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 DALA2024032503734Skin · crackedCRACK ON SKIN STA Y=370 BTW L20 AND L22 APROX AT FWD DOOR CARGO COMPARMENT. SUMMARY OF NRC 00227: SKIN STA Y=370 BTW L20 AND L22 APROX AT FWD DOOR CARGO COMPARMENT WAS REPAIRED PER PRI 616337-14 REV 0 AND ERA 616337-14 REV ORIG SECTION I: PERMANENT REPAIR. ASSSDR DALA2024032303707Cylinder · faultedSHIP 9584 -ATB/GEAR/DE- FOLLOWING TAKEOFF AND LANDING GEAR RETRACTION, THE CREW RECEIVED A "LEFT MAIN GEAR UNSAFE" MESSAGE. AN EMERGENCY WAS DECLARED, AND THE CREW RETURNED THE AIRCRAFT TO ATL AND LANDED WITHOUT FURTHER INCIDENT. CORRECTIVE ACTION: MAINTENANCESDR DALA2024032303705Web · corrodedCORROSION ON WEB BTW Y=200 TO Y=208 X=56. SUMMARY OF NRC 00734: CORROSION LEVEL 2. CORROSION ON WEB BTW Y=200 TO Y=208 X=56 WAS REPAIRED PER PRI 616504-14 REV. 1 AND ERA 616504-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ERA 14-616504 ADDED FOR AC SDR DALA2024032303704Pan · crackedCRACK ON PAN FWD UPPER CORNER AT FWD CARGO COMPARMENT DOOR. SUMMARY OF NRC 00155: PAN FWD UPPER CORNER AT FWD CARGO COMPARMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 1. (LP #0257725)SDR DALA2024050805017Aileron · unknown-AD- PERFORM BALANCE PROCEDURE ON AILERON LH. SUMMARY OF NRC 00770: AILERON LH BALANCE PROCEDURE WAS PERFORMED PER B717-200 SRM 51-60-01-0G, ALSO AILERON LH WAS REMOVED / INSTALLED PER B717-200 AMM 27-10-01. ADJUSTMENT / TEST OK; AILERON CONTROL TAB L/H WAS RESDR DALA2024050805016Web · damagedELONGATED HOLES ON WEB BTW STA 370 TO 360 AND LONGERONS 24 RH TO 26 RH AT CUT OUT FORWARD CARGO COMPARTMENT DOOR (CCD). SUMMARY OF NRC 00131: WEB BTW STA 370 TO 360 AND LONGERONS 24 RH TO 26 RH AT CUT OUT FORWARD CARGO COMPARTMENT DOOR (CCD) WAS REPAIRED PER BSDR DALA2024032303703Skin · crackedCRACKS ON SKIN WERE FOUND AFTER REMOVAL STOP FITTING ON AFT EDGE BEAM 2 APROX. SUMMARY OF NRC 00531: SKIN ON AFT EDGE BEAM 2 APROX WAS REPAIRED PER PRI 615938-14 REV 1 AND ERA 615938-14 REV ORIG SECTION I: PERMANENT REPAIR. ASSOCIATED ERA 14-615938 ADDED FOR ASDR DALA2024032303702Rib · wornWEAR ON RIBS (3 EA) BETWEEN STA XIS 174 TO XIS 186 INSIDE FIXED LEADING-EDGE AT LH WING. SUMMARY OF NRC 00621: RIBS (3 EA) BETWEEN STA XIS 174 TO XIS 186 INSIDE FIXED LEADING-EDGE AT LH WING WERE REPAIRED PER ERA 616112-14 REV ORIG SECTION 1 PERMANENT REPAIR. SDR DALA2024032203636Frame · corrodedCORROSION WAS FOUND ON PREVIOUS REPAIR SPLICES AND FRAME, STA Y=927 LONGERON 29LH TO 29RH AT AFT CARGO COMPARMENT. SUMMARY OF NRC S/N 00339: CORROSION LEVEL 2. FRAME STA Y=927 LONGERON 29LH TO 29RH AT AFT CARGO COMPARMENT CORROSION WAS REMOVED PER B717-200 51-SDR DALA2024032203635Seat Track · corrodedCORROSION ON RH SEAT TRACKS X-54.0 BTW STA Y=200-256 AT PAX CABIN. SUMMARY OF NRC 00493: CORROSION