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 DALA2025022101363Web · corrodedCORROSION OUT OF LIMITS FOUND AT WEB STA 200 TO STA 216 X=25 TO X=54. SUMMARY OF NRC 00492: CORROSION LEVEL 2. WEB STA 200 TO STA 216 X=25 TO X=54 WAS FABRICATED PER DWG 9910078 REV JC. AND REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-08-0G. (LP #0821476)SDR DALA2025032602224Not Reported · not reported-AD- DAMAGE TOLERANCE EVALUATION, ER/A 622334-14 SECT II WITH AMOC TO AD 2024-21-01. DTA MONITOR INSPECTION REQUIRES DTA / AMOC APPROVAL BEFORE THE 1ST OF 30 DAYS OR 177 CYCLES. CONTACT MSP LIAISON ENGINEERING. DISCONTINUE REVENUE SERVICE ON OR BEFORE 30 DAYS SDR DALA2025022101362Web · corrodedCORROSION ON WEB BTW STA Y=225 TO STA Y=228 X=56 AT FWD CABIN PASSENGER. SUMMARY OF NRC 00280: CORROSION LEVEL 2. CUSP WEB STA 216 TO 237 X=45 TO X=57 WAS FABRICATED PER DWG 993053 REV CF. AND WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #082SDR DALA2025022101359Pan · crackedCRACK WAS FOUND ON AFT SIDE ON BEAM 4 OUTER PAN AT FWD CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00508: AFT SIDE ON BEAM 4 OUTER PAN AT FWD COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0819812)SDR DALA2025022001286Cusp Web · corrodedCORROSION ON CUSP WEB, REWORKED AREAS AT X=58 STA 866 AND STA 840-847 WAS FOUND OUT OF LIMITS WITH MINIMUM REMAINING THICKNESS OF 0.010IN PER B717 SRM 53-00-55-1A PROCEDURE 1 ALLOWABLE DAMAGE 1 PAR 4.C. FIG 101. SUMMARY OF NRC 00531: CORROSION LEVEL 2. CUSP WESDR DALA2025022101361Fastener · loose-AD- LOOSE FASTENERS OF RH VERTICAL STABILIZER LEADING EDGE STRUCTURE SPLICE (STA ZFS=52.267) WERE FOUND IN REFERENCE TO AMDS 5530-01048-02 STEP 3 "AA 5530-01048" AND "AD 2018-10-08". SUMMARY OF NRC 00058: FASTENERS (5 EA) OF RH VERTICAL STABILIZER LEADING EDGSDR DALA2025022101360Door · damagedC-1 FWD CARGO DOOR HAS EXCESSIVE DAMAGE. REPLACED FWD CARGO DOOR. LOG CREATED FOR PARTS CHANGE DOCUMENTATION. INSTALLED ON ROUTINE CARD 5231-4003. (LP #0818827)SDR DALA2025022001287Lock Link Assy · damagedSHIP 9524 -IFSD/DE- THE CREW RECEIVED A "LEFT REVERSER UNLOCK" MESSAGE. THE QRH WAS COMPLIED WITH, WHICH INCLUDED SHUTTING DOWN THE LEFT ENGINE. CORRECTIVE ACTION: MAINTENANCE REPLACED THE #1 ENGINE OUTBOARD UPPER AND LOWER LOCK LINK ASSEMBLY. THEY ALSO REPLACSDR DALA2025021801196Seat Track · corrodedCORROSION OUT OF LIMITS IN REF NRC 188: CORROSION ON SIDE TRACK (RH) BWT STA 644 TO 648 SEAT TRACK FLANGE: WITH ORIGINAL THICKNESS =0.060" AND MINIMUM REMAINING THICKNESS IS 0.025". THEREFORE, IT IS OUT LIMITS PER B717-200 SRM 53-20-52-1A PROCEDURE 2 ALLOWABLESDR DALA2025021801197A/C Pack · smokeSHIP 9585 -ATB/SMKE/DE- THE CREW RETURNED THE FLIGHT BACK TO SDF DUE TO VISIBLE SMOKE AND ODOR IN THE MAIN CABIN. CORRECTIVE ACTION: MAINTENANCE ISOLATED THE SOURCE TO THE LEFT PACK SYSTEM WITH APU OR ENGINE AIR. PLACED LEFT PACK ON MEL. (LP #6779456)SDR HALA20250218008Pump · faulted"INFO TO MX" RTO;BTB TAKEOFF AND THROTTLE ADVANCE LEFT ENGINE N1 STAGNANT. L ENGINE N1 AT 25 WHEN R ENGINE AT N1 55. REMOVED AND REPLACED FUEL PUMP ENG #1 REF AMM 73-12-01. LEAK CHECK FAIL. FUEL PUMP LEAKING (BAD FROM STOCK) S/N #0431. REMOVED BAD FUEL PUMP ATSDR DALA2025021801198Autopilot Sys · failedSHIP 9578 -DIV/DE- THE CREW DECLARED AN EMERGENCY WITH ATC AND DIVERTED THE AIRCRAFT TO JAX (VFR) DUE TO LOSS OF AUTOPILOT AND LATERAL ROLL MODE GUIDANCE ON APPROACH FOR LANDING AT ATL (IMC). CORRECTIVE ACTION: MAINTENANCE REPLACED THE GLARE SHIELD CONTROL PANSDR DALA2025021801195Skin · dentedPERFORM PERMANENT REPAIR DUE TO DENT ON EXTERNAL SKIN OF AFT CARGO DOOR LOWER EDGE 7 INCH FROM AFT EDGE. SUMMARY OF NRC 00299: EXTERNAL SKIN OF AFT CARGO DOOR LOWER EDGE 7 INCH FROM AFT EDGE WAS REPAIRED PER B717-200 SRM 52-00-01-02R PROCEDURE 8 REPAIR 8 FIGURSDR DALA2025021801201A/C Pack · odorSHIP 9585 -ATB/SMKE/DE- THE FLIGHT CREW AND CABIN CREW BOTH REPORTED SMOKE IN COCKPIT AND CABIN SOON AFTER TAKEOFF. AN EMERGENCY WAS DECLARED WITH ATC AND THE AIRCRAFT RETURNED TO ATL. CORRECTIVE ACTION: MAINTENANCE FOUND ODOR FROM PACKS WHEN RUNNING OFF APU BSDR DALA2025021801199Transmitter · out of toleranceSHIP 9579 -ATB/DE- THE CREW ACCOMPLISHED AN AIR TURN BACK TO ATL DUE TO A "FLAPS DISAGREE" MESSAGE AFTER FLAP AND SLAT RETRACTION. AN EMERGENCY WAS DECLARED WITH ATC. CORRECTIVE ACTION: MAINTENANCE FOUND THE RIGHT FLAP POSITION TRANSMITTER OUT OF TOLERANCE, RESDR DALA2025021801200Oven · contaminatedSHIP 9538 -DIV/SMK/DE- THE FLIGHT CREW NOTED SMOKE IN COCKPIT WHILE ENROUTE TO MCI. AN EMERGENCY WAS DECLARED, AND THE AIRCRAFT WAS DIVERTED TO A NORMAL SAFE LANDING IN ORD. CORRECTIVE ACTION: MAINTENANCE INSPECTED THE GALLEY OVEN CONNECTOR, AND NO TROUBLE WASSDR DALA2025021801194Cable · out of positionTAILCONE DEPLOYMENT SYSTEM CABLE OUT POSITION OF PULLEY STA 1225 IN 2 O'CLOCK POSITION AT AFT ACCESSORY COMPARTMENT. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. SUMMARY OF NRC 00952: CABLE ROSDR DALA2025021401141Cusp Web · crackedCRACK ON CUSP WEB BTW STA Y=218/Y=237 AND X-54/X-44 AND CUSP WEB BTW STA Y=200/Y=218 AND X-54/X-24 AT PAX CABIN. SUMMARY OF NRC 00495: CUSP WEB BTW STA Y=218/Y=237 AND X-54/X-44 AND CUSP WEB BTW STA Y=200/Y=218 AND X-54/X-24 WERE REPAIRED PER B717-200 SRM 53-0SDR DALA2025021401140Frame · crackedCRACK ON FRAME STA Y=1037, L-17L AND L-17R AT CPAX. SUMMARY OF NRC 00379: FRAME STA Y=1037, L-17L AND L-17R AT CPAX WERE REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #0808878)SDR DALA2025021401139Floor Support · corrodedCORROSION ON FLOOR SUPPORTS (3 EA) BTW