N588AS
Service difficulty reports · 577
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 = 'N588AS' 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 = 'N588AS' 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 ASAA2018071225350Wire Harness · wornWHILE ACCOMPLISHING T/C N8420001 FOUND CONNECTOR PROTECTION WORN BEYONG LIMITS ON J8 ON NR 2 ENGINE. GROUNDED - YES. REMOVED AND REPLACED J8 HARNESS ON NR 2 ENG. REF MM 73-21-06/401 OPS CK GOOD. PULLED, COLLARED, AND RESET 2 CBS.SDR ASAA2018071225349Heater · leakingNR 1 ENGINE SERVO FUEL HEATER LEAKING. GROUNDED - YES. REMOVED AND REPLACED NR 1 ENG SERVO FUEL HEATER IAW AMM 73-11-07-000-801-F00 AND 73-11-07-400-801-F00. LEAK CHECK & OPS CK GOOD.SDR ASAA2018071225348Pump · leakingWHILE PERFORMING ENGINE RUN ON THE NR 1 ENGINE FOUND FUEL LEAKING UNDER COWLING. GROUNDED - YES. OPENED FAN COWL AND INSPECTED NR 1 ENGINE. CLEANED AREA AND PERFORMED ENGINE RUN FOR 20 MIN'S. ONE LEAK FOUND AT FUEL PUMP PAD DRAIN (5 DROPS PER MIN.) I/B FAN COWSDR ASAA2018062625209Blade · wornFOUND BLADE PAIR NR 4 S/N DB186689-C WITH SHIM WEAR CONVEX AREA L AND NR 16 S/N DB187438-2 WITH CU-NI ON CC SURFACE TE BEYOND LIMITS. ESN 896150. GROUNDED - YES. REMOVED NR 4 DB186689-C AND S/N DB187438-2 AND INSTALLED NEW FAN BLADES S/N DC891306-4 AND S/N DD8SDR ASAA2018062625208Blade · damagedWHILE ACCOMP T/C 78472002 FOUND BLADE PAIR NR 7 S/N DD863333-01 WITH CU-N1 COATING CC TE BEYOND LIMITS AND NR 19 S/N DE055856F WITH CU-N1 COATING CC TE BEYOND LIMITS ESN-896150. GROUNDED - YES. REMOVED FAN BLADE NR 7 S/N DD863333-M AND NR 19 S/N DE055856F AND SDR ASAA2018062625207Blade · damagedWHILE ACL TC 78472002 FOUND NR 10 FAN BLADE S/N DE055720-9 WITH CU-NI COATING DAMAGE CC. TE BEYOND LIMITS ESN-896150. GROUNDED - YES. REMOVED NR 10 FAN BLADE S/N DE055720-9 AND INSTALLED NEW FAN BLADE S/N DM019014-7 IAW FAN BLADE MAP. ALSO AND OPPOSE TO THE MASDR ASAA2018062625206Tank Unit · failedACCOMPLISHED T/C NG-28FCD-18090-1 FOR NR 2 TANK AND FOUND TANK UNIT 1, 2, AND 3 OUT OF LIMITS PER AMM 28-41-21-710-801. GROUNDED - YES. REF T/C NG-28FCD-18090-1. REMOVED AND REPLACED TANK UNIT NR 1, TANK UNIT NR 2 AND TANK UNIT NR 3 REF AMM 28-41-21-400-801. ASDR ASAA201806255176Spinner · damagedWHILE ACCOMPLISHING FAN BLADE LUBE IAW TC 78472002, FOUND DAMAGE ON THE REAR SPINNER AT TWO PLACES. ACFT GROUNDED. REPLACED THE REAR SPINNER IAW TC 78472002.SDR ASAA2018062025194Elastomer · damagedON DESCENT INTO KSJC NUMBER 1 ENGINE READ VIB OF 2.5. GROUNDED - YES. DURING DISASSEMBLY OF NR 1 ENG FOUND 12 EACH PLATFORMS WITH DAMAGED/ MISSING ELASTOMER, REPLACED 12 EACH PLATFORMS WITH 340-001-216-0 DURING REASSEMBLY OF FAN LUBE TASK CARD 78472002.SDR ASAA2018060724970Shroud · damagedWHILE ACCOMPLISHING TC 