Boeing 717-200
Service difficulty reports · 18,771
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 DALA2023071705776Unknown · unknownCRACK ON INTERCOSTAL FROM STA Y=1002 TO STA Y=1022 AND X=0 AT PAX CABIN. SUMMARY OF NRC 00438: INTERCOSTAL FROM STA Y=1002 TO STA Y=1022 AND X=0 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 51-70-11-2R PROCEDURE 1 REPAIR 1 PAR 4 FIGURE 201 AND 51-41-05-0G. (LP #SDR DALA2023071705775Unknown · unknownCORROSION OUT OF LIMIT ON FLOOR SUPPORTS (2 EA) LH SIDE FROM STA Y=1022 TO STA Y=1053 AND X=44, AND FROM STA Y=1022 TO STA Y=1053 AND X=53.5 AT CABIN PAX. (W2) IN REF NRC 0441. SUMMARY OF NRC 00622: FLOOR SUPPORTS (2 EA) LH SIDE FROM STA Y=1022 TO STA Y=1053 ASDR DALA2023071405738Unknown · unknownCORROSION ON GIRT BAR FITTINGS AT R1 DOOR. SUMMARY OF NRC 00691: CORROSION LEVEL 2. GIRT BAR FITTINGS (2 EA) WERE REPLACED PER B717 SRM 51-40-08-0G. (LP #2865125)SDR DALA2023071405737Unknown · unknownAFTER LONGERON 26 LH BTW STA Y=900 TO STA Y=1053 REMOVAL, CORROSION WAS FOUND AT FUSELAGE SKIN BTW STA 1000 TO STA 1006 L-26 LH. SUMMARY OF NRC 00688: CORROSION LEVEL 2. FINGER DOUBLER AT STA 946 TO 1006 LONGERON 26 LH WAS REPLACED PER B717-200 SRM 51-41-02-0GSDR DALA2023071405736Unknown · unknownCORROSION ON TRIM PANELS (2 EA) FROM SERVICE DOOR STA Y=148 - Y=200. SUMMARY OF NRC 00472: CORROSION LEVEL 2. TRIM PANELS (2 EA) FROM SERVICE DOOR STA Y=148 - Y=200 WERE REPLACED PER B717 SRM 51-40-08-0G AND DWG 957828 REV AB. (LP #2863315)SDR DALA2023071305679Unknown · unknownAFT F/A READY LIGHT COVER MISSING. RESECURED AFT F/A EMERGENCY LIGHT LENS COVER PER B717 AMM 33-51. A/C OK FOR SVC. (LP #4984108)SDR DALA2023071305678Unknown · unknownCRACKED CUSP WEB BTW STA 658 TO STA 664 RH SIDE AT PAX CABIN. SUMMARY OF NRC 00399: CUSP WEB BTW STA 658 TO STA 664 RH SIDE AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R REPAIR 4. (LP #2862517)SDR DALA2023071305677Unknown · unknownWHILE PERFORMING AA 5530-01048 AND AD 2018-10-08, FOUND 3 CRACK INDICATIONS ON LT. LOWER FIXED LEADING EDGE SKIN (MARKED). COMPLIED WITH ER/A 610352-14AD REV ORIGINAL PRI REV 0. COMPLIED WITH PRI 610352-14AD PRI REV 1, ER/A 610352-14 REV. ORIGINAL MATCHES PRI SDR DALA2023071205667Unknown · unknownFOUND ONE CRACK INDICATION ON RH VERTICAL STAB WHILE PERFORMING AA5530-01048 AND AD 2018-10-08 (MARKED). ONE CRACK INDICATION RH VERTICAL STAB IN SPAR AND WHILE REINSPECTING AREA IN QUESTION WHILE PERFORMING AA5530-01048 AND AD2018-10-08. COMPLIED WITH ER/A 61SDR DALA2023071205666Unknown · unknownR/H VERTICAL STAB, WHILE ACCOMPLISHING INSPECTION PER WORK CARD 5530-0148-02 FAA AD 2018, FOUND A CRACK INDICATION TO ONE HOLE OF THE FRONT SPAR CAP. COMPLIED WITH ER/A 610356-14AD REV ORGINAL PRI REV 0. COMPLIED WITH ER/A 610356-14AD REV