N517AS
Service difficulty reports · 449
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N517AS' AND registry_match = 'registration' 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 n_number = 'N517AS' AND registry_match = 'registration' 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 ASAA2023040842763Unknown · unknownAT CRUISE L FUEL QUANTITY TOTAL FUEL QUANTITY WOULD BLANK INTERMITTENTLY. GROUNDED - YES. PERFORMED B737-800 FIM TASK 28-41 TASK 813 FOR FUEL QUANTITY INDICATION BLANK NO DEFECTS NOTED. INTERMITTENT FAULT. PERFORMED FQIS BITE PROCEDURE PER FIM 28-41 TASK 801 NSDR ASAA2023032842618Pitot Head · failedAUX PITOT LIGHT AFTER ENGINE START DURING TAXI OUT. GROUNDED - YES. PER B737-800 FIM 30-31 TASK 801. AUX PITOT HEATER C/B OUT, RESET, TRIED OPS CHECK. AFTER A FEW SECONDS LIGHT CAME BACK ON. C/B REMAINED IN. EXAMINED C/B. CHECK GOOD. AUX PITOT RESISTANCE CHECKSDR ASAA2023031942425Sensor · faultyCONT CAB TEMP CONTROL FAULT ON MASTER CAUTION RECALL. GROUNDED - YES. C/W TECH SERVICE, REF B737-800 FIM 21-62 TASK 801, PERFORMED BITE TEST AND FOUND TRIM VALVE/FLT DECK FAULT. REMOVED AND REPLACE FLIGHT DECK TEMP SENSOR AND FILTER PRECAUTIONARY REF B737-800 SDR ASAA2023031342326Probe · faultyON TAXI, L TEMP PROBE LIGHT ILLUMINATED. GROUNDED - YES. REF B737-800 FIM 30-31 TASK 810 FOUND TAT PROBE AT FAULT. REPLACED TAT PROBE REF B737-800 AMM 34-21-06/401. ALL REQUIRED TESTS PASSED.SDR ASAA2023022642096Actuator · faultyL PACK LIGHT ILLUMINATED IN FLIGHT. CLEARS ON RESET RETURNS ON RECALL. GROUNDED - YES. REMOVED AND INSTALLED NEW L RAM AIR INLET ACTUATOR PER B737-800 AMM 21-51-21/401, OPS NORMAL. NO FAULTS.SDR ASAA2023022542060Unknown · unknownLEFT PACK LIGHT ILLUMINATES ON RECALL. GROUNDED - YES. PERFORMED BITE CHECK FOUND ACTUATOR FAULT ON PREVIOUS LEG FAULT CLEARED. RAN BITE SEVERAL MORE TIMES FAULT NO LONGER PRESENT SUSPECT INTERMITTENT.SDR ASAA2023012041605Modulating Valve · faultedFLIGHT DECK TEMP CONTROL INOP. ZONE TEMP CAUTION EXTINGUISHES ON RESET. GROUNDED - YES. REMOVED AND REPLACED ZONE TRIM AIR MODULATING VALVE (V143). REF. B737-800 AMM 21-61-21. ORIG SUB DATE: 1/24/2023SDR ASAA2023010641514Skin · crackedCRACK FOUND JUST INBOARD OF STAB. STA 147.90 LOWER SKIN, RIGHT HAND STABILIZER APPROX . 1.25" IN LENGTH. MARKED. GROUNDED - YES. REPAIRED RIGHT HORIZONTAL LOWER SKIN AT STAB STA 147.90 PER B737-800 SRM 55-10-01-2R-11; REPAIR IS CAT "B" AND HAS INSPECTION THRESSDR ASAA2023010641513Skin · crackedCRACK JUST INBOARD OF STAB STA 101.90 FOUND IN LOWER SKIN APPROX. 