STA Y=1022 TO STA Y=1074 AND -X=44 TO -X=56 AT AFT PASSENGER CABIN (W2). SUMMARY OF NRC 00271: CORROSION LEVEL 2. CORRODED FLOOR SUPPORTS (3 EA) BTW STA Y=1022 TO STA Y=1074 AND -X=44 TO -X=56 AT AFT CABIN (W2) WERE REPLASDR DALA2025021401138Floor Support · corrodedCORROSION ON FLOOR SUPPORT BTW STA Y=1022 TO STA Y=1074 AND X=44 AT AFT PASSENGER CABIN (W2). SUMMARY OF NRC 00275: CORROSION LEVEL 2. CORRODED FLOOR SUPPORT BTW STA Y=1022 TO STA Y=1074 AND X=44 AT AFT CABIN (W2) WAS REPLACED PER DWG 9981474-15 REV L AND PER SDR HALA20250213006Compressor · stalledLVL 2- ENG L COMP STALL ON EAD DURING LANDING ( NO OTHER INDICATIONS). PERFORMED FIM 72-00 TASK 803, REMOVED AND REPLACED LH ENG N2 SHARED SPEED PROBE PER AMM 77-12-01, OPS AND LEAK CHECK GOOD. NO DEFECTS NOTED. OK FOR SERVICE.SDR DALA2025021201090None · noneIN REFERENCE NRC 00924: LEVEL AND SHORE AIRCRAFT IN ACORDANCE WITH AMM 07-11-00 AS WELL AS PER FIGURE 4 OF BOEING SERVICE SKETCH 3268E PER PRI 621176-14 REV 0 STEP 1 A) AND PERFORM DAILY CHECK UNTIL REMOVED. SUMMARY NRC 00981: SHORINGS WERE INSTALLED AND VERIFSDR DALA2025030401653Access Panel · missingLH WING LANDING LIGHT TOOLING ACCESS COVER MISSING. MAINTENANCE DEFERRED IT TO MONITOR PER ERA 607941-14TR REV ORIGINAL. C/W TEMP REPAIR PER SECTION I. ENGINEERING APPROVED REPAIR PER DAL P.S. 900-5-1, #04. REPETATIVE CHECK DUE EVERY 50 FLIGHT HOURS, TERMINATISDR DALA2025021201092Support · corrodedAFT CARGO DOOR INNER SUPPORT AT LOWER END IS CORRODED. SUMMARY SEE NRC 001-0467:2000-1002/191 00296: CORROSION LEVEL 1. AFT CARGO DOOR WAS REPLACED ON NRC 293. (LP #0806189)SDR DALA2025021201091Light · unknownTHE F/A REPORTED THAT THE EXIT ROW EMERGENCY LIGHT ILLUMINATED IN FLIGHT. MAINTENANCE PERFORMED A TEST OF THE EMERGENCY LIGHT SYSTEM AND NO FAULTS WERE FOUND. ALSO, THERE IS NOT ANY HISTORY OF EMERGENCY LIGHTS MALFUNCTIONING IN THE LAST 30 DAYS. ALL CHECKS ARESDR DALA2025021201089Fitting · damagedPERFORM COLDWORK ON INBOARD BRACE FITTING DOUBLER XRS=164 AT LH WING. SUMMARY OF NRC 00924: INBOARD BRACE FITTING DOUBLER XRS=164 AT LH WING WAS REPAIRED PER PRI 621176-14 REV 10 AND ERA 621176-14AD REV ORIGINAL SECTION I: PERMANENT REPAIR. ALSO FAIRING WAS RESDR DALA2025021101060Attach Bracket · cracked-AD- PRI 622371-14AD, REV 3 HOLE #9 ON OUTBOARD FAIRING ATTACH BRACKET HAS CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLACED DURING LEFT WING LOWER SKIN DOUBLER REPAIR ON ER/A 622371-14AD, REV O. JOB COMPLETE. A/C OK FOR SERVICE. (LP #0803598)SDR DALA2025021101059Attach Bracket · cracked-AD- PRI 622371-14AD, REV 3 HOLE #8 ON OUTBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLACED DURING LEFT WING LOWER SKIN DOUBLER REPAIR ON ER/A 622371-14AD, REV O. A/C OK FOR SERVICE. (LP #0803594)SDR DALA2025021101058Attach