Boeing 717-200
Service difficulty reports · 18,771
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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 DALA2023010308523Web · corrodedCORROSION ON WEB AT LWR SILL AREA BTW STA Y=946-954 PROJECTION LONG 28R-29R OF AFT CARGO COMPARTMENT. CORROSION LEVEL 2. WEB AT LWR SILL AREA BTW STA 946 TO STA 1002 PROJECTION LONG 28R-29R OF AFT CARGO WAS REPLACED IAW SRM 51-41-01-0G, SRM 51-41-02-0G PAR 4,SDR DALA2022123008501Door Frame · corrodedCORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT DOOR (C2). LOWER DOOR JAMB AT AFT CARGO COMPARTMENT DOOR WAS REPLACED IAW SRM 53-20-15- 2R REPAIR 7, SRM 51-40-02-0G, SRM 51-41-05-0G, AND SRM 51-41-01- 0G.SDR DALA2022123008503Battery Pack · inoperativeTHE EMERGENCY LIGHTS ON THE GALLEY OVERHEAD, AT SEATS 1-14, AND AT SEATS 24-29 ARE INOPERATIVE. MAINTENANCE FOUND BAD BATTERY PACKS AND BATTERY RACKS AT B5- 259, B5-227, AND B5-120. ALL WERE REPLACED PER AMM 33-51. OPERATIONAL CHECKS WERE GOOD. OK FOR SERVICESDR DALA2022123008502Battery Pack · inoperativeTHE OVERWING EMERGENCY EXIT LIGHTS AT ROW 20 ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK AT SEAT ROW 20 IAW AMM 33-51. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE.SDR DALA2022123008500Seat Track · corrodedSEAT TRACK SECTION X=-56 BTW STA=479 WAS FOUND CORRODED OUT LIMITS. SEAT TRACK SECTION X=-56 BTW STA=479 WAS REPAIRED IAW SRM 53-20-52-2R REP. 1 FIG. 201.SDR DALA2022122908460Seat Track · corrodedRIGHT SEAT TRACK SECTION X=-44 BTW STA Y=210 TO Y=275 WAS FOUND CORRODED OUT LIMITS. SUMMARY OF NRC 00503: CORROSION LEVEL 2. RH SEAT TRACK SECTION X =-44 BTW STA Y=218 TO Y=342 WAS REPAIRED PER B717-200 SRM 53-20 -52-2R PROCEDURE 5.SDR DALA2022122908459Seat Track · crackedAFTER REMOVAL RH SEAT TRACK SECTION X=-44 BTW STA Y= 218 TO Y=342 A CRACK WAS FOUND IN THE CUSP WEB AT STA Y=294 TO Y=300. SUMMARY OF NRC 00516: CUSP WEB STA Y=294 TO Y=300 WAS PERMANENTLY REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG. 222. (LP #2558235)SDR DALA2022122908458Seat Track · corrodedIN REF TO NRC 00325: SEAT TRACK SECTION X=-56 BTW STA=920 TO STA=922 WAS FOUND CORRODED OUT LIMITS. SUMMARY OF NRC 00496: CORROSION LEVEL 2. SEAT TRACK SECTION X=- 56 BTW STA=920 TO STA=922 WAS REPAIRED PER ER/A 604805-14 SECTION I PERMANENT REPAIR REV ORIGINASDR HALA2022123000014Frame · corrodedFRAME TEE CORRODED AT LT 6:10 POSITION. CLEANED AND TREATED IAW SRM 51-10-04. REMAINING THICKNESS .012. REPAIRED PER E105-485299-PERM.SDR HALA2022123000013Floor Support · corrodedFLOOR SUPPORT WAS FOUND WITH SURFACE CORROSION. REMOVED THE FLOOR SUPPORT. FABRICATED A NEW FLOOR SUPPORT IAW DWG 9936534 AND INSTALLED.SDR DALA2022122908461Pan · wornWEAR ON SKIN PAN NEAR TO AFT LATCH FITTING AT AFT CARGO COMPARTMENT DOOR (PTAS). SUMMARY OF NRC 00061: SKIN PAN NEAR TO AFT LATCH FITTING AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 8, REPAIR 8. FIG. 206.SDR DALA2022122908457Longeron · crackedCRACK ON LOGERON 2LH ON STA Y=1144 AT AFT ACCESSORIES COMPARTMENT (CAT). SUMMARY OF NRC 00469: LONGERON 2LH ON STA Y=1144 AT AFT ACCESSORIES COMPARTMENT WAS REPAIRED PER B717 SRM 53-00-05-2R