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 DALA2024081208007Hinge · damagedELONGATED HOLES ON INTERNAL PAN AT FWD CARGO DOOR HINGE ATTACH POINTS (FWD/AFT). (PTAS). SUMMARY OF NRC 00106: HOLES ON INTERNAL PAN AT FWD CARGO DOOR HINGE ATTACH POINTS (FWD/AFT) WERE REPAIRED PER ERA 559577-14MA REV ORIGINAL, PER PRI 618954-14 REV 4, AND ERSDR DALA2024081208006Skin · crackedCRACKS WERE FOUND ON UPPER AND LOWER SKIN OF OUTBOARD TIP ELEVATOR LH. SUMMARY OF NRC 00701: UPPER AND LOWER SKIN OF OUTBOARD TIP ELEVATOR LH WAS REPAIRED PER ER/A 618920-14 REV ORIGINAL SECTION I: PERMANENT REPAIR ACCOMPLISH SECTION II REPETITIVE INSPECTION ISDR DALA2024081208005Housing · crackedCRACK AT SETTLEMENT AREA OF HANDLE HOUSING WAS FOUND WHILE HOUSING REMOTION DOOR L1. SUMMARY OF NRC 00708: EXTERNAL SKIN ON SETTLEMENT AREA OF HANDLE HOUSING AT PASSENGER DOOR L1 WAS REPAIRED PER ER/A 619355-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI SDR DALA2024080907921Cap · corrodedCORROSION ON SEAT TRACK X=22 STA Y=197-225, -X=44.5 Y=200-237, AND FLOOR SUPPORT AT -X=54.5 Y=210. SUMMARY OF NRC 00719: CORROSION LEVEL 2. SEAT TRACK X=22 STA Y=197-225, AND SEAT TRACK -X=44.5 Y=200-237, WERE REPAIRED PER B717-200 SRM 53-20-52-2R PROCEDURE 5 SDR DALA2024080907920Cap · crackedCRACK ON UPPER CAP STA Y=1022 AND LONGERON #7 RH AT CABIN PAX. SUMMARY OF NRC 00816: UPPER CAP STA Y=1022 AND LONGERON #7 RH AT CABIN PAX WAS REPAIRED PER PRI 619643-14 REV 1 AND ER/A 619643-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-61964SDR DALA2024080907919Stabilizer · distortedTHE COUNTERSINK OF THE FASTENERS HOLES OF THE VERTICAL STABILIZER LEADING EDGE WERE NOTED WORN ALL AROUND EDGES BETWEEN ZFS 52.267 TO 153.938. SUMMARY OF NRC 00748: THE LEADING EDGE OF THE VERTICAL STABILIZER IS OUT OF LIMITS, AS REPAIRABLE HOLE LIMITS PER B71SDR DALA2024080807887Skin · dentedDENTS (2EA) ON FUSELAGE SKIN BTW STA Y=120 TO 144 APPROX AND LONG 18LH TO 19LH. ALSO PJECTION LONG-16LH TO LONG-17LH. SUMMARY OF NRC 00669: FUSELAGE SKIN BTW STA Y=120 TO 144 APPROX AND LONG 18LH TO 19LH. ALSO PJECTION LONG-16LH TO LONG-17LH WAS REPAIRED PER ESDR DALA2024080807886Beam · crackedCRACK WAS FOUND ON AFT BEAM 3 AT PAN. SUMMARY OF NRC 00254: PAN AFT SIDE BEAM 3 WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 3 REPAIR 3. (LP #0489872)SDR DALA2024080807885Pan · crackedCRACK ON PAN (BEAM 3) AT AFT CARGO COMPARTMENT DOOR AFT EDGE. SUMMARY OF NRC 00402: PAN (BEAM 3) AT AFT CARGO COMPARTMENT DOOR AFT EDGE WAS REPAIRED PER PRI 618569-14 REV 7 AND ERA 618569-14 REV ORIGINAL. SECTION I PERMANENT REPAIR. (LP #0489565)SDR DALA2024080807881Angle · corrodedCORROSION ON RH CUSP ANGLE Y=200, Y=219-224 AT PAX CABIN (W1.) SUMMARY OF NRC 00467: CORROSION LEVEL 2. CUSP ANGLE Y=200, Y=219-224 AT PAX CABIN WAS REPAIRED PER PRI 