Bracket · cracked-AD- PRI 622371-14AD, REV 3 HOLE #5 ON OUTBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLACED DURING LEFT WING LOWER SKIN DOUBLER REPAIR ON ER/A 622371-14AD, REV O. JOB COMPLETE. A/C OK FOR SERVICE. (LP #0803588)SDR DALA2025021101057Attach Bracket · cracked-AD- PRI 622371-14AD, REV 3 HOLE #1 ON OUTBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLACED DURING LEFT WING LOWER SKIN DOUBLER REPAIR ON ER/A 622371-14AD, REV O. JOB COMPLETE. A/C OK FOR SERVICE. (LP #0803577)SDR DALA2025021101056Attach Fitting · cracked-AD- PRI 622371-14AD, REV 2 HOLE #6 ON INBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLACED DURING LEFT WING LOWER SKIN DOUBLER REPAIR ON ER/A 622371-14AD, REV O. JOB COMPLETE. A/C OK FOR SERVICE. (LP #0803565)SDR DALA2025021101055Attach Fitting · cracked-AD- PRI 622371-14AD, REV 2 HOLE #5 ON INBOARD FLAP FAIRING ATTACH BRACKET HAS CRACK INDICATION. FLAP FAIRING ATTACH BRACKET REPLCAED DUEING LEFT WING LOWER SKIN DOUBLER REPAIR ON ER/A 622371-14AD, REV O. JOB COMPLETE. A/C OK FOR SERVICE. (LP #0803562)SDR DALA2025021001047Lens · missingTHE FIRST EMERGENCY LIGHT ON CATWALK IN EMPENNAGE IS MISSING THE LENS COVER. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD. (LP #0803705)SDR DALA2025021001046Spar Cap · damaged-AD- AWR, AA, AD, IN REF TO AMDS 5720-01103-01B STEP 7: REPAIR IN PROGRESS AT RIGHT WING LOWER REAR SPAR CAP THATS INCLUDES LOWER WING SKIN AND DOUBLER BTW STA XRS 150 AND XRS 177. SUMMARY OF NRC 00918: THIS REPAIR PROVIDED WITH FAA AMOC APPROVAL AND INCLUDES SDR DALA2025021001045Pan · crackedCRACK WAS FOUND ON INNER PAN OF THE AFT EDGE AT FWD CARGO DOOR. SUMMARY OF NRC-00306: AFT EDGE AT FWD CARGO DOOR CRACK ON INNER PAN WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 3 REPAIR 3. (LP #0800119)SDR DALA2025100807321Hinge Fitting · corrodedIN REFERENCE TO NRC 00309: AFTER REMOVAL SEALANT WAS FOUND CORROSION ON CENTER FLAP HINGE AT LH WING. CENTER WING FLAP HINGE FITTING WAS REMOVED PER B717 AMM 57-55-25-000-802 AND CENTER WING FLAP HINGE (0797513)SDR HALA20250206004Bleed Valve · faultedDIVERSION TO HNL. DURING FLIGHT LEFT BLEED FLUCTUATES FROM 8-67. WITH NO POWER CHANGES FLUCTUATIONS HAPPENING DURING ALL PHASES OF FLIGHT. REMOVED AND REPLACED ENG #1 PRESSURE REGULATOR PILOT VALVE REF AMM 36-12-03. OPS CHECK GOOD. OK FOR SVCSDR DALA2025020500883Lamp · failedTHE LEFT AND RIGHT EXTERIOR EMERGENCY LIGHTS DIM WITH THE SWITCH OFF. THE SYSTEM WAS DEFERRED PER MEL 33-51-02A AND PLACARDS WERE INSTALLED. MAINTENANCE VERIFIED 2232 LAMPS WERE INSTALLED PER B-717 IPC 33-50-30-01 ITEM #130J. (NOTE: LEFT LAMP IS BAD, NASI BWI)SDR DALA2025020500882Battery · no testTHERE ARE MULTIPLE EMERGENCY EXIT LIGHTS INOPERATIVE IN THE AFT CABIN. MAINTENANCE REPLACED