N581AS
Service difficulty reports · 484
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 = 'N581AS' 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 = 'N581AS' 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 ASAA2013032494257Relay · failedDURING CRUISE, FL350, WITH 10,000 LBS FUEL REMAINING IN CENTER TANK, LT CENTER TANK LOW PRESSURE LIGHT ILLUMINATED. ACCOMPLISHED FUEL PUMP LOW PRESSURE QRH PROCEDURE, TURNED OFF PUMP AND OPENED CROSSFEED. REMAINDER OF CENTER TANK FUEL BURNED NORMALLY VIA RT SDR ASAA2013031394159Warning Light · false activationLEFT CENTER TANK FUEL BOOST PUMP LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT IN CRUISE AT 33,000 FT. MASTER CAUTION ALSO ILLUMINATED. 16, 800 LBS IN CENTER TANK. PERFORMED CENTER TANK BOOST PUMP AUTO SHUTOFF FUNCTIONAL TEST IAW MM 28-22-00, OPS CHECKED GOOD. SDR ASAA2013030394050Warning Light · false activationCONT CAB ZONE TEMP ILLUMINATED ON RECALL EXTINGUISHES ON MASTER CAUTION RESET. PERFORMED PACK/ZONE TEMP CONTROLLER BITE CK IAW AMM REF 21-61-00-700-806-002, TEST PASSED, OPERATED PACKS NO FAULTS NOTED, CONT CAB ZONE TEMP DOES NOT ILLUMINATE ON RECALL.SDR ASAA2013020393818Shim · damagedACCOMPLISHING NR 1 NG FAN BLADE LUBE T/C 78472002 FOUND FAN BLADE SHIMS MISSING MORE THAN 25 MOLY DAG COATING. REF MM 72-21-02, PG 615, STEP L (1)(A)(1). INSTALLED NEW FAN BLADE SHIMS REF T/C 78472002, STEP 44.SDR ASAA2013012993785Converter · failedAPU FAULT LIGHT IS ON APU WILL NOT START. FOUND FAULT CODE 49-41250 START CONVERTER UNIT R & R APU START CONVERTER UNIT IAW AMM 49-41-46. APU OPS CHECK NORMAL IAW AMM 49-11-00.SDR ASAA2013011693699Valve · failedON DEPARTURE NOTICED DUCT SPLIT. PERFORMED ENGINE BLEED AIR HEALTH CHECK ON NR 2 ENGINE IAW TASK CARD NG-36WC-00001, SYS PASSED ALL CHECKS. HSV SEEMED TO RATCHET SLIGHTLY UPON OPEN AND CLOSED SO PART WAS REPLACED. REMOVED HSV REF AMM 36-11-06-000-801, REPLSDR ASAA2012122893573Warning Light · false activationON TAXI OUT, FMC DISAGREE WAS ANNUNICATED ON THE NDS. QRH PROCEDURES WERE ACCOMPLISHED WITH NO FURTHER PROBLEMS NOTED. PERFORMED FIM 34-61, TASK 835 IAW INSTRUCTIONS FROM AMM 34-61-01-800-801. FMC DISAGREE ON GROUND IS A NUISANCE ANOMALY AND WAS CLEARED.SDR ASAA2012122693547Controller · malfunctionedLEFT PACK TRIPPED ON SHORT FINAL. FOUND PACK ZONE CONTROLLER FAULT LIGHT ON LT PACK ZONE TEMP CONTOLLER. RESET FAULT & ACCOMPLISHED BITE IAW MM 21-61-00. NO FAULTS NOTED & PACK LIGHTS EXTINGUISH ON RECALL. OK FOR SERVICE.SDR ASAA2012120793426Compensator · inoperativeNR 2 FUEL QTY GAUGE FLUCTUATING 500 LBS. ACCOMPLISHED NR 2 FUEL TANK QTY BITE PROCEDURE IAW FIM TASK 