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 DALA2023032602319Unknown · unknownSHIP 9574-ATB-DE/ENVIROMENTAL. PERFORMED AN AIR RETURN DUE TO A BIRD STRIKE TO THE RADOME AND LOSS OF WEATHER RADAR. CORRECTIVE ACTION: MAINTENANCE PERFORMED A BIRD STRIKE INSPECTION, REPLACED THE RADOME AND THE WEATHER RADAR DRIVE UNIT ASSEMBLY. (LP 4043168,4SDR DALA2023032602318Unknown · unknownAIRCRAFT 9513, INITIAL INSPECTION: CORROSION ON FLOOR SUPPORTS BTW STA Y=148 TO STA Y= 200 AND BTW X=-43 TO X=-54. CORRECTIVE ACTION: FLOOR SUPPORTS BTW STA Y=148 TO STA Y= 200 AND BTW X=-43 TO X=-54 WERE REPLACED PER B717-200 SRM 51-41-02-0G. (LP 2686942)SDR DALA2023032602317Unknown · unknownAIRCRAFT 9571, CORROSION AT SLIDE SUPPORTS LOCATED AT RBL 53 BETWEEN STA-163 AND STA-186. CORRECTIVE ACTION: NEW SUPPORTS (2EAS) WERE REPLACED PER B717-200 SRM 51-41-01-0G PAR 6. (LP 2686865)SDR DALA2023032602316Unknown · unknownAIRCRAFT 9513, INITIAL INSPECTION: CORROSION ON LONGERON END 24RH STA Y 944 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: CLIP ON LONGERON END 24RH STA Y 944 AT AFT CARGO COMPARTMENT WAS REPLACED PER B-717-200 SRM 51-40-02-0G. AND SRM 51-41-05-0G. (LP 2686715)SDR DALA2023032602315Unknown · unknownAIRCRAFT 9571, DURING OK TO TREAT RH WING BOX AREA WITH CIC, CRACKED CUSP MEMBRANE WEB WAS FOUND ON STA Y= 715-720 X=-44 AT PASSENGER CABIN FLOOR STRUCTURE. CORRECTIVE ACTION: CUSP MEMBRANE WEB ON STA Y= 715-720 X=-44 AT PASSENGER CABIN FLOOR STRUCTURE WAS REPSDR DALA2023032602314Unknown · unknownAIRCRAFT 9577, TAIL COMPT FRAME CRACKED STA 1133 AT STR 2R-MARKED. CORRECTIVE ACTION: COMPLIED WITH ER/A 607133-14 REV. ORIG. PRI REV. "0" ALL INSTRUCTIONAL STEPS. I ALL INSTRUCTIONAL STEPS ON ER/A 607133-14 REV. ORIG. PRI REV. "0" MATCH FINALE ER/A 607133-14 SDR DALA2023032602313Unknown · unknownAIRCRAFT 9513, INITIAL INSPECTION: CORROSION ON RH CUSP WEB STA. Y= 198 TO Y=202 (R1) RBL50 AT PASSENGER CABIN. CORRECTIVE ACTION: RH CUSP WEB STA. Y=200 TO Y=218 (R1) RBL50 AT PASSENGER CABIN WAS FABRICATED AND REPLACED PER DWG 9936535 REV. CS ITEM: -95 AND BSDR DALA2023032402308Unknown · unknownAIRCRAFT 9513, CORROSION ON DIAPHRAGM STA Y=200 RBL45 - 55 (UNDER R1) VIEW FROM E/E COMPARTMENT. CORRECTIVE ACTION: REPAIR ON DIAPHRAGM STA Y=200 RBL45 - 55 (UNDER R1) VIEW FROM E / E COMPARTMENT WAS PERFORMED PER B-717-200 SRM 51-70-10 REPAIR 2 PAR. 4 FIG. 20SDR DALA2023032402307Unknown · unknownAIRCRAFT 9513, CUSP ANGLE ON R1 DOOR JAMB WAS FOUND CORROSION ON CUSP WEB TO BTW STA 218 TO STA 237 RH. CORRECTIVE ACTION: CUSP WEB TO BTW STA 218 TO STA 237 RH WAS FABRCATED AND REPAIRED PER B 717-200 SRM 53-00-55-2R-4 FIG 226, DWG 9930538-109 REV. CC AND WASSDR DALA2023032402306Unknown · unknownAIRCRAFT 9513, CUSP ANGLE ON R1 DOOR JAMB WAS