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 DALA2024111410955Door · out of adjustMAIN CABIN DOOR HARD TO OPEN AND CLOSE. F/O HAD TO OPEN DOOR ON ARRIVAL. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE FOUND L1 DOOR SETTING TOO HIGH IN ITS FRAME. HEIGHT WAS ADJUSTSDR DALA2024111410951Floor Panel · corrodedCORROSION ON FLOOR PANELS 221GF & 222MF. SUMMARY OF NRC 00320: CORROSION LEVEL 2. CORROSION ON FLOOR PANEL 221GF & 222MF WAS REMOVED PER B717-200 SRM 51-10-04-0G AND EVALUATED WITHIN LIMITS FOR FLOOR PANEL 221GF. BUT FLOOR PANEL 222MF WAS REPAIRED PER DRAWING SDR DALA2024111410950Retainer · crackedCRACK WAS FOUND ON LH CLEARVIEW WINDOW REATINER. SUMMARY OF NRC 00667: UPPER AFT LH CORNER ON LH CLEARVIEW WINDOW RETAINER WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1, REPAIR 1. (LP #0659031)SDR DALA2024111410949Frame · crackedCRACKS ON UPPER CAP STA Y 1022 AND LONGERON 7R AT C PAX. SUMMARY OF NRC 00487: UPPER CAP STA Y 1022 AND LONGERON 7R AT C PAX WAS REPAIRED PER ER/A 622035-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR AND PRI 622035-14 REV 1. ASSOCIATED ER/A 14-622035 ADDED FOR SDR DALA2024120311391Bulkhead · abnormal-AD- ACCOMPLISH ER/A 542233-14AD REV B SEC II. ACCOMPLISH ER/A 542233-14AD REV B SEC II FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATED. INSPECTIONS CANNOT BE PUSHED PAST 04DEC24. ASSOCIATED ER/A 14-542233 ADDED FOR AC 9506. ACCOMPLISSDR DALA2024111410952Power Supply · inoperativeTHE AFT OVER WING EXIT DOOR EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY (B5-230) AND THE LIGHT OPERATIONALLY CHECKED GOOD IAW B717 AMM 33-51. (LP #6413923)SDR DALA2024111410948Diaphragm · crackedCORROSION ON DIAPHRAGM BTW STA Y=200/218 AND X-54/X-22 AT CABIN PAX. SUMMARY OF NRC 00632: CORROSION LEVEL 2. DIAPHRAGM BTW STA Y=200 /218 AND X-54/X-22 WAS REPLACED PER DRAWING 9936535 REV CS. (LP #0658856)SDR DALA2024111410947Intercostal · crackedCRACKED INTERCOSTAL BTW STA Y=1002 AND STA Y=1022, X=0 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00310: INTERCOSTAL BTW STA Y=1002 AND STA Y=1022, X=0 WAS REPAIRED PER B717 SRM 51-70-11-2R REP. 1. (LP #0658130)SDR DALA2024120911531None · none-AD- ACCOMPLISH ER/A 622306-14AD SECTION I B717 FUSELAGE STA 1178.558 ALTERNATIVE INSPECTION FOR PREVIOUS REPAIR. ACCOMPLISH ER/A 622306-14AD SECTION I FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATED. INSPECTIONS CANNOT BE PUSHED PASTSDR DALA2024111210891Strap · corrodedCORROSION ON FLOOR PANEL STRAP AND WEB (LINES BOTTOM FLOOR PANELS) AT LOWER SILL. SUMMARY OF NRC 00456: CORROSION LEVEL 2. CORROSION ON FLOOR PANEL STRAP AND WEB WAS REMOVED PER B717-200 SRM 51-10-04-0G AND EVALUATED. PANEL STRAP IS WITHIN OF LIMITS BUT WEB