78472000 NR 2 ENGINE FOUND ABRAIDABLE SHROUD CRATER AND SHOWING PARENT METAL AT 12 O’CLOCK POSITION. PARENT METAL HAS NO DEFECTS. GROUNDED - YES. ACCOMPLISHED RECONDITION OF THE ABRAIDABLE SHROUD PER AMM 72-24-02-200-802-F00. THIS CLEARSSDR ASAA2018060324941Switch · stuckDUE TO A REPORT OF THE APU START SWITCH BEEN STUCK IN THE OFF POSITION AND PREVENTING THE APU START, ACFT GROUNDED. REMOVED AND REPLACED THE APU MASTER SWITCH. OPS CHECKED GOOD. IAW AMM 49-41-01 AND WDM 49-62-11-7.SDR ASAA2018060624894Warning Message · false activationAPU OVERSPEED WITH AUTO SHUTDOWN. ACFT GROUNDED. PERFORMED AN APU OPS TEST, AND APU BITE PROCEDURE. OPS TESTED GOOD AND NO NO FAULTS IN APU BITE CURRENT STATUS. IAW FIM 49-30 TASK 802.SDR ASAA2018052824829Panel · looseREF T/C 78472000 NR 1 ENG INLET AND FAN BLADES-DETAILED INSP FOUND NR 1 STRUT PANEL, JUST TO THE RIGHT OF 12 O'CLOCK STRUT, LOOSE. GROUNDED - YES. TIGHTENED SCREWS DOWN ON NR 1 STRUT PANEL REF AMM 72-23-07-400-801-F00.SDR ASAA2018052824828Panel · damagedNR 1 ENGINE INLET AND FAN BLADES, DETAILED INSPECTION FOUND ONE LOOSE FASTENER ON THE LOWER OTBD SIDE, AT THE 3 O'CLOCK POSITION. STRUT FAIRING PANEL APPEARS TO BE DAMAGED FROM LOOSE FASTENER. ACFT GROUNDED. REMOVED DAMAGED STRUT FAIRING PANEL. INSTALLED NEWSDR ASAA2018032424029Lamp · failedLEFT EXTERIOR SLIDE AT THE OVERWING, THE EMERGENCY LIGHT INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMPS IAW AMM 33-51-04-960-801. VISUAL OP CHECKED GOOD.SDR ASAA2018030723791Terminal · brokenON PREFLIGHT, FIRE DETECTION TEST, THE NR 1 ENGINE A LOOP WOULD NOT SELF TEST. ACFT GROUNDED. VERIFIED DEFECT, FOUND ENGINE CORE DETECTOR A LOOP TERMINAL BROKEN. TERMINATED THE A LOOP TERMINAL IAW AMM 26-11-02, OPS TEST PASSED IAW AMM 26-11-00.SDR ASAA2018030423763Warning Message · intermittentON APPROACH, THE FMC DISAGREE ILLUMINATED MOMENTARILY ON BOTH THE CAPTAIN`S AND FIRST OFFICER`S NAVIGATIONAL DISPLAYS. ACFT GROUNDED. IAW FIM 34-61/ 835, PULLED AND RESET THE CIRCUIT BREAKERS FOR THE NR 1 & 2 FMCS. MESSAGE CLEARED, AIRCRAFT OK FOR SERVICESDR ASAA2018012023242Wire Harness · faultyNR 2 ENG EEC CHANGED, EEC BITE TEST FAILS FOR FAULTS: 75-10422 HMU VBV CNTL CURRENT OUT OF RANGE, 73-10342 FMV POSITION IS OUT OF RANGE. NR 2 ENG RUN FAILS WITH FAULTS: 73-31162 THE MECHANICAL OVERSPEED PROTECTION IS OUT OF RANGE, 73-10342 FMV POSITION IS OUT SDR ASAA2018011623184Eec · faultedWHILE PERFORMING T/C 78273000, NR 2 ENGINE SHOWED SHORT TERM FAULT CODE 75-10372, THE HMU VSV CONTROL CURRENT IS OUT OF RANGE. ACFT GROUNDED. ACCOMPLISHED T/C 78273000 AND FOUND THE FAULT CODE 75-10372 ACTIVE ON EVERY LEG. PERFORMED FIM 75-31 TASK 801. SDR ASAA2018011523179Lens · detachedEMERGENCY EXIT SIGN LENS FELL OFF IN THE AFT GALLEY, RIGHT