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 DALA2024062106296Longeron · crackedCRACK ON LONGERON 13R STA Y=1032 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00545: LONGERON 13R STA Y=1032 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2 FIG. 201. (LP #0404102)SDR DALA2024062106295Web · crackedPUNCTURE ON MEMBRANE (LWR SURFACE) STA Y=316 AND X=55 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00515: MEMBRANE (LWR SURFACE) STA Y=316 AND X=55 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55 2R PROCEDURE 4 REPAIR 4 FIG 220. (LP #040401SDR DALA2024062106294Intercostal · crackedCRACK ON INTERCOSTAL WAS FOUND ON STA Y=636 X=0 AT PAX CABIN. SUMMARY OF NRC 00838: CRACK ON INTERCOSTAL ON STA Y=636 X=0 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-00-2R PROCEDURE 2 REPAIR 2. (LP #0403676)SDR DALA2024062006271Beam · damagedCRACK BEYOND STOP DRILL ON DOOR BEAM 1 BTW STA 190-200 (UPPER AFT CORNER) AT FWD PASSENGER DOOR L1. SUMMARY OF NRC 00174: DOOR BEAM 1 BTW STA 190-200 (UPPER AFT CORNER) AT FWD PASSENGER DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R REPAIR 7 PAR. 6 FIGURE 2SDR DALA2024062006270Frame · crackedCRACK ON MAIN FRAME STA Y=1037 L17L, L17R AT PAX CABIN. SUMMARY OF NRC 00441: MAIN FRAME STA Y=1037 L17L, L17R AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R-4, PAR 5A. (LP #0402943)SDR DALA2024062006269Door Frame · corrodedCORROSION ON LOWER EDGE AND FWD EDGE DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00297: CORROSION LEVEL 2. DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7, 51-41-02-0G, AND 51-41-05-0G. (LP #0402912)SDR DALA2024062106299Latch · looseSHIP 9582 -GEAR/DE- DURING THE FINAL APPROACH FOR LANDING THE AIRCRAFT INDICATED A "GEAR UNSAFE" CONDITION FOR ALL 3 GEAR POSITIONS. AN EMERGENCY WAS DECLARED WITH ATC, THE QRH WAS COMPLIED WITH, AND THE ALTERNATE GEAR EXTENSION PROCEDURES WERE UTILIZED, WHICHSDR DALA2024062006268Beam · crackedCRACK ON INTERNAL PAN IN BEAM 3 AND 4 AT FWD CARGO COMPARTMENT DOOR AFT EDGE. SUMMARY OF NRC 00685: INTERNAL PAN IN BEAM 3 AND 4 AT FWD CARGO COMPARTMENT DOOR AFT EDGE WAS REPAIRED PER B717-200 SRM 52-30- 02-2R PROCEDURE 1 REPAIR 1. (LP #0402498)SDR DALA2024061906217Battery · inoperativeEXIT SIGNS ABOVE LT & RT OVERWING FWD EXIT DOORS DO NOT ILLUMINATE. T/S PER B717 FIM 33-50-00-201. R&R B5-121 BATTERY ASSEMBLY PER B717 AMM 33-51-03. OPERATIONAL CHECK WAS GOOD. (LP #5891885)SDR DALA2024061906216Window Frame · crackedCRACK ON UPPER REAR CORNER AT CUTOUT OF RH SLIDING WINDOW IN REF TO NRC 00027. SUMMARY OF NRC 00661: UPPER REAR CORNER AT CUTOUT OF RH SLIDING WINDOW WAS REPAIRED PER B717-200 SRM 56-10-02-2R-1 PROCEDURE 1, REPAIR 1. (LP #0400469)SDR DALA2024061906215Window Frame · crackedCRACK ON RETAINER AND FRAME AT LH SLIDING WINDOW