N596AS

Service difficulty reports · 549

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 = 'N596AS' 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 ASAA2013053194946Lens · brokenL1 FLOOR EMERGENCY LIGHTS BROKEN. ACFT GROUNDED. REPLACED LIGHT COVER & RE-INSTALLED BULB. OPS CK GOOD IAW MM 33-20-00-710.May 31, 2013 · N596AS · Boeing 737890 · Emergency LightingSDR ASAA2013052794913Satcom · malfunctionedSATCOM NOT DISPLAYED ON MCDU MENU PAGE. ACFT GROUNDED. PERFORMED OPS CHECKED SATCOM SYS REF 23-15-00-730-801. VERIFIED SAT PROMPT.May 27, 2013 · N596AS · Boeing 737890 · Communications SystemSDR ASAA2013052294876Unknown · unknownSAT NOT DISPLAYED ON THE MCDU MENU PAGE. ACFT GROUNDED. UNABLE TO DUPLICATE. RAN APU POWER AND GATE POWER. SWITCHING BACK TO APU AND GROUND NO FAULT. SATCOM TEST GOOD REF AMM 23-15-00.May 22, 2013 · N596AS · Boeing 737890 · Communications SystemSDR ASAA2013050894738Pump · leakingHYD LEAK AT NR 2 ENG. ACFT GROUNDED. RAN NR 2 ENG FOUND FUEL DRIPPING FROM FUEL PUMP PAD DRAIN AT 48 DROPS PER MINUTE, BELOW THRESHOLD LIMIT REF AMM 71-71-00-200-801-F00. REPLACED MAIN ENGINE FUEL PUMP IAW AMM 73-11-01. LEAK AND OPS TESTS GOOD.May 8, 2013 · N596AS · Boeing 737890 · Hydraulic Pump (Electric/Engine), MainSDR ASAA2013042594693Floor Panel · damagedAFT CARGO FLOOR PANEL 140AF HAS ELONGATED HOLES. ACFT GROUNDED. FABRICATED FLOOR PANEL 140AF IAW DWG 453A2610-38, REV B.Apr 25, 2013 · N596AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2013042494695Floor Support · crackedAFT CARGO UNDER FLOOR, FLOOR SUPPORT VERTICAL ANGLE AT BSTA 727G, RBL 13.5, CRACKED. ACFT GROUNDED. REMOVED AND INSTALLED FLOOR SUPPORT VERTICLE ANGLE AT STA 727G, RBL 13.5 IAW SRM 51-40-02 AND DWG 146A1310. FABRICATED NEW ANGLE IAW DWG 146A1310. PRIMED AApr 24, 2013 · N596AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2013042494694Transition Panel · damagedAFT CARGO COMPARTMENT LT TRANSITION PANEL HAS ELONGATED HOLE. ACFT GROUNDED. REMOVED DAMAGED AREA IAW SRM 53-00-53-2R-5, REPAIR 5. MATERIAL ID IS BAC 1496-377-7075-T62 AND SPLICE MATERIAL ID IS BAC 1496-377-7075-T62 IAW SRM 53-00-53-2R-5, REPAIR 5. FABRICAApr 24, 2013 · N596AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2013042494646Transition Panel · crackedAFT CARGO TRANSITION PANEL AT BS 727I TO 727J, RBL 19, CRACKED. R & R TRANSITION PANEL IAW SRM 53-00-53-2R-5, REPAIR 5.Apr 24, 2013 · N596AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2013042494645Floor Support · corrodedFWD CARGO AFT FLOOR SUPPORT CORRODED ENTIRE LENGTH. R & R FLOOR SUPPORT.Apr 24, 2013 · N596AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2013042494644Floor Support · damagedAFT CARGO UNDER FLOOR SUPPORT ANGLE HAS ELONGATED BOLT HOLE, RBL 13.5, BETWEEN BS 727B AND 727C. REPAIRED AFT CARGO FLOOR SUPPORT.Apr 24, 2013 · N596AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2013042394643Floor Panel · corrodedFWD CARGO FLOOR PANEL 120DF IS CORRODED ON EDGES. FABRICATED NEW FLOOR PANELApr 23, 2013 · N596AS · Boeing 737890 · Fuselage Floor PanelSDR ASAA2013041594493Warning Light · false activationAMBER LIGHT ILLUMINATED ON OVERHEAD PANEL. OVERHEAD