LEVEL 2. RH SEAT TRACKS X-54.0 BTW STA Y=200-256 AT PAX CABIN WAS REPAIRED PER B717 SRM 53-20-52-2R PROCEDURE 5. (LP #0256135)SDR DALA2024032203634Beam · crackedCRACK ON BEAM 1 LH EDGE AT AFT CABIN PRESSURE BULKHEAD. SUMMARY OF NRC 00097: WEB WAS REPLACED PER B717-200 SRM 51-41-05-0G, 51-41-02-0G, AND DWG 9915565 REV BD. (LP #0256085)SDR DALA2024032203633Skin · corrodedCORROSION ON INTERNAL SKIN AND CUT OUT OF FWD AIR STAIRWELL DOOR. SUMMARY OF NRC 00109: FWD AIR STAIRWELL DOOR WAS REPLACED PER B717-200 AMM 52-63-01. (LP #0255910)SDR DALA2024032203632Skin · crackedCRACKS ON FUSELAGE SKIN (2 EA) ON STA Y1154 BTW L3 LH AND L3 RH (UPPER SECTION) AT FUSELAGE. SUMMARY OF NRC 00072: FUSELAGE SKIN ON STA Y1154 BTW L3 LH AND L3 RH (UPPER SECTION) WAS REPAIRED PER ERA 615858-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. REPETITIVSDR DALA2024032203631Frame · crackedCRACK ON FRAME STA Y=1037 BTW LONG 14 RH AND 15 RH AT CABIN PAX. SUMMARY OF NRC 00386: FRAME STA Y=1037 BTW LONG 14 RH AND 15 RH AT CABIN PAX WAS REPAIRED PER ERA 616076-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 616076-14 REV 3. (LP #0255676)SDR DALA2024032203630Cusp Web · crackedCRACK ON RH CUSP WEB STA X=-56 TO -60 AND Y=1012 AT PASSENGER CABIN. SUMMARY OF NRC 00514: RH CUSP WEB STA X=-56 TO -60 AND Y=1012 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R. (LP #0255600)SDR DALA2024032103594Diaphragm · corrodedCORROSION ON RIGHT DIAPHRAGM ON STA X=-44 AND X=-56 FROM STA Y 200 TO Y 218 AT W1 AREA. SUMMARY OF NRC 00697: CORROSION LEVEL 2. RIGHT DIAPHRAGM ON STA X=-44 AND X=-56 FROM STA Y 200 TO Y 218 AT W1 AREA WAS REPLACED PER DWG 9936535 REV CS, PER B717-200 SRM 51-SDR DALA2024032103593Guide Vane · puncturedPUNCTURE ON AFT MOVABLE GUIDE VANE AT RH WING. SUMMARY OF NRC 00042: AFT MOVABLE GUIDE VANE AT RH WING WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 AND 51-70-02-0G PROCEDURE GENERAL. (LP #0254635)SDR DALA2024032103592Window Frame · crackedCRACK ON UPPER AFT CORNER CUTOUT OF LH SLIDING WINDOW, AT COCKPIT. SUMMARY OF NRC 00439: UPPER AFT CORNER CUTOUT OF LH SLIDING WINDOW AT COCKPIT WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 REPAIR 1. BRACKET OF UPPER AFT CORNER CUTOUT OF LH SLIDING WISDR DALA2024032103591Skin · crackedCRACKS ON FUSELAGE SKIN STA 1076.0 AND STA 1087 OVER LONGERON 14 RH. FUSELAGE SKIN STA 1076.0 AND STA 1087 OVER LONGERON 14 RH WAS REPAIRED PER ERA 616042-14 REV ORIGINAL SECTION 1 PERMANENT REPAIR. ASSOCIATED ERA 14-616042 ADDED FOR AC 9564. (LP #0254610)SDR DALA2024032103590Longeron · crackedCRACKED LONGERON 17LH STA 1022 PAX CABIN. SUMMARY OF NRC 00352: LONGERON 17LH STA 1022 PAX CABIN WAS REPAIRED PER B717 SRM 53-00-05-2R. (LP #0254278)SDR DALA2024032103589Frame · crackedCRACKED LH FRAME STA 1037 AT LONG 17LH