N562AS

Service difficulty reports · 600

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 = 'N562AS' 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.

SDR ASAA2013091695988Warning Light · no indicationDURING TAXI, NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED DID NOT EXTINGUISH UNTIL ENGINE WAS SHUTDOWN. ACFT GROUNDED. IAW FIM 79-05, TASK 817, STEP E2 CDU INPUT MONITORING/OIL FILTER SCREEN OTHER THAN CLOGGED CONDITION DISPLAYED IAW STEP G2. REMOVED, INSep 16, 2013 · N562AS · Boeing 737890 · Engine Oil Distribution (Airframe Furnished)SDR ASAA2013091295965Oil System · lowAFTER APU START, MAINTENANCE LIGHT ILLUMINATED. ACFT GROUNDED. PERFORMED APU BITE RECEIVED MAINTENANCE MESSAGE 49-91227 LOW OIL QTY. SERVICED APU OIL REF MM 12-13-31. VERIFIED APU BITE SHOWS OIL QTY FULL.Sep 12, 2013 · N562AS · Boeing 737890 · APU Oil SystemSDR ASAA2013080695739Control Module · inoperativeFLT ALTITUDE DISPLAY INOPERATIVE. ACFT GROUNDED. REPLACED CABIN PRESSURE CONTROL MODULE IAW AMM 21-31-02. ALL GROUND VERIFICATION TESTS PASS.Aug 6, 2013 · N562AS · Boeing 737890 · Cabin Pressure Control SystemSDR ASAA2013080395736Skin · crackedEVIDENCE OF CRACKING ON LT STAB LOWER SKIN AT STA 129.50. CRACKING IN 2 SEPARATE AREAS. ACFT GROUNDED. INSTALLED DOUBLER IAW SRM 55-10-01-22-11. (REPAIR 11)Aug 3, 2013 · N562AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2013072695686Display · malfunctionedNEITHER MCDU MENU PAGES HAS A SAT OPTION. SATCOM IS INSTALLED, NO WAY TO ACCESS IT. ACFT GROUNDED. CYCLED SYS POWER AND SAT OPTION RETURNED ON MCDU, SYS CHECKED GOOD IAW AMM 23-15-00.Jul 26, 2013 · N562AS · Boeing 737890 · Central DisplaySDR ASAA2013072195653Connector · damagedNR 2 ENGINE, DP1101 CONNECTOR ON MW0311 HARNESS DAMAGED. ACFT GROUNDED. REPLACED HARNESS ON NR 2 ENG, REF MM 73-21-06-000-802-F00 AND 73-21-06-400-802-F00. OPS AND LEAK CHECKED NORMAL.Jul 21, 2013 · N562AS · Boeing 737890 · Engine Fuel System WiringSDR ASAA2013072195651Duct · damagedNR 2 ENGINE PNEUMATIC INTERSECT DUCT DAMAGED. ACFT GROUNDED. R & R NR 2 INTERSECTION MANIFOLD IAW P/P BUILDUP, FIG 16-1, PG 16 - 25. LEAK CHECKED GOOD.Jul 21, 2013 · N562AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2013072195565Actuator · leakingFUEL LEAK FROM NR 2 ENGINE, NOTED LEAKING FROM THE RT VSV ACTUATOR. ACFT GROUNDED. REMOVED NR 2 ENG RT VSV ACTUATOR REF MM 75-31-01-000-802-F00 AND INSTALLED SERVICEABLE VSV ACTUATOR REF MM 75-31-01-400-802-F00 COMPLETING STEPS F. 1-7 STARTED VSV ACTUATOR LEJul 21, 2013 · N562AS · Boeing 737890 · Compressor Bleed ControlSDR ASAA2013071995636Warning Light · false activationPRIOR TO TAXI, FMC DISAGREE MESSAGE ANNUNICATED. ACFT GROUNDED. QRH PROCEDURE COMPLIED WITH, OPS NORMAL.Jul 19, 2013 · N562AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013071095545Control Valve · malfunctionedPASSING FL 340, CLIMBING TO FL 350, THE AIR CONDITIONING WENT TO A HIGH FLOW VOLUME. ACFT PRESS IS NORMAL. TURNING OFF RECIRC FANS HAS NO EFFECT ON THE VOLUME. VERY NOTICABLE IN FLIGHT DECK AND FIRST CLASS LAV NOT AS NOTICABLE IN REAR OF ACFT. VOLUME RETURNJul 