A COCKPIT. SUMMARY OF NRC 00182: FRAME AT LH SLIDING WINDOW A COCKPIT WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1, REPAIR 1 AND RETAINER LH SLIDING WINDOW COCKPIT WAS REPLACED PER B717-200 SRM 51-41-02SDR DALA2024061806171Battery Pack · inoperativeDURING SERVICE, FOUND THE EMERGENCY LIGHTS IN AFT CABIN AT ROWS 24-29, TO BE INOPERATIVE. MAINTENANCE REPLACED THE AFT CABIN BATTERY PACK PER B717 AMM 33-55. OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT IS OK FOR SERVICE. (LP #5640369)SDR DALA2024061806170Skin · crackedCRACK ON SKIN OF CUT OUT EDGE AT AFT CARGO DOOR STA Y=992 BTW L25R. SUMMARY OF NRC 00226: CRACK ON SKIN OF CUT OUT EDGE AT AFT CARGO DOOR STA Y=992 BTW L25R WAS REPAIRED PER B717-200 SRM 53-20-15- 2R PROCEDURE 12. PERFORM AN EXTERNAL GVI EVERY 8000 CYCLES TO TSDR DALA2024061806169Skin · damagedCORROSION WAS FOUND ON VERTICAL AND HORIZONTAL UPPER HOLES LH #10, 11, AND LOWER HOLE #29, LOWER HOLES RH #29 AND 39 AT CENTER BOX OF HORIZONTAL STABILIZER. UPPER HOLES LH #10, 11, AND LOWER HOLE #29, LOWER HOLES RH #29 AND 39 AT CENTER BOX OF HORIZONTAL STABISDR DALA2024061606114Seat Track · corrodedCORROSION OUT OF LIMITS ON RH INBOARD SEAT TRACK X=-22 BTW STA Y=200-276 AT PAX CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00664: CORROSION LEVEL 2. SEAT TRACK X=-22 BTW STA Y=200-276 WAS REPLACED PER B717-200 SRM 51-41-01-0G AND 51-41-05-0G. (LP #0396078)SDR DALA2024061606113Window Frame · crackedDURING INSPECTION AFTER REMOVAL OF INTERNAL CAP UPPER AFT SIDE, A CRACK WAS FOUND ON THE UPPER REAR CORNER AT CUTOUT OF LH SLIDING WINDOW IN REF TO NRC 00024. SUMMARY OF NRC 00660: UPPER REAR CORNER AT CUTOUT OF LH SLIDING WINDOW WAS REPAIRED PER B717-200 SRM SDR DALA2024070106608Apu · fireSHIP 9510 -FIRE- WORKING APU MEL FOR NO START, TECHNICIANS REPLACED FCU AND START FUEL PURGE VALVE. APU WAS RUNNING FOR 15 MINUTES FOR LEAK AND OPS CHECKED WHEN FIRE WARNING ANNUNCIATION SOUNDED. FIRE WAS CONFIRMED, FIRE HANDLE PULLED, BOTTLE DISCHARGED. DUE TSDR DALA2024061606116Fire Detector · false indicationSHIP 9575 -ATB/DE- AS THE AIRCRAFT CLIMBED OUT ON DEPARTURE, THE APU FIRE WARNING (LEVEL 2) ACCOMPANIED BY THE MASTER CAUTION, ALL ILLUMINATED. THE CREW DECLARED AN EMERGENCY AND RETURNED THE AIRCRAFT BACK TO DTW. THE LANDING WAS UNEVENTFUL AND ARFF SCANNED THSDR DALA2024061606115Relay · failedSHIP 9569 -MISC/DE- THE "ANTI-SKID FAIL" ALERT POSTED WHEN THE LANDING GEAR WAS SELECTED DOWN. A GO-AROUND WAS PERFORMED. DUE TO WET RUNWAYS, THE CREW DECLARED AN EMERGENCY. THE AIRCRAFT LANDED SAFETY WITHOUT FURTHER INCIDENT. CORRECTIVE ACTION: MAINTENANCE RESDR DALA2024061606112Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA 148 TO STA 200 X=5 AT PAX CABIN FLOOR STRUCTURE. IN REFERENCE NRC 00604. SUMMARY OF NRC 00789: CORROSION