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 DALA2024042404675Power Supply · inoperativeTHE EMERGENCY EXIT SIGN ON ROW 19CDE IS INOPERATIVE. MAINTENANCE THE FOUND POWER SUPPLY INOPERATIVE. THE POWER SUPPLY (B5-121) WAS REPLACED PER B717 AMM 33-51. THE OPERATIONAL CHECK WAS GOOD. (LP #4343895)SDR DALA2024042404674Cusp Web · corrodedCORROSION ON RH CUSP WEB (BELOW) STA Y=579 TO 598 AND X=-55 APPROX AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00525: CORROSION LEVEL 2. RH CUSP WEB (BELOW) STA Y=579 TO 598 AND X=-55 APPROX AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-SDR DALA2024050504925Access Panel · missingSHIP 9562 -PDA- DURING PREFLIGHT INSPECTION FOUND MISSING ACCESS PANEL ON LEFT HAND OUTER PORTION OF WING NEAR NAVIGATION LIGHT. PERFORMED TEMP REPAIR IAW SECTION 1 OF ERA 617613-14, WITH PERMANENT REPAIR TO BE COMPLIED WITH IN 1 FLT CYCLE. ATL MAINTENANCE INSDR DALA2024042404673Skin · crackedCRACK ON FUSELAGE SKIN BTW STA 1078 AND LONGERON 14R. SUMMARY OF NRC 00041: FUSELAGE SKIN BTW STA 1078 AND LONGERON 14R WAS REPAIRED PER ERA 617080-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ACCOMPLISH REPETITIVE INSPECTIONS WITHIN EVERY 24 MONTHS AFTER ACCOSDR DALA2024042304669Cusp Web · crackedCRACK LH CUSP WEB STA 657 TO 663 X=55 AT PAX CABIN. SUMMARY OF NRC 00394: CRACK LH CUSP WEB STA 657 TO 663 X=55 AT PAX CABIN WAS REPAIRED PER B717 SRM-53-00-55-2R-4. (LP #0307832)SDR DALA2024042304672Relay · faultedSHIP 9582 -MISC/DE- THE FLIGHT CREW RECEIVED AN "ANTI-SKID FAIL" MESSAGE DURING LANDING GEAR EXTENSION ON APPROACH INTO MSP. AN EMERGENCY WAS DECLARED BY THE CREW. THE MESSAGE EXTINGUISHED BEFORE LANDING. CORRECTIVE ACTION: AFTER LANDING, ALL BRAKE TEMPERATURESDR DALA2024042304671Limit Switch · out of adjustWHILE WORKING A.A. WORKCARD 2740-01114-07 HORIZONTAL JACK SCREW INSPECTION FAILED ONLY DURING ALTERNATE NOSE UP. HITS THE UPPER STOP. WITH PRIMARY SWITCH WORKS OK REF B717 AMM 27-40-00-820-801. ADJUSTED HORIZONTAL STABILIZER TRIM SYS & SHUT OFF CONTROLS PER B7SDR DALA2024042304668Longeron · crackedCRACK ON LONGERON 2LH FROM STA 1133 OF AFTER ACCESSORIES. SUMMARY OF NRC 00389: LONGERON 2LH STA 1121 TO STA 1136 WAS REPAIRED PER B717-200 SRM 53-00-05-2R-2 REPAIR 2. (LP #0307355)SDR DALA2024042304667Cusp Web · crackedCRACK ON RH CUSP WEB STA Y=610 AND X=-55 APPROX AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00527: RH CUSP WEB STA Y=610 AND X=-55 APPROX AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R-PROCEDURE 4. REPAIR 4. (LP #0306797)SDR DALA2024042304666Not Reported · corroded-AD- CORRORION WAS FOUND ON LH HORIZ STAB BARREL NUT HOLE #26. SUMMARY OF NRC 00719: CORROSION LEVEL 2. LH HORIZ STAB BARREL NUT HOLE #26 WAS REPAIRED