28-41-801. SHOWS CURRENT FAULT 28-41208, TANK 2 COMPENSATOR DATA BAD. ACCOMPLISHED T/C NR 78528000 FUEL TANK ENTRY PERMIT. FQIS BITE FAULTS NR 2 COMPENSATOSDR ASAA2012112193352Transceiver · failedWEATHER RADAR IN ALL SELECTORS. PWS FAIL. WEATHER RADAR WILL NOT GO IN TEST MODE. VERIFIED INSTRUMENT BLOWER OPS GOOD. REPLACED WEATHER RADAR TRANSCEIVER. GROUND VERIFICATION TEST NORMAL REF AMM 34-43-00-710-802-001.SDR ASAA2012111593309Transmitter · failedRADAR IDENT (ENGAGE). DOES NOT REDUCE GROUND CLUTTER OTHER WISE RADAR WORKS OK. TRIED NEW WEATHER RADAR CONTROL PANEL NO CHANGE. R & R WEATHER RADAR TRANSCEIVER. INSTALLATION TEST GOOD REF AMM 34-43-41, 34-43-91. ORIGINAL CONTROL PANEL REINSTALLED.SDR ASAA2012110893282Pump · leakingDURING NR 1 ENGINE TEST 3A IDLE LEAK CHECK FOUND FUEL PUMP PAD DRAIN LEAKING AT RATE OF 25 DROPS PER MIN. R & R NR 1 ENGINE FUEL PUMP REF MM 73-11-01-400-801-F00, STEPS 3.G. THRU 3.I.(3). COMPLETED LEAK/ OPS GROUND VERIFICATION CHECKS. NO LEAKS NOTED. REF MMSDR ASAA2012110893274Indicator · trippedNR 1 ENGINE, IDG OIL PRESSURE DIFFERENTIAL INDICATOR TRIPPED. ACCOMPLISHED FIM TASK 24-11 TASK 803 IDG DIFF PRESSURE IND FAULT ISOLATION, ACCOMPLISHED TASK CARDS 78273000 INTERROGATE CDU FOR ENG. FAULTS AND 78424000 IDG FILTER AND OIL CHANGE, THIS IS THE SECOSDR ASAA2012090892859Ecu · faultedNR 2 ENGINE HAS A SHORT TERM FAULT, FAULT 75-20572 (HMU, TBV SIGNAL OUT OF RANGE ). FAULT IS CURRENT. FOUND WHILE PERFORMING T/C 78273000. ACFT GROUNDED. REMOVED EEC FROM NR 2 ENGINE REF AMM 73-21-60-000-801-F00. INSTALLED EEC ON NR 2 ENGINE, REF AMM 73-2SDR ASAA2012092792976Warning Light · false activationAFTER LANDING FMC DISAGREE LIGHT ILLUMINATED ON PFD. PERFORMED BITE TEST PROCEDURE FMC SYS, INREF FIM 34-61-00-810-801, NO FAULT NOTED.SDR ASAA2012092592955Warning Message · false activationSHORTLY AFTER PUSH, RECEIVED AN FMC DISAGREE. MESSAGE RESOLVED WITH QRH, SYS NORMAL.SDR ASAA2012091292877Probe · faultyMANUFACTURER DIAGNOSTICS REPORTED, NR 2 ENGINE TREND DATA SHOWS A SHIFT IN EGT HOT DAY MARGIN. ALL OTHER PARAMETERS NORMAL. EGT INDICATION ERRORS ARE SUSPECT. ACFT GROUNDED. FOUND NR 2 ENG HAD LOGGED FAULT CODE NR 77-20872 TOP LT EGT OUT OF RANGE, ON LAST SDR ASAA2012090192800Controller · malfunctionedON MASTER CAUTION RECALL ON LANDING CHECKLIST AFT CAB ZONE TEMP LIGHT, CONT CAB ZONE TEMP LIGHT AND PACK TRIP LIGHT ILLUMINATED, EXTINGUISHED WITH MASTER CAUTION RESET. ACFT GROUNDED. NR 1 PACK ZONE TEMP CONTROLLER HAD A FAULT LT ON CONTROLLER. REF MM 21-6SDR ASAA2012081792737Eec · inoperativeNR 2 ENGINE CONTROL LIGHT ILLUMINATED AFTER LANDING. ACFT GROUNDED. PERFORMED