PAX CABIN. SUMMARY OF NRC 00449: LH FRAME STA 1037 AT LONG 17LH PAX CABIN WAS REPAIRED PER B717 SRM 53-20-07-2R PROCEDURE 4. (LP #0254275)SDR DALA2024032103588Longeron · crackedCRACKED LONGERON 17RH STA 1022 PAX CABIN. SUMMARY OF NRC 00353: LONGERON 17RH STA 1022 PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-05-2R. (LP #0254033)SDR DALA2024032103587Doubler · corrodedCORROSION ON FWD AND AFT PREVIOUS REPAIR DOUBLER OF FWD CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 0069: CORROSION LEVEL 2. FWD AND AFT DOUBLERS OF FWD CARGO COMPARTMENT DOOR JAMB WERE REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 6 PAR. 5. (LP #0253957)SDR DALA2024032103586Skin · wornWEAR ON EXTERNAL FUSELAGE SKIN STA Y=994 BTW LONGERON 25R/L26R. SUMMARY OF NRC 00018: EXTERNAL FUSELAGE SKIN STA Y=994 BTW LONGERON 25R/L26R WAS REPAIRED PER ERA 577681-14 REV B SECTION II: PERMANENT REPAIR AND PRI 577681-14 REV 1 PART C. REPAIR APPROVAL IS LISDR DALA2024032103585Pan · crackedCRACK ON SPLICE AND PAN NEAR TO AFT TORQUE TUBE AREA AT FWD CARGO COMPARTMENT DOOR C1. SUMMARY OF NRC 00219: SPLICE (REPAIR DOUBLER) NEAR TO AFT TORQUE TUBE AREA AT FWD CARGO COMPARTMENT DOOR C1 WAS REPLACED PER B717-200 SRM 52-30-02-2R PROCEDURE 4 REPAIR 4. (SDR DALA2024032103584Longeron · corrodedCORROSION ON LONGERON END 25RH AT AFT CARGO COMPARTMENT C-2. SUMMARY OF NRC 00686: CORROSION LEVEL 2. LONGERON END 25RH AT AFT CARGO COMPARTMENT C-2 WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0252387)SDR DALA2024032103579Cusp Web · corrodedCORROSION ON RH CUSP ANGLE BTW STA Y=148 TO Y=218. SUMMARY OF NRC 00438: CORROSION LEVEL 2. RH CUSP ANGLE BTW STA Y=148 TO Y=218 WAS REPAIRED PER ERA 616020-14 REV ORIGINAL. SECTION I: PERMANENT REPAIR. ASSOCIATED ERA 14-616020 ADDED FOR AC 9541. (LP #0251319)SDR DALA2024032103580Battery Pack · inoperativeFOUND LEFT AND RIGHT AFT EMERGENCY EXIT DOOR LOCATOR SIGNS INOPERATIVE AT THE AFT OVERWING DOORS. MAINTENANCE REPLACED THE EMERGENCY BATTERY (B5-115) POWER SUPPLY PER B717 AMM 33-51-03. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #5333890)SDR DALA2024032103578Skin · dentedDENTS OUT LIMITS WERE FOUND ON REVALUATION DENTS OF LOWER SKIN FWR MOVABLE VANE FLAP AT LH WING. SUMMARY OF NRC 00659: PERMANENT REPAIR WAS PERFORMED ON FWD MOVABLE FLAP VANE (LOWER SKIN) OF LH WING PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 PAR 4. (LP SDR DALA2024032303706Battery Pack · inoperativeTHE EMERGENCY OVERHEAD EXIT SIGN AT ROW 19 IS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND POWER SUPPLY B5-120 REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #5441945)SDR DALA2024032103577Diaphragm · crackedCRACK AND PUNCTURE ON DIAPHRAGM BTW STA X=-44 AND X=-56 FROM STA Y=257 APPROX AT PASSENGER CABIN. SUMMARY OF NRC 00707: DIAPHRAGM BTW STA X=-44 AND X=-56 FROM STA Y=257 APPROX AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 AND 53-00-00SDR DALA2024032103576Spar · crackedCRACK ON REAR SPAR APPROX XW151 AT RH WING. SUMMARY OF NRC 00175: REAR SPAR, LOWER CAP APPROX XW151 AT RH WING WAS REPAIRED PER ERA 614420-14AD REV ORIGINAL AND PRI 614420-14 REV 16. TIME CONTROLLED ITEMS. SECTION DTA: PENDING DTA, NOT TO EXCEED 07/MAR/2026, MSDR DALA2024032103575Fitting · wornWEAR ON TRACK FITTING SUPPORT OF SETTLEMENT AREA OF INBD SPOILER STA XTE 162 AND OTBD SPOILER XTE 341. SUMMARY OF NRC 00134: FITTING SUPPORT OF SETTLEMENT AREA OF INBD SPOILER STA XTE 162 WAS REPLACED PER B717-200 SRM 51-41-02-0G, 51-41-05-0G, AND 51-41-08-0G SDR DALA2024032103574Floor Support · corrodedCORROSION ON FLOOR SUPPORT BTW STA Y=160-200 X=6, X=0 AND X=-6. SUMMARY OF NRC 00620: CORROSION LEVEL 2. FLOOR SUPPORTS BTW STA Y=160-200 X=6, X=0 AND X=-6 WERE REPLACED PER B717-200 SRM 51-41-01-0G, 51-41-02-0G, AND 51-41-05-0G. (LP #0246907)SDR DALA2024032103573Cusp Web · corrodedCORROSION AT CUSP ANGLE WAS FOUND ON STA Y=200 AND X=54 - 60. SUMMARY OF NRC 00713: CUSP ANGLE WAS ON STA Y=200 AND X=54 - 60 REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 3 REPAIR 3. (LP #0246718)SDR DALA2024032103572Cusp Web · corrodedCORROSION ON RH CUSP WEB BTW STA X=-56 TO -60 STA 568 (BELOW) AT PASSENGER CABIN. SUMMARY OF NRC 00749: CORROSION LEVEL 2. RH CUSP WEB BTW STA X=- 56 TO -60 STA 568 (BELOW) AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIGURE 215. (LP #0246687SDR DALA2024032103571Cusp Web · crackedCRACK ON RH CUSP WEB STA X=-56 TO -60 AND Y=660 AT PASSENGER CABIN. SUMMARY OF NRC 00513: RH SECTION CUSP WEB WAS FABRICATED AND REPAIRED ON STA X=-56 TO -60 AND Y=660 AT PASSENGER CABIN PER B717-200 SRM 53-00-55-2R PROCEDURE 4, REPAIR 4, FIGURE 223. (LP #0246SDR DALA2024032103570Cusp Web · crackedCRACK ON RH CUSP WEB STA X=-56 AND Y=636-655 ALSO CORROSION AND MISSING FASTENERS AT PASSENGER CABIN. SUMMARY OF NRC 00512: CORROSION LEVEL 2. RH CUSP WEB STA X=-56 AND Y=636-655 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4, REPAIR SDR DALA2024031503377Angle · corrodedCORROSION ON FRAME CLIP STA Y=1087 AND LONGERON 18R AT AFT ACCESORY COMPARTMENT. SUMMARY OF NRC 00101: CORROSION LEVEL 2. FRAME CLIP STA Y=1087 AND LONGERON 18R AT AFT ACCESORY COMPARTMENT WAS FABRICATED PER B717 DWG S2931622 REV B AND REPLACED PER B717 SRM 51SDR DALA2024031503376Floor Support · corrodedCORROSION ON CABIN FLOOR SUPPORTS AT X=-53, STA Y=160 TO 200; X=-15 TO -40, STA Y=180; STA Y=200, X=-44.5 TO -55; AND X=-12 STA Y=210. SUMMARY OF NRC 00677: CORROSION LEVEL 2. FLOOR SUPPORTS AT X=-53, STA Y=160 TO 200; X=-15 TO -40, STA Y=180; STA Y=200, X=-44SDR DALA2024031503375Frame · crackedCRACK ON FRAME STA Y=64 