10, 2013 · N562AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2013053094945Control Unit · failedRT SIDE WINDOW HEAT WONT TURN ON. ACFT GROUNDED. CHANGED WHCU, APPLIED WET TOWEL TO SENSOR AREA, ON LIGHT CAME ON, OPS NORMAL, REF MM 30-41-11.May 30, 2013 · N562AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2013052294875Unknown · unknownSATCOM INSTALLED. SAT IS NOT SELECTABLE ON THE MCDV. ACFT GROUNDED. PERFORMED CYCLIING OF POWER TO SATCOM 10X AND PROMPT RETURNED WITHIN 50 SECONDS. NO FAULTS FOUND, REF MM 23-15-00.May 22, 2013 · N562AS · Boeing 737890 · Communications SystemSDR ASAA2013050594705Control Unit · faultedNR 1 ENG RECORDED FAULT CODE 73-11681 ADIRU PS AND THE ENG PO SIGNALS DISAGREE. SHORT TERM FAULT. FAULT ACTIVE ON 2 OF LAST 4 LEGS, FLT LEGS 2 & 3. ACFT GROUNDED. ACCOMPLISHED T/C 78273000, FOUND CURRENT FAULT MSG 73-11681 AND FAULT HIST PAGE LOGGED MSG 76May 5, 2013 · N562AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2013042794628Warning Light · false activationNR 1 ENG RECORDED FAULT CODE 73-10171 INTERNAL EEC FAULT LONG-TERM FAULT. FAULT ACTIVE ON FLT LEGS 2-6. NR 1 ENG RECORDED FAULT CODE 73-11681 ADIRU PS & ENG PO SIGNALS DISAGREE SHORT-TERM FAULT. FAULT ACTIVE ON FLT LEGS 1-7. ACFT GROUNDED. RAN EEC TEST IAWApr 27, 2013 · N562AS · Boeing 737890 · Engine Indicating SystemSDR ASAA2013042794626Warning Light · false activationON TAXI OUT THE FMC DISAGREE PROMPT WAS ILLUMINATED. ACFT GROUNDED. CHECK LIST ACCOMPLISHED. NO FURTHER WARNING NOTED.Apr 27, 2013 · N562AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013042294579Electrical Sys · malfunctionedDURING POWER TRANSFER FROM GPU TO APU, ELEC LIGHT CAME ON WITH SPCU 1 FAIL. CYCLED NORM SPCU AND STBY SPCU CIRCUIT BREAKERS THEN CLEARED FAULT IAW FIM 24-31 TASK 801, GROUND FUNCTIONAL CHECK GOOD IAW AMM 24-34-11-400-801 PARA G, NO HISTORY LAST 30 DAYS.Apr 22, 2013 · N562AS · Boeing 737890 · DC Generating SystemSDR ASAA2013041794543Satcom · malfunctionedAFTER GETTING INCOMING CALL ON SATCOM. SATCOM MENU ON MCDU WAS NO LONGER DISPLAYED. CALL LIGHT ON CENTER PEDESTAL FOR SATCOM IS CONTINUALLY ILLUMINATED. CHIME FOR HF SELCAL SEEMS TO BE INOP. LIGHT ILLUMINATES ON SELCAL PANEL, BUT NO CHIME. ACFT GROUNDED. Apr 17, 2013 · N562AS · Boeing 737890 · Communications SystemSDR ASAA2013041594495Fmc · false indicationFMC DISAGREE ON TAXI OUT. QRH PROC FOLLOWED. OPS NORMAL.Apr 15, 2013 · N562AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2013041294430Control Valve · failedIAW ACARS RECEIVED FROM FLT 480 INBD SAN AND ALSO CONVERSATION W/ PILOT AFTER LANDING, DUCT SPLIT INDICATED L 23 PSI R 42 PSI AT FL370. GAP NARROWED AS FLIGHT PROGRESSED TO L 28 PSI R 40 PSI. NO OTHER PROBLEMS NOTED. DUCT SPLIT WITHIN LIMITS. PRECAUTIONARILApr 12, 2013 · N562AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2013040694404Transceiver · inoperativeSATCOM MENU CHOICE IS NOT AVAILABLE ON FMC CDU. ACFT GROUNDED. REPLACED SDU. SATCOM COMMUNICATION SYS TEST MM23-15-00-730-801. OPS NORMAL. SATCOM NR 1 AND NR 2 BOTH SEND AND RECEIVE CLEAR COMMUNICATIONS WITH DISPATCH. ACCOMPLISHED