EEC BITE TEST FAULT CODE 73-31392 PRESENT. PERFORMED FIM TASK 73-22-00-810-807 FOUND EEC INOPERATIVE. REPLACED EEC REF AMM 73-21-60. OPS CHECKED GOOD. ETOPS GROUND VERIFICATION SDR ASAA2012070792505Panel · looseNR 2 ENG FAN BLADE INSPECTION FOUND THREE LOOSE SCREWS IN NOSE COWL LOWER OTBD VENT PANEL AT 6 O`CLOCK POS (ALF) (M), POSSIBLE DAMAGE TO SCREW HOLES IN PANEL. ACFT GROUNDED. REMOVED LOOSE LOCK FASTENERS AND REPLACED WITH LOCK BOLTS IAW EA 800-71EA-09724. SDR ASAA2012070792504Fastener · looseNR 2 ENGINE FAN BLADE INSPECTION. FOUND TWO FASTENERS LOOSE ON OTBD COWL AFT LIP AT 2 O`CLOCK POS (ALF) (M). ACFT GROUNDED. INLET COWL REPLACED.SDR ASAA2012072992642Detector · failedAPU DETECTOR INOPERATIVE. INSPECTED APU FIRE DETECTOR IAW 26-110-00, STEP H. FOUND TAIL PIPE DETECTOR WITH LOW RESISTANCE OF 37.70K OHMS. ACTUAL READING SHOULD BE 3945 OHMS. REMOVED AND INSTALLED TAIL PIPE DETECTOR M1925. OPS CHECKED 26-15-00-710-801. SSDR ASAA2012071292546Start Valve · failedNO ROTATION ON N2 & N1 ON NR 1 ENG WHEN START SWITCH ROTATED TO GROUND. ACFT GROUNDED. WHEN MOTORING NR 1 ENG FOUND START VALVE SLOW TO OPEN. R & R NR 1 ENGINE START CONTROL VALVE, LEAK AND OPS CK NORMAL. REF AMM 80-11-03.SDR ASAA2012063092448Regulator · failedDUCT PRESSURE READING LT 25 PSI, RT 44 PSI BOTH FL370 & FL 340. GROUNDED - YES. PERFORMED PNEU SYST. TROUBLESHOOTING REF 36-11-00-700-804. R & R PRECOOLER CONTROL VALVE REF 36-12-02. R & R PRSOV REF 36-11-04. R & R HIGH STAGE REGULATOR REF 36-11-07, LEAKSDR ASAA12511354Landing Gear · malfunctionedAFTER TAKEOFF, GEAR HANDLE SELECTED TO OFF (RED UNSAFE LIGHT NO GREEN) NOSE GEAR EXTENDED. GEAR SELECTED UP, NOSE GEAR RETRACTED. GEAR HANDLE SELECTED OFF, NOSE GEAR STAYED RETRACTED, NORMAL OPERATIONS. ACCOMPLISHED FIM TASK 32-30-00-810-809 PERFORMED NOSDR ASAA12511195Filter Element · defectiveFOUND NR 1 ENG DPI BUTTON EXTENDED. REPLACED FILTER AND RESET NR 1 ENG DPI INDICATOR PER FIM TASK 24 11 00 810 803.SDR ASAA12511162Control Panel · failedWEATHER RADAR FAIL EN ROUTE THE WXR FAIL CONT STAB LIGHT IS ILLUMINATED. VERIFIED DEFECT WXR TEST INOP. DISPLAYS WXR STAB MESSAGE FOLLOWED BY WXR FAIL NO CALLOUTS OR TEST PATTERN. REPLACED WXR R/T REF MM 34 43 41, NO HELP. REPLACED WXR CONTROL PANEL REF MMSDR ASAA12511142Drive Unit · failedWEATHER RADAR FAILED EN ROUTE. REF WDM 34 41 11 FOUND WXR R/T RACK CONNECTOR D189B PINS C13 & E10 PUSHED BACK RESEATED PINS. WXR TEST STILL FAILS ANT. REPLACED WXR ANT DRIVE UNIT REF MM 34 43 11 RE-INSTALLED WXR R/T REF MM 34 43 41 WXR, OPS CHECKS NORMAL.SDR ASAA12511076Wire Harness · shortedC/B LABELED ENG NR 1 ENGINE AND WING