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 DALA2024103110526Skin · crackedCRACK ON SKIN ON CUTOUT OF RH SLIDING WINDOW AT COCKPIT (UPPER AFT CORNER). SUMMARY OF NRC 00355: SKIN ON CUTOUT OF RH SLIDING WINDOW AT COCKPIT (UPPER AFT CORNER) WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 REPAIR 1 PAR 5 FIGURE 201. (LP #0636659)SDR DALA2024103010506Battery Pack · inoperativeTHE OVERWING EXIT LIGHT IS INOPERATIVE. MAINTENANCE REPLACED THE OVERWING EXIT LIGHT BATTERY PACK PER B717 AMM 33-51. THE AIRCRAFT IS OK FOR SERVICE. (LP #6703153)SDR DALA2024103010505Frame · corrodedCORROSION ON FRAME STA Y=1022 INTERSECTION WITH LONG 30 AT AFT CARGO COMPARTMENT. SUMMARY OF NRC 00752: CORROSION LEVEL 2. CORROSION ON FRAME STA Y=1022 INTERSECTION WITH LONG 30 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 RESDR DALA2024103010504Web · crackedCRACKED WEB BTW STA Y=696 AND X=45 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00432: WEB BTW STA Y=696 AND X=45 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55-2R PROCEDURE 4 FIGURE 204. PERFORM A GENERAL VISUAL INSPECTION EVERY C-CHECK PSDR DALA2024103010503Beam · crackedCRACK ON BEAM #1 AFT SECTION AT FWD PASSENGER DOOR. SUMMARY OF NRC 00266: BEAM #1 AFT SECTION AT FWD PASSENGER DOOR WAS REPAIRED PER B717-200 SRM 52-10-02-2R PROCEDURE 7 REPAIR 7. (LP #0634844)SDR DALA2024103010502None · none-AD- WORKING PRI 615810AD REV 3. C/W ALL STEPS OF ERA 615810-14AD REV A SECTION IV TIME LIMITED REPAIR II. THESE STEPS ARE C/W AND MATCH PRI 621847-14AD REV 0, 1, 2, AND PRI 615810-14AD REV 3. (LP #0634418)SDR DALA2024103010501Fuel Cell · leaking-AD- L/H WING REAR SPAR LOWER CAP LEAKING FUEL. C/W PRI 621847-14AD REV 2. C/W ALL STEPS OF ERA 615810-14AD REV A SECTION IV TIME LIMITED REPAIR II. THESE STEPS MATCH PRI 621847-14AD REV 0, 1, 2, AND PRI 615810 REV 3. (LP #0634404)SDR DALA2024103010500Fuel Cell · leaking-AD- FUEL LEAK FOUND DURING INSPECTION OF THE LH WING REAR SPAR LOWER CAP. CONTACT LIAISON ENG. REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT, AA#FC5720-01103. LEAK IDENTIFIED ORIGINATED FROM FASTENER. C/W PRI 621847-14AD REV ORIGINAL THRU REV 2. C/W PRI 615810-14SDR DALA2024102910498Battery Pack · failedTHE EMERGENCY LIGHTS AT LOCATION SEAT ROW 20 ARE INOPERATIVE. MAINTENANCE FOUND THAT THE BATTERY PACK AT LOCATION B5-230 WAS BAD. THE BATTERY AT LOCATION B5-230 WAS REPLACED PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #6658874)SDR DALA2024112111101Spar · cracked-AD- LH WING REAR SPAR XRS 164 CRACKED. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) REQUIRED FOR CONTINUED SERVICE BEYOND 06NOV2024 (AD EFFECTIVE DATE). A NEW FAA FORM 8100-9 AND AMOC APPROVAL TO AD 2024-21-01 IS REQUIRED FOR CONTINUED SERVICE BEYOND SDR DALA2024102910497Duct · disconnectedSHIP 9560 -FUME/DE- DURING THE DECENT WHEN THE POWER WAS REDUCED TO IDLE, THE F/A REPORTED A "BURNT CARPET/CRAYON" SMELL IN THE CABIN. F/O NOTIFIED THE CAPT THAT HE TOO SMELLED IT IN THE COCKPIT AND BOTH DONNED O2 MASKS. THE CAPT DECLARED AN EMERGENCY WITH ATCSDR DALA2024103010499Web · crackedCRACK ON WEB BTW STA Y=674 AND X=45 AT PASSENGER CABIN STRUCTURE. SUMMARY OF NRC 00378: WEB BTW STA Y=674 AND X=45 AT PASSENGER CABIN STRUCTURE WAS REPAIRED PER B717-200 SRM 53-00-55 2R PROCEDURE 4, REPAIR 4, FIGURE 217. (LP #0627536)SDR DALA2024102510401Window Frame · crackedCRACK ON CUTOUT (DRAIN AREA) OF LH SLIDING WINDOW AT FWD UPPER FUSELAGE. SUMMARY OF NRC 00047: CRACK ON CUTOUT (DRAIN AREA) OF LH SLIDING WINDOW AT FWD UPPER FUSELAGE WAS REPAIRED PER PRI 621091-14 REV 1 AND ER/A 621091-14 REV ORIGINAL SECTION I: PERMANENT REPSDR HALA20241025060Stick Shaker · warning messageABORTED TO @ 30-40 KTS PSEU AND STICK PUSHER FAIL MSG. PERFORMED SLAT DISAGREE BITE PER FIM 27-80 TASK 803. COULD NOT DUPLICATE FAULT. OK TO CONTINUESDR HALA20241024059Power Supply · inoperativeDURING OVERNIGHT CK FOUND CEILING EMERGENCY EXIT LIGHT OUT AT OVERWING EXIT. REPLACED OVERWING EMER LIGHTS POWER SIUPPLY AND BATTERY POS B5-121 IAW 33-51-03. OPS CK GOOD. OK FOR SVCSDR HALA20241024058Spring · faultedAFTER T/O LEFT GEAR UNSAFE LIGHT ILLUMINATE WITH GEAR HANDLE UP. REMOVED AND REPLACED UP LATCH SPRING FOR LEFT MLG DOOR. OPS CHK AND SECURITY CHK OK. OK FOR SVC.SDR DALA2024102410343Longeron · damagedLONGERON R8 AT STATION Y1133 DAMAGED. REMOVED DAMAGED R8 LONGERON 16.5 INCHES OF MATERAL SURROUNDING Y1133 REF 53-00-05-2R PROCEDURE 2. PERFORMED DAMAGE CONTAMENT HFEC IAW MDC93K0393-NDT SPM. NO FURTHER DAMAGE FOUND. FABRICATED, PAINTED, AND INSTALLED R8 REPAISDR DALA2024102310323Angle · corrodedCORROSION ON RH CUSP ANGLE STA 198 X=-59 AT PAX CABIN. SUMMARY OF NRC 00387: CORROSION LEVEL 2. CORROSION ON RH CUSP ANGLE STA 198 X=-59 AT PAX CABIN WAS REPAIRED PER PRI 621192-14 REV 3 AND ER/A 621192-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. ASSOCIATED ESDR DALA2024102310322Doubler · corrodedEXFOLIATION ON UPPER DOUBLER ON INTERNAL CANTED KEEL STA Y=685 APROX BTW LONGERON 30-29R AT FUSELAGE (FUS). SUMMARY OF NRC 00523: CORROSION LEVEL 2. EXFOLIATION ON UPPER DOUBLER ON INTERNAL CANTED KEEL STA Y=685 APROX BTW LONGERON 30-29R AT FUSELAGE, WAS REPAISDR HALA20241023057Battery · inoperativeDURING OVERNIGHT CK FOUND EMERGENCY EXIT LIGHT AT AFT BULKHEAD DOOR. REPLACED AFT BULKHEAD DOOR POWER SUPPLY AND BATTERY POS B5-260, FOUND LOOSE WIRE CONNECTION BEHIND BULKHEAD DOOR EMER EXIT SIGN, RESCURED CONNECTION. OPS CK GOOD, OK FOR SVCSDR DALA2024102210316Access Panel · damagedELONGATED NUT HOLES ON OTBD ACTUATOR ACCESS PANEL AT RH ELEVATOR. SUMMARY OF NRC 00563: INTERNAL DOUBLER WAS FABRICATED PER B717-200 SRM 51-41-02-0G, AND DWG 9918480 REV BF, AND RIB PER DWG 9918471 REV B, AND INTERNAL DOUBLER AND RIB WERE REPLACED PER B717 SRMSDR HALA20241022056Pseu · faultedGEAR DOOR OPEN INFLIGHT. TROUBLESHOT PER FIM 32-60 TASK 802. NO FAULTS EXIST ON PSEU CURRENT FAULTS. COMPLETED "FIM 32-60 TASK 802 STEP F. WIRE CHECKS PASSED. REPLACED PSEU PER AMM 32-61-01 AND RTS PASS. OK TO CONTINUE.SDR DALA2024102210315Frame · crackedCRACK ON FRAME BTW STA Y=1037 AND LONG 14L AT AFT PAX CABIN. SUMMARY OF NRC 00289: FRAME BTW STA Y=1037 AND LONG 14L AT AFT PAX CABIN WAS REPAIRED PER ER/A 621344-14 REV ORIG SECTION I, PERMANENT REPAIR. ASSOCIATED ER/A 00-621344 ADDED FOR AC 9529. (LP #062103SDR DALA2024120911532Duct · temp repairCRACK ON RIGHT ENG BYPASS DUCT NEAR PRECOOLER INLET WAS TEMPORARILY REPAIRED. RE-INSPECTION REQUIRED PER ER/A 620571-14 REV ORIGINAL. REFER TO LOG #0580374 FOR PRIOR INSPECTION. SECTION 4 INSPECTION MUST BE ACCOMPLISHED BETWEEN 220 AND 180 FLIGHT CYCLES PER ERSDR DALA2024102110285Battery · malfunctionedEMERGENCY EXIT LIGHT ON TOP OF TAILCONE IS INTERMITTENTLY FLASHING. MAINTENANCE REPLACED THE BATTERY AND BATTERY POWER SUPPLY PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. AIRCRAFT OK FOR SERVICE. (LP #6449074)SDR DALA2024102110284Pan · crackedCRACKS ON INNER PAN LOWER EDGE (MID SECTION) AT AFT CARGO COMPARTMENT DOOR. SUMMARY OF NRC 00726: INNER PAN LOWER EDGE (MID SECTION) AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 620733-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 620733-14 REV 2SDR DALA2024102110283Frame · corrodedCORROSIONS ON FRAME STA Y=870 BTW L-29L AND L-29R AT AFT CARGO. SUMMARY OF NRC 00206: CORROSION LEVEL 2. CORROSION ON FRAME STA Y=870 BTW L-29L AND L-29R AT AFT CARGO WAS REPAIRED PER B717-200 SRM 53-20-07-2R PROCEDURE 3 REPAIR 3. PERFORM AN INITIAL INTERNAL ASDR DALA2024102110282Skin · dentedSEVERAL DENTS ON (UPPER AND LOWER) SKIN OF FWD MOVABLE VANE AT LH WING. SUMMARY OF NRC 00630: DENTS (9 LOCATIONS) ON LOWER SKIN OF FWD MOVABLE VANE AT LH WING WERE EVALUATED WITH THE FOLLOWING DIMENTIONS WERE: DENT #1 W=0.250" Y=0.003" W/Y=83.33, DENT #2 W=0.3SDR HALA20241018054Coalescer Bag · odorAFTER #2 ENG START (AT THE GATE) + R PACK SWITCH ON ... FA REPORTED BURNING RUBBER SMELL IN FWD GALLEY. PILOT ASSITED WITH RUNNING #2 ENG AND RT PACK. ENGINE AMM 71-00-04 SMELL PERSISTS. 