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 DALA2024041204362Cusp Web · corrodedCRACK ON LH CUSP WEB (BELOW) STA Y=655 TO 715 AND X=55 APPROX AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00596: LH CUSP WEB (BELOW) STA Y=655 TO 715 AND X=55 APPROX AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP SDR DALA2024041204361Pan · corrodedCORROSION ON LOWER PAN AREA AT AFT CARGO DOOR JAMB. SUMMARY OF NRC 0070: CORROSION LEVEL 2. LOWER PAN AREA AT AFT CARGO DOOR JAMB WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G AND WAS REPAIRED PER B717-200 SRM 53-00-15-2R PROCEDURE 1. (LP #0289228)SDR DALA2024041204360Doubler · corrodedCORROSION ON INTERNAL PRODUCTION DOUBLER BTW PAN AND FUSELAGE SKIN AT AFT CARGO COMPARTMENT LOWER DOOR JAMB. SUMMARY OF NRC 0273: CORROSION LEVEL 2. INTERNAL PRODUCTION DOUBLER BTW PAN AND FUSELAGE SKIN AT AFT CARGO COMPARTMENT LOWER DOOR JAMB WAS REPAIRED PERSDR DALA2024041204359Web · crackedCRACK ON OUT WEB AREA STA 674 PROYECTION L 14L AT LH FWD EMERGENCY DOOR. SUMMARY OF NRC 00252: OUTER WEB AREA STA 674 PROYECTION L 14L AT LH FWD EMERGENCY DOOR WAS REPAIRED PER B717-200 SRM 52-20-02-2R REPAIR 1. (LP #0288528)SDR DALA2024041204358Beam · crackedCRACK ON AFT PANE BEAM 5 AT FWD CARGO DOOR. SUMMARY OF NRC 00242: AFT PANE BEAM 5 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0287685)SDR DALA2024062106298Floor Panel · gougedFWD CARGO FLOOR PANEL HAS GOUGE AND UPPER SURFACE CRACKED. REPAIRED FLOOR PANEL 121NF FWD CARGO IAW B717-200, SRM 53-20-50-2R, ACCOMPLISH PERMANENT REPAIR WITHIN 500 FLIGHT HOURS PARTS REQUIRED 9936599-501 PANEL OR MATERIAL S00096. REDEFERRED LOG TO QC, ESTAB SDR DALA2024041204357Door Frame · corrodedCORROSION ON AFT CARGO DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00091: CORROSION LEVEL 2. AFT CARGO DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPLACED PER B717 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7, 51-41-05-0G, AND 51-41-02-0G. (LP #0287200)SDR DALA2024041004264Union · leakingAN EMERGENCY WAS DECLARED WITH ATC DUE TO THE RIGHT HYDRAULIC FLUID QUANTITY DECREASING. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR DOWN TEE ASSEMBLY. OPERATIONAL AND LEAK CHECKS WERE BOTH GOOD. THE AIRCRAFT HAS RETURNED TO SERVICE. (LP #5300792)SDR DALA2024041004262Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN LOCATED Y=1022 BETWEEN L-9L AND L-8L. SUMMARY OF NRC 00496: CRACK ON EXTERNAL FUSELAGE SKIN LOCATED Y=1022 BETWEEN L-9L AND L-8L WAS REPAIRED PER PRI 616777-14 REV 1 AND ERA 616777-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR.SDR DALA2024041004263Screw · damagedAD - BURRS WERE FOUND ON THE THREADS OF THE ACME SCREW AT THE HORIZONTAL STABILIZER. SUMMARY NRC 00437: HORIZONTAL STABILIZER JACKSCREW ASSEMBLY WAS REPLACED UNDER AMDS 2740-01114-05. (LP #0282538)SDR DALA2024040804184Lens · wrong partPASSENGER EXIT SIGN IS MISSING THE WORD "EXIT". MISSING FROM LIGHT NEAREST CLOSET. MAINTENANCE FOUND THAT THE SIGN HAD BEEN INSTALLED BACKWARDS. ADJUSTED FWD CABIN EXIT SIGN PER B717 AMM 33-51. (LP #4601783)SDR DALA2024040804186Hinge Fitting · wornCORROSION AND WEAR IN THE HINGE BOLT BORE OF THE OUTBOARD FLAP IDLER HINGE ON THE RH WING. ER/A 541841-14 ISSUED FOR REPAIR. THIS IS THE LOG PAGE THAT TRACKS THE DTA REQUIREMENTS FOR ER/A 541841-14. DTA MUST BE ACCOMPLISHED WITHIN 24 MONTHS. ENGINEERING PURPOSSDR DALA2024040804185Hinge Fitting · wornCORROSION AND WEAR IN THE HINGE BOLT BORE OF THE OUTBOARD FLAP IDLER HINGE ON THE RH WING. ER/A 541845-14 ISSUED FOR REPAIR. THIS IS THE LOG PAGE THAT TRACKS THE DTA REQUIREMENTS FOR ER/A 541845-14. DTA MUST BE ACCOMPLISHED WITHIN 24 MONTHS. ENGINEERING PURPOSSDR DALA2024041004265Jackscrew · damagedAD - DURING HORIZONTAL STABILIZOR JACKSCREW INSPECTION FOUND NICKS ON THE JACKSCREW THREADS. REPLACED JACKSCREW REF TO AMDS CARD #2740-01114-05 AND B717 AMM 27-41-04-401. OK TO INSTALL P/A BY QC5363, INSTALL BUY OFF OF HORIZONTAL STABILIZER ACTUATOR P/A BY QC2SDR DALA2024040804183Door Frame · damagedCRACK DOOR ON FRAME DOOR ANGLE BTW STA 195 (AFT UPPER CORNER) AT FWD SERVICE DOOR R1. SUMMARY OF NRC 00075: ANGLE WAS FABRICATED PER DOUGLAS AIRCRAFT COMPANY DRAWING: 9911579 REV: L AND REPLACED PER B717-200 SRM 51-41-05-0G. (LP #0279803)SDR DALA2024040804182Beam · damagedCRACK BEYOND STOPDRILL, (PREVIOUS REPAIR) ON DOOR BEAM 1 BTW STA 190-200 (UPPER AFT CORNER) AT FWD PASSENGER DOOR L1. SUMMARY OF NRC 00071: DOOR BEAM 1 BTW STA 190-200 (UPPER AFT CORNER) AT FWD PASSENGER DOOR L1 WAS REPAIRED PER B717-200 SRM 52-10-02-2R, PROCESDR DALA2024040504135Skin · dentedDENT ON EXTERNAL FUSELAGE SKIN STA Y=588 AND LONG 30 ABOVE BUTT SPLICE. SUMMARY OF NRC 00338: DENT ON EXTERNAL FUSELAGE SKIN STA Y=588 AND LONG 30 ABOVE BUTT SPLICE WAS REPAIRED PER PRI 616805-14 REV 1 AND ER/A 616805-14 REV ORIG. SECTION I. ACCOMPLISH SECTIONSDR DALA2024040504134Spar · crackedCRACK ON REAR SPAR XRS 150 AT LH WING. SUMMARY OF NRC 0054: REAR SPAR XRS 150 AT LH WING WAS REPAIRED PER ERA 615810-14 REV ORIGINAL SECTION I: TEMPORARY REPAIR. TIME CONTROLLED ITEMS, SEC II ACCOMPLISH SECTION II: INITIAL HFEC SURFACE INSPECTION AND DVI PRIORSDR DALA2024040404051Web · corrodedCORROSION ON L1 DOOR JAMB WEB STA Y=200-207, BTW LONG 17LH-18LH. SUMMARY OF NRC 00651: CORROSION LEVEL 2. CORROSION ON L1 DOOR JAMB WEB STA Y=200-207, BTW LONG 17LH-18LH WAS REPAIRED PER PRI 616779-14 REV 1 AND ER/A 616779-14 REV ORIGINAL SECTION I: PERMANENT SDR DALA2024040504130Nut · out of limitsAD -- DURING FUNCTIONAL TEST OF THE TRIM ACME SCREW AND NUT FOUND DIMENSION BG IS OUT OF LIMIT. UNSAFTIED TURNBUCKLE CONNECTING CABLES 130B TO 130A AND CABLE TURNBUCKLE TO 129B AND 129A. BROKE SAFTEY