SEVERAL POWER TRANSFERSApr 6, 2013 · N562AS · Boeing 737890 · Communications SystemSDR ASAA2013032994297Engine · faultedFOUND NR 1 ENGINE WITH LONG TERM FAULT 76-31361, START LEVER SIGNALS DISAGREE. PERFORMED EEC TEST IAW MM 73-21-00 AND TASKCARD 78273000 FMC CDU, FAULT APPEARS TO BE AN INTERMITTENT, 1 TIME FAULT SYS. OP CHECKED GOOD.Mar 29, 2013 · N562AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2013032694271None · noneNO SAT PROMPT ON MCDU. PERFORMED SATCOM TESTS REF M/M TASK 23-15-00-730-801. NO DEFECTS NOTED.Mar 26, 2013 · N562AS · Boeing 737890 · Communications SystemSDR ASAA2013031894195Starter · failedNR 2 ENGINE STARTER FAILED WHILE LEAK CHECKING CHIP DETECTORS. REPLACED NR 2 ENG STARTER REF MM 80-11-01, STARTER TEST IAW 71-00-00.Mar 18, 2013 · N562AS · Boeing 737890 · Engine CrankingSDR ASAA2013031294150Control Panel · inoperativeCPTS COURSE SELECTOR KNOB INOPERATIVE. FFR SHOW NO FAULT. UNABLE TO DUPLICATE DUE TO HISTORY R & R MCP. INSTALLATION TEST GOOD REF MM 22-11-34. BITE TEST GROUP 49 32 AND 58 GOOD. REF MM 22-11-00.Mar 12, 2013 · N562AS · Boeing 737890 · Autopilot SystemSDR ASAA2013031194146Autopilot Sys · malfunctionedCAPTAIN SIDE MCP COURSE SELECTOR KNOB TURNS, BUT WILL NOT ALLOW NEW COURSE SELECTION. UNABLE TO DUPLICATE, RAN COURSE SELECTOR 360 DEGREES BOTH CW AND CCW SEVERAL TIMES. NO HISTORY LAST 30 DAYS. PERFORMED INSTALLATION TEST REF MM 22-11-34-740-801, DFGS BITEMar 11, 2013 · N562AS · Boeing 737890 · Autopilot SystemSDR ASAA2013022493987Satcom · malfunctionedNO SATCOM PROMPT ON MCDU. PULLED & RESET CIRCUIT BREAKER SATCOM. OPS GOOD IAW 23-15-00-730-801.Feb 24, 2013 · N562AS · Boeing 737890 · Communications SystemSDR ASAA2013021893938Satcom · malfunctionedSATCOM INOPERATIVE. NO SAT OPTION APPEARS ON FMC MENU PAGE. RESET POWER TO SATCOM BY PULLING & RESETTING SATCOM CIRCUIT BREAKER ON P18-2 PANEL. SAT OPTION RE-APPEARED ON FMC MENU AND SUCCESSFULLY CONTACTED DISPATCH ON BOTH SATCOM-1 & SATCOM-2, OPS NORMAL REFeb 18, 2013 · N562AS · Boeing 737890 · Communications SystemSDR ASAA2013012393726Warning Light · false activationCONT CAB ZONE TEMP ILLUMINATED ON RECALL AFTER ENG START ACCOMPLISHED GROUND CHECKLIST. AFTER SELECTING COOLER TEMP AND PUSHING TRIP RESET ZONE TEMP LIGHT STAYED ILLUMINATED. PERFORMED PACK/ZONE TEMP CONTROLLER BITE IAW FIM 21-62. NO DEFECTS NOTED.Jan 23, 2013 · N562AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2013011793688Fastener · looseNR 1 ENGINE FAN DUCT PANEL FASTENER FOUND LOOSE AND RETORQUED SCREWS ON ALL PANELS IAW AMM 72-23-07.Jan 17, 2013 · N562AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2013010793714Skin · gougedEXTERNAL FUSELAGE SKIN GOUGED FWD OF PILOTS WINDSHIELD. BS 196REPAIRED AREA IAW ASA EA 800-53EA-09649, REV A DATED 23 JAN 2013 AND REO G15858 REV B.Jan 7, 2013 · N562AS · Boeing 737890 · Fuselage Main, Plate/SkinSDR ASAA2013010793693Seat Track · gougedMAIN CABIN SEAT TRACK AT RBL 25 , BS 520 GOUGED. GOUGE FOUND TO BE OUT OF SRM 53-00-52 LIMITS. CUT & REMOVED DAMAGED SECTION OF SEAT TRACK, FABRICATED & INSTALLED NEW SECTION OF SEAT TRACK & SPLICE IAW SRM 53-00-52-2R-4 REPAIR 4 & EA 800-53EA-09615, REV NEW Jan 7, 2013 · N562AS · Boeing 737890 · Fuselage, Seat/Cargo Attach FittingsSDR ASAA2012122793568Control Valve · faultedRIGHT PACK LIGHT ILLUMINATED ON RECALL. PERFORMED RT TEMP CONTROLLER BITE ND FOUND THIS PACK TCV LOGGED. RESET FAULT, REF 21-61, TASK 801. GROUND RAN RT PACK REF 21-00-00 FOR HALF HOUR. PERFORMED RT PACK BITE AFTER GROUND OPS CHECK OF RT PACK. NO FAULTS LODec 27, 2012 · N562AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2012122593541Transceiver · unknownPWS FAIL AND WEATHER RADAR FAIL, FLAGS DISPLAYED ON DISPLAY. FAULT CODE 34401000. FOUND CIRCUIT BREAKER D13 OUT ON P6-1. VISUALLY INSPECTED ACCESSIBLE WIRING BEHIND P6-1. NO DEFECTS NOTED. RESET CIRCUIT BREAKER IAW MM 20-60-01-860-801. PRECAUTIONARY R & RDec 25, 2012 · N562AS · Boeing 737890 · Weather Radar SystemSDR ASAA2012120693418Compensator · failedNR 2 FUEL TANK QUANTITY DROPPED TO 8300 LBS FROM 8700 LBS SHORTLY AFTER FUELING WAS COMPLETED ON THE RAMP. AFTER APPROX 1.5 HOURS OF FLYING THE NR 2 TANK INDICATED 8700 LBS, THE SAME AS NR 1 TANK. LATER, NR 2 TANK AGAIN INDICATED 8300 LBS. 400LB DIFFERENCE Dec 6, 2012 · N562AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2012110493242Transceiver · failedNR 1 HF RADIO IS VERY GARBLED ON THE RECEIVING SIDE IT APPEARS TO TRANSMIT OK AND SEL CALL WORKS OK. R & R NR 1 HF TRANSCEIVER IAW AMM 23-11-21-000-801. OPS CHECKED.Nov 4, 2012 · N562AS · Boeing 737890 · HF Communications SystemSDR ASAA2012101393111Panel · looseNR 1 ENG INLET AND FAN BLADES -DETAILED INSPECTION FOUND 1 FAN STRUT DUCT PANEL THAT HAS TWO FASTENERS LOOSE WITH POSSIBLE DAMAGE TO PANEL. R & R 1 FAN STRUT DUCT PANEL REF AMM 72-23-07.Oct 13, 2012 · N562AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2012090292804Filter · trippedDURING PDC FOUND RT ENGINE DPI INDICATOR POPPED. ACFT GROUNDED. ACCOMPLISHED IDG SCAVENGE AND CHARGE FILTER INSPECT. CK IAW AMM TASK 24-11-41-200-801. NO FAULTS FOUND. RAN ENGINE AND LEAK CHECKED . OPS CK GOOD. NO LEAKS FOUND.Sep 2, 2012 · N562AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2012080692674Transceiver · inoperativeHF 2 WILL RECEIVE BUT NOT TRANSMIT. ACFT GROUNDED. VERIFIED FAULT. R & R NR 2 HF COUPLER IAW AMM 23-11-61. R & R NR 2 HF TRANSCEIVER IAW AMM 23-11-21. NR 2 HF OPS NORMAL IAW SAME REF.Aug 6, 2012 · N562AS · Boeing 737890 · HF Communications SystemSDR ASAA2012080492654Hf Comm · malfunctionedHF NR 2 WOULD NOT TRANSMIT AT N1. PERFORMED FIM 23-11, TASK 806 HF RECEIVE/TRANSMIT PROBLEM. ALL CHECKS PASSED & PERFORMED HF BITE PROCEEDURE IAW FIM 23-11, TASK 801 ALL LRU TESTS PASSED. NO HISTORY LAST 30 DAYS.Aug 4, 2012 · N562AS · Boeing 737890 · HF Communications SystemSDR ASAA2012083092812Eec · faultedWHILE PERFORMING TC 78273000 INTERROGATE THE FMC CDU FOR FAULTS FOUND MAINT MSGS 73-10011 AND 73-20131. ACFT GROUNDED. REPLACED NR 1 ENG EEC REF. AMM 73-21-60-000-801-F00 FADEC SYS TEST C/W TASK 73-21-00-700-802-F00 A-E.Aug 3, 2012 · N562AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2012082892787Fire Detector · inoperativeAPU