LEVEL 2. FLOOR SUPPORT STA 148 TO STA 200 X=5 AT PAX CABIN FLOOR STRUCTURE WAS FABRICATED AND INSTALLED PER DWG 9936534 REV SDR DALA2024061606111Web · crackedCORROSION ON WEB FROM STA 218 COORDINATE X=55 PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00695: CORROSION LEVEL 2. WEB FROM STA 218 COORDINATE X=55 WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0394095)SDR DALA2024061606110Cusp Web · crackedCRACKS CUSP WEBS STA Y=670 AND X=60 ALSO STA Y=476 AND X=-60 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00610: CUSP WEBS STA Y=670 AND X=60 ALSO STA Y=476 AND X=-60 AT PASSENGER CABIN WERE REPAIRED PER B717- 200 SRM 53-00-55-2R-4. (LP #0393751)SDR DALA2024061606109Pan · crackedCRACK ON INTERNAL PAN IN BEAM 3 AT FWD CARGO COMPARTMENT DOOR FWD EDGE. SUMMARY OF NRC 00686: INTERNAL PAN IN BEAM 3 AT FWD CARGO COMPARTMENT DOOR FWD EDGE WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0393395)SDR DALA2024061606108Frame · damagedTOOL MARKS ON OVERWING FRAME STA737 L-18R AT WING BOX. SUMMARY OF NRC 00533: OVERWING FRAME STA737 L-18R AT WING BOX WAS REPAIRED PER PRI 618675-14 REV.0 AND ERA 618675-14 REV. ORIGINAL ASSOCIATED ER/A 14-618675 ADDED FOR AC 9567. (LP #0392376)SDR DALA2024061406097Cusp Web · corrodedCORROSION ON CUSP MEMBRANE FROM STA Y=794 TO 813 BTW X=-55 TO -60 APPROX AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00663: CORROSION LEVEL 2. REPAIR PARTS WERE FABRICATED PER B717-200 SRM 53-00-55 2R-4 FIG. 215 AND INSTALLED PER B717-200 SRM 51-41-02-0G. (LPSDR DALA2024061306056Cusp Web · corrodedCORROSION ON LH CUSP WEB STA Y=936-940 AND X=55 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00791: CORROSION LEVEL 2, LH CUSP WEB STA Y=936-940 AND X=55 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4 FIGURE 216. (LP #0391165)SDR DALA2024061306055Beam · crackedCRACK ON BEAM 1 APROX STA Y=192 AT PASSENGER ENTRANCE DOOR L1. SUMMARY OF NRC 00235: BEAM 1 APROX STA Y=192 AT PASSENGER ENTRANCE DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7 FIGURE 201. (LP #0390916)SDR DALA2024061306054Pan · crackedCRACK INNER PAN OVER BEAM #3 FWD SIDE OF FWD CARGO DOOR (C1). SUMMARY OF NRC 00227: INNER PAN OVER BEAM #3 FWD SIDE OF FWD CARGO DOOR (C1) WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0390698)SDR DALA2024061005957Battery · inoperativeBOTH RT AND LT AFT EMERGENCY DOOR EXIT SIGNS OVER WINGS DO NOT ILLUMINATE.T/S PER B717 FIM 33-50. REPLACED EMERGENCY BATTERY FOR POWER SUPPLY B5-230 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #5640344)SDR DALA2024061005955Battery Pack · inoperativeDURING SVC CHK FOUND R FWD AND L FWD OVERWING EXIT IDENTIFIER INOPERATIVE. T/S PER B717 WD 33-51-14, FOUND BATTERY PACK B5-118 INOPERATIVE. REPLACED BATTERY PACK PER B717 AMM 33-51, OPERATIONAL CHECK WAS GOOD. (LP #5958700)SDR DALA2024061105984Doubler · damagedRT WING LE REFUEL PANEL DOOR CUTOUT JAMB DOUBLER DAMAGED AT BOTH CENTER LATCH LAND LOCATIONS. CUTOUT DAMAGED AT BOTH CENTER LATCH LAND LOCATIONS PER B717 SRM 57-40-01-2R PROCEDURE 3 FIG 3 SHT 1. PERFORMED HFEC IAW B717 PER B717 SRM 57-40-01-2R PROCEDURE 3 AND SDR DALA2024061005958Door · bentON ARRIVAL FOUND FUEL SELECTOR PANEL DOOR BENT OPEN. DAMAGE TO THE SLAT SEAL, DAMAGE TO FUEL SELECTOR PANEL, AND DAMAGE TO THE GUARDED SWITCHES. ALL REFUEL ASSOCIATED LATCHES WERE FOUND OPEN / UNLATCHED. REPLACED GUARDED SWITCHES IAW B717 AMM 28-21-14. REPAIRESDR DALA2024061306057Beam · crackedCRACKS ON INTERNAL BEAM #1 AT AFT CABIN BULKHEAD DOOR (CPAX). SUMMARY OF NRC 00356: INTERNAL BEAM #1 (UPPER WEB) AT AFT CABIN BULKHEAD DOOR (CPAX) WAS FABRICATED AND REPLACED PER DWG 9915565 REV BD, B717-200 SRM 51-41-01-0G, 51-41-02-0G, AND 51-41-05-0G. (LP #SDR DALA2024061005956Actuator · faultedSHIP 9504 -GEAR/DE- ON APPROACH FOR LANDING THE FLIGHT CREW RECEIVED AN "NLG UNSAFE" INDICATION AFTER SELECTING THE GEAR TO EXTEND. THE QRH WAS COMPLIED WITH, AN EMERGENCY WAS DECLARED, AND THE ALTERNATE GEAR EXTENSION PROCEDURES WERE PERFORMED. THE NOSE LANDISDR DALA2024061005954Bolt · missingNLG LOCK LINK ASSY FOUND UPPER PIN RT I/B BOLT MISSING, LT I//B DAMAGED, AND PROTRUDING WITH EMANATING CORROSION ON UPPER LOCK LINK PIN REF B717 IPC 32-22-01-01. FOUND BOTH BOLTS REF B717 IPC 32-22-01-01 TO BE SHEARED AND PIN DAMAGED. FOUND NO SEALANT WITH TRASDR DALA2024081908240Skin · damagedLIGHTING STRIKE R/H O/B ELEVATOR. C/W REP CHK PER ERA 618187-14 REV A SECTION 2. NO FURTHER DAMAGE FOUND ON RIGHT ELEVATOR. OK TO CONT ON MON. TIME LIMITS FOR SECTION I: TIME LIMITED REPAIR EXTENDED FROM 24 DAYS TO 34 DAYS PER ER/A 618187-14 REV B. ASSOCIATEDSDR DALA2024060705877Skin · damagedFUSELAGE SKIN DAMAGED BETWEEN STA 954 AND 974 LONGERON 20L AND 21L. COMPLIED WITH STEPS 1-3 PER RI 618607-14. PERFORMED HFEC PER RI 618607-14 STEP 4 W/ NO DEFECTS NOTED. COMPLIED WITH STEPS 5 & 6 PER RI 618607-14. ADDITIONAL INFORMATION: STEPS 1-3, 5-6 PERFORMSDR DALA2024060605813B-Nut · looseSHIP 9586 -ATB/HYD/DE- THE CREW RETURNED THE AIRCRAFT BACK TO MSP AND DECLARED AN EMERGENCY WITH ATC DURING THE APPROACH DUE TO THE LOSS OF THE RIGHT HYDRAULIC SYSTEM FLUID QUANTITY. THE LANDING GEAR WAS EXTENDED USING THE ALTERNATE GEAR EXTENSION PROCEDURES. SDR DALA2024060605812Stringer · corrodedCORROSION AT APPROX STATION 1053 ON STRINGER 26. RIVETS POPPED WITH SKIN PROTRUDING. REMOVED STR END FITTING AT STR 26 STA 1053 FOUND TO BE 100% LOSS. OUT OF LIMITS. INSPECTED AREA AFTER END FITTING REMOVAL, NO ADDITIONAL CORROSION FOUND. LOCATED, DRILLED, ALOSDR HALA2024060529Window Frame · corrodedLH SIDE CABIN WINDOW: WINDOW #16 HAS CORROSION. FWD SIDE OF WINDOW (MARKED)M66 