FOUND CORROSION ON ANGLE SUPPORT BTW STA 137 TO STA 160. CORRECTIVE ACTION: ANGLE WAS FABRICATED PER DWG 5910085 REV DE. (LP 2685491)SDR DALA2023032402305Unknown · unknownAIRCRAFT 9513, CUSP ANGLE ON R1 DOOR JAMB WAS FOUND CORROSION ON ANGLE SUPPORT BTW STA 200 TO STA 210. CORRECTIVE ACTION: ANGLE SUPPORT WAS REPLACED PER DRAWING 5910085 ITEM 15 REV. DJ. (LP 2685489)SDR DALA2023032402304Unknown · unknownAIRCRAFT 9513, CORROSION ON FLOOR SUPPORTS BTW STA Y=148 TO STA Y= 200 AND BTW X=-9 TO X=-42. CORRECTIVE ACTION: FLOOR SUPPORTS WERE REPLACED PER DWG 9936534 REV. BW AND PER B717-200 SRM-51-41-02-0G PAR. 4. (LP 2685485)SDR DALA2023032402303Unknown · unknownAIRCRAFT 9513, CRACKS (2EAS) AND ELONGATED HOLES ON LH CUSP WEB BTW STA=656 TO STA=715 AND X=44 TO X=60 AT PAX CABIN. CORRECTIVE ACTION: CUSP WEB BTW STA=656 TO STA=715 AND X=44 TO X=60 AT PAX CABIN WAS FABRICATED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 REPAISDR DALA2023032302264Unknown · unknownAIRCRAFT 9551, INITIAL INSPECTION: CRACK ON BEAM NO. 2 STA Y=157 AT PASSENGER FWD ENTRANCE DOOR (L1). CORRECTIVE ACTION: BEAM NO. 2 STA Y=157 AT PASSENGER FWD ENTRANCE DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 8 REPAIR 8. (LP 2683386)SDR DALA2023032302263Unknown · unknownAIRCRAFT 9551, INITIAL INSPECTION: CRACK ON UPPER BEAM NO. 1 STA Y=157 AND STA Y=194 AT PASSENGER DOOR (L1). CORRECTIVE ACTION: UPPER BEAM NO. 1 STA Y=157 AND STA Y=194 AT PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP 26828SDR DALA2023032202172Unknown · unknownAIRCRAFT 9538, EMERGENCY LIGHTS ROW 3-11 INOP. CORRECTIVE ACTION: REPLACED THE BATTERY PACK B5-227. (LP 9653534)SDR DALA2023032202171Unknown · unknownAIRCRAFT 9513, CRACK ON FITTING ON FWD PAN NEAR TO BEAM 1 OF AFT CARGO COMPARTMENT DOOR WAS FOUND. CORRECTIVE ACTION: FITTING ON FWD PAN NEAR TO BEAM 1 OF AFT CARGO COMPARTMENT DOOR WAS FABRICATED AND REPLACED PER B717-200 SRM 51-41-01-0G, SRM 51-41-05-0G AND SDR DALA2023032202170Unknown · unknownAIRCRAFT 9513, INITIAL INSPECTION: CORROSION ON FLOOR SUPPORT BTW STA Y= 200 TO STA Y=218 AND X=-11 AT CABIN PAX. CORRECTIVE ACTION: FLOOR SUPPORT BTW STA Y= 200 TO STA Y=218 AND X=-11 AT CABIN PAX WAS REPLACED PER B717-200 SRM 51-41-05-0G. PAR.8. (LP 2681442)SDR DALA2023032202169Unknown · unknownAIRCRAFT 9513, INITIAL INSPECTION: CRACK ON FRAME BTW STA=1037 BTW LONGERON 17RH AND LONGERON #18RH OF PAX CABIN. CORRECTIVE ACTION: REPAIR WAS PERFORMED PER B717-200 SRM 53- 20-07-2R PROCEDURE 4 REPAIR 4. (LP2680687)SDR DALA2023032202168Unknown · unknownAIRCRAFT 9513, INITIAL INSPECTION: CRACK ON UPPER PAN STA Y 389 AT FWD CARGO COMPARTMENT DOOR. CORRECTIVE ACTION: UPPER PAN ON STA Y 389 AT FWD CARGO COMPARTMENT DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1, REPAIR 