18922 9/16/24. REMOVED AND REPLACED LT + RT COELESCER BAGS. OPS CK GOOD. SDR HALA20241018053Test Unit · faultedCARGO SMOKE FWD FAIL. RESET CARGO SMOKE TEST C/B. TEST PASSED. OK FOR SERVICE.SDR DALA2024101810191Pan · crackedCRACK PAN INTERNAL SIDE FWD EDGE ON BEAM #4 AND #5 (2 EA) AT AFT CARGO DOOR. SUMMARY OF NRC 00129: INNER PAN ON FWD EDGE BETWEEN BEAM #4 AND #5 AT AFT CARGO COMPARTMENT DOOR WAS REPAIRED PER ER/A 620739-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 62073SDR DALA2024101810190Vane · wornWEAR ON LEADING EDGE OF AFT MOVABLE VANE LH WING. SUMMARY OF NRC 00770: WEAR ON LEADING EDGE OF AFT MOVABLE VANE LH WING WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1. (LP #0614293)SDR DALA2024101810189Bushing · crackedCRACK ON BUSHING WAS FOUND, PREVIOUSLY TO INSTALL NEW LOWER BRACKET ON LEADING EDGE AT VERTICAL STABILIZER. SUMMARY OF NRC 00927: CRACK ON BUSHING OF VERTICAL STABILIZER L.E. ZFS=46.300 TO ZFS=52.267 WAS REPAIRED PER ER/A 620945-14 REV ORIGINAL SECTION I: PERMSDR DALA2024101810188Longeron · crackedCRACK ON LONG=1 IN STA Y=794 AT PASSENGER CABIN. SUMMARY OF NRC 00324: LONG=1 IN STA Y=794 AT PASSENGER CABIN WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. PERFORM A GVI INSPECTION PER B717-200 SRM 53-00-05-2R-2 STEP 7 A TABLE 202 EVERY "C" CSDR DALA2024101710154Skin · wornWEAR ON UPPER SURFACE OF UPPER FIXED GUIDE VANE STA XRS=140.000 RH WING. SUMMARY OF NRC 00010: UPPER SURFACE OF UPPER FIXED GUIDE VANE STA XRS=140.000 RH WING WAS REPAIRED PER B717-200 SRM 57-53-01-2R PROCEDURE 1 REPAIR 1 PAR 4 D AND 51-70-02-0G PROCEDURE GENESDR DALA2024101710153Door Frame · wornWEAR ON FUSELAGE CUTOUT STA Y=130 OF PASSENGER DOOR HOOK CAVITY ALSO VERIFY IF RADIUS MEET WITH SRM ON FWD LOWER CORNER. SUMMARY OF NRC 00048: WEAR ON FUSELAGE CUTOUT STA Y=130 OF PASSENGER DOOR HOOK CAVITY WAS REPAIRED PER B717-200 SRM 53-10-01-2R PROCEDURE 7SDR DALA2024101410045Pan · crackedCRACK PAN INTERNAL SIDE OF AFT EDGE ON BEAM #3, #4, AND #5 AT AFT CARGO DOOR. SUMMARY OF NRC 00127: INNER PAN OF AFT EDGE ON BEAM #3 AT AFT CARGO DOOR WAS REPAIRED PER ER/A 620695-14 REV ORIGINAL, SECTION I: PERMANENT REPAIR AND PRI 620695-14 REV 2. ALSO (ET) SDR DALA2024101410044Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN EDGE, AROUND HANDLE ON PASSENGER DOOR (L1). SUMMARY OF NRC 00302: EXTERNAL FUSELAGE SKIN EDGE AROUND HANDLE ON PASSENGER DOOR (L1) WAS REPAIRED PER ER/A 620705-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 620705-14 REV 1.SDR DALA2024101410043Vane · dentedDENTS ON UPPER SURFACE OF AFT MOVABLE FLAP VANE ON RIGHT WING. SUMMARY OF NRC 00623: DENTS (9 LOCATIONS) ON UPPER SURFACE OF AFT MOVABLE FLAP VANE ON RIGHT WING WERE DENT #1 W=0.400" Y=0.001" W/Y=400 DENT #2 W=0.350" Y=0.001" W/Y=350 DENT #3 W=0.343" Y=0.001" SDR DALA2024101410042Vane · dentedDENTS ON LWR SURFACE OF FWD MOVABLE FLAP VANE ON RIGHT WING. SUMMARY OF NRC 00624: DENTS (7 LOCATIONS) ON LWR SURFACE OF FWD MOVABLE FLAP VANE ON RIGHT WING (DENT #1 W=0.218" Y=0.005" W/Y=43.6, DENT #2 W=0.320" Y=0.012" W/Y=26.66, DENT #6 W=0.250" Y=0.008" W/YSDR DALA2024101109968Skin · crackedCRACK INTERNAL SKIN UNDER CAP UPPER AFT