619420-14 REV 2 AND ER/A 619420-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A SDR DALA2024080807882Frame · crackedCRACK ON FRAME STA Y=694 LH SIDE AT CANTED KEEL INTERNAL STRUCTURE. SUMMARY OF NRC 00340: LH SIDE FRAME STA Y=694 INBOARD EDGE WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1 AND OUTBOARD EDGE WAS REPAIRED PER ERA 545683-14MA REV ORIGINAL. ASSOCSDR DALA2024080707853Skin · crackedCRACK ON INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT LH SLIDING WINDOW CUTOUT AREA WAS FOUND. SUMMARY OF NRC 00628: INTERNAL FUSELAGE SKIN JUST AFT UPPER CORNER AT LH SLIDING WINDOW WAS REPAIRED PER B717-200 SRM 56-10-02-2R REPAIR 1 PARAGRAPH 5 FIGURE 201.SDR DALA2024080707852Intercostal · corrodedCORROSION ON INTERCOSTAL 29R STA Y=1002 TO Y=1005 AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00332: CORROSION LEVEL 2. INTERCOSTAL 29R STA Y=1002 TO Y=1005 AT AFT CARGO COMPARTMENT (C2) WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0487811)SDR DALA2024080707851Frame · crackedCRACK ON FRAME STA Y=694 LH SIDE AT CANTED KEEL INTERNAL STRUCTURE. SUMMARY OF NRC 00340: LH SIDE FRAME STA Y=694 INBOARD EDGE WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1 AND OUTBOARD EDGE WAS REPAIRED PER ERA 545683-14MA REV ORIGINAL. (LP #SDR DALA2024080607843Light · inoperativeCABIN OVERWING EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENANCE FOUND THE BATTERY PACKS AT B5-118 & B5-130 BAD. REPLACED THE EMERGENCY BATTERY PACKS PER B717 AMM 33-51. OPERATIONAL CHECK OK. AIRCRAFT OK FOR SERVICE. (LP #6186026)SDR DALA2024080607842Autobrake Sys · intermittentCRACK ON FRAME CAP STA Y=1133 AND BTW LONG 2LH TO 3LH AT AFT ACCESSORY COMPARTMENT. SUMMARY OF NRC 00685: FRAME CAP (STIFFENER) STA Y=1133 AND BTW LONG 2LH TO 3LH AT AFT ACCESSORY COMPARTMENT WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1. (LP SDR DALA2024080607841Skin · crackedCRACKS ON FUSELAGE SKIN LH SIDE BTW LONGERON 13L-14L AND STA 1022, 1037, 1087 AT AFT FUSELAGE. SUMMARY OF NRC 00046: (ET) HFEC INSPECTION WAS ACCOMPLISHED ON FUSELAGE SKIN LH SIDE BTW LONGERON 13L-14L AND STA 1037, 1087 AT AFT FUSELAGE ON STA 1037 THREE CRACKSSDR DALA2024080607840Wing Root · corrodedCORROSION ON LH CENTER WING UPPER SURFACE (WING BOX) BTW STGR 6-5 AND STGR 5-4 PAX CABIN. SUMMARY OF NRC 00693: CORROSION LEVEL 2. CORROSION ON LH CENTER WING UPPER SURFACE (WING BOX) BTW STGR 6-5 AND STGR 5-4 PAX CABIN WAS REPAIRED PER PRI 619399-14 REV 3 ANDSDR DALA2024080607839Cusp Web · corrodedCORROSION ON CUSP WEB MEMBRANE STA 565 X=- 59, STA 576 X=-58, STA 579-589 X=-60 AND X=-58 (UPPER AND UNDER), STA 589-617 X=-57 AND X=-59, STA 636 X=-49, STA 647 X=-58 AT PAX CAB. SUMMARY OF NRC 00491: CORROSION LEVEL 2. CUSP WEB MEMBRANE STA 565 X=-59, STA 579SDR HALA20240805037Battery · inoperativeEMERGENCY