CONTROL ON P18 3 POSITION A 6 IS POPPED. C/O T/S 3 O'CLOCK STRUT HARNESS AND FOUND SHORTED CONDUCTOR TO WTAI SOLENOID IN HARNESS. REPLACED 3 O'CLOCK STRUT HARNESS IAW AMM 73 21 06 400 802 1 00 AND C/O, ALL OPS TEST.SDR ASAA12510900Unknown · malfunctionedNR 1 ENGINE WING CONTROL CB FOUND POPPED AFTER PUSHBACK & ENGINE START. P18 3 A6. INSPECTED BEHIND P18 3 C/B PANEL AND ENG & WING ANTI ICE PANEL & ASSOC WIRING NO DEFECTS. RESET C/B REF MM 20 60 01 & WDM 30 21 11. WING & ENG ANTI ICE TEST PASSED REF MM 30 1SDR ASAA12510908Unknown · unknownLEFT AUTO SHUTOFF FUEL TEST FAILS. PERFORMED CENTER TANKS BOOTS PUMP AUTO SHUTOFF FUNCTIONAL TEST REF MM 28 22 00 720 805, TEST PASSED.SDR ASAA12510929Trans Panel · crackedAFT CARGO BILGE AREA RT TRANSITION PANEL IS CRACKED AT BS 747. CUT OUT DAMAGED SECTION AND FABRICATED ZEE CHANNEL SIDEPLATE AND SPLICE SIDEPLATE (ITEM 1 & 2) P/N BAC1496 377 7075 T62 IAW B737 800 SRM 53 00 53 FIG 202 REPAIR 5. ALODNED AND PRIMED IAW B737 800SDR ASAA12510930Seat Track · corrodedFORWARD CARGO COMPARTMENT AFT BULKHEAD LT/SIDE SEAT TRACK MOUNT CORRODED. REPAIRED TRACK IAW B737 800 SRM 53 00 53 REPAIR 3. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW B767 800 SRM 53 00 53. REMOVED DAMAGED SECTION IAW B737 800 SRM 53 00 53 REPAIR SDR ASAA1150839Unknown · malfunctionedL ENG ANTI ICE "BLUE" LIGHT BULB BURNED OUT. FOUND LT ENG CWL ANTI ICE VLV C/B A 7 OPEN. VISUALLY INSP CWL ANTI ICE VLV C/B BEHIND PANEL. NO DEFECT NOTED. RESET C/B IAW AMM TASK 20 60 01 860 801. TESTED LT ENG CWL ANTI ICE IAW AMM TASK 30 21 00 710 801. SDR ASAA11510710Unknown · malfunctionedON GROUND GOT "FMC DISAGREE". ACCOMPLISHED QRH PROCEDURE. OPS CHECK NORMAL.SDR ASAA11510598Connector · dirtyRIGHT SIDE WINDOW HEAT OVERHEAT LIGHT CAME ON AT 32000 FEET SWITCH OFF AND BACK ON AFTER 5 MINUTES OPS OK. CLEANED AND RESEATED CONNECTORS ON WINDOW CABLE. OPS CHECK GOOD REF AMM 30 41 00.SDR ASAA11510577Warning System · intermittentAPU FAULT LIGHT ON START UP TAXIING INTO GATE SAN. PERFORMED FIM TASK 49 40 00 810 821 FOUND TO BE INTERMITTENT FAULT OP`S CHECKED GOOD.SDR ASAA11510514Transceiver · malfunctionedPWS FAIL LIGHT ILLUMINATED DURING PREFLIGHT. ADDITIONALLY WX RADAR SHOWS FAULT INDICATION "RT" ON DISPLAY DURING T/S. PERFORMED FIM TASK 34 43 00 810 815 PREDICTIVE WINDSHEAR SYSTEM PROBLEM FAULT ISOLATION AND TASK 34 43 00 710 802 001 WEATHER RADAR SYSTEM OSDR ASAA11510483Transceiver · malfunctionedON PREFLIGHT PWS FAILED & WXR FAIL ILLUMINATED ON ND. REPLACED WX TRANSCEIVER PER AMM 34 43 41, OPS CHECK PER AMM 34 43 00.SDR ASAA11510393Screw · out of toleranceNR 1 ENGINE TREND DATA SHOWS