ISSDR DALA2024111210890Floor Panel · corrodedCRACK AND CORROSION ON FLOOR PANELS 211PF, 211LF, 211AJF. SUMMARY OF NRC 00168: CORROSION LEVEL 2. CORROSION ON FLOOR PANELS 211PF, 211LF, 211AJF WAS REMOVED PER B717-200 SRM 51-10-04-0G AND PANELS EVALUATED. FOUND WITHIN OF LIMITS ON FLOOR PANELS 211PF & 211LSDR DALA2024111210889Door Frame · corrodedCORROSION ON DOOR JAM BTW STA Y-954 TO 994 AT AFT CARGO COMPARMENT. SUMMARY OF NRC 00076: CORROSION LEVEL 2. CORROSION ON DOOR JAM BTW STA Y-954 TO 994 AT AFT CARGO COMPARMENT WAS REPAIRED PER B717-200 SRM 53-20-15-2R PROC 7 REPAIR 7. (LP #0655665)SDR DALA2024111210888Vane · dentedDENT ON LWR SURFACE AT FWD MOVABLE FLAP VANE OF LEFT WING WAS FOUND OUT OF LIMITS DUE TO DISTANCE. SUMMARY OF NRC 00674: AREA BTW XF 85 TO XF 95 ON LWR SURFACE AT FWD MOVABLE FLAP VANE OF LEFT WING WAS REPAIRED PER B717-200 SRM 51-70-02-0G PROCEDURE GENERAL INSDR DALA2024111210887Seat Track · misinstalledWRONG INSTALLED FASTENERS ON SEAT TRACK AND CUSP WEB STA Y=914-919 & X =56 AT PASSENGER CABIN. SUMMARY OF NRC 00427: CUSP WEB STA Y=914-919 & X =56 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4. (LP #0655354)SDR DALA2024111210886Vane · dentedDENTS: 2, 3, 4, 5, AND 6 BTW XF89 AND XF95 (10 TO 13.5 INCHES FROM T.E.) ON RH AFT MOVABLE FLAP VANE WERE FOUND OUT OF LIMITS BY DISTANCE BTWN OTHER DAMAGES. SUMMARY OF NRC 00628: DENTS: 2, 3, 4, 5, AND 6 BTW XF89 AND XF95 (10 TO 13.5 INCHES FROM T.E.) ON RH ASDR DALA2024111110806Channel · corrodedCORROSION AT CHANNEL BETWEEN STA 827 AND 832 L22R EXTERNAL FUSELAGE. SUMMARY OF NRC 407: CORROSION LEVEL 2. CHANNEL BTW STA Y=827 AND Y=832 L22R EXTERNAL FUSELAGE WAS FABRICATED PER DWG 5924872 REV BT AND REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. SDR DALA2024111410946Door · corrodedCORROSION ON STAIRWELL DOOR. ALSO RUSTED HINGE. SUMMARY OF NRC 00071: CORROSION LEVEL 2. FORWARD STAIRWELL DOOR WAS REPLACED PER B717 AMM 52-63-01. (LP #0653912)SDR DALA2024111110805Access Panel · corrodedCORROSION ON ACCESS PANEL 5971074 -1 BTW STA Y=636 TO STA Y=655 L29L TO L29R AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00616: CORROSION LEVEL 2. ACCESS PANEL 5971074-1 BTW STA Y=636 TO STA Y=655 L29L TO L29R AT FWD CARGO COMPARTMENT WAS REPLACED PER B717-200 SRSDR DALA2024111110804Doubler · corrodedCORROSION WAS FOUND ON DOUBLER AT E/E COMPARTMENT ON INTERNAL FUSELAGE SKIN PANEL STA Y=215 TO STA Y=221 BTW LONGERON 28R AND 29R. SUMMARY OF NRC 00626: CORROSION LEVEL 2. DOUBLER ON INTERNAL FUSELAGE SKIN PANEL STA Y=215 TO STA Y=221 BTW LONGERON 28R AND 29R SDR DALA2024111110803Vane · dentedDENTS OUT OF LIMITS: 8, 12, 19, 22, AND 24 BTW STA XF95 AND XF103 (4 TO 7 INCHES FROM T.E.) ON UPPER SURFACE AT LH AFT