THE BATTERIES IN POWER SUPPLY B5-116 AND B5-260 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6411235)SDR DALA2025020500881Door Frame · corrodedCORROSION ON AFT CARGO DOOR JAMB AT AFT CARGO BIN. SUMMARY OF NRC 00064: CORROSION LEVEL 2. THE AFT CARGO DOOR JAMB AT AFT CARGO BIN WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. (LP #0796316)SDR DALA2025020500884Spar · crackedTHE #13 FASTENER HOLE SHOWS A CRACK INDICATION WITH BHEC IN SPAR LAYER. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/024 00024: NR TRANSFERRED TO H-CK PKG#P-384718220250123 - NR# 31. (LP #0795830)SDR DALA2025020500880Spar Cap · crackedA CRACK COMMON TO THE RH WING LOWER REAR SPAR CAP. AS A PRECAUTION AN ER/A HAS BEEN ISSUED REQUIRING MAINTENANCE TO ACCOMPLISH INSPECTIONS OF THE LH WING LOWER REAR SPAR CAP TO ENSURE NO CRACKS ARE FOUND. SUMMARY SEE NRC 003-0001:0514-2001/042 00042: NR TRANSFSDR DALA2025020500879Spar · crackedTHE #12 FASTENER HOLE SHOWS A CRACK INDICATION WITH BHEC IN SPAR LAYER. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/028 00028: NR TRANSFERRED TO H-CK PKG #P-384718220250123 - NR# 35. (LP #0795839)SDR DALA2025020500878Spar · crackedTHE #16 FASTENER HOLE SHOWS MULTIPLE CRACK INDICATIONS WITH BHEC IN SPAR AND SKIN LAYERS. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/027 00027: NR TRANSFERRED TO H-CK PKG#P-384718220250123 - NR# 34. (LP #0795837)SDR DALA2025020500877Spar · crackedTHE #15 FASTENER HOLE SHOWS MULTIPLE CRACK INDICATIONS WITH BHEC IN SPAR AND SKIN LAYERS. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/026 00026: NR TRANSFERRED TO H-CK PKG#P-384718220250123 - NR# 33. (LP #0795835)SDR DALA2025020500876Skin · crackedTHE #14 FASTENER HOLE SHOWS MULTIPLE CRACK INDICATIONS WITH BHEC IN SPAR AND SKIN LAYERS. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/025 00025: NR TRANSFERRED TO H-CK PKG#P-384718220250123 - NR# 32. (LP #0795831)SDR DALA2025020500875Spar · crackedTHE #11 FASTENER HOLE SHOWS A CRACK INDICATION WITH BHEC IN SPAR LAYER. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/023 00023: NR TRANSFERRED TO H-CK PKG#P-384718220250123 - NR# 30. (LP #0795829)SDR DALA2025020500874Spar · crackedTHE #10 FASTENER HOLE SHOWS MULTIPLE CRACK INDICATIONS WITH BHEC IN SPAR LAYER. RH WING REAR SPAR LOWER SURFACE. MARKED. SUMMARY SEE NRC 003-0001:0514-2001/022 00022: NR TRANSFERRED TO H-CK PKG#P-384718220250123 - NR# 29. (LP #0795826)SDR DALA2025020500873Spar Cap · cracked-AD- CRACK COMMON TO THE RH WING LOWER REAR SPAR CAP, COMMON TO THE RH WING REAR SPAR INST AT APPROXIMATELY 5.0" INBD OF XRS 164.000. THE MAIN CRACK MEASURES APPROXIMATELY 0.945" LONG, TERMINATING AT A FASTENER LOCATION. COMPLY WITH RH WING / LOWER REAR SPAR C
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