SIDE. ACFT GROUNDED. INSTALLED A NEW SIGN LENS ASSY IAW AMM 33-51-01.SDR ASAA2018011423163Anti-Ice Valve · failedDURING TAKEOFF, WITH ENGINE ANTI-ICE SWITCHES ON, THE MASTER CAUTION AND THE ENGINE NR 1 COWL ANTI-ICE LIGHTS BRIEFLY ILLUMINATED JUST AFTER THE TOGA SWITCH WAS PUSHED. ACFT GROUNDED. REMOVED AND REPLACED THE ENGINE COWL ANTI-ICE VALVE. RAN ENGINE, OPS CHECSDR ASAA2018010823115Fault Code · false activationFOUND THE NR 2 ENGINE, SHORT TIME FAULT MESSAGE 75-10372, THE HMU CONTROL CURRENT IS OUT OF RANGE. ACFT GROUNDED. ACCOMPLISHED EEC TEST, NO FAULTS LOGGED ON FLT LEGS 1 AND 2. ACCOMPLISHED FIM 75-31 - 801, HMU VSV CONTROL OUT OF RANGE FAULT ISOLATION, RESISSDR ASAA2018010723102Hf Comm · malfunctionedNR 1 HF RADIO INOPERATIVE. ACFT GROUNDED. ACCOMPLISHED FIM 23-11 TASK 806, NR 1 HF OPS NORMAL. OKAY FOR SERVICE.SDR ASAA2017122223001Stator Vane · out of toleranceWHILE ACCOMPLISHING TC 78273000 NR 2 ENGINE LOGGED SHORT TIME FAULT 75-10372. THE HMU VSV CONTROL CURRENT IS OUT OF RANGE FOR LEGS 0 AND 1. ACFT GROUNDED. IAW TC 78273000, NO RECENT FAULTS. PERFORMED FIM 75-31, TASK 801. OPENED AND CLOSED FOUR CIRCUIT BREAKSDR ASAA2017112122661Snubber · brokenL1 DOOR SNUBBER BROKEN. DOOR HARD TO OPEN. ACFT GROUNDED. REPLACED THE L1 DOOR SNUBBER IAW AMM 52-11-51-400-801. OPS CHECKED GOOD.SDR ASAA2017110122447Attach Angle · crackedFWD CARGO STRINGER 24L WEB ATTACH ANGLE CRACKED ON THE AFT SIDE OF BS 500H. ACFT GROUNDED. REMOVED AND REPLACED THE WEB ATTACH ANGLE IAW SRM 51-40-02, AND DWG 143A7505, REV A.SDR ASAA2017103022445Baffle · corrodedBAFFLE ASSY AT BS 500H, RBL 24 HAS CORROSION AROUND NUTPLATES. ACFT GROUNDED. REMOVED THE CORROSION IAW SRM 51-10-02, AND FOUND TO BE OUT OF LIMITS. REMOVED THE BAFFLE IAW SRM 51-40-02. LOCATED AND DRILLED A NEW BAFFLE IAW SRM 51-40-05 AND DWG 143A7505 REV SDR ASAA2017102922497Intercostal · corrodedCOCKPIT FLOOR PANEL SUPPORT FOR (211AF) AT BS 268.25 HAS CORROSION AROUND NUTPLATE AND FASTENER. GROUNDED - YES. REMOVED CORROSION ON MAIN CABIN FLOOR STRUCTURE LATERAL INTERCOSTAL AT STA 270 BETWEEN LBL10-RBL2.25 ORIGINAL THICKNESS .50, REMAINING THICKNESS .0SDR ASAA2017102522465Skin · dentedSKIN DENTED BETWEEN BS 500D AND 500E, STRINGERS 21R AND 22R. ACFT GROUNDED. FOUND DENT TO BE CREASED AND OUT OF LIMITS IAW SRM 53-00-01-1A-1, FIG 103. REPAIRED THE SKIN IAW SRM 53-00-01-2R-3, CAT B.SDR ASAA2017102522381Transition Panel · corrodedFWD CARGO BAY TRANSITION PANEL CORRODED RT SIDE BS 500C-500F. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED THE DAMAGED SECTION IAW SRM 51-10-02. LOCATED AND DRILLED A REPAIR IAW SRM 53-00-53-2SDR ASAA2017102522379Attach Angle · crackedFWD PIT STR24R WEB ATTACH ANGLE CRACKED BOTH FWD AND AFT SIDE OF STA 500H. GROUNDED - YES. REMOVED AND REPLACED FWD PIT STR 24R WEB ATTACHED ANGLES BOTH FWD AND AFT STR OF STA 500H IAW SRM 51-40-01 AND BAC DWG G143A7505 REV A.SDR ASAA2017102422479Web · corrodedAFT CARGO DOOR SURROUND, LOWER MAIN SILL WEB IS CORRODED. ACFT GROUNDED. REMOVED THE WEB IAW SRM 51-40-02, & IAW DWG 146A5340, REV-. FABRICATED A NEW WEB IAW DWG 146A8123 REV-. INSTALLED THE WEB IAW SRM 51-40-02, & DWG 146A8340 REV-.SDR ASAA2017102422446Channel · corrodedAFT CARGO BAY FLOOR, RT ZEE CHANNEL SECTION BS 727E+10 TO 767 IS CORRODED. ACFT GROUNDED. REMOVED THE CORROSION AND FOUND BEYOND LIMITS IAW 53-00-53-1A-2. ACCOMPLISHED A SPLICE REPAIR IAW SRM 53-00-53-2R-5.SDR ASAA2017102422414Channel · corrodedAFT CARGO BAY FLOOR CHANNEL BS 755 TO 820 IS CORRODED. ACFT GROUNDED. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED DAMAGED SECTION IAW SRM 53-00-53-2R-5. FABRICATED SPLICES IAW B737-800 SRM 53-00-53-2R-5. INSTALLED THE NEW CSDR ASAA2017102422409Channel · corrodedAFT CARGO BAY FLOOR CHANNEL, BS 727F+10 TO 727J+13 IS CORRODED. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE BEYOND LIMITS IAW SRM 53-00-53-1A-2. REMOVED, FABRICATED, AND INSTALLED A NEW CHANNEL IAW SRM 53-00-53-20-5 AND IAW DWG 146A7500, REV-.SDR ASAA2017102422390Channel · corrodedAFT CARGO BAY FLOOR CHANNEL BS 727B+10 - 727E+10 IS CORRODED. ACFT GROUNDED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-0053-1A-2. REPAIRED IAW SRM 53-00-53-2R-5.SDR ASAA2017102422388Channel · corrodedAFT CARGO BAY CHANNEL SECTION BS 727C+8 - 727F+10 IS CORRODED. ACFT GROUNDED. REMOVED CORROSION AND FOUND TO BE BEYOND ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED THE CHANNEL IAW SRM 53-00-52-2R-5, SRM 53-00-53-2R-5, 51-20-81, SOPM 20-41SDR ASAA2017102422378Shield · corrodedAFT CARGO COMPARTMENT DOOR SURROUND, FWD SHIELD STA 767-794 IS CORRODED. GROUNDED - YES. REMOVED CORROSION FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-60-15-1A-1, ORIGINAL MAT THICKNESS IS .050. REMAINING IS .043, REMOVED .007. REMOVED AND INSTALLED NEW SHIELD IASDR ASAA2017102322500Web · chafedLOWER FUSELAGE E&E DOOR CUTOUT, RIGHT SIDE SURROUND STRUCTURE IS CHAFED AND GOUGED FROM DOOR LOCKPIN CONTACT. GROUNDED - YES. DAMAGE FOUND NOT WITHIN LIMITS IAW SRM 53-10-15. FABRICATED NEW WEB IAW BAC DWG 141A8503. ALODINED AND PRIMED IAW SRM 51-20-01. REMOVESDR ASAA2017100922148Oil Cooler · contaminatedAFTER ENGINE START, THE NR 1 GENERATOR WOULD NOT COME ONLINE WITH DRIVE LIGHT ILLUMINATED. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 IDG IAW AMM 24-11-11. FOUND CONTAMINATION IN FILTERS. REMOVED AND REPLACED IDG AIR/OIL COOLER IAW AMM 24-11-21. REMOVED ANSDR ASAA2017100822149Warning Light · false activationON VECTORS FOR APPROACH, NR 1 SOURCE OFF LIGHT ILLUMINATED. FOLLOWED QRH AND PUT APU ONLINE. ACFT GROUNDED. PERFORMED THE INSTRUMENT LANDING OPERATIONAL TEST IAW AMM 34-31-00-710-801 AND THE AIR DATA REFERENCE SYSTEM SELECT OPERATIONAL TEST IAW AMM 34-21-0SDR ASAA2017100822147Warning Light · false activationCONTROL CABIN ZONE TEMP LIGHT ILLUMINATED DURING MASTER CAUTION RECALL. CONTROL CABIN ZONE TEMP LIGHT EXTINGUISHED WHEN MASTER CAUTION SYSTEM RESET. ACFT GROUNDED. PERFORMED THE PACK ZONE TEMPERATURE CONTROL BITE TEST IAW AMM 21-61-00-806-002. NO FAULTS FOUNSDR ASAA2017092822082Connector · damagedCARGO FIRE PANEL DISCHARGE LIGHT FOUND ILLUMINATED. ACFT GROUNDED. TROUBLESHOT IAW FIM 26-23 TASK 802. DISCHARGE LIGHT GOES OFF WITH RT CONNECTOR FIRE BOTTLE CONNECTED. DISCHARGE LIGHT ILLUMINATES WHEN RT CARGO FIRE BOTTLE CONNECTOR CONNECTED. CLEANED & INSPESDR ASAA2017092722069Control Panel · faultedCARGO FIRE DISCHARGE LIGHT ILLUMINATED. ACFT GROUNDED. VERIFIED FAULT. INSPECTED BOTH BOTTLES NO DEFECTS. REPLACED CARGO FIRE CONTROL PANEL. ACCOMPLISHED ALL INSTALLATION TESTS, ALL PASSED.SDR ASAA2017092522046Fire Bottle · failedUPON ENTERING FLIGHT DECK, NOTED THAT CARGO FIRE SUPPRESSION SYSTEM BOTTLE DISCHARGE LIGHT WAS ILLUMINATED. GROUNDED - YES. REF TASK CARD 78226001, REMOVAL AND REPLACEMENT OF CARGO FIRE BOTTLE. MEL 26-19L CLEARED.SDR ASAA2017092021989Control Unit · failedWHILE TROUBLESHOOTING THE NR 1 IDG, SWITCHING BUSSES BACK AND FORTH CAUSED P5-13 ELEC LIGHT TO ILLUMINATE. SHOWS SPCU INOPERATIVE FAULT. ACFT GROUNDED. REMOVED & REPLACED THE SPCU IAW AMM 24-34-11. OPS NORMAL.SDR ASAA2017091921983Idg · failedTHE NR 1 GENERATOR SOURCE OFF LIGHT ILLUMINATED. COMPLIED WITH QRH PROCEDURE. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 IDG IAW AMM 24-11-11. VISUAL INSPECTION OF FILTERS SHOWS NO VISIBLE CONTAMINATION. OPS CHECKED GOOD AT THIS TIME IAW AMM 24-11-00.SDR ASAA2017083121803Fmc · malfunctionedTAXIING OUT FOR DEPARTURE, GOT FMC FAIL MSG FOR RIGHT FMC. NO RIGHT MAP AND VTK CAME ON RIGHT SIDE. ACCOMPLISHED QRH AND AFTER 1 MINUTE HAD NORMAL INDICATIONS. GROUNDED - YES. ACCOMP FMC BITE PROCEDURE FOR BOTH FMC'S SENSORS ALL SHOW OK AND INFLT FAULTS THERE SDR ASAA2017083121799Fmc · failedRIGHT FMC FAIL AFTER SECOND ENGINE START. ACCOMPLISHED QRH AND SYSTEM RETURNED TO NORMAL. ACFT GROUNDED. REMOVED AND REPLACED RIGHT FMCS COMPUTER IAW AMM 34-61-02/401. FMCS OPS TESTED NORMAL IAW AMM TASK 34-61-00-710-801.SDR ASAA2017081421635Seal · crackedDURING INSPECTION OF THE NR 1 ENGINE INLET IAW TC 78472000, FOUND FIVE FAN OUTLET GUIDE VANE SEALS CRACKED AND/OR MISSING AT APPROXIMATELY 8 O'CLOCK POSITION LOOKING FWD. ACFT GROUNDED. REPLACED THE DAMAGED OGV SEALS IAW EA 800-72EA-19168, REV 00, AND AMM 7
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