WIRE ON STOP BOLT (AB) PER B717 AMM 27-40-00 FIGURES 504 ANDSDR DALA2024040504129Battery · inoperativeTAIL CONE INTERIOR EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND POWERPACK REF B717 AMM 33-51-04. OPERATIONAL CHECK WAS GOOD. (LP #0275902)SDR DALA2024040404052Battery · inoperativeON SERVICE CHECK, FOUND AFT OVERWUNG EXIT SIGNS ABOVE DOOR TO BE INOPERATIVE. MAINTENANCE FOUND THE BATTERY CASE CRACKED. INSTALLED NEW BATTERY IAW B717 AMM 33-51-04. REPLACED POWER PACK ASSY PER B717 AMM 33-51-04. OPERATIONAL CHECK WAS GOOD. (LP #0275763)SDR HALA20240405019Indication Sys · false indicationHYD L TEMP HI INDICATION DURING TAXI ONTO RUNWAY EXIT RUNWAY RETURN TO GATE AFTER CYCLING FLIGHT CONTROLS AND INDICATION REMAINING. PERFORMED FIM 29-30 TASK 803 TO STEP D(2) NEED TO CONTINUE FROM STEP D(3) ENG RUN 24094 4/2/24 RAN #1 ENG & OPERATED L HYD SYSSDR HALA20240403018Engine · faultedFLIGHT DECK CREW AND CABIN HEARD 2 LOUD POPS. ENG LEFT COMPRESSOR STALL ALERT CAME ON. CREW FOLLOWED QRH CHECKLIST, LEFT ENGINE WAS SHUT DOWN. ENG GAUGES SHOWED ERRATIC INDICATIONS. TGT WENT TO 940. REMOVED #1 ENG PER TC E1128-717-72-003-REMOVAL. INSTALLED #1 SDR DALA2024040504131Support · crackedAD -- DURING JACK SCREW LUBE, CYCLED HORIZ STAB FULL NOSE UP, SUPPORT ASSY CONTACTED STOP AND CRACKED. REMOVED HORIZONTAL STABILIZER ACTUATOR ASSEMBLY AND REPLACED JACKSCREW FOR HORIZONTAL STAB PER B717 AMDS WORKCARD 2740-0114-05. ALL RII TASK COMPLETE. (LP #5SDR DALA2024040203984Connector · dirtySHIP 9501 -MISC/DE- THE "TAILCONE UNLOCK" MASTER CAUTION ILLUMINATED THREE TIMES DURING FLIGHT. THE QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DECLARED BY ATC FOR THE CREW. EWR MAINTENANCE CLEANED THE CONNECTOR PLUGS OF BOTH THE INTERNAL AND EXTERNAL TAILCONE SDR HALA20240401017Blade · damaged#5 FAN BLADE #2 ENGINE MAJOR DAMAGE. REMOVED #2 ENG BLADE SET PER AMM72-38-15. 17601 3-29-24 PERFORMED INSPECTION OF #2 ENGINE FOR FOD PER AMM 72-00-00--200-809. INSTALLLED #2 ENGINE BLADE ASSEMBLY PER AMM 72-38-15.SDR DALA2024040103937Longeron · corrodedCORROSION WAS FOUND ON LONGERON 22LH FROM STA 1017/STA 1049 AND LONGERON ENDS 22LH AND 24 LH STA 1053. ALSO CORROSION ON SHIMS OF LONGERONS 22LH, 23LH, AND 24LH BTW STA 1037-1042 AND FILLERS AT STA 1053 AND STR 21LH/STR 23LH AT AFT CARGO COMPARTMENT (C2). SUMMSDR DALA2024040504133Skin · crackedAD -- OPEN HOLE HFEC (BHEC) INDICATED CRACK 2 FASTENER HOLES BELOW EXISTING DOUBLER ON RT VERT L/E. MARKED. FOUND ON STEP 12 OF AA 5530-01048 AD 2018-10-08. SEPERATED EXTERIOR LATERS ON R/H VERT STAB FRONT SPAR CAP PER AA 5530-01048-02 STEP 13. PERFORMED OPEN SDR DALA2024040504132Longeron · out of limitsTHICKNESS MEASUREMENT WAS ACCOMPLISHED ON LONGERON L-23L BETWEEN Y=994 AT AFT CARGO COMPARTMENT. ORIGINAL THICKNESS IS 0.080 IN. REMAINING THICKNESS IS 0.043 IN. THEREFORE, IT IS OUT