LOW PRESSURE ROTOR VIBRATION LEVELS TO BE TRENDING HIGHER THAN EXPECTED CURRENT LEVELS NEAR 1.2 UNITS. ACCOMPLISHED ON NR 1 ENG ON BOARD FAN TRIM REF MM 71 00 00 750 803 FOO. FOLLOWING BALANCE WEIGHT CHANGES: NR 10 PO11 TO P07 NSDR ASAA11510362Unknown · malfunctionedWXR FAIL ANNUNCIATOR ON BOTH DU'S. PERFORMED FIM TASK 34 43 00 810 801 WEATHER RADER SYSTEM BITE CLEARED FAULTS INTERMITTENT FAULT OBSERVED GROUND VERIFICATION SUCCESSFUL SYSTEM OP'S NORMAL.SDR ASAA11510258Connector · dirtyGE DIAGNOSTICS REPORTS NR 2 ENGINE TREND DATA SHOWS A SUDDEN SHIFT IN DELTA EGT. ALL OTHER PARAMETERS NORMAL. EGT INDICATION ERRORS ARE SUSPECT. PRE-CLEANING READINGS: S1 156.73 S2 98.49 S3 91.71 S4 151.13. CLEANED CONNECTORS DP0901 DP0911 DP0912 DP0913 DSDR ASAA1159920Fuel/Oil Cooler · leakingFOUND FUEL LEAKING FROM FUEL / OIL HEAT EXCHANGER DRAIN LINE ON NR 1 ENGINE. NUMBER ONE ENGINE MAIN OIL / FUEL HEAT EXCHANGER DEFERRED FOR 75 CYCLES REF AMM 71 71 00 200 801 PARA F (1)(B)1. LEAKAGE RATE IS 10 DROPS PER MINUTE WITH ENGINE RUNNING AND NO LEAKASDR ASAA1159648Control Unit · malfunctionedDURING CLIMB RIGHT SIDE WINDOW OVERHEAT ILLUMINATED. TROUBLESHOT PER FIM INTERMITTENT FAULT. NO HARD FAULTS FOUND. REPLACED WHCU & COIL CORD REF MM 30 41 11. OPS NORMAL.SDR ASAA1159569Warning System · false activationR2 WINDOW OVERHEAT ILLUMINATED AT FL 360 FOLLOWED CHECKLIST AND CONTINUED NORMAL OPERATIONS. ACCOMPLISHED WINDOW HEAT SYS OPERATIONAL TEST PER AMM TASK 30 41 00 710 801. OPERATIONAL TEST NORMAL.SDR ASAA1159417Connector · looseLEFT SIDE WINDOW OVERHEAT LIGHT ON. FOLLOWED QRH LIGHT REMAINED ON. PERFORMED FIM TASK 30 41 TASK 801. BITE OF CONTROLLER INDICATED LEFT SIDE WINDOW SENSOR. PERFORMED FIM TASK 30 41 TASK 811. AFTER FINDING SENSOR CONNECTOR LOOSE AND REMOVING AND RECONNECTSDR ASAA1159406Transceiver · faultyNR 1 HF RADIO WILL NOT TRANSMIT. REPLACED NR 1 HF TRANSCEIVER PER AMM 23 11 21. REPLACED NR 1 HF COUPLER PER AMM 23 11 61. OPS CHECK GOOD PER FIM TASK 23 11 00.SDR ASAA1159401Unknown · malfunctionedON TAXI OUT "FMC DISAGREE" DISPLAYED. ACCOMP CHECKLIST MESSAGE WENT AWAY PROCEEDED NORMALLY.SDR ASAA1159382Warning System · false activationAT F320 RIGHT SIDE WINDOW HEAT "OVERHEAT" LIGHT ILLUMINATED. RAN QRH LIGHT REMAINS EXTINGUISHED. ACCOMPLISHED BIT FIM TASK 30 41 00 810 OPERATIONAL CHECK NORMAL. NO FAULT NOTED.SDR ASAA1159378Wire Harness · damagedON TAXI IN LEFT SIDE WINDOW OVERHEAT ILLUMINATED FOLLOWED QRH OVERHEAT LIGHT EXTINGUISHED. REMOVED AND REPLACED DAMAGED SIDE WINDOW CONNECTING CORD REF FIM 30 41 00 810 811, OPS CHECK GOOD.
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