SIDE OF RH SLIDING WINDOW CUTOUT AT FLIGHT COMPARTMENT. SUMMARY OF NRC 702: INTERNAL SKIN UNDER CAP UPPER AFT SIDE OF RH SLIDING WINDOW CUTOUT AT FLIGHT COMPARTMENT WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 RSDR DALA2024101109967Skin · crackedCRACK INTERNAL SKIN UNDER CAP UPPER AFT SIDE OF RH SLIDING WINDOW CUTOUT AT FLIGHT COMPARTMENT. SUMMARY OF NRC 702: INTERNAL SKIN UNDER CAP UPPER AFT SIDE OF RH SLIDING WINDOW CUTOUT AT FLIGHT COMPARTMENT WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 RSDR DALA2024101109966Skin · crackedCRACK NTERNAL SKIN UNDER CAP UPPER AFT SIDE OF LH SLIDING WINDOW CUTOUT AT FLIGHT COMPARTMENT. SUMMARY OF NRC 701: INTERNAL SKIN UNDER CAP UPPER AFT SIDE OF LH SLIDING WINDOW CUTOUT AT FLIGHT COMPARTMENT WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 RESDR DALA2024101109970Skin · crackedCRACK NTERNAL SKIN UNDER CAP UPPER AFT SIDE OF LH SLIDING WINDOW CUTOUT AT FLIGHT COMPARTMENT. SUMMARY OF NRC 701: INTERNAL SKIN UNDER CAP UPPER AFT SIDE OF LH SLIDING WINDOW CUTOUT AT FLIGHT COMPARTMENT WAS REPAIRED PER B717-200 SRM 56-10-02-2R PROCEDURE 1 RESDR DALA2024101109965Door · broken-AD- BROKEN INBD BUTE DOOR OUTBD EDGE AT RH WING. (AD) SUMMARY OF NRC 00171: INBD BUTE DOOR OUTBD EDGE AT RH WING WAS REPAIRED PER ERA 618696-14TR REV ORIGINAL SECTION I. ASSOCIATED ER/A 14-618696 ADDED FOR AC 9528. (LP #0598854)SDR DALA2024100909842Cusp Web · crackedCRACKS ON CUSP WEB STA 658 AND X=58, STA 516 AND X=49 AT PAX CABIN. SUMMARY OF NRC 00386: CUSP WEB STA 658 AND X=58, STA 516 AND X=49 AT PAX CABIN WERE REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIGURE 203 AND 205. (LP #0599143)SDR DALA2024100909841Longeron · crackedCRACKED LONGERON 2LH AT STA Y=1133 AT AFT ACCESSORIES COMPARTMENT. SUMMARY OF NRC 00408: LONGERON 2LH AT STA Y=1133 AT AFT ACCESSOIRES COMPARTMENT WAS REPAIRED PER B717-200 SRM 53-00-05-2R PROCEDURE 2 REPAIR 2. (LP #0599134)SDR DALA2024100809791Longeron · crackedCRACKS ON LONGERONS (3 EA), LONG 5L AND LONG 6L ON STA Y=1022. ALSO LONG 5R ON STA Y=1022 AT AFT PAX CABIN. SUMMARY OF NRC 00283: LONGERONS (3 EA), LONG 5L AND LONG 6L ON STA Y=1022 ALSO LONG 5R ON STA Y=1022 AT AFT PAX CABIN WERE REPAIRED PER B717-200 SRM 53-SDR DALA2024100809790Skin · damagedCREASE IN FUSELAGE SKIN WAS FOUND ON REPAIR AREA. SUMMARY 00593: CREASE WAS REPAIRED PER ER/A 620891-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 620891-14 REV 0. ACCOMPLISH SECTION II REPETITIVE INSPECTION INSTRUCTIONS WITHININ EVERY 8,000 FLIGHT CYCLESDR DALA2024100709735Battery Pack · inoperativeTHE OVERHEAD EMERGENCY EGRESS LIGHTS ARE INOPERATIVE FROM ROW 24 THROUGH TO ROW 29. MAINTENANCE REPLACED THE EMERGENCY BATTERY PACK AT 25DEF (B5-231) PER B717 AMM 33-51. CHECK IS GOOD. (LP #6103393)
Back to Boeing 717-200