ORGINAL PRI REV 1. COSDR DALA2023071205665Unknown · unknownCORROSION TYPE EXFOLATION ON FUSELAGE SKIN (LOWER CUTOUT) AT AFT CARGO COMPARTMENT STA 974. SUMMARY OF NRC 00512: CORROSION LEVEL 2. FUSELAGE SKIN LOWER CUTOUT AT AFT CARGO COMPARTMENT STA 974 WAS REPAIRED PER PRI 610235-14 REV 1 AND ER/A 610235-14 REV ORIGINASDR DALA2023080406299Unknown · unknownER/A 610235-14; FUSELAGE SKIN AFT CARGO DOOR CUTOUT SKIN AND DOUBLER STA Y=954 TO 994, L-28R IS CORRODED. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH ER/A 610235-14, SECTION II REPETITIVE INSPECTION WITHIN 8,000 FLIGHT CYCLES FROM 32,098 TOTAL FLIGHT SDR DALA2023071305676Unknown · unknownFOUR CRACK INDICATIONS ON LH VERTICAL STAB WHILE PERFORMING AA5530- 01048 AND AD 2018-10-08 (MARKED). REINSPECTED AREA FOUND 3 CRACK INDICATIONS IN LOWER SPAR CAP WHILE PERFORMING AA5530-01048 AND AD 2018-10-08. THE ABOVE 3 CRACK INDICATIONS ARE ON LT LOWER SKSDR DALA2023071205664Unknown · unknownCORROSION ON WEBS BTW STA Y=148/218 AND BTW STA X=-60/60 AT PAX CABIN (W1). SUMMARY OF NRC 00373: CORROSION LEVEL 2. WEB STA Y=158/200 AND BTW X=-3.5/-60 AND Y=158/200 AND BTW X 48/60 WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 1 REPAIR 1. (LP #2861223SDR DALA2023071305675Unknown · unknownTHE TAIL CONE RELEASE CAM IS CLOCKED INCORRECTLY. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE ADJUSTED THE RELEASE CAM REF AMDS WORKCARD 5352-2001. (LP #2859456)SDR DALA2023071205670Unknown · unknownTHE EMERGENCY EXIT COVER DIFFUSER LENS IS MISSING AT LOCATION 600. MAINTENANCE REPLACED THE EMERGENCY EXIT COVER AT R1 DOOR. (LP #2858553)SDR DALA2023072606039Unknown · unknownCREW TURNED ON WINDOW ANTI-FOG AND IMMEDIATELY NOTICED SMOKE FROM NEAR WINDOW FIN, ACCOMPANIED WITH AN ELECTRICAL BURN SMELL. CONTRACT MAINTENANCE INSPECTED F/O WINDOW AND CONFIRMED THE SMOKE AND ODOR WHEN THE SWITCH IS TURNED ON. NO EVIDENCE OF SMOKE OR ODOR SDR DALA2023071205663Unknown · unknownCORROSION ON FRAME STA Y=1021 LONGERON 30+1.5 IN RH/LH. SUMMARY OF NRC 00513: CORROSION LEVEL 2. FRAME STA Y=1021 LONGERON 30 WAS REPAIRED PER B717 SRM 53-20-07-2R PROCEDURE 3, REPAIR 3. (LP #2857160)SDR DALA2023071205662Unknown · unknownCORROSION ON BULKHEAD STA 1053 BTW L28R/L28L AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00314: CORROSION LEVEL 2. BULKHEAD DOUBLER STA 1053 BTW L28R/L28L AT AFT CARGO COMPARTMENT (C2) WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2856373)SDR DALA2023071205661Unknown · unknownCORROSION ON RH ANGLE CUSP FROM STA Y=200 TO Y=219 AT PAX CABIN. SUMMARY OF NRC 00253: CORROSION LEVEL 2. RH ANGLE CUSP FROM STA Y=160 TO Y=219 WAS REPAIRED PER ERA 609394-14 REV ORIGINAL SECTION I. PERMANENT REPAIR. ASSOCIATED ER/A 14-609394 ADDED FOR AC 9535SDR DALA2023071205660Unknown · unknownCORROSION ON CUSP ANGLE BTW STA Y=158/171 APROX, BTW STA Y=195/207 APROX AND BTW RBL=54/60 AT PAX CABIN (W1). SUMMARY OF NRC 00413: CORROSION LEVEL 2. CUSP ANGLE BTW STA Y=158/171 APROX, BTW STA Y=195/207 APROX AND BTW RBL=54/60 WAS REPAIRED PER ER/A 609285-14SDR DALA2023071205659Unknown · unknownAFTER REMOVAL OF THE RECHARGEABLE BATTERY ASSEMBLY, THE RECEPTACLE PINS WERE FOUND DAMAGED. THE OVERWING EMERGENCY EVACUATION BATTERY POWER SUPPLY WAS REMOVED PER B717-200 AMM 33-51-06 000-801. SUMMARY OF NRC 00257: THE OVERWING EMERGENCY EVACUATION BATTERY POSDR DALA2023071205669Unknown · unknownTHE AFT EXIT DOOR EMERGENCY LIGHT ILLUMINATED WITH THE SWITCH IN THE ARMED POSITION. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY AND POWER SUPPLY (B5-260) IAW B717 FRM FIM 33-50-00 810-801. OPERATIONAL CHECK WAS GOOD. AIRCRAFT IS OK FOR SERVICE. (LP #4397SDR DALA2023071205668Unknown · unknownTHE EMERGENCY LIGHT IS FLICKERING ON THE L SIDE OF GRATE. IS NOT RELATED TO AIR SWITCH/CONTROLS. *** CONTRACT MAINTENANCE EVENT - OCM: 265651 *** RESET EMERGENCY LIGHT C/B. THE AFT EMERGENCY LIGHTS NOW OPERATES NORMALLY REF B717 AMM 33-51. (LP #2854005)SDR DALA2023070705488Unknown · unknownCRACK ON FRAMES STA=680 AND 715 AND LONGERON 26RH UNDER WING BARREL KEEL BEAMS AND CANTED KEEL INTERNAL STRUCTURE FUSELAGE. SUMMARY OF NRC 00291: FRAMES STA=680 AND 715 AND LONGERON 26RH UNDER WING BARREL KEEL BEAMS AND CANTED KEEL INTERNAL STRUCTURE FUSELAGE SDR DALA2024101109977Skin · dentedPD: SPOILER UPPER SKIN DENTED IN MULTIPLE LOCATIONS / CA: INSPECTED PER CMM CSVE 27-60-02; REPAIRED PER ERA 570523-14TR REV B; ERA 574648-14MA. REV. B; B717 CMM 27-60-02 REV. 07/01/2021. INSPECTED PER CMM CSVE 27-60-02; REPAIRED PER ERA 570523-14TR REV B; ERASDR DALA2023070705489Unknown · unknownTHE MAIN CABIN DOOR GIRT BAR STRAP NOT ATTACHED. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REATTACHED THE GIRT BAR STRAP AS PER B717 AMM 25-61. (LP #4951546)SDR DALA2023070605439Unknown · unknownCORROSION ON FLOOR SUPPORT BELOW ACCESORY COMPARMENT DOOR BTW LBL16 AND RBL16 STA 1053. SUMMARY OF NRC 00367: CORROSION LEVEL 2. FLOOR SUPPORT BELOW ACCESORY COMPARMENT DOOR BTW LBL16 AND RBL16 STA 1053 WAS REPAIRED PER PRI 609849-14 REV 0 AND REV 1 AND ERA 60SDR DALA2023070605438Unknown · unknownCORROSION ON FLOOR SUPPORTS BTW STA Y=197/158 AND LBL=54 AND FLOOR SUPPORTS STA Y=200 AND BTW RBL=44/54 AT PAX CABIN WERE FOUND OUT OF LIMITS (W1). SUMMARY OF NRC 00676: CORROSION LEVEL 2. FLOOR SUPPORTS BTW STA Y=197/158 AND LBL=54 AND FLOOR SUPPORTS STA Y=20SDR DALA2023070605437Unknown · unknownCORROSION ON FLOOR SUPPORTS STA Y=197 AND BTW LBL=15/43 WAS FOUND OUT LIMITS AT PAX CABIN (W1). SUMMARY OF NRC 00677: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=197 BTW