APPROX AND X=18 LH SIDE AT NLG W/W. SUMMARY OF NRC 00705: FRAME STA Y=64 APPROX AND X=18 LH SIDE AT NLG W/W WAS REPAIRED PER B717-200 SRM 53-00-00-2R REPAIR 1. (LP #0245021)SDR DALA2024031403330Skin · wornWORN FUSELAGE SKIN AT STA Y=994 & LONG 23 - 25 (ADJACENT TO AFT DOOR JAMB). SUMMARY OF NRC 00013: FUSELAGE SKIN AT STA Y=994 & LONG 23 - 25 (ADJACENT TO AFT DOOR JAMB) WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 10 REPAIR 10. PERFORM VISUAL INSPECTION SDR DALA2024031403329Web · corrodedCORROSION ON DIAPHRAGM MEMBRANE APPROX -X=53 STA Y=156 AT PAX CABIN. SUMMARY OF NRC 00488: CORROSION LEVEL 2. DIAPHRAGM MEMBRANE APPROX -X=53 STA Y=156 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 1 REPAIR 1. (LP #0243883)SDR DALA2024031403328Tee Angle · corrodedCORROSION ON ANGLE "TEE" STA 1053 LONGERON 30 AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00559: CORROSION LEVEL 2. ANGLE "TEE" STA 1053 LONGERON 30 AT AFT CARGO COMPARMENT WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0242409)SDR DALA2024031403327Seat Track · corrodedCORROSION ON SEAT TRACK BTW Y=200 TO STA Y=256, COORDINATE X=-44 (RH SIDE). SUMMARY OF NRC 00696: CORROSION LEVEL 2. SEAT TRACK BTW Y=200 TO STA Y=341, COORDINATE X=-44 (RH SIDE) WAS FABRICATED PER DRAWING #5930547 REV CW AND REPLACED PER B717 SRM 51-41-01-0G,SDR DALA2024031303282Skin · wornWORN FUSELAGE SKIN AT STA Y=994 & LONG 23 - 25 (ADJACENT TO AFT DOOR JAMB). SUMMARY OF NRC 00013: FUSELAGE SKIN AT STA Y=994 & LONG 23 - 25 (ADJACENT TO AFT DOOR JAMB) WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROCEDURE 10 REPAIR 10. (LP #0242390)SDR DALA2024031303281Pan · crackedCRACK ON PAN BTW STA Y=427 AND BEAM 5 APROX AT FWD DOOR CARGO COMPARMENT. SUMMARY OF NRC 00226: PAN BTW STA Y=427 AND BEAM 5 APROX AT FWD DOOR CARGO COMPARMENT WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0242328)SDR DALA2024031303280Cusp Web · corrodedCORROSION ON RH CUSP WEB LOWER SURFACES BTW STA 446 TO STA 465 AND STA 494 TO STA 500. SUMMARY OF NRC 00669: CORROSION LEVEL 2. RH CUSP WEBS BTW STA 446 TO STA 465 AND STA 494 TO STA 500 WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #024SDR DALA2024031303279Frame · crackedCRACK ON CANTED FRAME ON STA 1200 APROX. BTW L-17L AND L-18L AT AFT INTERNAL FUSELAGE. SUMMARY OF NRC 00232: CANTED FRAME ON STA 1200 APROX. BTW L-17L AND L-18L AT AFT INTERNAL FUSELAGE WAS REPAIRED PER B717-200 SRM 53-00-00-2R-1. (LP #0241299)SDR DALA2024031203225Spar · crackedCRACK ON REAR SPAR APPROX XRS 145 AT LH WING. ERA 61543-14 REV ORIG SECTION I AND II ACCOMPLISHED ON NRC 628 IN TOMX. NEEDS SECTION III ACCOMPLISHED. SUMMARY OF NRC 001-0002:0500-2000/001 00001: ACCOMPLISHED PERMANENT REPAIR PER ERA 615453-14 SECTION III PER E
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