1 PAR. (LP2680219)SDR DALA2023031802045Unknown · unknownAIRCRAFT 9513, INITIAL INSPECTION: CORROSION AND CRACK ON LH CUSP WEB (UPPER-LOWER SURFACE) STA. Y= 636 TO Y=655 AT PASSENGER CABIN. CORRECTIVE ACTION: LH CUSP WEB ON STA. Y=636 TO Y=655 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 SDR DALA2023031802044Unknown · unknownAIRCRAFT 9513, INITIAL INSPECTION: CRACK ON INNER AFT PAN ABOVE BEAM 5 AT FWD CARGO DOOR. CORRECTIVE ACTION: INNER AFT PAN ABOVE BEAM 5 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1, REPAIR 1. (LP 2675859)SDR DALA2023031802047Unknown · unknownAIRCRAFT 9577, TAIL COMPT STR 2L CRACKED AT STA 1133. CORRECTIVE ACTION: REPAIRED PER B717 SRM 53-00-05-2R PROCEDURE 2. (LP 2675309)SDR DALA2023031802046Unknown · unknownSHIP 9512 - MISC/HYD - DECLARED EMERGENCY FOR THE RIGHT HYDRAULIC SYSTEM QUANTITY DROPPING. CORRECTIVE ACTION: FOUND RUDDER LIMITER ACTUATOR LINE LEAKING. FOUND LEAK ON PIPE ASSY CONNECTED TO RUDDER LIMITER CONTROL. PIPE WAS CHAFING AGAINST WORN ADEL CLAMP (91SDR DALA2023031802043Unknown · unknownAIRCRAFT 9513, INITIAL INSPECTION: CORROSION ON LUGS (FLOOR SUPPORT) STA=147 BTW RBL=30 TO RBL=50 AT COCKPIT. CORRECTIVE ACTION: FLOOR SUPPORT ON STA=147 BTW RBL=30 TO RBL=50 AT COCKPIT FABRICATED PER DWG 9936533-89 REV. CM AND WAS REPLACED PER B717-200 SRM 51SDR DALA2023031802042Unknown · unknownAIRCRAFT 9513, INITIAL INSPECTION: CRACK ON BEAM NBR 1, (FWD EDGE) OF L1 PASSENGER ENTRANCE DOOR. CORRECTIVE ACTION: ENTRANCE DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP 2675276)SDR DALA2023031802041Unknown · unknownAIRCRAFT 9513, INITIAL INSPECTION: CRACK INTERCOSTAL ATTACH LOWER PAN STA Y 389 AT FWD CARGO COMPARTMENT DOOR. CORRECTIVE ACTION: INTERCOSTAL ATTACH LOWER PAN STA Y 389 AT FWD CARGO COMPARTMENT DOOR WAS REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 51-41-05-0GSDR DALA2023031802040Unknown · unknownAIRCRAFT 9513, INITIAL INSPECTION: CRACK ON CLIP ON LOWER PAN SECTION STA Y 389 AT FWD CARGO COMPARTMENT DOOR. CORRECTIVE ACTION: CLIP OF LOWER PAN SECTION STA Y 389 AT FWD CARGO COMPARTMENT DOOR WAS REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G. (SDR DALA2023031702017Unknown · unknownAIRCRAFT 9513, INITIAL INSPECTION: CRACKED RH CUSP WEB STA. Y=389 (UNDER SEAT TRACK) AT PASSENGER CABIN. CORRECTIVE ACTION: RH CUSP WEB STA. Y=389 (UNDER SEAT TRACK) AT PASSENGER CABIN. WAS REPAIRED PER B717-200 SRM 53-00-55-2R. REP. 4. (LP2674411)SDR DALA2023031702016Unknown · unknownAIRCRAFT 9513, INITIAL INSPECTION: CRACK ON CLIP ON LOWER PAN SECTION STA Y 427 AT FWD CARGO COMPARTMENT DOOR. MAINTENANCE ACTION: CLIP ON LOWER PAN SECTION STA Y 427 WAS REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP 2674408)SDR DALA2023040402603Unknown · unknownSHIP 