LBL=15/43 WAS FABRICATED AND REPLACED PER DWG 99365534 REV BW AND B717-200 SRM 51-41-02-0G AND SDR DALA2023070605440Unknown · unknownSHIP 9579 -DIV- THE AIRCRAFT WAS DIVERTED TO IAD DUE TO A SUSPECTED HIGHER THAN NORMAL FUEL CONSUMPTION. CORRECTIVE ACTION: MAINTENANCE DETERMINED THAT THE CENTER TANK FUEL QUANTITY INDICATION SYSTEM IS FAULTY. CENTER FUEL QUANTITY INDICATION SYSTEM WAS FORWARSDR DALA2023070505394Unknown · unknownCORROSION ON CUSP ANGLE (LWR SURFACE AREA) BTW STA Y=200 AND X=55 TO X=60 AT PASSENGER CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00633: CORROSION LEVEL 2. CUSP ANGLE (LWR SURFACE AREA) BTW STA Y=200 AND X=55 TO X=60 AT PASSENGER CABIN FLOOR STRUCTURE WAS REPAIRED SDR DALA2023070505393Unknown · unknownFLOOR SUPPORT STA Y=200 LBL=6 WAS FOUND CORRODED OUT OF LIMITS AT PAX CABIN (W1). SUMMARY OF NRC 00678: CORROSION LEVEL 2. FLOOR SUPPORT STA Y=200 LBL=6 TO RBL=6 WAS REPLACED PER B-717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #2849660)SDR DALA2023070405377Unknown · unknownTHE CEILING EMERGENCY EXIT LIGHT COVER FELL OFF AT ROW 22. MAINTENANCE RESECURED THE LIGHTING COVER. THE AIRCRAFT IS NOW OK FOR SERVICE. (LP #8310082)SDR DALA2023070405375Unknown · unknownTHE EMERGENCY EXIT LIGHT LENS COVER AT ROW 19 NEEDS TO BE REATTACHED. MAINTENANCE ATTACHED THE EMERGENCY LIGHT LENS COVER AT ROW 19CDE. THE AIRCRAFT IS OK FOR SERVICE. (LP #4642349)SDR DALA2023070405374Unknown · unknownCORROSION ON INTERCOSTAL BTW STA Y=946-954 AND LONGERON 30 TO 29RH AT AFT CARGO COMPARTMENT (C2). SUMMARY OF NRC 00181: CORROSION LEVEL 2. INTERCOSTAL BTW STA Y=946-954 AND LONGERON 30 TO 29RH AT AFT CARGO COMPARTMENT (C2) WAS REPLACED PER B717 SRM 51-41-02-0GSDR DALA2023070405373Unknown · unknownCORROSION ON DOOR JAMB SEVERAL POINTS AT AFT COMPARTMENT (C2). SUMMARY OF NRC 00176: CORROSION LEVEL 2. DOOR JAMB AT AFT COMPARTMENT WAS REPLACED PER B717 SRM 51-41-02-0G & 51-41-05-0G. (LP #2848116)SDR DALA2023070405372Unknown · unknownCRACK ON MEMBRANE (LWR SEAT TRACK AREA) IN STA Y=220 AND X=55 AT PASSENGER CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00648: MEMBARANE WAS REPLACED PER B717-200 SRM 53-00-55-0R PROCEDURE 4 REPAIR 4 AND 53-20-51-0I PROCEDURE 1. (LP #2847901)SDR DALA2023070405371Unknown · unknownDURING REMOVAL OF FLOOR SUPPORT, CRACK AND CORROSION ON CUSP WEB Y=199 TO Y=160 X54 (CPAX) WAS FOUND. SUMMARY OF NRC 00598: CORROSION LEVEL 2. CUSP WEB WAS REPAIRED PER B-717-200 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #2847871)SDR DALA2023070405370Unknown · unknownCRACK ON INTERCOSTAL STA 636 X=0 CEILING AREA, FWD CARGO. SUMMARY OF NRC 00507: INTERCOSTAL STA 636 X=0 CEILING AREA WAS REPAIRED PER B717 SRM 51-70-11-2R PROCEDURE 1. (LP #2847519)SDR DALA2023070405369Unknown · unknownCORROSION