MOVABLE VANE AT LH WING. SUMMARY OF NRC 00618: IN REFERENCE TO NRC 00501 DENTS OUT OF LIMITS: 8, 12, 19, 22, AND 24 BTW STA XF95 AND XF103 (4SDR DALA2024111110802Vane · dentedDENT #1 (1EA) OUT OF LIMITS UPPER SURFACE RH FWD MOVEABLE FLAP VANE. DISTANCE TO AFT EDGE 6.650, DISTANCE OF OUTER EDGE 34.900 RH WING. SUMMARY OF NRC 00620: ON REF NRC 00503 DENT #1 (1EA) OUT OF LIMITS UPPER SURFACE RH FWD MOVEABLE FLAP VANE DISTANCE TO AFT ESDR DALA2024111110801Skin · crackedCRACKED FUSELAGE SKIN STA Y 1087 LONG 14R LOCATED CLOSE TO THE LAP SKIN JOINT AND PREVIOUS REPAIR DOUBLER. SUMMARY OF NRC 00052: FUSELAGE SKIN STA Y 1087 LONG 14R LOCATED CLOSE TO THE LAP SKIN JOINT AND PREVIOUS REPAIR DOUBLER WAS REPAIRED PER ER/A 621691-14 RSDR DALA2024111110800Unknown · unknown-AD- EXISTING REPAIRS FOUND. PERFORMED ALL REPAIRS PER PRI 621136-14, REV 13. REPAIR LEAK CHECK WAS GOOD. REPAIRS COMPLETED IAW ER/A 621136-14AD, REV O, SECTION 1. A/C OK FOR SERVICE. ALL CDCCL AND SFAR 88 REQUIREMENTS HAVE BEEN MET. RII + NDT C/W PER ERA 6211SDR DALA2024111110799Fuel Cell · leaking-AD- FOUND FUEL SEEPING FROM FWD FLAP CARRIAGE MOUNT AND DOUBLER ON RT WING INBOARD FLAP AT XRS 164. (FC 5720-01103) PERFORMED ALL REPAIRS PER PRI 621136-14, REV 13. LEAK CHECK WAS GOOD. REPAIRS COMPLETED IAW ER/A 621136-14AD, REV O, SECTION 1. A/C OK FOR SERVSDR DALA2024112611223Bulkhead · mechanic error-AD- ACCOMPLISH ER/A 551838-14AD REV A SECTION II FUSELAGE / BULKHEADS / CANTED STA 1178 FRAME / MISDRILLED HOLES. ACCOMPLISH ER/A 551838-14AD REV A SECTION II FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATED. INSPECTIONS CANNOT BE PUSSDR HALA20241119075Fitting · corrodedSEVERE CORROSION ON RIGHT AFT NOSE GEAR DOOR AFT FITTING (M). 1. REMOVED AND REPLACE RIGHT AFT NOSE GEAR DOOR AFT HINGE FITTING PER LBD #5914984. PERFORMED ADJUSTMENT OF THE NOSE LANDING GEAR AFT DOORS PER AMM 32-20-01-830-802SDR HALA20241119074Cable · damagedRH INBD FLAP TRACK PULLEY AFT CABLE NYLON TORN. COMPLETED REPLACING 4EA FLAP BUS CABLES 33A, 33B, 34A, AND 34B. PER B717 DRAWING # 5940898 REV5.SDR DALA2024111410953Doubler · cracked-AD- FUSELAGE PLATE SKIN DOUBLERS STA Y=1178 BTW L1-L3 LH CRACKED. ACCOMPLISH ER/A 546495-14AD REV A SECTION III FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATED. INSPECTIONS CANNOT BE PUSHED PAST 04DEC24. ASSOCIATED ER/A 14-546495 ADDSDR DALA2024111110798Frame · crackedCRACK ON MAIN FRAME STA Y=1037 LONGERON 17R AT PAX CABIN. SUMMARY OF NRC 00381: CRACK ON MAIN FRAME STA Y=1037 LONGERON 17R AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-20-07-2R, PROCEDURE 4, REPAIR 4. (LP #0650804)SDR DALA2024111110797Longeron · crackedCRACK ON LONGERON #8RH STA Y1022 AT PAX CABIN. SUMMARY OF NRC 00501: LONGERON #8RH STA Y1022 AT PAX CABIN WAS REPAIRED PER B-717-200 SRM 53-00-05-2R-2. (LP #0650326)SDR DALA2024111110796Longeron · crackedCRACKS ON LONGERONS 17R, 13R, 12L, AND 13L STA Y 1037 AT C. PAX. SUMMARY OF NRC 00485: (ET) HFEC INSPECTION WAS PERFORMED. CRACK WAS FOUND ON LONG 13R, THE REST NO CRACKS WERE FOUND PER B717 DC/MD NDT SPM PART 6, 06-10-01.001. LONGERON 13R STA Y 1037 AT C. PAXSDR DALA2024110810727Skin · gougedGOUGE ON EXTERNAL SKIN BTW STA 123 AND L-29L TO L-30 AT FUSELAGE. SUMMARY OF NRC 00092: EXTERNAL SKIN BTW STA 123 AND L-29L TO L-30 AT FUSELAGE WAS REPAIRED PER B717-200 SRM 53-03-01-2R PROCEDURE 1, REPAIR 1 PAR 6.A. FIG 202. PERFORM A VISUAL INSPECTION EVERY SDR DALA2024110810726Vane · dentedDENTS (2 EA) ON UPPER SURFACE AFT MOVABLE VANE APPROX BTW STA XRS=69 AND XRS=91 AT RH WING. SUMMARY OF NRC 00143: UPPER SURFACE AFT MOVABLE VANE APPROX BTW STA XRS=69 AND XRS=76 OF RH WING WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1. (LP #06SDR DALA2024110710703Longeron · crackedCRACK ON LONGERON 6LH STA Y=1022 AT PAX CABIN. SUMMARY OF NRC 00499: LONGERON 6LH STA Y=1022 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2, REPAIR 2. (LP #0647976)SDR DALA2024112611224Bulkhead · cracked-AD- ACCOMPLISH ER/A 619268-14AD REV A SECTION II - FUSELAGE MAIN FRAME BULKHEADS AT FS 1178, X=10 X=0.0. AFT WEB CRACKED & ELONGATED HOLE. ACCOMPLISH ER/A 619268-14AD REV A SECTION II FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATED. SDR DALA2024111410954Doubler · cracked-AD- STA 1178.225 LONGERON 3L BULKHEAD DOUBLER CRACKED. ACCOMPLISH ER/A 565522-14AD REV A SECTION IV FOR THE INSPECTION OF THE REAR CANTED BULKHEAD REPAIR. THIS IS AD RELATED. INSPECTIONS CANNOT BE PUSHED PAST 04DEC24. ASSOCIATED ER/A 14-565522 ADDED FOR AC 95SDR DALA2024110710702Floor Support · corrodedCORROSION ON FLOOR SUPPORTS (2 EA) X=-55/X=55 FROM STA Y=1022 TO STA Y=1053 AT PASSENGER CABIN. SUMMARY OF NRC 00475: CORROSION LEVEL 2. FLOOR SUPPORTS (2 EA) X=-55/X=55 FROM STA Y=1022 TO STA Y=1053 WERE REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. SDR DALA2024110510647Battery Pack · inoperativeMAINTENANCE FOUND SEVERAL EMERGENCY LIGHTS IN TAIL COMPARTMENT TO BE INOPERATIVE. DETERMINED THAT THE BATTERY PACK B5-116 WAS BAD. BATTERY PACK WAS REPLACED REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #6585244)SDR HALA20241105068Radome · no discrepancyDIV - BIRD STRIKE DEPARTING OGG. INSPECTED AIRCRAFT PER AMM 05-52-01-210-801, NO DAMAGE FOUND. NOTED BOTTOM OF RADOME L/H HAS A MARK BUT NO REMENANTS OR DAMAGE FROM BIRD. OK FOR SVC.SDR HALA20241105067Battery · inoperativeEXTERIOR EMERGENCY LIGHTS NOT WORKING. REMOVED AND REPLACED EXT EMERG. LIGHT BATTERY PER AMM 33-51-06. OPS