PER ER/A 616773-14AD REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 616773-14 REV 1. ASSOCIATED ER/A 14-616SDR DALA2024042304665Longeron · crackedCRACKS ON LONGERON (3 EA) 5L, 5R, AND 17L STA=Y 1022 AT AFT LAVATORY ENGINE PYLON SUPPORT BULKHEAD AREA. SUMMARY OF NRC 0245: LONGERON (2 EA) 5L & 5R AT AFT LAVATORY ENGINE PYLON SUPPORT BULKHEAD AREA WERE REPAIRED PER B-717-200 SRM 53-00-05-2R REPAIR 2 AND LOSDR DALA2024042304664Frame · cracked-A.D.- CRACK OF 0.250IN LENGTH WAS FOUND ON UPPER RADIUS OF THE FRAME TAB ON THE LH OVERWING FRAME STA Y=696, IN REF CARD 5310-01436-04B JOB #063-0002 STEP: 10. SUMMARY OF NRC 00522: FRAME TAB ON THE LH OVERWING FRAME STA Y=696 WAS REPLACED PER B717-200 SRM 51SDR DALA2024042204626Skin · damaged-AD- CRACK ON SKIN DRILL FOUND. SUMMARY OF NRC 00852: FUSELAGE SKIN STA 1133 BTW L1-L3LH WAS REPAIRED PER ER/A 617266-14AD REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 617266-14 REV 5. ASSOCIATED ER/A 14-617266 ADDED FOR AC 9542. (LP #0305492)SDR DALA2024042204625Pan · crackedCRACK ON PAN OF L1 DOOR, BTW EDGE DOOR AND BEAM #1 STA Y=160. SUMMARY OF NRC 00191: PAN OF L1 DOOR, BTW EDGE DOOR AND BEAM #1 STA Y=160 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDER 3 REPAIR 3. (LP #0305244)SDR DALA2024042204624Pan · crackedCRACK ON PAN OF L1 DOOR, BTW EDGE DOOR AND BEAM #1 STA Y=200. SUMMARY OF NRC 00193: PAN OF L1 DOOR, BTW EDGE DOOR AND BEAM #1 STA Y=200 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 3 REPAIR 3. (LP #0305238)SDR DALA2024042204623Unknown · crackedCRACK ON LOWER MATING SURFACE BTW ACCESS 330XB AND ELEVATOR LEADING EDGE STA XE=171 AT RH ELEVATOR. SUMMARY OF NRC 00385: LOWER MATING SURFACE BTW ACCESS 330XB AND ELEVATOR LEADING EDGE STA XE=171 OF RH ELEVATOR WAS REPAIRED PER ER/A 616815-14 REV ORIGINAL SECSDR DALA2024060405770Window · missing17A OUTER GLASS WINDOW MISSING ON POST FLIGHT INSPECTION. REPLACED OUTER PANE AT SEAT 17A PER B717 AMM 56-20. NO LEAKS A/C OK FOR SVC. (LP #5307957)SDR DALA2024042304670Bearing · faultedTHE GATE AGENT REPORTS THAT THE 1L DOOR WAS HARD TO OPEN. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. MAINTENANCE REMOVED 1L DOOR LINER, FOUND ROLLER BEARING NOT FALLING INTO DOOR HANDLE DETESDR DALA2024042204627Battery Pack · malfunctionedTHE TAIL EXIT LIGHT STAYS FLASHING WITH THE EMERGENCY POWER SWITCH ARMED. MAINTENANCE REPLACED THE BATTERY PACK AND CRADLE ASSEMBLY B5-260 PER B717 AMM 33-51. NOW OPERATES NORMALLY. (LP #5832652)SDR HALA20240422021Eec · faultedATB - ENG LEFT SYS FAIL. PERFORMED WIRE CHECK PER FIM 77-21 TASK 803 ENGINE 1 J8, PIN 42 AND 43 - AVERAGE 9.15 OHMS NO SHORT TO GROUND. J7, PIN 42 AND 43 - AVERAGE 12.5 OHMS NO SHORT TO GROUND. REMOVED AND REPLACED #1 EEC PER AMM 73-21-01. RTS TEST GOOD. OK FOSDR DALA2024042204622Beam · crackedCRACK ON BEAM #1 OF L1 DOOR STA Y=200. SUMMARY OF NRC 00194: BEAM #1 OF L1 DOOR STA Y=200 WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #0302430)SDR DALA2024042204621Spar Cap · damagedPERFORM PERMANENT REPAIR ON RH WING TRAILING EDGE LOWER SPAR CAP DUE TO MISDRILLED HOLES WITH TIME LIMITED REPAIR. SUMMARY OF NRC 00856: RH WING TRAILING EDGE LOWER SPAR CAP WAS REPAIRED PER PRI 608531-14 REV 1 AND ERA #608531-14 REV C. SECTION II: TIME LIMITESDR DALA2024041904571Membrane · corrodedCORROSION ON LEFT MEMBRANE STA 200 TO 207 X=54 AT PAX CABIN IN REFERENCE NRC 00391. SUMMARY OF NRC 00591: CORROSION LEVEL 2. LEFT MEMBRANE STA 200 TO 207 X=54 AT PAX CABIN WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2. (LP #0301180)SDR DALA2024041904570Cusp Web · corrodedCORROSION ON LH CUSP WEB, OUT OF LIMITS PER B717 SRM 53-00-55-1A-1 ON STA Y=560 TO 578 X=55 APPROX AT PASSENGER CABIN. SUMMARY OF NRC 00701: CORROSION LEVEL 2. RING DOUBLER ON STA Y=560 TO 578 X=55 APPROX AT PASSENGER CABIN STRUCTURE WAS FABRICATED AND REPLACESDR DALA2024041904569Cusp Web · crackedCRACK (3 EA) ON LH CUSP WEB STA Y=655 TO 715 AND X=55 APPROX AT CPAX. SUMMARY OF NRC 00717: LH CUSP WEB STA Y=655 TO 715 AND X=55 APPROX AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 REPAIR 4 FIG 205. (LP #0300923)SDR DALA2024041904568Door Frame · corrodedCORROSION ON DOOR JAMB WEB BTW STA Y=201 TO 203 AND L-17L TO L-18L AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00700: CORROSION LEVEL 2. DOOR JAMB WEB BTW STA Y=201 TO 203 AND L-17L TO L-18L AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 51-70-10-SDR DALA2024041904567Cusp Web · crackedCRACK LH CUSP WEB STA 606 X=59 AT PAX CABIN PAX. SUMMARY OF NRC 00393: CRACK LH CUSP WEB STA 606 X=59 AT PAX CABIN, WAS REPAIRED PER B717 SRM-53-00-55-2R-4. (LP #0300915)SDR DALA2024041904566Diaphragm · crackedCRACK ON DIAPHRAGM BTW STA Y=171 TO STA Y=172 AND -X56 APPROX AT CABIN PAX (W1). SUMMARY OF NRC 00689: DIAPHRAGM BTW STA Y=171 TO STA Y=172 AND -X56 APPROX AT CABIN PAX WAS REPAIRED PER B717-200 SRM 51-70-10- 2R REPAIR 2 FIG 201. (LP #0300282)SDR DALA2024041904565Door Frame · corrodedCORROSION ON LOWER DOOR JAMB AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00070: CORROSION LEVEL 2. LOWER DOOR JAMB AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0300206)SDR DALA2024041804534Pan · crackedCRACK ON PAN AT FWD UPPER CORNER AND AFT UPPER CORNER OF FWD CARGO DOOR. SUMMARY OF NRC 00320: PAN AT FWD UPPER CORNER AND AFT UPPER CORNER OF FWD CARGO DOOR WERE REPAIRED PER B717-200 SRM 52-30-02-2R REPAIR 1. (LP #0298813)SDR DALA2024041804533Cusp Web · corrodedCORROSION ON CUSP