ON FLOOR SUPPORT OF MAIN ENTRANCE DOOR FROM STA Y=162 TO STA Y=194 & LBL 54 AT PASSENGER CABIN (CPAX). SUMMARY OF NRC 00381: CORROSION LEVEL 2. SUPPORT WAS FABRICATED AND REPLACED PER DWG S00074, B-717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #284750SDR DALA2023070405368Unknown · unknownPUNCTURES (2 EA) ON CTR FIXED GUIDE VANE UPPER SKIN AT RH WING. SUMMARY OF NRC 00172: CTR FIXED GUIDE VANE UPPER SKIN AT RH WING WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1. (LP #2847265)SDR DALA2023070305312Unknown · unknownPUNCTURES (4 EA) ON INBR FIXED GUIDE VANE UPPER SKIN AT RH WING. SUMMARY OF NRC 00033: INBR FIXED GUIDE VANE UPPER SKIN AT RH WING WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1. PERFORM DECAL INSPECTION CONDITION EVERY "C" CHECK PER TOPP 30-10SDR DALA2023070305311Unknown · unknownDENTS (2 EA) ON INBR FIXED GUIDE VANE LOWER SKIN AT RH WING. SUMMARY OF NRC 00178: DENTS (2 EA) WITH THE MEASUREMENTS OF: DENT1 "D DIAMETER=2.000 IN, X DEPTH=0.0450, RATIO=44.444". DENT2 "D DIAMETER=1.200 IN, X DEPTH=0.0150, RATIO=80". (ET) HFEC WAS ACCOMPLISHSDR DALA2023070305310Unknown · unknownCORROSION ON LONGERON END 24 RH BTW FRAME 1022 TO 1002 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00212: CORROSION LEVEL 2. LONGERON END 24 RH BTW STA Y=1022-Y=1002 WAS REPLACED PER B717-200 SRM 51-41-05-0G. (LP #2846590)SDR DALA2023070305309Unknown · unknownCORROSION ON WEB SEVERAL POINTS AT AREA DOOR AFT COMPARTMENT (ENTRY AREA) (C2). SUMMARY OF NRC 00175: CORROSION LEVEL 2. WEB AREA DOOR AFT COMPARTMENT WAS REPLACED PER B717 SRM 51-41-02-0G & 51-41-05-0G. (LP #2846580)SDR DALA2023070305308Unknown · unknownCORROSION ON FRAME CLIP STA 1002 LONGERON 29RH TO 29LH AT AFT CARGO. SUMMARY OF NRC 00496: CORROSION LEVEL 2. FRAME CLIP STA 1002 LONGERON 29RH TO 29LH WAS REPLACED PER B717 SRM 51-41-02-0G. (LP #2846532)SDR DALA2023070305307Unknown · unknownCORROSION ON FLOOR SUPPORTS BTW STA Y=158/200 AND RBL=44, STA Y=179 AND BTW RBL=8/43, STA Y=200 AND BTW RBL=8/44. SUMMARY OF NRC 00604: CORROSION LEVEL 2. FLOOR SUPPORTS (3 EA) WERE REPLACED PER B717-200 SRM 51-40-02-0G AND 51-41-05-0G PAR 8.A. (LP #2846527)SDR DALA2024022002335Hinge Fitting · corrodedCORROSION ON INBD/OUTBD ATTACHMENT POINTS OF CENTER WING FLAP HINGE FITTING STA 251.6 AT LH WING REAR SPAR. SUMMARY OF NRC 00167: CENTER WING FLAP HINGE FITTING STA 251.6 AT LH WING REAR SPAR WAS REPLACED PER B717 AMM 57-55-25. LEVEL N/A BECAUSE IS NOT A PRIMASDR DALA2024022002330Panel · corrodedAREA OF CORROSION NOTED DIRECTLY FWD OF LEFT SLANT PANEL (MARKED). COMPLIED WITH ERA 610004-14 REV ORIG. PRI 610004-14 REV 0 MATCHES ERA 610004-14 REV ORIG. ASSOCIATED ERA 14-610004 ADDED FOR AC 9503. (LP #2846122)
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