1" IN LENGTH. GROUNDED - YES. REPAIRED RIGHT HORIZONTAL LOWER SKIN AT STAB STA.101.90 PER B737-800 55-10-01-2R-11, REPAIR IS CAT "B" AND HAS AN INSPECTION THRESHOLD OF 56,000 TOTAL FLIGHT CYCLESSDR ASAA2023011741541Skin · damagedRH ELEVATOR HAS A DAMAGE SCREW HOLE ON SKIN AT #6 HINGE WHERE COVER PANEL IS INSTALLED. GROUNDED - YES. REPAIRED R/H ELEVATOR DAMAGED SCREW HOLE AT #6 HINGE COVER AREA IAW B737-800 SRM 55-20-01, 51-70-04-2R-9, 51-60-04-0G-0NEW CBM IS -112.015LBFIN.SDR ASAA2022121741152Warning Message · false activationCONT CAB ZONE TEMP ILLUMINATED AND CLEARS ON MASTER RECALL. GROUNDED - YES. PERFORMED PACK/ZONE TEMP CONTROLLER BITE TEST IAW B737-800 AMM 21-61-00-700-806-002. RIGHT PACK ZONE TEMP CONTROLLER (2) SHOWED FLT DECK TRIM VALVE FAULT. FAULT CLEARED AND IS NO LONGESDR ASAA2022121641172Pump · leaking#2 ENGINE OIL LEAK ON SHUTDOWN AT HYD PUMP DRIVE PAD REF. ASA MIG-2C# 40-0038356 ITEM #3. GROUNDED - YES. REMOVED AND REPLACED ENG #2 HYD PUMP AND SEALOL SEAL PER B737-800 AMM 29-11-11-400-801 AND AMM 72-60-00-400-801-F00.SDR ASAA2022121541171Engine · damagedWHILE ACCOMPLISHING ASA C SB CFM56-7B7B-72-1074-A ON #2 ENGINE S/N # 896912 MULTIPLE LOCATION, 3RD STG VSV SLAB HEAD PIN HAD LIBERATED AND CAUSED DAMAGE TO COMPRESSOR HUB. GROUNDED - YES. REMOVED #2 ENGINE S/N 896-912 REF. ASA T/C # 78471000 ON ASA W/O # 19322SDR ASAA2022120741104Generator · crackedAPU OIL CONSUMPTION INSPECTION DUE TO REPORT OF EXCESSIVE SERVICING GROUNDED - YES. PERFORMED GVI ON APU REF B737-800 FIM 49-95 TASK 801, FOUND STARTER GENERATOR LEAKS OIL FROM CRACK FOUND ON BOTTOM OF GENERATOR. PERFORMED OPERATION OF THE APU AND FOUND EVIDENSDR ASAA2022090539819Unknown · unknownSEVERAL ATTEMPTS TO MAKE/RECEIVE SAT CALLS BUT UNABLE TO HEAR DISPATCH ON BOTH 1 & 2, VOLUMES SET HIGH. DISPATCH HEARD ME. GROUNDED - YES. REF B737-800 FIM TASK 23-15-00-23-801, VERIFIED BOTH SATCOM OPS CHECKED LOUD AND CLEAR WITH DISPATCH DIR. NO DEFECTS HISTSDR ASAA2022082839690Fmc · intermittentCAPT SIDE VTK ON LANDING INTERMITTENT ALSO BOTH FMC'S BLANKING AFTER LANDING. GROUNDED - YES. REF B737-800 FIM 34-61 TASK 836 RESET BOTH FMC'S COMPUTERS BOTH FM'S COMPUTERS OPS NORMAL.SDR ASAA2022080739393Sensor · faultedR1 WINDOW OVERHEAT LIGHT ILLUMINATED ON PREFLIGHT. QRH CHECKLIST COMPLETED AND LIGHT REMAINS ILLUMINATED. GROUNDED - YES. REFERENCE B737-800 FIM 30-41-TASK 801 PERFORMED WHCU BITE FOUND RH FWD SENSOR FAULT REFERENCE FIM 30-41 TASK 812 SWAPPED FWD WINDOW HEAT SSDR ASAA2022072939276Impeller · inoperativeRIGHT AFT FUEL LOW PRESSURE LIGHT ILLUMINATED AT TOP OF DESCENT. EXTINGUISHED SHORTLY AFTER. GROUNDED - YES. REMOVED & REPLACED #2 AFT BOOST PUMP MOTOR IMPELLER REF B737-800 AMM 28-22-41. OPS CHECK GOOD.SDR ASAA2022072739228Pump · false indicationRIGHT AFT MAIN TANK FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED AT TOP OF CLIMB. QRH COMPLETED. GROUNDED - YES. RELEASED PER MEL 28-3E. R WING BOOST PUMP LOW PRESSURE. PER B737-800 FIM 28-22 TASK 805, ACCOMPLISHED INITIAL EVALUATION. TANK 2 AFT