CHECK GOOD.SDR DALA2024110410591Hinge · wornWEAR ON DOBLER AND FLIGHT ATTENDANT SEAT HINGES OF AFT CABIN BULKHEAD VENTRAL DOOR. AND WEAR ON UPPER / LWR SIDE FITTING (7 EA) 0F AFT CABIN BULKHEAD VENTRAL DOOR. SUMMARY OF NRC-00452: UPPER / LWR SIDE FITTINGS (7 EA) AND FLIGHT ATTENDANT SEAT HINGES WERE BLESDR DALA2024110410592Battery Pack · inoperativeBOTH AFT OVERWING LOWER SIDE WALL EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK B5-119 PER B717 AMM 33-51. OPERATIONAL TEST WAS GOOD. (LP #6342840)SDR DALA2024110410590Skin · gougedGOUGE ON EXTERNAL SKIN BTW STA 123 AND L-29L TO L-30 AT FUSELAGE. SUMMARY OF NRC 00092: EXTERNAL SKIN BTW STA 123 AND L-29L TO L-30 AT FUSELAGE WAS REPAIRED PER B717-200 SRM 53-03-01-2R PROCEDURE 1, REPAIR 1 PAR 6.A, FIG 202. (LP #0642594)SDR DALA2024110410589Frame · crackedCRACK ON MAIN FRAME BTW STA Y=1037 AND L17L AT AFT CABIN PASSENGER. SUMMARY OF NRC 00433: MAIN FRAME BTW STA Y=1037 AND L17L AT AFT CABIN PASSENGER WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 4 REPAIR 4. (LP #0639803)SDR DALA2024110510646Frame · damagedR/H FRAME ON STATION Y1133 DAMAGED NEAR LONGERON R8. REMOVED DAMAGED FRAME REF B717 SRM 53-20-07-2R PROCEDURE 1. FABRICATED, ALODINE, PRIMED, AND PAINTED REPAIR FRAME SPLICE PARTS FOR SPLICE R4-R5 LONGERON. FRAME GOES DOWN TO PRODUCTION SPLICE RIGHT PER B717 SSDR DALA2024110110568Pan · crackedCRACK ON INNER PAN FWD/AFT UPPER CORNER AT FWD CARGO COMPRTMENT. SUMMARY OF NRC 00112: INNER PAN FWD/AFT UPPER CORNER AT FWD CARGO COMPARMENT WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0638113)SDR DALA2024110110567Web · crackedCRACK ON WEB BTW STA Y=674 AND -X=45 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00380: WEB BTW STA Y=674 AND -X=45 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. FIGURE 217. -PERFORM DECAL INSPECTION CONDITION EVERY "C" CSDR DALA2024110110566Longeron · crackedCRACK ON LONGERON BTW STA Y=1022 AND L6L AT AFT CABIN PASSENGER. SUMMARY OF NRC 00434: LONGERON BTW STA Y=1022 AND L6L AT AFT CABIN PASSENGER WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #0637160)SDR HALA20241031063Valve · disconnected"BLEED AIR R FAIL" IN FLIGHT. COMPLIED WITH QRH PROCEDURE. MSG REMAINED ILLUMINATED WITH ADDITIONAL "AIR SYS R NOT OFF". RIGHT SYSTEM INDICATED 80 PSI. FOUND PRSOV VALVE DISCONNECTED IN #2 ENGINE WITH FAV STILL CONNECTED. CORRECTED (M) PROCEDURES OF CURRENT MESDR DALA2024103110527Pan · crackedCRACK WAS FOUND ON INNER PAN AFT EDGE BTW BEAM 1 AND BEAM 2 AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00486: INNER PAN AFT EDGE BTW BEAM 1 AND BEAM 2 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 8. (LP #0636755)
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