LIGHTS ROW 10 - 14 INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PER AMM: 33-51-11. OPS CHECK GOOD. OKAY FOR SERVICE.SDR DALA2024080507766Power Supply · no testDURING SERVICE CHECK, THE EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE FROM THE FLIGHT ATTENDANT PANEL. MAINTENANCE FOUND THAT THE CABIN EMERGENCY LIGHTS WOULD WORK WITH COCKPIT SWITCH ARMED AND FLIGHT ATTENDANT SWITCH SET TO "ON" ONLY, BUT NOT FROM FLIGHT ATSDR DALA2024080507765Battery Pack · no testFORWARD SMALLER EMERGENCY LIGHTS ARE INOPERATIVE AT DOORS 1LT & 1RT. MAINTENANCE REPLACED THE EMERGENCY BATTERY AT LOCATION B5-118 IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #9569211)SDR DALA2024080507764Battery Pack · no testBOTH AFT EMERGENCY DOORS "EMERGENCY EXIT IDENTIFIER" LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHTS BATTERY PACK POWER SUPPLY B5-119 PER B717 AMM 33-51-03. OPERATIONAL TEST WAS GOOD. (LP #5908832)SDR DALA2024080507763Skin · crackedCRACKS ON FUSELAGE SKIN RH SIDE BTW LONGERON 13R-14R AND STA 1116, 1144, LONGERON 7R AND STA 1022 AT AFT FUSELAGE. SUMMARY OF NRC 00047: FUSELAGE SKIN RH SIDE BTW LONGERON 13R-14R AND STA 1116, 1144, LONGERON 7R AND STA 1022 AT AFT FUSELAGE WAS REPAIRED PER PRSDR DALA2024080507762Frame · crackedCRACK ON MAIN FRAME STA Y=1037 LONGERON 17L AT PAX CABIN. SUMMARY OF NRC 00354: MAIN FRAME STA Y=1037 LONGERON 17L AT PAX CABIN WAS REPAIRED PER PRI 619352-14 REV 1 AND ERA 619352-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A 14-619352 ADDED FOSDR DALA2024080507761Longeron · crackedCRACKS ON LONGERONS 3, 4, 5, 6, AND 17 LH STA Y=1022 AT CABIN PAX. SUMMARY OF NRC 00371: LONGERON 3 BTW STA Y=1012 TO STA Y=1027 LH, LONGERON 4 BTW STA Y=1011 TO STA Y=1053 LH, LONGERON 5 BTW STA Y=1012 TO STA Y=1053 LH, LONGERON 6 BTW STA Y=1013 TO STA Y=1053SDR HALA20240802036Hydraulic Line · leakingATB: L HYD QTY LO CLIMIBING THROUGH 11,000. REMOVED LEAKING HYD LINE PN- 7972138-616 - ROUTED TO HYD SHOP. REPAIRED HYD LINE PER AMM 20-10-01. INSALLATION, OPS + LEAK CHECK PENDING. INSTALLED HYD LINE P/N 7972138-616 PER AMM 20-10-03 OPS CHECK GOOD LEAK CHECK SDR DALA2024080207725Sign · malfunctionedAFT REAR LEFT EXIT SIGN FLASHING. DISCOVERED BOARDING AIRCRAFT. MAINTENANCE REPLACED THE AFT PASSENGER CABIN DROP CEILING EMERGENCY LIGHT BATTERY ASSY PER B717 AMM 33-51. (LP #6186958)SDR DALA2024080807884Unknown · unknownER/A 610692-14 SECTION II INSPECTIONS. ER/A 610692-14, REV A AT OR PRIOR TO 46,893 TOTAL FLIGHT CYCLES, AND REPETITIVELY EVERY 3,000 FLIGHT CYCLES THEREAFTER ACCOMPLISH SECTION II INSPECTION INSTRUCTIONS. AT THE TIME OF THIS LP CREATION, /FOR IAI SHOWS AIRPLANSDR DALA2024080107659Battery · no testFOUND OVERWING EMERGENCY EXIT LIGHTS OVERHEAD EXIT LIGHTS IN ROW 20 TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY FOR ROW 20 LIGHT PER B717 AMM 33-51. OPERATIONAL CHECK OF EMERGENCY LIGHTS WAS GOOD. OK FOR SERVICE. (LP #6008052)SDR DALA2024073007625Frame · damagedNICKS ON FRAME STA Y=351 BTW LONGERON 17R / L18R. SUMMARY OF NRC 00711: FRAME'S STA Y=351 BTW LONGERON 17R / L18R WAS REPAIRED PER B717-200 SRM 53-00-07-2R PROCEDURE 1 REPAIR 1. (LP #0473575)SDR DALA2024073007624Longeron · crackedCRACKS ON LONGERONS 3, 4, 5, 6, AND 8 RH STA Y=1022 AT CABIN PAX. SUMMARY OF NRC 00370: LONGERONS 3, 4, 5, 6, AND 8 RH STA Y=1022 AT CABIN PAX WERE REPAIRED PER B717-200 SRM 53-00-05-2R REPAIR 2 FIG.201. (LP #0473110)SDR HALA20240729035Electrical Sys · faultedAIR TURNBACK (ATB) IN CLIMB BETWEEN 10,000 + 11,000 THERE WERE TWO (2) SEPARATE POWER INTERRUPTIONS, EACH LASTING 2-3 SECONDS, RESULTING IN MOMENTARILY LOSS OF ALL DU'S + VHFS. PERFORMED BITE OF EPCU PER AMM 24-21-02. NO FAULTS. RESET VIA 1+2. PERFORMED VIA 1+SDR DALA2024072907540Cusp Web · corrodedCRACK ON CUSP WEB BTW STA Y=579/598 AND STA X=-45 AT PAX CABIN. SUMMARY OF NRC 00453: CUSP WEB BTW STA Y=579/598 AND STA X=-45 AT PAX CABIN WAS FABRICATED PER B717 SRM 53-00-55-2R-4 AND REPLACED PER B717 SRM 51-41-01-0G, 51-41-02-0G, AND 51-41-05-0G. (LP #0471SDR DALA2024072907542Battery Pack · inoperativeCEILING PANEL 6,7,8, AND MID CABIN OVERHEAD EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED #5 EMERGENCY BATTERY PACK PER B717 FRMFIM 33-50. OPERATIONAL CHECK WAS GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME. (LP #6057526)SDR DALA2024072907541Battery · inoperativeTHE OVERWING EMERGENCY EVACUATION LIGHT IS INOPERATIVE. OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY WAS REPLACED PER B717 AMM 33-51-06. SATISFACTORY TEST. (LP #5841724)SDR DALA2024072907539Cusp Web · corrodedCORROSION ON CUSP WEB MEMBRANE STA Y=794 TO Y=813, X=-44 X=-60, AND Y=832/Y=835 AND X=-57. ALSO, CORROSION ON THE REPAIR DOUBLER OF THE CUSP WEB MEMBRANE STA Y= 865 TO Y=870, X=-53 TO X=-60. CABIN PAX. SUMMARY OF NRC 00764: CORROSION LEVEL 2. CUSP WEB MEMBRANESDR DALA2024072907538Cusp Web · crackedCRACK WAS FOUND AFTER REMOVED CUSP WEB BTW STA Y=218 TO STA Y=238, -X=56 TO -X=44 AT CABIN PAX. SUMMARY OF NRC 00820: CUSP WEB BTW STA Y=218 TO STA Y=238, -X=56 TO -X=44 AT CABIN PAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4 FIG 203. (LP #0468164)SDR DALA2024072907549Hub Cap · missingSHIP 9527 -ATO- THE CREW SAFELY ABORTED THE TAKEOFF AT 65 KTS DUE TO RIGHT "ANTI-SKID FAIL" MESSAGE. CORRECTIVE ACTION: MAINTENANCE FOUND THE #4 MAIN GEAR HUBCAP AND CLAMP MISSING. THE HUBCAP AND CLAMP WERE REPLACED AND ALL ANTI-SKID RETURN TO SERVICE TESTS WESDR DALA2024072907537Cusp Web · crackedCRACKS ON CUSP WEB BTW STA Y=579/598 AND BTW STA X=44/60 AT PAX CABIN. SUMMARY OF NRC 00443: CUSP WEB BTW STA Y=579/598 AND BTW STA X=44/60 AT PAX CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R-4 AND 51-41-02-0G. (LP #0467746)SDR DALA2024072907536Skin · corrodedSEVERAL SPOTS OF CORROSION ON WING CENTER SECTION UPPER SKIN BTW STA Y=655 TO 674, Y=674 TO 696, Y=696 TO 715, AND BTW X=45 TO X=60 AT PASSENGER COMPARTMENT (CPAX). SUMMARY OF NRC 00346: CORROSION LEVEL 2. WING CENTER SECTION UPPER SKIN BTW STA Y=655 TO 674, YSDR DALA2024072907535Pan · corrodedCORROSION ON AFT CARGO COMPARTMENT LOWER DOOR JAMB PAN. SUMMARY OF NRC 00131: CORROSION LEVEL 2. LOWER DOOR JAMB PAN ON AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-15-2R REPAIR 7. (LP #0467185)SDR DALA2024072607479Cusp Web · damagedTOOL MARK ON CUSP WEB (LOWER FACE) STA Y=614 AND STA X=-54 AT PAX CABIN. SUMMARY OF NRC 00452: CUSP WEB STA Y=614 AND STA X=-54 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4. (LP #0466500)SDR DALA2024072607481Oxygen Mask · inoperativeSHIP 9552 -MISC- REFERENCE LOG PAGE #5879904 ABOUT A RAPID DECOMPRESSION EVENT. MASKS AT SEAT ROWS 11C, 18A, 19C, 21C, 24C, 25A, 29A, & AFT F/A SEAT DID NOT DROP DURING THE ODI EVENT. MAINTENANCE FORWARDED THE O2 SYSTEM TO MEL 35-21-01A. "M" PROCEDURES COMPLIESDR DALA2024072607480Duct · disconnectedSHIP 9552 -DIV/PRESS/DE- THE FLIGHT CREW DIVERTED THE AIRCRAFT TO MEM FOLLOWING THE RAPID LOSS OF CABIN PRESSURIZATION. CREW DONNED O2 MASKS, DECLARED AN EMERGENCY, AND INITIATED AN EMERGENCY DESCENT TO 10K FEET. CABIN MASKS AUTOMATICALLY DEPLOYED. LANDED SAFESDR DALA2024072607478Pan · corrodedCORROSION ON FWD CARGO COMPARTMENT PAN LOWER DOOR JAMB. SUMMARY OF NRC 00129: CORROSION LEVEL 2. FWD CARGO COMPARTMENT PAN LOWER DOOR JAMB WAS REPAIRED PER B717-200 SRM 53-20-15-2R REPAIR 6. (LP #0466095)SDR DALA2024072607477Frame · crackedCRACK ON FRAME STA Y=1037 AND STR 17 RH AT C PAX. SUMMARY OF NRC 00360: FRAME STA Y=1037 AND STR 17 RH WAS REPAIRED PER B717 SRM 53-20-07-2R REP 4. (LP #0466007)SDR DALA2024072507457Cusp Web · crackedCRACKS ON CUSP WEB BTW STA Y=655/715 AND BTW STA X=44/60 AT PAX CABIN. SUMMARY OF NRC 00444: CUSP WEB BTW STA Y=655/715 AND BTW STA X=44/60 AT PAX CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R-4. (LP #0464713)SDR DALA2024072507456Vane · dentedDENTS ON LH WING LOWER MOVABLE FLAP VANE INTRADOS BETWEEN XF=69+8 AND XF=111-10. ADDL TIME RLTD MON 0464583 ADDED. SUMMARY OF NRC 00260: DENTS ON LH WING LOWER MOVABLE FLAP VANE INTRADOS BETWEEN XF=69+8 AND XF=111-10 WERE MEASURED AND EVALUATED AND ARE WITHIN SDR DALA2024072507455Vane · dentedDENTS ON LH WING LOWER MOVABLE FLAP VANE INTRADOS BETWEEN XF=69+8 AND XF=111-10. ADDL TIME RLTD MON 0464590 ADDED. SUMMARY OF NRC 00260: DENTS ON LH WING LOWER MOVABLE FLAP VANE INTRADOS BETWEEN XF=69+8 AND XF=111-10 WERE MEASURED AND EVALUATED AND ARE WITHIN
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