PROCEDURE 2.SDR DALA2022122708379Skin · dentedSEVERAL DENTS ON LOWER SKIN OF RT WING FLAP FIXED VANE, THE SKIN WAS REPAIRED IAW SRM 57-53-01-2R-1, AND SRM 51-70-02-0G.SDR DALA2022122808451Vane · damagedDURING TAP-TEST INSPECTION OF DENTS AT RHS FWD MOVABLE VANE, A DISBONDED AREA OF 4.750 IN LENGTH AND 2.000 IN WIDTH WAS FOUND ON THE RUB STRIP. RT FWD MOVABLE VANE WAS REPAIRED IAW SRM 51-70-02-0G PAR. 15, 17A, AND SRM 57-53-01-2R-1 PAR. 4 D.SDR DALA2022122708380Lens · missingTHE PILOT NOTICED THAT THE EMERGENCY EXIT SIGN WAS MISSING ABOVE THE SERVICE DOOR. MAINTENANCE REATTACHED THE LENSE COVER.SDR DALA2022122708378Web · corrodedCORROSION ON WEB BS 256, X=49. THE WEB WAS REPAIRED IAW SRM 53-00-55-2R-4R.SDR DALA2022122708377Cusp Web · crackedCRACK ON LT CUSP WEB INNER FACE AT BS 898, X=44. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R, REPAIR 4.SDR DALA2022122708376Cusp Web · crackedCRACK IN RT CUSP WEB BTW BS 617-636, X=-53 TO X=-59 IN PASSENGER CABIN. CUSP WEB WAS REPAIRED IAW SRM 53-00-55-2R-4, REPAIR 4.SDR DALA2022122708375Seat Track · corrodedSEAT TRACK X=-22 BTW BS 200-266 WAS FOUND CORRODED OUT LIMITS. SEAT TRACK REPLACED IAW SRM 51-41-01-0G & SRM 51-41-05-0G.SDR DALA2022122308316Angle · corrodedCORRODED OUT OF LIMITS AT CLIPS STA Y=829, Y=875, Y=912. ORIGINAL THICKNESS IS 0.032 IN AND MINIMUM REMAINING THICKNESS IS 0.10 IN, THEREFORE THE AREA IS OUT OF LIMITS IN REF NRC 00376 AT PAX CABIN. CLIPS STA Y=829, Y=875, Y=912 AT PAX CABIN WERE REPLACED PER SDR DALA2022122308315Skin · corrodedLEFT WING UPPER SURFACE: PAINT BUBBLING WITH EVIDENCE OF POSSIBLE CORROSION AT TWO LOCATIONS JUST AFT OF #3 SLAT. REMOVED CORROSION AT XRS 317 STR 2 LH WING AND REPAIRED PER ERA 604553-14 REV O, SRM 57-10-01-1A PROCEDURE 1.SDR DALA2022122308314Skin · corrodedLEFT WING, CORROSION FOUND AROUND FUELING CAP. REMOVED CORROSION AT XRS 425 STR 2 LT WING AND REPAIRED IAW ERA 604553-14 REV O. ASSOCIATED ER/A 14-604553.SDR DALA2022122308313Angle · crackedAFTER SEAL RETAINER REMOVAL, CRACKED INTERNAL ANGLE WAS FOUND ON APROX STA Y=390 AT FWD CARGO DOOR. INTERNAL ANGLE ON AFT LOWER EDGE APROX STA Y=390 AT FWD CARGO DOOR WAS FABRICATED AND REPLACED PER DWG 9957664 REV N, B717-200 SRM 51-30-07-0G, SRM 51-41-05-0GSDR DALA2022122308312Fitting · crackedAFTER SEAL RETAINER REMOVAL, CRACK WAS FOUND ON FITTING. FITTING ON AFT LOWER EDGE AT FWD CARGO DOOR WAS REPLACED IAW SRM 51-41-01-0G AND SRM 51-41-02-0G.SDR DALA2022122208293Web · crackedCRACK ON LH CUSP WEB EDGE AT STA Y=717 AND X =56. SUMMARY OF NRC 00373: LH CUSP WEB EDGE AT STA Y=717 AND X=56 WAS PERMANENTLY REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 FIGURE 203. (LP #2548917)SDR HALA2022122200012Seal · damagedLOUD SQUEAL BY 1L DOOR AIRBORNE IN CRUISE FOR 10 MINUTES THAT WENT AWAY DURING DESCENT. PERFORMED SEAL REPAIR TO FWD LOWER CORNER OF MED PER E105-C10707-INI. DUE TO ACCOMPLISHING E105, PERFOMRED LEAK CHK PER AMM 21-30-00-790-801. NO DEFECTS NOTED. OK TO COMTSDR DALA2022122208295Buckle · dirtyAFT FLIGHT ATTENDANT JUMPSEAT HARNESS BUCKLE WILL NOT RELEASE. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REMOVED DEBRIS FROM THE HARNESS BUCKLE PER B717 AMM 25-23. (LP #9831886)SDR DALA2022122208294Support Rib · wornWORN INBD RIB SUPPORT ON FIXED LEADING EDGE WS XRS 267.000 APPROX AT RH WING. AD. SUMMARY OF NRC 00166: INBD RIB SUPPORT ON FIXED LEADING EDGE WS XRS 267.000 APPROX AT RH WING WAS REPAIRED PER ER/A 604521-14 REV ORIGINAL SECTION 1 PERMANENT REPAIR AND PRI 6045SDR DALA2022122208292Angle · crackedCRACK ON INTERNAL ANGLE LOWER EDGE STA Y=389 APROX AT FWD CARGO COMPARTMENT. (CCD). SUMMARY OF NRC 00048: INTERNAL ANGLE LOWER EDGE STA Y=389 APROX AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 52-30-02 -2R PROCEDURE 1 REPAIR 1. (LP #2548249)SDR DALA2022122108269Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA Y=218 - X=0 (CPAX)(W1). SUMMARY OF NRC 00363: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=218 - X=0 WAS REPLACED PER B717-200 SRM 51-41-02-0G. (LP #2547442)SDR DALA2022122108268Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA Y=200 BTW X=5 AND X=-5 (CPAX)(W1). SUMMARY OF NRC 00335: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=200 BTW X=5 AND X=-5 WAS FABRICATED AND REPLACED PER DWNG 936534 REV BW AND B717-200 SRM 51-41-02-0G. (LP #2547431)SDR DALA2022122108267Support · corrodedCORROSION ON GALLEY SUPPORT STA Y=210 & STA Y=217 - X=-11 (CPAX)(W1). SUMMARY OF NRC 00361: CORROSION LEVEL 2. GALLEY SUPPORT STA Y=210 & STA Y=217 - X=-11 WERE REPLACED PER B717-200 SRM 51-41-02- 0G. (LP #2547311)SDR DALA2022122008238Web · puncturedPUNCTURE ON WEB STA Y=217 - X=-11 WAS FOUND DURING REMOVAL OF GALLEY SUPPORT ON NRC 00361. (CPAX)( W1). SUMMARY OF NRC 00456: WEB STA Y=217 - X=-11 WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2. PAR 4 FIG. 201. (LP #2545920)SDR DALA2022122008237Floor Support · corrodedSECONDARY NRC, IN REF NRC 00364: AFTER REMOVAL PARTS TO ATTEND DISCREPANCY, CORROSION ON FLOOR SUPPORT STA Y=200 AND X=-55 WAS FOUND AT PASSENGER CABIN FLOOR AREA. SUMMARY OF NRC 00462: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=200 AND X=-55 WAS REPLACED PER B717SDR DALA2022122008239Pseu · failedSHIP 9513- MISC/DE - WHILE ON APPROACH FOR LANDING THE CREW NOTED THE MASTER CAUTION WITH EICAS MESSAGE OF "PSEU FAIL". WHICH REQUIRED A NO SLAT / NO FLAP LANDING BE ACCOMPLISHED. THE CREW DID DECLARE AN EMERGENCY WITH ATC AND COMPLIED WITH THE QRH. CORRECTIVESDR DALA2022121908181Frame Angle · puncturedPUNCTURE ON FRAME CLIP STA Y=908 BTW LONGERON 29R-30 AFT CARGO COMPARTMENT (C2) IN REF 00227. SUMMARY OF NRC 00261: FRAME CLIP WAS REPLACED PER B717-200 SRM 53-20-07-0I. (LP #2544352)SDR DALA2022121908180Frame · corrodedCORROSION AT FRAME STA Y=974 BTW LONGERON 29R-30 AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00223: LEVEL CORROSION 2. FRAME STA Y=974 BTW LONGERON 29R-30 WAS REPAIRED PER B717-200 SRM 53-20-07-0G REPAIR 3. (LP #2544348)SDR DALA2022121908173Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA Y=180 BTW X=-9 - X=-42. CORROSION LEVEL 2. FLOOR SUPPORT WAS REPLACED IAW SRM 51-41-02-0G AND B717-200 SRM 51-41-05-0G.SDR DALA2022121908179Door Frame · corrodedCORROSION ON LOWER DOOR JAMB EXTRNAL SURFACE FROM STA 370 TO 427 AT FWD CARGO COMPARTMENT (CCD). SUMMARY