DETECTOR INOPERATIVE B ILLUMINATED. APU FIRE SWITCH DOES NOT ILLUMINATE DURING OVERHEAT/FIRE TEST. ACFT GROUNDED. R & R APU TAILPIPE FIRE DETECTOR IAW AMM REF 26-15-01-000-802/26-15-01-400-802. RESET C/BS, APU FIRE DETECTOR OPS CKS GOOD.Aug 2, 2012 · N562AS · Boeing 737890 · Fire DetectionSDR ASAA2012081792740Warning Light · false activationWHILE PERFORMING T/C 78273000 FOUND FAULT 76-31361 ENG NR 1. INITIAL EVALUATION OF FMC CDU SHOWED NO FAULTS EITHER IN CURRENT FAULTS OR STORED FAULT HISTORY. ACCOMPLISHED FIM 76-11-00-810-801-F00 WITH NO DISCREPANCIES NOTED. ACCOMPLISHED EEC BITE AND EEC TEAug 1, 2012 · N562AS · Boeing 737890 · Central WarningSDR ASAA2012081992749Autoland Sys · malfunctionedPERFORMED AUTOLAND. AUTOLAND UNSATISFACTORY AUTOPILOT FLARED LATE AND AGGRESSIVE BUT NOT ENOUGH. TOUCHDOWN WAS VERY FIRM AND APPROX 15 FT LEFT OF CENTERLINE. ACCOMPLISHED FLIGHT FAULT REVIEW FOR BOTH FCC A & B. NO FAULTS NOTED. ACCOMPLISHED FIM TASK 22-1Aug 1, 2012 · N562AS · Boeing 737890 · Autopilot SystemSDR ASAA2012081592725Warning Light · false activationWHILE ON TAXI OUT, PDX FMC DISAGREE MASTER CAUTION ANNUNCIATED. ACFT GROUNDED. RAN QRH FOR ON GROUND ISSUE AND ISSUE WAS RESOLVED.Aug 1, 2012 · N562AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2012072792634Unknown · unknownDURING PERFORMANCE OF TASK CARD 78273000. NR 1 ENGINE SHOWED A SHORT TERM FAULT, (50 FLIGHT HOURS) FAULT CODE 73-10011, INTERNAL EEC FAULT. PERFORMED EEC BITE IAW MM 73-21-00-700-804F00, NO FAULTS FOUND. PERFORMED RECENT FAULT TEST IAW 73-21-00-740-803F00 AJul 2, 2012 · N562AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2012072392595Filter · cloggedDPI FOR NR 1 IDG POPPED. REPLACED NR 1 IDG CHARGE & SCAVENGE FILTERS & OIL. NO DEFECTS NOTED. RESET DPI. REF MM 24-11-41-00-801, 24-11-41-200-801 & 24-11-41-400-801.Jul 2, 2012 · N562AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA12511671Warning Light · illuminatedFMC DISAGREE MESSAGE DISPLAYED DURING TAXI. ACCOMPLISHED QRH PROCEDURE. DISAGREE MESSAGE WAS NO LONGER DISPLAYED.Jun 7, 2012 · N562AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2012061692364Eec · faultedWHILE PERFORMING TASKCARD 78273000 FMC, CDU, ENGINE FAULTS FOUND FAULT CODE 73-10011 AND 73-20131 ON THE NR 1 AND NR 2 ENGINE INTERNAL EEC FAULT, SHORT TERM FAULT. ACFT GROUNDED. PERFORMED FIM 73-21, TASK 801, EEC TEST PASSED FOR NR 1 AND NR 2 ENGINES. NO FJun 1, 2012 · N562AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2012061792353Control Valve · failedLEFT PACK LIGHT ILLUMINATES DURING MASTER CAUTION RECALL. LIGHT EXTINGUISHES WHEN MASTER CAUTION SYSTEM IS RESET. ACFT GROUNDED. R & R LEFT TEMPERATURE CONTROL VALVE IAW AMM 21-51-10-000-801 AND 21-51-10-400-801. OPS CHECK GOOD IAW AMM 21-51-00-400-801 PARJun 1, 2012 · N562AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA12511532Fmc · warning lightFMC DISAGREE ON GROUND. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURE. OPS NORMAL.May 9, 2012 · N562AS · Boeing 737890 · Flight Management Computing Hardware System
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