SUBMITTED. REPAIRED PER E105-494100-PERM.SDR DALA2024060505796Pan · crackedCRACK ON PAN BTW 5 AND STOP FITTINGS NBR 5 OF AFT CARGO DOOR. SUMMARY OF NRC 00781: INNER PAN ON BEAM 5 AT AFT CARGO DOOR WAS REPAIRED PER ERA 617933-14. REV ORIGINAL AND PRI 617933-14 REV 2 ASSOCIATED ER/A 14-617933 ADDED FOR AC 9536. (LP #0376682)SDR DALA2024060505795Lug · corrodedCORROSION ON FITTING LUGS OF ELEVATOR HINGE EYEBOLT STA XHS=50 AROUND BUSHINGS, WAS FOUND ON LH AND RH SIDE. SUMMARY OF NRC 00775: ELEVATOR HINGE EYEBOLT STA XHS=50 ON LH AND RH SIDE WERE REPAIRED PER ER/A 618032-14 REV ORIGINAL SECTION I: PERMANENT REPAIR ANDSDR DALA2024060405771Engine · stalledSHIP 9546 -DIV/IFSD/DE- THE FLIGHT CREW NOTED THAT THE #1 ENGINE STALLED MULTIPLE TIMES IN FLIGHT WHICH RESULTED IN A "LT ENG SYS FAIL" MESSAGE. FLIGHT CREW SHUT DOWN THE ENGINE PER THE QRH, THEY DECLARED EMERGENCY WITH ATC, AND DIVERTED THE AIRCRAFT TO LAND ASDR DALA2024060305739Battery Pack · inoperativeON SERVICE CHECK, MAINTENANCE FOUND THAT BOTH OF THE FWD OVERWING UPPER EMERGENCY EXIT LIGHTS WERE INOPERATIVE. THE #6  EMERGENCY LIGHT BATTERY PACKS WERE REPLACED REF B717 AMM 33-51-04. OPERATIONAL CHECK WAS GOOD. (LP #5891524)SDR DALA2024060305737Jackscrew · corroded-AD- FOUND CORROSION ON LOWER JACKSCREW THREADS APPROX 6"ABOVE LOWER STOP. SUMMARY SEE NRC 006-0001:2740-01114-05 /002 00007: REPLACED JACK SCREW PER AMDS 2740-01114-05. CLOSING REQUIREMENTS RII: INSPECTOR 00260220. (LP #0373180)SDR DALA2024060305738Battery Pack · inoperativeTHE FORWARD DOOR LEVER EXIT SIGN IS NOT ILLUMINATING. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY PACK REF B717 AMM 33-61. OPERATIONAL TEST WAS GOOD. (LP #5920917)SDR DALA2024053105689Fuel Tank · corroded-AD- CORROSION ON THE LOWER SKIN OF THE CENTRAL TANK APPROX STA Y=748 AND STA XCW=-25 AND Z=-29 IN THE FRONT WALL ON RH MLG WHEEL WELL. SUMMARY OF NRC 00777: LOWER SKIN OF THE CENTRAL TANK APPROX STA Y=748 AND STA XCW=-25 AND Z=-29 IN THE FRONT WALL ON RH MLG SDR DALA2024053105690Cover · missingTHE EMERGENCY LIGHT COVER BY THE FWD LAVATORY IS MISSING. MAINTENANCE INSTALLED THE CEILING LENS REF B717 AMM 33-51. (LP #6015231)SDR HALA20240528028Compressor · stalledLEFT ENG COMPRESSOR STALL. REMOVED ENG1 BOOSTER BLEED VALVE (BBV) PER AMM 75-32-01 5/26/24 24713. INSTALLED BOOSTER BLEED VALVE IN SERVCABLE CONDITION ON #1 ENG PER AMM 75-32-01 UP TO STEP F.2.(E). REMOVED #1 ENG SN 13438 PER HAL TASKCARD E1128-717-72-0003-REMSDR HALA20240528027Compressor · stalledENG R COMP STALL IN CRUISE. COMPLIED WITH QRH PROCEDURE. "ENGINE VIB HI" AT HIGH POWER SETTINGS. PREPPED FOR BOROSCOPE INSP. PER AMM 72-00-00-200-801 TO STEP 2E(7). REMOVED 5 BYPASS PANEL AND 4 OF THE CORE COMPRESSOR PANELS PER FOM. 20807. COMPLETED BORESCO
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