AC/DC ELECTRICAL PANEL LOGGED AUX BATTERY CHARGER AND SPCU FAULT. STANDBY POWER SYSTEM BITE TESTED IAW MM 24-31, TASK 801 AND ALL FAULTS CLEARED. LIGHT EXTINGUISHED AND NO CURRENT FAULT. ALL DC SYS GROUNDApr 15, 2013 · N596AS · Boeing 737890 · Central WarningSDR ASAA2013032294234Battery Pack · failedAFT GALLEY LT EMERGENCY LIGHTS FAILED TIME CHECK. R & R BATTERY PACK M1673 IAW AMM TASK 33-51-06-960-805 AND WDM 33-51-14. BATTERY PACK TEST PASSED.Mar 22, 2013 · N596AS · Boeing 737890 · Emergency LightingSDR ASAA2013022894044Probe · out of toleranceWHILE PERFORMING T/C 78273000, FOUND FAULT CODE 77-10851 THE BOTTOM RT EGT SIGNAL IS OUT OF RANGE T495 S2 FOR ENG NR 1. ACFT GROUNDED. REMOVED NR 1 ENGINE LOWER LT AND RT T49.5 PROBES IAW MM 77-21-01-000-801-F00. INSTALLED RT LOWER T49.5 PROBE IAW MM 77-21-Feb 28, 2013 · N596AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2013022894042Shim · wornFOUND COATING WORN ON FAN BLADE SHIMS FOR NR 1 ENGINE. R & R FAN BLADE SHIMS IAW T/C 78472002.Feb 28, 2013 · N596AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2013011993706Autoland Sys · malfunctionedAUTOLAND FAILED, TOUCHDOWN WAS GREATER THAN 35 LT OF CENTERLINE, BUT IN THE TOUCHDOWN ZONE OF THE RUNWAY. NO FAULT LOGGED IN DFCS FFR, CURRENT STATUS PASSED. PERFORMED LAND VERIFY TEST REF FIM 22-11 TASK 825. ACFT REMAINS CAT IIIA AUTOLAND & HGS QUALIFIED, SJan 19, 2013 · N596AS · Boeing 737890 · Autopilot SystemSDR ASAA2013011293674Cover · dislodgedFORWARD ENTRY EMERGENCY LIGHT COVER FELL OFF. REPLACED LIGHT COVER AND LIGHT ASSY.Jan 12, 2013 · N596AS · Boeing 737890 · Emergency LightingSDR ASAA2013011093667Eec · faultedWHILE ACCOMPLISHING T/C 78273000 - FMC CDU ENG FAULTS NR 1 ENG LOGGED FAULT CODE 73-31611 - ADIRU2 DATA FROM DEU IS MISSING. ACFT GROUNDED. REMOVED NR 1 ENG EEC REF AMM 73-21-60-000-801-F00. INSTALLED SERVICEABLE EEC, REF MM 73-21-60-400-801-F00 STEPS 3.E.(Jan 10, 2013 · N596AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2013010593630Indication Sys · noneWHILE ACCOMPLISHING T/C 78273000, FOUND FAULT MSG 77-10851. BOTTOM RT EGT SIGNAL IS OUT OF RANGE. PERFORMED TC 78273000 AGAIN, NO FAULTS.Jan 5, 2013 · N596AS · Boeing 737890 · Engine EGT/TIT Indicating SystemSDR ASAA2012112693375Fmc · unknownLEFT FMC FAILURE IN FLIGHT. PERFORMED FIM 34-61 TASK 807 FMC HARDWARE /SOFTWARE FAULTS, NO FAULT FOUND.Nov 26, 2012 · N596AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2012112693373Lens · unsecureEMERGENCY LIGHT COVER CAME OFF L1 DOOR BULKHEAD. INSPECTED EMERGENCY LIGHT COVER, SECURED AND PERFORMED OPS CHECK AS REQUIRED, NO DEFECTS NOTED.Nov 26, 2012 · N596AS · Boeing 737890 · Emergency LightingSDR ASAA2012110793265Wire Harness · damagedNR 1 ENGINE J9 AND J10 HARNESSES HAS PERSISTENT EGT INDICATION SYS ERRORS. R & R UPPER LT & UPPER RT T49.5 PROBES REF MM 77-21-01-400-801-F00. R & R CJ9 HARNESS REF MM 73-21-06-400-802-F00. PERFORMED FADEC SYS TEST REF MM 73-21-00-700-802-F00. PERFORMED EEC Nov 7, 2012 · N596AS · Boeing 737890 · Engine Indicating System WiringSDR ASAA2012110393229Control Panel · failedMODE SELECT SWITCHES (RT/ F/O SIDE ) WILL NOT STAY DOWN, ON