FUEL BOOST PUMP OPSDR ASAA2022071639152Cdu · inoperativeACARS ALPHANUMERIC KEY WON'T TYPE IN ACARS MODE ONLY. WORK NORMAL IN FMC MODE. GROUNDED - YES. REPLACED CDU L/H CA'S REF B737-800 AMM 34-61-01/401. ALL BUTTON FUNCTIONS RESTORED.SDR ASAA2022071539097Door · out of adjustR1 DOOR IS VERY DIFFICULT TO CLOSE. GROUNDED - YES. ADJUSTED R1 DOOR GUIDE, HORIZONTAL CONTROL ROD, DOOR STOP PINS, AND UPPER AFT LATCH RECEIVER REF B737-800 AMM 52-41-00-820-801. ACCOMPLISHED GALLEY SERVICE DOOR SYSTEM TEST REF AMM 52-41-00-700-801.SDR ASAA2022061438644Cdu · distortedCPT FMC CDU HAS LINES @ BOTTOM OF DISPLAY. GROUNDED - YES. REPLACED CPT CDU REF. B737-800 AMM 34-61-00-400-802. OPS CK OK.SDR ASAA2022052138416Sensor · failedENG #2 VIBRATION INDICATOR DISAPPEARED INFLIGHT. GROUNDED - YES. ACCOMPLISHED AAVM SYSTEM BITE TEST, "N2 TACHO LOSS E2" LOGGED REF B737-800 AMM 77-31-00-970-803-F00 AND B737-800 FIM 77-31 TASK 801. TROUBLESHOOT PER FIM 77-31 TASK 805, B737-800 WDM 77-31-21 ANDSDR ASAA2022052038415Sensor · failedGE CNR 20220520046 #2 ENG (S/N 896912) EXPERIENCED ERRATIC SHIFTS IN CORE VIBRATIONS AT CRUISE AND TAKEOFF. PERFORM T/S PER DEFER TAB. #PRI2. GROUNDED - YES. ACCOMPLISHED AAVM SYSTEM BITE TEST, "N2 TACHO LOSS E2" LOGGED REF. B737-800 AMM 77-31-00-970-803-F00 ASDR ASAA2022051338329Rod · brokenAPU INLET DOOR LOWER ROD BROKEN. GROUNDED - YES. REPLACED THE APU INLET DOOR PER B737-800 AMM 49-15-22.SDR ASAA2022051238328Drain Line · leakingREF T/C 7847000 #2 ENG INLET AND FAN BLADES- DETAILED INSPT. FOUND HEAT EXCHANGER, OIL FUEL, DRAIN LINE LEAKING FUEL. GROUNDED - YES. REMOVED AND REPLACED MAIN OIL/ FUEL HEAT EXCHANGER REF B737-800 AMM 79-21-02/401. #2 FUEL/OIL HEAT EXCHANGER AND SERVO HEATER SDR ASAA2022051238323Shroud · crackedREF T/C #78472000 #2 ENG INLET AND FAN BLADES - DETAILED INSP FOUND 12 O'CLOCK POS STRUT O/B END BLACK PANEL R/H AFT END HAS 2 CRACKS COMING OUT OF FWD FASTENER HOLE. GROUNDED - YES. REMOVED SHROUD SEGMENT ON #2 ENG AT 12 O'CLOCK POSITION REF B737-800 AMM 72-2SDR ASAA2022051238320Shroud · scratchedREF ASA T/C # 78472000 #2 ENG INLET AND FAN BLADES- DETAILED INSPT. FOUND UPPER 2 O'CLOCK POS. AFT STRUT PANEL HAS 2 EACH SCRATCHES COMING OUT OF TOP FWD FASTENER HOLES. GROUNDED - YES. REMOVED AND REPLACED SHROUD SEGMENT AT UPPER 2 O'CLOCK POSITION IAW B737-SDR ASAA2022051238319Panel · looseREF ASA T/C # 78472000 #2 ENG. INLET AND FAN BLADES- DETAILED INSPT. FOUND #8,11, &12 I/B FAN DUCT PANELS LOOSE. GROUNDED - YES. TIGHTENED THE SCREWS OF #8,11, & 12 FAN DUCT PANELS IAW B737-800 AMM 72-23-07.SDR ASAA2022042138079None · faultyWHILE STARTING ENG #2 SPAR VALVE CLOSED LIGHT ILLUMINATED BRIGHT BLUE AND REMAINED BRIGHT. ENG STABILIZED AT AROUND 48% N1 AND HUNG. DISCONTINUED START. AFTERWARD WE FOUND FUEL SPAR VALVE