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 ASAA2017072321454Wire Harness · chafedNR 1 ENGINE WIRE HARNESS MW0311 IS CHAFED THRU INTERIOR LOOM NEAR 12 O'CLOCK POSITION. ACFT GROUNDED. REPLACED THE WIRE HARNESS IAW MM 73-21-06-000-802-F00, AND 400-802-F00. OPS CHECKED IAW MM 73-21-06-400-802-F00. TWO CIRCUIT BREAKERS OPENED AND CLOSED. SJul 23, 2017 · N596AS · Boeing 737890 · Engine Fuel System WiringSDR ASAA2017072321453Bearing · wornNR 1 ENGINE SUPPORT ROD BELOW PRSOV BEARING IS WORN. ACFT GROUNDED. FOUND BEARING TO BE BAD IN DUCT AND SUPPORT ROD. REPLACED BOTH THE DUCT & SUPPORT ROD IAW 71-00-02, FIGURE 16-1. LEAK CHECKED GOOD.Jul 23, 2017 · N596AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2017070121232Control Panel · failedPRESSURE CONTROLLER DISPLAY FROZE. ACFT GROUNDED. REPLACED CABIN PRESSURE CONTROL SELECTOR PANEL. IAW MM 21-31-02-400-801. OPS CHECKED GOOD.Jul 1, 2017 · N596AS · Boeing 737890 · Cabin Pressure Control SystemSDR ASAA2017063021236Warning Light · false activationCONTROL CABIN ZONE TEMP LIGHT ILLUMINATED ON RECALL. ACFT GROUNDED. INITIAL INSPECTION FOUND THE NR 2 TEMP CONTROLLER SHOWING FLT DECK TRIM VALVE FAULTED. PERFORMED AMM 21-51-00-700-803, PACK/ZONE TEMPERATURE CONTROLLER BITE TEST. PASSED. RESET FAULT AND Jun 30, 2017 · N596AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2017062621211Fuel Control · failedPERFORMED CSS ON APU BY DISPATCH RELEASE DIRECTION AND PER FOM 5.1 PAGE 4. FIRST ATTEMPT PRIOR TO TOD AT FL380: NORMAL SEQUENCE UNTIL EGT REACHED 800 DEGREES FOLLOWED BY 'FAULT' LIGHT, WHICH EXTINGUISHED WHEN APU SWITCH WAS MOVED TO 'OFF'. SECOND ATTEMPT ALSO Jun 26, 2017 · N596AS · Boeing 737890 · APU Engine Fuel and ControlSDR ASAA2017062421178Igniter · inoperativeAPU WONT START, TRIED 3 TIMES. ACFT GROUNDED. PERFORMED APU BITE IAW FIM 49-60, TASK 801. APU HAS FAULT MSG 49-41011 NO FLAME SHUTDOWN. COMPLIED WITH FIM TASK 49-40 TASK 802, CDS REPORTS NO FLAME LAST THREE STARTS AS RECOMMENDED BY FIM TASK. REMOVED AND REPLAJun 24, 2017 · N596AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA2017061621118Warning Light · false activationWHILE PERFORMING T/C 7827300, FOUND FAULT 77-108582, THE BOTTOM RIGHT EGT SIGNAL IS OUT OF RANGE. ECONOMIC FAULT. ACFT GROUNDED. NR 2 ENGINE BITE SHOWS NO CURRENT FAULTS, NO FAULTS IN HISTORY. TEMPS OUT OF RANGE. WIRING HARNESS RESISTANCE WITHIN LIMITS. CJun 16, 2017 · N596AS · Boeing 737890 · Engine Temperature Indicating SystemSDR ASAA2017060820987Blade · damagedNR 1 ENGINE FAN BLADES 3 AND 12 HAVE MISSING COATING MISSING AT AREA Y CONCAVE SIDE PRESSURE FACE. ACFT GROUNDED.Jun 8, 2017 · N596AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2017060820988Shim · wornNR 1 ENGINE FAN BLADE SHIMS REQUIRE REPLACEMENT DUE TO WEAR. FAN BLADE PLATFORMS HAVE MISSING ELASTOMER, OUT OF LIMITS. ACFT GROUNDED. REMOVED AND REPLACED THE FAN BLADE SHIMS IAW 78472002.Jun 8, 2017 · N596AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2017060620967Fmc · intermittentUNABLE TO MAKE EDITS IN LEFT FMC. SCRATCHPAD MESSAGE FOR INVALID ENTRY WOULD SHOW ON ALL FMC PAGES. NO OTHER INDICATIONS NOTED. ACFT GROUNDED. PERFORMED FIM 34-61 TASK 801, NEITHER FMC LOGGED ANY FAULTS IN FLIGHT FAULT HISTORY. FMC OPS CHECKED NORMAL IAW AMJun 6, 2017 · N596AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2017060220951Fmc · malfunctionedLEFT FMC INOPERATIVE. ACFT GROUNDED. PULLED AND RESET THE LT FMC COMPUTER CIRCUIT BREAKER NR 1 FMC. NO 1 FLT NR 1 FMC OPS CHECKED NORMAL IAW AMM 34-61-00-710-801.Jun 2, 2017 · N596AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2017051820824Autothrottle Sys · malfunctionedAUTOTHROTTLE WILL NOT ENGAGE. ACFT GROUNDED. PERFORMED AUTOTHROTTLE BITE IAW FIM 22-31, TASK 801. NO CURRENT FAULTS. INFLIGHT FAULTS FLT LEG 7 AND 8. PERFORMED IAW FIM 22-32 TASK 819. ALL TESTS OK. NO HISTORY 90 DAYS.May 18, 2017 · N596AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2017051620782Warning Light · false activationLEFT PACK LIGHT ILLUMINATED DURING RECALL. EXTINGUISHED AT RESET. ACFT GROUNDED. PERFORMED PACK TEMP CONTROL BITE IAW FIM 21-62 TASK 801. PACK TCV VALVE WAS FAULTED ON PREVIOUS FLIGHT. CLEARED FAULT BY VERIFYING SWITCH ACTUATION. FAULT CLEARED, RAN PACK OMay 16, 2017 · N596AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2017040920409Satcom · lockedSATCOM LOCKED UP 4 HOURS INTO ETOPS FLIGHT. PERFORMED SATCOM LOCKUP ABNORMAL PROCEDURE. GROUNDED - YES. VERIFIED SATCOM OPS CHECK OK, REF FIM TASK 23-15 TASK 801.Apr 9, 2017 · N596AS · Boeing 737890 · Communications SystemSDR ASAA2017040620386Satcom · lockedSATCOM LOCKUP, ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE PER QRH. SATCOM RESTORED NORMAL.Apr 6, 2017 · N596AS · Boeing 737890 · Communications SystemSDR ASAA2017032020232Satcom · lockedSATCOM LOCK-UP. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. SATCOM OPS RESTORED NORMAL.Mar 20, 2017 · N596AS · Boeing 737890 · Communications SystemSDR ASAA2017031320156Satcom · malfunctionedDURING CLIMBOUT, SATCOM NOT DISPLAYED ON MCDU MENU PAGE. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. SATCOM OPS RESTORED NORMAL.Mar 13, 2017 · N596AS · Boeing 737890 · Communications SystemSDR ASAA2017013019601Satcom · unknownSATCOM INOPERATIVE, COMPLETED QRH PROCEDURE. ACFT GROUNDED. PERFORMED SATCOM SYSTEM TEST, IAW AMM 23-15-00-730-801. TESTS OK.Jan 30, 2017 · N596AS · Boeing 737890 · Communications SystemSDR ASAA2017011119321Satcom · lockedSATCOM LOCKUP. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURES IAW QRH. SATCOM OPS RESTORED NORMAL.Jan 11, 2017 · N596AS · Boeing 737890 · Communications SystemSDR ASAA2017010319236Satcom · malfunctionedSATCOM LOCKUP. GROUNDED - YES. ACCOMPLISHED RESET PROCEDURES PER QRH. SATCOM OPS RESTORED NORMAL.Jan 3, 2017 · N596AS · Boeing 737890 · Communications SystemSDR ASAA2016122919200Unknown · malfunctionedAUTOTHROTTLES DISCONNECTED ON DEPARTURE - WOULD NOT REENGAGE. GROUNDED - YES. FFR LOGGED 22-31688, RATE MONITOR ASM 2. DURING INITIAL EVALUATION VERIFIED NR 2 THROTTLE WOULD NOT ADVANCE WITH SERVO MOTOR TEST. RESET ASM'S. AUTOTHROTTLES OPS CHECK NORMAL, REF FIDec 29, 2016 · N596AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2016122819177Autothrottle Sys · malfunctionedDURING CLIMBOUT, AUTOTHROTTLES WOULD NOT STAY ENGAGED. RIGHT THROTTLE WOULD MOVE, LEFT WOULD NOT, AUTOTHROTTLE WOULD DISCONNECT. NO ABNORMAL FRICTION NOTED IN MANUAL MODE. ACFT GROUNDED. ACCOMPLISHED A/T BITE CHECK IAW FIM TASK 22-31 TASK 801. NO CURRENT FAULDec 28, 2016 · N596AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2016120918979Controller · faultedON RECALL CHECK DURING AFTER START, RECEIVED AN AIR CONDITIONING ANNUNCIATOR AND ALL 3 ZONE TEMP LIGHTS. ALL LIGHTS WOULD EXTINGUISH WITH MASTER CAUTION RESET, BUT COULD NOT CONTROL THE CABIN TEMP. ACFT GROUNDED. ACCOMPLISHED BITE OF BOTH PZTC IAW IAW FIM 2Dec 9, 2016 · N596AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016112718846Compensator · out of toleranceAPPROXIMATELY TWO HOURS INTO THE FLIGHT, FUEL BURN WAS 200 LBS ABOVE FLIGHT PLAN. APPROXIMATELY ONE HOUR LATER, WENT FROM 200 UNDERBURN TO 1200 LBS OVERBURN. THE ONLY THING THAT CHANGED DURING THAT HOUR WAS THE CENTER TANKS RAN DRY. FUEL BURN WAS STABLE BEFORENov 27, 2016 · N596AS · Boeing 737890 · Fuel Indicating SystemSDR ASAA2016110718591Lamp · inoperativeL1 DOOR EMERGENCY LIGHT INOPERATIVE. ACFT GROUNDED. REPLACED THE LAMP, OPS CHECKED GOOD IAW AMM 33-51-04.Nov 7, 2016 · N596AS · Boeing 737890 · Emergency LightingSDR ASAA2016102718496Warning Light · false activationDURING AFTER START CHECKLIST AT RECALL CHECK, LEFT PACK LIGHT ILLUMINATED AND WENT OUT WITH MASTER CAUTION RESET. ACFT GROUNDED. ACCOMPLISHED BITE OF BOTH PTZC, IAW FIM 21-62 TASK 801. NR 1 FAULTED THIS PACK TCV ON BITE AND PREVIOUS FLIGHT, GREEN ON GO LT. ROct 27, 2016 · N596AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016092718138Control Valve · failedLEFT PACK LIGHT ILLUMINATES ON RECALL & EXTINGUISHES WITH RESET. ACFT GROUNDED. REMOVED AND REPLACED LEFT PACK TEMP CONTROL VALVE IAW AMM 21-51-10-401.Sep 27, 2016 · N596AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016092618132Warning Light · false activationAFTER ENGINE START AND RECALL ZONE TEMP CONTROL CABIN LIGHT ILLUMINATED. RAMN QRH NO CHANGE. LIGHT CLEARS WITH MASTER CAUTION RESET. ACFT GROUNDED. ACCOMPLISHED PACK TEMPERATURE CONTROL BITE, IAW FIM 21-62 TASK 801. BITE PASSES.Sep 26, 2016 · N596AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2016092518127Seal · exposedNR 2 ENGINE NR 1 FAN BLADE RUBBER DAMPNER COMING OUT OF SPINNER. ACFT GROUNDED. TRIMMED THE FAN BLADE PLATFORM SEAL, REMOVED .5 OF SEAL FROM FWD EDGE OF PLATFORM. WITHIN LIMITS, IAW AMM 72-21-02.Sep 25, 2016 · N596AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2016092218108Warning Light · illuminatedLEFT PACK LIGHT ILLUMINATED ON MASTER CAUTION RECALL. LIGHT EXTINGUISHED