9512 -HYD/MISC- THE FLIGHT CREW DECLARED AN EMERGENCY FOLLOWING THE ILLUMINATION OF THE "RIGHT HYD LO" MESSAGE AND THE RIGHT HYDRAULIC SYSTEM QUANTITY DROPPING. THE QRH WAS COMPLIED WITH AND THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE FOUNDSDR DALA2023040402600Unknown · unknownA TRAY TABLE WAS DISCOVERED TO BE INSTALLED IN THE EMERGENCY EXIT ROW ON SEAT 21B. THIS COULD PREVENT PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REMOVED TRAY TABLE ASSEMBLY FROM THE SEAT BACK. THE AIRCSDR DALA2023031702015Unknown · unknownAIRCRAFT 9513, INITIAL INSPECTION: CRACK ON FITTING ATTACH UPPER PAN STA Y 389 AT FWD CARGO COMPARTMENT DOOR. MAINTENANCE ACTION: UPPER FITTING STA Y 389 WAS REPLACED PER B717-200 SRM 51-41-02-0G AND SRM 51-41-05-0G. (LP 2673904)SDR DALA2023031702008Unknown · unknownAIRCRAFT 9513, INITIAL INSPECTION: CRACKED RH CUSP WEB (2 EA) STA. Y= 655 TO Y=674 AT PASSENGER CABIN. CORRECTIVE ACTION: CUSP WEB RH (2 EA) STA. Y= 655 TO Y=674 AT PASSENGER CABIN WERE REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4. CONFIGURATION 7003 CUSPSDR DALA2025013000727Skin · corroded-AD- CENTER WING BOX LOWER SKIN XCW=20 TO XCW=42 REAR SPAR TO STRINGER #12 HAS CORROSION AND ELONGATED HOLES. REPAIR APPROVAL IS LIMITED TO 24 MONTHS FROM 14MAR23. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE OF THIS RSDR DALA2023031702019Unknown · unknownSHIP 9500 -ATB- THE CREW DECLARED AN EMERGENCY AND RETURNED THE AIRCRAFT MYR DUE THE #2 BRAKE OVER TEMPERATURE WARNING ILLUMINATING. QRH PROCEDURES FAILED TO LOWER THE TEMPERATURE INDICATION. THE LANDING WAS UNEVENTFUL AND THE AIRCRAFT BRAKING WAS NORMAL. CORRSDR DALA2023031601914None · noneONE CATWALK CEILING EMERGENCY LIGHT IN THE TAIL COMPARTMENT IS INOPERATIVE. MAINTENANCE REPLACED THE PSU ASSEMBLY ABOVE THE AFT RIGHT LAVATORY. OPERATIONAL CHECK WAS GOOD. (LP #4026860)SDR DALA2023031601913Unknown · unknownDAMAGE T: HOLE CAUSED BY TOOLING DAMAGE ON ELEVATOR RH BTW XHR 214 AND XHR 218.762, AND 13 INCHES FWD APROX OF ELEVATOR TRAILING EDGE. SUMMARY OF NRC 00680: ELEVATOR RH BTW XHR 214 AND XHR 218.762, AND 13 INCHES FWD APROX OF ELEVATOR TRAILING EDGE WAS REPAIREDSDR DALA2023031501886Unknown · unknownIN REF NRC 00485 CORROSION ON RH CUSP WEB BTW STA Y=600 TO Y=615 AT PAX CABIN. SUMMARY OF NRC 00640: CORROSION LEVEL 2. CUSP WEB BTW STA Y=600 TO Y=615 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIGURE 216. (LP #2671432)SDR DALA2023031501887Unknown · unknownSHIP 9574 -ATB- THE FLIGHT CREW ACCOMPLISHED AN AIR TURN BACK AFTER THE CONTROL TOWER INFORMED THEM OF SOMETHING OBSERVED TRAILING THE AIRCRAFT. THE CREW CONFIRMED A 2000# FUEL IMBALANCE BETWEEN THE LEFT AND THE RIGHT WING TANK QUANTITIES. THE LANDING WAS UNEVSDR DALA2023031401856Unknown · unknownTHE FORWRD EMERGENCY OVERWING LIGHTS ARE INOPERATIVE. MAINTENACE REPLACED THE EMERGENCY BATTERY POWER SUPPLY B5-118 IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #4076686)SDR DALA2023031401854Unknown · unknownTHE OVERHEAD EMERGENCY LIGHT OVER THE CATWALK IS INOPERATIVE. MAINTENACE REPLACED THE POWER SUPPLY B5-116 REF B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. OK FOR SERVICE. (LP #4076685)SDR DALA2023031401853Unknown · unknownCRACK ON INTERNAL ANGLE ON AFT PAN MIDDLE SECTION AT LH FWD OVERWING EMERGENCY EXIT DOOR. (PTAS) SUMMARY OF NRC 00073: INTERNAL ANGLE AT LH FWD OVERWING EMERGENCY EXIT DOOR WAS FABRICATED AND REPLACED PER DWG 9957735 REV G, B717-200 SRM 51-41-02-0G AND 51-41-0SDR DALA2023031401855Unknown · unknownTHE AFT 3 CENTER AISLE CEILING EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENACE REPLACED THE EMERGENCY LIGHT BATTERY PACK ROW 24-29 IAW B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT IS OK FOR SERVICE. (LP #9989192)SDR DALA2023031401852Unknown · unknownINTERFERENCE BETWEEN FITTING TO ATTACH RIGHT WING FLAP MOVABLE VANE CABLE AND PLATE THROUGH UPPER ACCESS PANEL 630AF AT RH WING FLAP INTERNAL STRUCTURE. SUMMARY OF NRC 00105: FITTING TO ATTACH RIGHT WING FLAP MOVABLE VANE CABLE AND PLATE THROUGH UPPER ACCESS PSDR DALA2023031401851Unknown · unknownINTERFERENCE BETWEEN FITTING TO ATTACH LEFT WING FLAP MOVABLE VANE CABLE AND PLATE THROUGH UPPER ACCESS PANEL 530AF AT LH WING FLAP INTERNAL STRUCTURE. SUMMARY OF NRC 00060: FITTING TO ATTACH LEFT WING FLAP MOVABLE VANE CABLE AND PLATE THROUGH UPPER ACCESS PANSDR DALA2023031401850Unknown · unknownCRACKED ON FWD PAN OF LH FWD OVERWING EMERGENCY EXIT DOOR. SUMMARY OF NRC 00655: FWD PAN OF LH FWD OVERWING EMERGENCY EXIT DOOR WAS REPAIRED PER B717-200 SRM 52-20-02-2R. (LP #2667352)SDR DALA2023031401849Unknown · unknownCORROSION AT INTERNAL FUSELAGE SKIN ON STA Y=636 TO Y=655 BTW STR 29LH AND STR 29RH AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00189: CORROSION LEVEL 2. CORROSION AT INTERNAL FUSELAGE SKIN ON STA Y=636 TO Y=655 BTW STR 29LH AND STR 29RH AT FWD CARGO COMPARTMENT SDR DALA2023031401848Unknown · unknownDENT ON ELEVATOR RH BTW XHS 55 AND XHS 76, AND 12.5 INCHES FWD APROX OF ELEVATOR TRAILING EDGE. SUMMARY OF NRC 00679: DENT ON ELEVATOR RH BTW XHS 55 AND XHS 76, AND 12.5 INCHES FWD APROX OF ELEVATOR TRAILING EDGE WAS REPAIRED PER B717-200 SRM 51-70-13-2R-1. ALSDR DALA2023031501885Unknown · unknownNLG WHEEL WELL AFT FRAME FOR GEAR DOOR CUTOUT DAMAGED 2 PLACES. (MARKED) SUMMARY SEE NRC 005-0003:3221-4001/002 00005: REPLACED NLG WHEEL WELL AFT FRAME FOR GEAR DOOR CUT OUT FRAME PER B717 SRM 53-10-15-2. AND DAC DWG 5913421. (LP #2665497)
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