LEVEL CORROSION 2. DOOR JAMB EXTRNAL SURFACE FROM STA 370 TO 427 WAS REPLACED PER B717-200 51-40-08-0G PAR 3 AND SRM 51- 41-02-0G AND 51-41-05-0G. (LP #254SDR DALA2022121908178Door Frame · corrodedCORROSION ON AFT CARGO COMPARTMENT DOOR JAMB REPAIR DOUBLER AT STA Y=954 BTW LONGERON PROJECTION 27RH AND 26RH. SUMMARY OF NRC 00138: CORROSION LEVEL 2. AFT CARGO COMPARTMENT DOOR JAMB REPAIR DOUBLER AT STA Y=954 BTW LONGERON PROJECTION 27RH AND 26RH WAS REPLASDR DALA2022121908177Skin · crackedCRACK ON EXTERNAL SKIN ABOVE LONGERON 15 RH AND STA 1087 AT FUSELAGE. SUMMARY OF NRC 00026: CRACK ON EXTERNAL SKIN ABOVE LONGERON 15 RH AND STA 1087 AT FUSELAGE WAS REPAIRED PER PRI 604254-14 REV 4 AND PER ER/A 604254-14 REV ORIGINAL, SECTION I: PERMANET REPAISDR DALA2022121908176Floor Support · corrodedCORROSION ON FLOOR SUPPORT STA Y=160-200 X=-44 (CPAX)(W1). SUMMARY OF NRC 00338: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=160-200 X=-44 (CPAX)(W1) WAS FABRICATED AND REPLACED PER DWG 9936534 -71 AND B717-200 SRM 51-41-02-0G PAR 4 AND SRM 51-41-05-0G PAR 8. (LP #SDR HALA2022122100011Control Unit · malfunctionedATB - ANTI SKID FAIL ALERT ON APPROACH WITH LANDING GEAR IN DOWN POSITION. AIR TURN BACK TO HNL. PERFORMED FIM 32-45 TASK 807 - NO FAULTS. PERFORMED AMM 32-45-00-741-001 ANTI-SKID SHUT-OFF VALVE TEST - NO FAULTS. REMOVED AND REPLACED BCU PER AMM 32-45-01-000SDR DALA2022121908182Battery Pack · no testDURING PRE-FLIGHT CHECK, FOUND BOTH AFT EMERGENCY OVER WING EXIT LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AT B5-119 IAW B717 AMM 33-51. OPERATIONAL CHECK WAS NORMAL. (LP #9509744)SDR DALA2022121908175Floor Support · corrodedCORROSION OUT OF LIMITS ON FLOOR SUPPORT AT STA Y=160-195. ORIGINAL THICKNESS IS 0.071 IN AND MINIMUM REMAINING THICKNESS IS 0.025 IN, THEREFORE THE AREA IS OUT OF LIMITS IN REF NRC 00352 AT PAX CABIN (CPAX)(W1). SUMMARY OF NRC 00457: CORROSION LEVEL 2. FLOOR SDR DALA2022122008236Doubler · corrodedCORROSION ON RH REPAIR DOUBLER BTWN STA 908 TO STA 927 AND FROM X=44 TO X=59 OF PASSENGER CABIN FLOOR. SUMMARY OF NRC 00333: CORROSION LEVEL 2. PREVIOS REPAIR DOUBLER BTW STA 908 TO STA 927 AND FROM X=-44 TO X=-59 OF FLOOR CABIN PASSENGER WAS REPLACED PER B-71SDR DALA2022121908174Floor Support · corrodedCORROSION ON FLOOR SUPPORT AT RBL 7 STA 192-200. SUMMARY SEE NRC 001-0010 2500-2647/058 00306: REPLACED FLOOR SUPPORT REF B-717 DWG 9936534. (LP #2540869)SDR DALA2022121608150Beam · crackedCRACK OF AFT EDGE OF BEAM NO 1 AT STA Y=199 AT FWD PASSENGER DOOR. (L1) SUMMARY OF NRC 00063: CRACK OF AFT EDGE OF BEAM NO 1 AT STA Y=199 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #2539977)SDR DALA2022121608149Pan · crackedCRACK ON UPPER PAN WAS FOUND IN REFERENCE NRC 0063. SUMMARY OF NRC 00256: CRACK ON UPPER PAN WAS REPAIRED PER B717- 200 SRM 52-10-02-2R PROCEDURE 3 REPAIR 3. (LP #2539972)SDR DALA2022121508126Skin · crackedCRACK ON LOWER EDGE OF FWD PASSENGER DOOR EXTERNAL SKIN BS 167. EXTERNAL SKIN STA Y=167 OF LOWER EDGE AT FWD PASSENGER DOOR (L1) WAS REPAIRED PER B717-200 SRM 52-10-01- 2R REPAIR 1 PROCEDURE 1 PAR. 4.
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