OF LIMITS. SUMMARY OF NRC 829: ON LONGERON L-23L BETWEEN Y=994 AT AFT CARGO WSDR HALA20240401016Battery Pack · inoperativeFWD ATTENDANT WORK LIGHT AND EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY ASSEMBLY AND POWER SUPPLY PER AMM 33-51-03. OPS CHECK GOOD. OKAY FOR SERVICE.SDR DALA2024040103938Generator · failedSHIP 9586 -DIV- THE FLIGHT WAS DIVERTED TO MCO FOLLOWING THE FAILURE OF THE RIGHT GENERATOR AFTER TAKEOFF, WHILE THE APU GENERATOR WAS ON MEL. THE CAPTAIN DECLARED AN EMERGENCY WITH ATC. CORRECTIVE ACTION: MAINTENANCE REPLACED THE RIGHT IDG AND PERFORMED ALL RSDR DALA2024040103936Pan · crackedCRACKS ON INNER PAN (3 EA) NEAR BEAMS #5 & #3 FWD SIDE. ALSO NEAR BEAM #2 AFT SIDE AT FWD CARGO DOOR. ER/A 554100-14 REV. A SECTION I WAS ACCOMPLISHED. SUMMARY OF NRC 00097: FWD AND AFT INNER PAN BETWEEN BEAMS #1 AND BEAM #4 AT FWD CARGO DOOR WAS REPAIRED PER SDR DALA2024040103935Hinge · obstructedINTERFERENCE BTW HEAD BOLT AND FWD OUTB FLAP HINGE AT RH WING. SUMMARY OF NRC 00808: FWD OUTB FLAP HINGE AT RH WING WAS REPAIRED PER ERA 616905-14 REV ORIGINAL SECTION I. ASSOCIATED ER/A 14-616905 ADDED FOR AC 9522. (LP #0268113)SDR DALA2025103107967Tab · corrodedCORROSION ON SKIN LT & RT SIDE AT RUDDER TAB. REPLACED BY SERVICIABLE RUDDER CONTROL TAB (0266679).SDR DALA2024040103934Floor Support · corrodedCORROSION ON RH FLOOR SUPPORT BTW STA 200-214 AND X=-56 PAX CABIN (W1). SUMMARY OF NRC 00464: CORROSION LEVEL 2. FLOOR SUPPORT BTW STA 200-214 AND X=-56 PAX CABIN WAS REPLACED AND INSTALLED PER B717-200 SRM 51-41-08-0G AND 51-41-01-0G. (LP #0267742)SDR DALA2024032803863Warning Message · false indicationSHIP 9523 -MISC/DE- ON CLIMB OUT, AT APPROXIMATELY 5,000 FEET, THE "PSEU FAIL" MESSAGE ILLUMINATED. THE QRH WAS COMPLIED WITH, AND AN EMERGENCY WAS DECLARED WITH ATC DUE TO THE PSEU FAILURE. THE PSEU RETURNED TO NORMAL ON DESCENT AND THE LANDING WAS UNEVENTFULSDR DALA2024032803862Drain · crackedCRACK ON DRAIN OF LH CLEAR VIEW WINDOW AT COCKPIT. SUMMARY OF NRC 00080: LH CLEAR VIEW WINDOW RETAINER AT COCKPIT WAS REPAIRED PER ERA 616781-14 REV ORIGINAL. ASSOCIATED ER/A 14-616781 ADDED FOR AC 9514. (LP #0264952)SDR DALA2024032703842Pan · crackedCRACKS ON PAN FWD END OF BEAM 5 AND BEAM 3 AT FWD CARGO COMPARTMENT DOOR C1. SUMMARY OF NRC 00222: DAMAGED SECTIONS OF PAN FWD END OF BEAM 5 AND BEAM 3 AT FWD CARGO COMPARTMENT DOOR C1 WERE REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #02641SDR DALA2024032703841Floor Support · corrodedCORROSION ON L/R FLOOR SUPPORTS BTW STA 160-200 AT X=7 AND X=-7 PAX CABIN (W1). SUMMARY OF NRC 00468: CORROSION LEVEL 2. L/R FLOOR SUPPORTS BTW STA 160-200 AT X=7 AND X=-7 PAX CABIN (W1) WERE REPLACED PER B717-200 SRM 51-41-01-0G. (LP #0264025)SDR DALA2024032703840Pan · crackedCRACK PAN ON AFT EDGE AT FWD CARGO COMPARMENT DOOR. SUMMARY OF NRC 00154: FWD