARY OF NRC 00406: CRACK AT LH CUSP MEMBRANE AT STA 800 X=55 ON CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0666517)SDR DALA2024111911027Longeron Splice · corrodedCORROSION ON UPPER AND LOWER SURFACE OF LONGERON AND LONGERON SPLICE (RH 29) FROM STA Y=218 TO Y=237. SUMMARY OF NRC 00344: CORROSION LEVEL 2. LONGERON L29 R/H STA Y=157 TO Y=237 AND LONGERON SPLICE (RH 29) FROM STA Y=218 TO Y=237 WERE REPLACED PER B717-200 SRSDR DALA2024111911029Light · inoperativeTHE CABIN CEILING MOUNTED EMERGENCY LIGHT AT 2AB IS INOPERATIVE. FORWARD TO MEL 33-51-01A. PLACARDS INSTALLED. ON 18NOV24 MAINTENANCE REPLACED THE 2AB CABIN CEILING STANBY LIGHTING ASSEMBLY PER B717 AMM 33-52. OPERATIONAL CHECK WAS GOOD. MCO AND PLACARD WERE RSDR HALA20241118072Battery · inoperativeOVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED OVERWING EMERGENCY LIGHT BATTERY PER 33-51-00. OPS CHK GPPD. OK FOR SERVICE.SDR DALA2024111911026Cusp Web · crackedCRACKS ON CUSP MEMBRANE AT STA 655 X=45 AND STA 674 X=46 IN CPAX. SUMMARY OF NRC 00405: CRACKS ON CUSP MEMBRANE AT STA 655 X=45 AND STA 674 X=46 IN CPAX WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. PERFORM GVI EVERY C-CHECK PER B717 SRM 53-00-55-2R SDR DALA2024111911025Vane · dented-AD- DENTS ON RH WING FWD MOVABLE VANE INBD SURFACE. SUMMARY OF NRC 00326: DENTS (3 LOCATIONS) ON LOWER SKIN OF FWD MOVABLE VANE RH WING WERE EVALUATED AND FOUND OUT LIMITS. RH WING FWD MOVABLE VANE WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR SDR DALA2024111911024Skin · crackedCRACK ON FUS SKIN BTW STA 1037 AND 1053 LONGERON 15R. SUMMARY OF NRC 0053: FUS SKIN BTW STA 1037 AND 1053 LONGERON 15R WAS REPAIRED PER ER/A 621624-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. MAINTENANCE REQUIREMENTS WERE VERIFIED AND THE FOLLOWING ACTIONS ARSDR DALA2024111510968Skin · crackedCRACKED FUSELAGE SKIN STA Y 1022 BTW LOG 7R-8R CLOSE TO THE LAP SKIN JOINT. SUMMARY OF NRC 00054: FUSELAGE SKIN STA Y 1022 BTW LOG 7R-8R CLOSE TO THE LAP SKIN JOINT WAS REPAIRED PER ER/A 621690-14 REV ORIGINAL SECTION I PERMANENT REPAIR AND PRI 621690-14 REV 1SDR DALA2024111510967Seat Track · corrodedCORROSION ON LH SEAT TRACK STA X=56 AND BTW STA Y=545-548 AT PAX CABIN. SUMMARY OF NRC 00686: CORROSION LEVEL 2. SEAT TRACK ON LH STA X=56 AND BTW STA Y=545 TO 548 AT PAX CABIN WAS REPAIR PER B717-200 SRM 53-20-52-2R PROCEDURE 1 REPAIR 1. (LP #0660518)SDR DALA2024111510966Cusp Web · corrodedCORROSION ON RH CUSP WEB UPPER/LOWER SURFACES ON STA Y=492, Y=501-503 AT PASSENGER CABIN. SUMMARY OF NRC 730: CORROSION LEVEL 2. RH CUSP WEB UPPER/LOWER SURFACES ON STA Y=492, Y=501-503 AT PASSENGER CABIN WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 SDR DALA2024111410956Battery Pack · no testTHE EMERGENCY EXIT SIGNS ARE INOPERATIVE AT STATION 180, STATION 247, AND STATION 706. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACKS B5-235, B5-259, AND B5-120 PER B717 AMM 33-51. OPERATION CHECK WAS NORMAL. (LP #5423934)
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