ENG 2 POPPED. GROUNDED - YES. REPLACED #2 ENG SPAR VALVE ACTUATOR REF B7SDR ASAA2022040837940None · leakingWHILE PERFORMING TSR711826 FOR #2 ENGINE EGT EXCEEDANCE TROUBLESHOOTING AND CHECKING FOR ENGINE BLEED AIR DISTRIBUTION SYSTEM LEAKS PER B737-800 FIM 71-06 TASK 805, FOUND PRSOV LEAKING FROM MANUAL OPEN/CLOSE SELECTOR. GROUNDED - YES. REMOVED AND REPLACED #2 ESDR ASAA2022040737946None · leakingON TAKE OFF, OBCE AIRBORNE, THROUGH FIRST POWER REDUCTION, BOTH ENG #1 AND ENG# 2 EGT EXCEEDED REDLINE AND EGT TURNED RED UNTIL POWER REDUCTION AT APROX 1000 FT AGL 26K MAX TAKEOFF. GROUNDED - YES. PERF POWER ASSURANCE CK REF B737-800 AMM TASK 71-00-00-700-813SDR ASAA2022040737921Egt Indication · out of adjustGE DIAGNOSTICS REPORTS THE #1 ENGINE EXPERIENCED AN EGT EXCEEDANCE DURING TAKEOFF THAT MAY HAVE EXCEEDED THE TRANSIENT AREA LIMITS. PEAK EGT RECORDED ON REPORT 06 WAS 966 DEGREES DURING TAKEOFF (FLIGHT PHASE 4) GROUNDED - YES. PERFORMED GVI OF #1 ENGINE INLET SDR ASAA2022013037316Unknown · unknownZONE TEMP CAUTION ON MASTER RECALL. GROUNDED - YES. ENROUTE MEL - #2 ZONE TEMP CONT LOGGED FLT DECK TRIM VALVE FAULT. FAULT CLEARED & SYS CKS NML PER B737-800 AMM 21-61-00. GND VERIFICATION SUCCESSFUL.SDR ASAA2022013037285Unknown · unknownCAPT FD INOP WITH FLAG ON PFD. GROUNDED - YES. CH A NOT AVAILABLE ON DFCS BITE, CYCLED 8 C/B FOR FCC-A, SYSTEM RESTORED, DFCS CURRENT STATUS PASS. ACCOMPLISHED LAND VERIFY TEST, PASS REF B737-800 FIM 22-11 TASK 801.SDR ASAA2022012737287Transceiver · inoperativeHF RADIO #2 INOP. GROUNDED - YES. CONFIRMED FAULT, #2 HF INOP, WILL NOT TEST. REMOVED & REPLACED #2 HF TRANSCEIVER REF B737-800 AMM 23-11-21. #2 HF SYSTEM GROUND VERIFICATION TEST NML (CONTACTED SFO RADIO) PER AMM 23-11-00-730-801 & AMM 23-11-00-710-801.SDR ASAA2022012737271Unknown · unknownHF #2 INOP. GROUNDED - YES. HF #2 PLACED ON MEL, REF L/P 60320019.SDR ASAA2021120536827Unknown · unknownSTARTING SOMETIME AFTER CENTER TANK FUEL COMPLETELY BURNED, THE CENTER TANK FUEL INDICATION OF "0.00" WILL GO BLANK, FOLLOWED SHORTLY THERE AFTER BY THE TOTAL FUEL INDICATION, BOTH INDICATIONS WILL RETURN A FEW SECONDS LATER. ALL OTHER FUEL QTY AND FLOW INDICASDR ASAA2021112236684Modulating Valve · inoperativeILLUMINATION OF THE ZONE TEMP CONT CAB ON RECALL OF MASTER CAUTION. EXTINGUISHES ON RESET. GROUNDED - YES. REMOVED AND REPLACED CONTROL CABIN TRIM MODULATING VALVE IAW B737-800 AMM 21-61-21-000-801 AND AMM 21-61-21-400-801, ETOPS GROUND FUNCTIONAL CHECK GOOD ISDR ASAA2021111836662Control Unit · faultyWINDOW OVERHEAT. RIGHT #2 SIDE WINDOW. GROUNDED - YES. PER B737-800 FIM 30-41 TASK 801 AND 806. WINDOW HEAT PWR RIGHT SIDE C/B WAS OPEN. RESET BREAKER. PERFORMED WHCU BITE. HISTORY OF BUS POWER FAULT. EXAMINED WINDOW TERMINALS AND BACK OF C/B. NO