RADAR CONTROL PANEL. REMOVED, REPLACED AND TESTED WEATHER RADAR CONTROL PANEL IAW MM 34-43-91-000-801/ MM 34-43-91-400-801. ALL TESTS PASS.Nov 3, 2012 · N596AS · Boeing 737890 · Weather Radar SystemSDR ASAA2012102693188Control Valve · malfunctionedAFTER ENGINE START, ACCOMPLISHED THE AFTER START CHECKLIST, RECEIVED AN AIR CONDITIONING ON RECALL TEST. OBSERVED PACK LIGHT ON RT ENG. ACCOMPLISHED QRH 2.7. LTS WENT OUT WHEN MASTER CAUTION RESET. ON SUBSEQUENT FLIGHT, RIGHT PACK LIGHT ILLUMINATED AND WOULOct 26, 2012 · N596AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2012102393187Eec · malfunctionedNR 1 ENGINE TREND DATA CONTINUES TO SHOW A SHIFT IN DELTA CRUISE AND TAKEOFF MARGIN INDICATIVE OF EGT INDICATION ERRORS. PREVIOUS MAINT, EGT CONNECTOR CLEAN AND HARNESS REPLACEMENT. REMOVED NR 1 ENGINE EEC IAW AMM 73-21-60-000-801-F00. INSTALLED EEC ON NR 1 Oct 23, 2012 · N596AS · Boeing 737890 · Fuel Controlling SystemSDR ASAA2012101493113Indicator · activatedWHILE ACCOMPLISHING ETOPS PDC, FOUND NR 2 ENG IDG DELTA P INDICATOR EXTENDED. ACFT GROUNDED. ACCOMPLISHED IDG SCAVENGE AND CHARGE FILTER INSP NO DEFECTS NOTED WITH FILTERS OR OIL. NEW FILTERS INSTALLED AND SERVICED IDG. DPI RESET DECAL MARKED. REF AMM 24-11Oct 14, 2012 · N596AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2012101093105Indicator · erraticAIR TEMP NEEDLE SHOWING ERRATIC INDICATIONS WITH SWITCH IN ALL DIFFERENT POSITIONS. REPLACED P5-17 TEMP. CONTROL MODULE AND CABIN TEMP CONTROL INDICATOR. REF TASK 21-61-15-400-801 AND TASK 21-61-32-400-801. TEMP CONTROL INDICATION OPS NORMAL, REF TASK 21-61-Oct 10, 2012 · N596AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2012090892860Switch · faultyWHILE ACCOMPLISHING T/C 78273000 ENG 1 LOGGED SHORT TIME FAULT 73-30311 THE START SWITCH SIGNAL AND BUS DATA DISAGREE FOR LEG 2. ACFT GROUNDED. PERFORMED FIM TASK 73-24-00-810-813 VERIFIED NR 1 ENG START SWITCH WAS FAULTY. REMOVED NR 1 ENG START SWITCH REF 8Sep 8, 2012 · N596AS · Boeing 737890 · Engine CrankingSDR ASAA2012090392817Autothrottle Sys · malfunctionedAUTO THROTTLES WILL NOT ENGAGE. ACFT GROUNDED. PERFORMED A/T INFLT FAULTS - SHOWS A ASM2 RATE MONITOR FAULT. PERFORMED FIM 22-31 TASK 805. A/T BITE PROCEDURES CURRENT STATUS AND A/T SERVO TEST GOOD NUMEROUS TIMES. IAW FIM, INTERMITTENT FAULT. NO HISTORY LSep 3, 2012 · N596AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2012092992973Display · malfunctionedIN CRUISE, LEFT CDU WENT BLANK, AFTER APROX 30 SECONDS CDU RECOVERED TO NORMAL. NO FURTHER PROBLEMS. ACCOMPLISHED FMC, CDU REPAIR CONFIRMATION FIM TASK 34-61-00-810-804, NORMAL DISPLAY RESTORED.Sep 2, 2012 · N596AS · Boeing 737890 · Central DisplaySDR ASAA2012092792953Wire Harness · damagedNR 1 ENGINE TREND DATA CONTINUES TO SHOW ERRORS INDICATIVE OF EGT INDICATION SYS ANOMALIES. FOUND AT PINS 3 & 4 A RESISTANCE READING OF 7 OHMS ONE WAY, LEADS SWAPPED, OPEN READING OTHER WAY. READ OUT S1 AND S4 PROBES REF. SAME MM, WITH IN TOL. REF. MM 73-21-0Sep 1, 2012 · N596AS · Boeing 737890 · Engine Indicating System WiringSDR ASAA2012091992914Keyboard · inoperativeF/O FMC 4R LINE SELECT BUTTON INOPERATIVE, R & R F/OS FMCS CDU KEYBOARD. CDU KEYBOARD TEST GOOD. CDU LAMP TEST GOOD. REF AMM 34-61-01-400-801.Sep 1, 2012 · N596AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2012083092811Probe · out of limitsNR 1 ENGINE TREND DATA IS SHOWING A SHIFT IN DELTA EGT INDICATIVE OF EGT INDICATION SYS ANOMALIES. ALL OTHER PARAMETERS ARE NORMAL. ACFT GROUNDED. ACCOMPLISHED STEPS 1-3, FOUND S4 PROBE RESISTANCE OUT OF LIMITS AND FOUND CORE ENG HARNESS TO THE S1 PROBE RESAug 3, 2012 · N596AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2012072392596Heat Exchanger · leakingNR 2 ENGINE FUEL LEAK AT DRAIN LINE FOR FUEL/ OIL HEAT EXCHANGER 10 DROPS IAW MINUTE. REMOVED NR 2 ENGINE OIL/ FUEL HEAT EXCHANGER. INSTALLED SERVICEABLE OIL/ FUEL HEAT EXCHANGER REF MM 79-21-02-400-801. STEPS A THRU H (1). COMPLETED INSTALLATION AND LEAK CJul 2, 2012 · N596AS · Boeing 737890 · Engine Oil Distribution (Airframe Furnished)SDR ASAA2012070292463Actuator · leakingRAMP REPORTS LIQUID STREAMING OUT OF NR 2 ENGINE. REMOVED NR 2 ENGINE RT VSV IAW MM 75-31-01-000-802-F00. INSTALLED RT VSV ACTUATOR IAW AMM TASK 75-31-01-400-802. INSTALLED NR 2 ENGINE RT THRUST MOUNT IAW AMM 73-23-04-000-801-F00. ATTACHED RT THRUST LINK TOJul 2, 2012 · N596AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2012071692557Battery · failedAPU WILL NOT START. INTEREGATED CDU FAULT CODE 49-41248. STARTER CONVERTER UNIT SHOWS SYS INOPERATIVE. DURING BATTERY START WITH NO EXTERNAL POWER APPLIED, BATTERY STARTING VOLTAGE 25 VDC THEN DROPS TO A MINIMUM OF 19VDC WITH A MAX CURRENT DRAW OF -210 AMPSJul 1, 2012 · N596AS · Boeing 737890 · Battery/Charger SystemSDR ASAA2012070192454Panel · damagedNR 2 ENGINE, BLEED DUCT LOUVER PANEL AT 9 O`CLOCK POS (AFT LOOKING FWD) HAS DAMAGE DUE TO LOOSE FASTENER. ACFT GROUNDED. INSTALLED NEW BLEED DUCT LOUVER PANEL NR 2 ENGINE. REF AMM 72-23-07.Jul 1, 2012 · N596AS · Boeing 737890 · Engine Bleed Air SystemSDR ASAA2012062792437Fcu · malfunctionedSTARTED APU AFTER LANDING AND ESTABLISHED APU GENERATOR ON LINE. AFTER ARRIVING AT GATE THE APU BLEED VALVE WOULD NOT OPEN. GROUND POWER WAS HOOKED UP AND PUT ON ACFT. SWITCHED BACK TO APU GENERATOR AND IT WOULD NOT STAY ON LINE. ACFT GROUNDED. PERFORMED Jun 2, 2012 · N596AS · Boeing 737890 · APU Engine Fuel and ControlSDR ASAA12511589Fmc · warning messageFMC DISAGREE MESSAGE ON TAXI OUT. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURE. OPS NORMAL.May 26, 2012 · N596AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA12511564Warning Light · false activationCONTROL CABIN "ZONE TEMP" AMBER LIGHT CAME ON DURING RECALL CHECK. LIGHT EXTINGUISHED ON RESET. ACFT GROUNDED. ACCOMPLISHED FIM 21-62T801, RT PACK ZONE TEMP CONTROLLER SHOWS "FLT DECK TRIM VALVE" FAULT. ACCOMPLISHED FIM 21-62T832 FAULT RESET.May 16, 2012 · N596AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA12511542Fmc · faultedAFTER PASSING 00HIL INTERSECTION, NR 1 CDU WENT BLANK, EXEC LIGHT ILLUMINATED, THIS LASTED FOR APPROX 10 SECS THEN SCREEN CAME BACK WITH SOME TEST DATA AND "BIT PASSED" ANNUNCIATION. ACFT GROUNDED. LT & RT FMC'S FFR FOR PREV FLT (1) SHOW "SCU LEFT B" FAULTS May 11, 2012 · N596AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA12511495Nozzle · failedAPU CT5ATP EGT TREND DATA SHOWS EGT HAS SHIFTED ABOVE THE ESTABLISHED THRESHOLD. ACFT GROUNDED. REMOVED ALL FUEL NOZZLES IAW MM 49-31-14, STEPS A, E. INSTALLED FUEL NOZZLES IAW MM 49-31-14, STEPS A, F. ACCOMPLISHED STEPS G AND H MM 49-31-14-400, LEAK CK GOOMay 4, 2012 · N596AS · Boeing 737890 · APU Engine Fuel and ControlSDR ASAA20120329297Switch · inoperativeAUTOTHROTTLE ARM SWITCH WILL NOT ENGAGE. PERFORMED AUTO THROTTLE BITE 22-31-00 REQS ASM 1 REPLACEMENT. REPLACED NR 1 ASM PER AMM TASK 22 31 91 020 801/ 22 31 91 400 801. OP'S CHECKED GOOD.Mar 23, 2012 · N596AS · Boeing 737890 · Auto Throttle SystemSDR ASAA12511144Warning System · false activationPACK LT ILLUMINATES WITH MASTER RECALL RESETS W/ MASTER CAUTION RESET. ACCOMPLISHED MASTER CAUTION TEST AND BITE CHECK OF CABIN PRESSURE CONT. ALL CHECK GOOD. RESET FAULTS AND ALL OPS NML. GROUND VERIFICATION SATISFACTORY.Feb 23, 2012 · N596AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA12511137Acm · malfunctionedAT THE GATE THE RIGHT PACK LIGHT ILLUMINATED AFTER THE PACK WAS RUNNING FOR APPROX 2 MIN. THE RIGHT PACK TEMP SHOWED 90 DEGREES. REPLACED RT ACM REF AMM 21 51 04 OPS & LEAK CK'D GOOD. PERFORMED RT PACK INITIAL EVALUATION CHECK REF AMM 21 53 00 810 812 STEPFeb 21, 2012 · N596AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA12511133Switch · defectiveON GRD AFTER TURNING ON BOTH PACKS FOR 2 MINS. THE RT PACK LIGHT CAME ON INDICATING A PACK TEMP OF 90 DEG NR 1 & NR 2 TEMP CONTROLERS SHOW NO FAULTS. BITE NORMAL REF MM 21 61 0. ACCOMP FIM 21 53 00 810 804 & 21 53 00 810 812. NO FAULTS. REPLACED R PACK DIFeb 21, 2012 · N596AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA12511075Sensor · defectiveDURING TAXI OUT THE APU WAS SHUT DOWN. SHORTLY AFTER THE APU FAULT LIGHT ILLUMINATED. THE LIGHT WENT OUT ABOUT 9 MINUTES LATER. VERIFIED FAULT FROM CDU ON FLT LEGS 0 1 & 2. REPLACED INLET TEMP SENSOR REF MM 49 61 31 NO FAULT FOUND ON CDU AFTER REPLACEMENT Feb 8, 2012 · N596AS · Boeing 737890 · APU Indicating SystemSDR ASAA12511034Bushing · seizedON PUSHBACK RIGHT PACK LIGHT CAME ON RIGHT PACK TEMP INDICATES 90 DEGREES C. FOUND RIGHT RAM AIR DEFLECTOR DOOR NOT MOVING AT ALL. CHECKED RAM AIR ACTUATOR MOVES OPENS AND CLOSES RAM AIR INLET. FOUND BOTH RT UPPER AND LOWER RAM AIR DOOR DEFLECTOR SUPPORT BUFeb 4, 2012 · N596AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA12511033Warning System · false activationRIGHT PACK LIGHT CAME ON CHECKLIST ITEMS WERE DONE. DID NOT CORRECT PROBLEM. PERFORMED #2 TC BITE REF 21 62 00. RESET SYSTEM. OPS CKD SYS NO FAULTS FOUND 21 00 01.Feb 2, 2012 · N596AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA1250991Unknown · malfunctionedAFTER STARTING APU & PLACING PACK SWITCHES TO AUTO AMBER "PACK" LIGHT ILLUMINATED ON RIGHT PACK. EXECUTED "PACK (800/900)" CHECKLIST PACK LIGHT EXTINGUISHED. PACK LIGHT DOES NOT ILLUMINATED ON RECALL. BITE CHECKED NR 2 CABIN TEMP CONTROLLER REF MM 21 61 00. Jan 24, 2012 · N596AS · Boeing 737890 · Cabin Cooling System
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