WEB BTW STA Y=396 AND Y=401, BTW STA Y=416 AND Y=420, BTW STA Y=429 AND Y=434, AND BTW STA Y=459 AND Y=462 X-56 (IN REFERENCE TO NRC 00542). SUMMARY OF NRC 00661: CORROSION LEVEL 2. CUSP WEB BTW STA Y=396 AND Y=401, BTW STA Y=416 AND Y=420, BSDR DALA2024042204628Lanyard · missingSLIDE DISARMING PIN ATTACHING LANYARD MISSING. LATCH MECHANISM MISSING TO SECURELY ARM TAILCONE. THIS COULD PREVENT THE PROPER OPERATION OF THE ESCAPE PATH AND IT IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. WILL REQUIRE NEW LOWER CATCH ASSY AND ATTACHING HSDR DALA2024041804535Bulb · inoperativeTHE LEFT WING LANDING LIGHT WAS REPLACED IN ORD DUE TO BEING INOPERATIVE. UPON ARRIVAL IN MSP, THE LEFT WING LANDING LIGHT BULB (PARTIAL) AND RETAINER RING WAS DISCOVERED TO HAVE DEPARTED THE AIRCRAFT WHILE IN FLIGHT BETWEEN ORD AND MSP. MAINTENANCE IN MSP REPSDR DALA2024041804532Skin · cracked-AD- FOUND 4 EA HOLES ON LT VERT BELOW EXISTING DOUBLER AT SPLICE SHOWING CRACK INDICATIONS. C/W ER/A 617313-14AD REV ORIG SECTION I PERMANENT REPAIR. ALL RII C/W (QC1430) REF TO LOG PAGE 0297160 AND BUFF NRC 001. ASSOCIATED ER/A 14-6173133SDR DALA2024041804531Skin · damagedREF LOG #0286119: C/W ER/A 617263-14 REV ORIG. C/W ER/A 617263-14 REV ORIG SECTION II STEPS 1 AND 2. NO FURTHER DEFECTS NOTED. CUT OUT DAMAGED SKIN AND DRILLED REPAIR DOUBLER PER ER/A 617263-14 REV ORIG SECTION II STEP 3. C/W DVI OF DENTS REF STEP 4 SECTION IISDR DALA2024041804530Skin · cracked-AD- VERTICAL STAB LEFT SIDE 4 EA HOLES HAVE CRACK INDICATIONS, IN SKIN LAYER ONLY, JUST BELOW ZFS 52.267. BHEC INSP CONFIRMS CRACKS IN 4 EA HOLES IN SKIN LAYER ONLY REF AA 5530-01048 AND AD 2018-10-08 -MARKED-. COMPLIED WITH PRI 617313-14AD REV 0. C/W PRI 617SDR DALA2024041804529Beam · crackedCRACKS ON FWD PANE BEAM 1 OF LOWER CORNER AT FWD CARGO DOOR. SUMMARY OF NRC 00245: FWD PANE BEAM 1 OF LOWER CORNER AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0296713)SDR DALA2024041804528Beam · crackedCRACKS 2 EA ON FWD PANE BEAM 5 AT FWD CARGO DOOR. SUMMARY OF NRC 00243: FWD PANE BEAM 5 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0296705)SDR DALA2024041804527Vane · debondedSEVEN DISBONDS WERE FOUND ON LH AFT MOVABLE VANE LOWER SKIN, 1) LENGTH 1.550IN AND WIDTH 1.125IN, 2) LENGTH 1.000IN AND WIDTH 0.850IN, 3) LENGTH 1.250IN AND WIDTH 0.850IN, 4) LENGTH 1.250IN AND WIDTH 1.250IN, 5) LENGTH 1.250IN AND WIDTH 1.250IN, 6) LENGTH 1.37SDR DALA2024041804526Guide Vane · damagedDAMAGE T DURING TEST OF FLIGHT SPOILER ACTUATOR. FLAPS WAS RETRACTED AND RH FLAP GUIDE VANE WAS DENTED WITH INDB FLAP INGE SUPPORT BRACKET (HINGE FAIRING REMOVAL). SUMMARY OF NRC 00077: RH FLAP GUIDE VANE WAS REPAIRED PER PRI 616775-14 REV 2 AND ER/A 616775-14SDR