DEFECTS. R2 WSDR ASAA2021111736628Unknown · unknownHF # 1 DISPLAY FAIL/FAIL. GROUNDED - YES. PERFORMED HF # 1 TEST PE B737-800 FIM 23-11 TASK 806 HF # 1 TEST OK, OK FOR SERVICE.SDR ASAA2021102436399Module · faultyRIGHT SIDE WINDOW HEAT OVERHEAT LIGHT CAME ON AND C/B IS OPEN AS WELL. GROUNDED - YES. T/S AND FOUND P5-9 PANEL AT FAULT. REMOVED AND REPLACED P5-9 PANEL IAW B737-800 AMM 30-41-41 & RT SIDE WINDOW OPS NML.SDR ASAA2021101536320Unknown · unknownR SIDE WINDOW HEAT OVERHEAT ON IN DESCENT, RAN QRH, OVERHEAT LIGHT LITE ILLUMINATED AGAIN AFTER 5 MIN WAIT PER QRH. GROUNDED - YES. ACCOMPLISHED WHCU BITE REF B737-800 FIM 30-41 TASK 801. LRU SHOWS FAULT FOR RIGHT SIDE WINDOW BUS POWER. ACCOMPLISHED FIM 30-41 SDR ASAA2021100236155None · damagedPER T/C 78472000 FOUND PANEL STRUT LPTACC SCREWS CHAFFING THRU. PANEL NEEDS REPLACEMENT. GROUNDED - YES. REMOVED PANEL P/N 340-084-003-0 PER B737-800 SRM 54-40-02. INSTALLED PANEL 340-084-003-0 REF B737-800 AMM 72-23-07.SDR ASAA2021092436070Control Panel · inoperativeCAPTAIN'S COURSE SELECT KNOB INTERMITTENTLY LOCKS. GROUNDED - YES. WITH A/C POWER OFF THE AIRPLANE REPLACED DFCS MODE CONTROL PANEL WITH SERVICEABLE UNIT. APPLIED GROUND POWER TO A/C. C/W DFCS MODE CONTROL PANEL ADJUSTMENT/TEST. TEST PASSED. REF B737-800 AMM 2SDR ASAA2021091035927Selector · stuckCAPT MCP COURSE SELECTOR STUCK ON 020* - WILL NOT MOVE AFTER SELECTING APU POWER, SELECTOR APPEARS NORMAL. GROUNDED - YES. ACCOMP LRU REPLACEMENT TEST FOR MCP. TEST PASS ALSO ACCOMP LAND VERIFY TEST BOTH PASS NO FAULTS. REF B737-800 AMM 22-11-34-839-001 & 22-1SDR ASAA2021072635534Satcom · malfunctionedBOTH SATELLITE PHONES SUCCESSFULLY COMPLETE AND RECEIVE CALLS BUT PILOT TRANSMISSIONS OVER BOTH CHANNELS ARE INOPERATIVE. AUDIO QUALITY FROM RECIPIANTS IS CLEAR & NORMAL. INBOUND CALLS ANSWER NORMALLY. GROUNDED - YES. ACCOMPLISHED CYCLING OF SATCOM CB. ACCOMPLSDR ASAA2021061935146Switch · faultedNUMBER 2 ENGINE VALVE CLOSED LIGHT ILLUMINATED BRIGHT BLUE AFTER ENGINE SHUT DOWN. GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE HPSOV SWITCH REF B737-800 AMM 73-21-09. NO EEC FAULTS LOGGED.SDR ASAA2021052334896Starter Gen · faultyDURING TROUBLE SHOOTING FOUND ACTIVE/CURRENT FAULT 49-41250 START CONVERTER UNIT SHOWS SYSTEM INOP ON APU. GROUNDED - YES. ACCOMPLISHED B737-800 FIM 49-40 TASK 811. INITIAL EVALUATION SHOWS NO CURRENT STATUS MESSAGE. APU START AND OPERATION IS NORMAL. PERFORMSDR ASAA2021052234893Modulating Valve · failedLEFT HAND PACK LIGHT ILLUMINATED ON RECALL. GROUNDED - YES. PERFORMED #1 PACK/ZONE TEMP CONTROL BITE TEST SHOWS TCV FAIL. REMOVED AND REPLACED #1 TEMP CONTROL VALVE REF B737-800 AMM 21-51-10. PERFORMED BITE CHK AND FAULT IS CLEARED. SUPPLIED PNEUMATIC PRESSURE
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