CARGO COMPARMENT DOOR WAS REPAIRED PER ERA 559551-14 REV A. SECTION II. ASSOCIATED ER/A 14-559551 ADDED FOR AC 9541. (LP #0263823)SDR DALA2024040404053None · noneTHE EMERGENCY EXIT SIGNS WERE DISCOVERED TO BE INOPERATIVE AT LOCATIONS: 600, 601, 604, AND 605. THE EXIT SIGNS WERE NOT ILLUMINATED WHEN THE CABIN LIGHTING WAS OFF AS DESIGNED. MAINTENANCE CHECKED AND DETERMINED THAT ALL EMERGENCY EXIT SIGNS OPERATED NORMALLYSDR DALA2024032703839Cusp Web · corrodedCORROSION ON RH CUSP ANGLE BTW STA Y=160-169 AND STA Y=200 AT PAX CABIN. SUMMARY OF NRC 00489: CORROSION LEVEL 2. CUSP ANGLE BTW STA Y=160-169 AND STA Y=200 AT PAX CABIN WAS REPAIRED PER ER/A 616043-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ER/A SDR DALA2024032703838Window Frame · crackedCRACK WAS FOUND ON FRAME ON UPPER AFT CORNER AT RH SLIDING WINDOW CUTOUT. SUMMARY OF NRC 00802: UPPER AFT CORNER AT RH SLIDING WINDOW CUTOUT WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 REPAIR 1 PAR 5 FIG 201 OPTION 2 FLAG NOTE E AND F. (LP #0262080)SDR DALA2024032503738Bulkhead Web · crackedCRACK ON WEB LH AND RH SIDE, (PROJECTION OF UPPER HINGE) AT AFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR. SUMMARY OF NRC 00558: WEB AT AFT CABIN PRESSURE BULKHEAD EMERGENCY EXIT DOOR WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. ALSO AFT CABIN SDR DALA2024032503737Skin · debondedTWO DISBONDS FOUND ON LH AFT MOVABLE FLAP VANE LOWER SKIN: 1) LENGTH=1.700IN, WIDTH=1.500IN AND 2) LENGTH=2.100IN, WIDTH= 1.000IN (IN REF MON/9541/0138992 JOB # 005-0001). SUMMARY OF NRC 00037: LH AFT MOVABLE FLAP VANE LOWER SKIN WAS REPAIRED PER ERA 595913-14SDR DALA2024032503736Skin · debondedTWO DISBONDS WERE FOUND OF: 0.500 IN LENGTH .X 0.500 IN. WIDTH. ON DENTS LOWER SKIN AT LH CENTER FLAP VANE 26.500 IN. INBOARD EDGE, 12.500 IN. TRAILING EDGE AND 28.000 IN. INBOARD EDGE, 12.500 IN. TRAILING EDGE. (IN REFERENCE JOB# 020-0001) SUMMARY OF NRC 0065SDR DALA2024032503735Frame · corrodedCORROSION ON FRAME FROM STA 1022 LONGERON 30 CORDENATED X=-4 TO X=4. SUMMARY OF NRC 00708: CORROSION LEVEL 2. FRAME FROM STA 1022 LONGERON 30 CORDENATED X=-4 TO X=4 WAS REPAIRED PER B717 SRM 53-20-07-2R-3, 51-41-02-0G, AND 51-41-05-0G. PERFORM AN INITIAL VISUASDR DALA2024032503740Power Supply · inoperativeDURING CHECK OF THE EXTERIOR LIGHTS, LH/RH EMERGENCY LIGHTS WERE INOPERATIVE. SUMMARY OF NRC 00959: OVERWING EMERGENCY EVACUATION LIGHTS BATTERY POWER SUPPLY WAS REPLACED WITH A SERVICEABLE ONE PER B717 AMM 33-51-06. (LP #0258403)SDR DALA2024032503739Power Supply · inoperativeDURING CHECK OF THE EXTERIOR LIGHTS, THE LH/RH EMERGENCY LIGHTS WERE INOPERATIVE. SUMMARY OF NRC 00959: OVERWING EMERGENCY EVACUATION LIGHTS BATTERY POWER SUPPLY WAS REPLACED WITH A SERVICEABLE ONE PER B717 AMM 33-51-06. (LP #0258406)
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