DALA2024041504429Lens · missingEMERGENCY LENS COVER AT 17CDE MISSING. MAINTENANCE INSTALLED NEW EMERGENCY LENS COVER AT 17CDE PER B717 AMM 33-51. (LP #5874313)SDR DALA2024041504428Beam · crackedCRACKS ON FWD PANE BEAM 3 AT FWD CARGO DOOR. SUMMARY OF NRC 00244: FWD PANE BEAM 3 AT FWD CARGO DOOR WAS REPAIRED PER B717-200 SRM 52-30-02-2R PROCEDURE 1 REPAIR 1. (LP #0292323)SDR DALA2024041504427Cusp Web · crackedCRACK ON RH CUSP WEB (BELOW) STA Y=813 AND X=-44 APPROX AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00526: RH CUSP WEB (BELOW) STA Y=813 AND X=-44 APPROX AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 51-70-10-2R REPAIR 1. (LP #0292417)SDR DALA2024041504426Beam · crackedCRACK ON BEAM #5 NEAR TO AFT HINGE AT FWD CARGO COMPARTMENT DOOR C1. SUMMARY OF NRC 00221: BEAM #5 NEAR TO AFT HINGE AT FWD CARGO COMPARTMENT DOOR C1 WAS REPAIRED PER PRI 616929-14 REV 1 AND ERA 616929-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ERSDR DALA2024041504421Angle · corrodedCORROSION WAS FOUND IN ANGLE OVER CENTER WING UPPER SKIN STA Y=748 X=0. SUMMARY OF NRC 00803: CORROSION LEVEL 2. CORROSION IN ANGLE OVER CENTER WING UPPER SKIN STA Y=748 X=0 WAS REPAIRED PER PRI 616932-14 REV 4 AND ER/A 616932-14 REV ORIGINAL SECTION I: PERMANSDR DALA2024041504425Web · crackedCRACKED WEB (BELOW) FROM STA Y=218 TO 223 AND X=45 APPROX AT CABIN FLOOR STRUCTURE. SUMMARY OF NRC 00580: WEB (BELOW) FROM STA Y=218 TO 223 AND X=45 APPROX AT CABIN FLOOR STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4. (LP #0290917)SDR DALA2024041504424Bulkhead Web · crackedCRACKED BULKHEAD WEB SYA Y=218, X=-8 AT FWD CARGO COMPARTMENT. SUMMARY OF NRC 00283: BULKHEAD WEB STA Y=218, X=-8 AT FWD CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2. (LP #0290830)SDR DALA2024041504423Frame · damagedELONGATE HOLES AND WRONG DRILLED ON FRAME STA Y=994 BTW LONGERONS 26RH/27RH AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00674: FRAME STA Y=994 BTW LONGERONS 26RH/27RH AT AFT CARGO COMPARTMEN WAS REPAIRED PER PRI 616818-14 REV 2 AND ERA 616818-14 REV ORIGINAL, SECSDR DALA2024041504422Angle · corrodedCORROSION ON FWD AND AFT PREVIOUS REPAIR DOUBLER OF AFT CARGO COMPARTMENT DOOR JAMB. SUMMARY OF NRC 00072: CORROSION LEVEL 2. FWD AND AFT PREVIOUS REPAIR DOUBLER OF AFT CARGO COMPARTMENT DOOR JAMB WERE REPLACED PER B717-200 SRM 53-20-15-2R REPAIR 7 FIG 201. (LSDR DALA2024041204363Beam · crackedCRACK ON BEAM #1 STA 161 AND STA 197 AT PASSENGER ENTRANCE DOOR (L1). SUMMARY OF NRC 00216: DAMAGED SECTIONS (STA 161 AND STA 197) OF BEAM #1 AT PASSENGER ENTRANCE DOOR WERE REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7, REPAIR 7, FIG 201 AND FIG 202. (LP
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