WITH MASTER CAUTION RESET. ACFT GROUNDED. NR 1 TEMP CONTROL LOGGED TCV FAULT - ACCOMPLISHED IAW AMM TASK 21-61-00-700-806-002. TESTS GOOD - FAULT RESET.Sep 22, 2016 · N596AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016090718034Transition Panel · corrodedAFT CARGO COMPARTMENT LT TRANSITION PANEL HAS SEVERAL AREAS OF CORROSION FROM STA 727B TO STA 787. ACFT GROUNDED. BLENDED AREA IAW SRM 51-10-02. ORIGINAL MATERIAL THICKNESS .040 MATERIAL LOSS .008. REMAINING MATERIAL .032. FOUND TO BE OUT OF LIMITS IAW SRSep 7, 2016 · N596AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016090718033Transition Panel · corrodedAFT CARGO COMPARTMENT RT TRANSITION PANEL HAS SEVERAL AREAS OF CORROSION FROM STA 727B TO 767. ACFT GROUNDED. REMOVED CORROSION FROM 727H+10 TO 767, ORIGINAL MATERIAL THICKNESS .040 IAW DWG 1496-377, REMOVED .001, REMAINING MATERIAL .039 IN LIMITS IAW SRM 53Sep 7, 2016 · N596AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016090618012Channel · corrodedFWD CARGO COMPARTMENT RT TRANSITION PANEL HAS SEVERAL AREAS OF CORROSION FROM BS 500A TO 500I. ACFT GROUNDED. FABRICATED A NEW TRANSITION PANEL SECTION IAW SRM 53-00-53, INSTALLED IAW SRM 53-00-53 AND FINISH RESTORED IAW SOPM 20-41-02 AND SRM 51-20-01. .Sep 6, 2016 · N596AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016090518027Support · corrodedAFT CARGO COMPARTMENT FLOOR PANEL SUPPORT TEE ASSY IS CORRODED. ACFT GROUNDED. RECEIVED NEW FLOOR PANEL SUPPORT TEE ASSY AND INSTALLED ON CUSTOMER CARD NR G717536. REMOVED CORROSION FROM SUPPORT TEE AND MATERIAL REMOVED .009, ORIGINAL THICKNESS .070, REMAINSep 5, 2016 · N596AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2016083017862Control Panel · failedAUTOPILOT ENGAGE BUTTON LIGHTS INOPERATIVE. AUTOPILOT FUNCTIONS NORMALLY. ACFT GROUNDED. DUPLICATED DISCREPANCY. REMOVED AND INSTALLED A NEW MCP, IAW AMM 22-11-34. ACCOMPLISHED INSTALL TEST, IAW AMM 22-11-34. ACCOMPLISHED LWMP CHECKLIST DFCS LRU INTERFACEAug 30, 2016 · N596AS · Boeing 737890 · Autopilot SystemSDR ASAA2016082417790Satcom · malfunctionedSATCOM LOCK-UP. ACFT GROUNDED. ACCOMPLISHED SATCOM RESET PROCEDURE IAW QRH. SATCOM OPS RESTORED NORMAL.Aug 24, 2016 · N596AS · Boeing 737890 · HF Communications SystemSDR ASAA2016081417698Warning Message · false activationLEFT PACK LIGHT ILLUMINATED DURING MASTER CAUTION RECALL AND RESETS ON MASTER CAUTION RESET. ACFT GROUNDED. PERFORMED ACAU BITE TEST AND OPS CHECKS NORMAL WITH ONE CLEARED TCV FAULT.Aug 14, 2016 · N596AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016080417615Satcom · malfunctionedSATCOM LOCKUP GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. SATCOM RESTORED NORMAL.Aug 4, 2016 · N596AS · Boeing 737890 · Communications SystemSDR ASAA2016080417612Motor · failedA/T WILL NOT ARM. ACFT GROUNDED. REF AMM 22-31-91, R & R NR 2 ASM. OPS NORMAL REF SAME AMM, CURRENT STATUS AND SERVO MOTOR TEST. THIS CLEARS MEL 22-4B. A/T GROUND VERIFICATION TEST GOOD REF SAME AMM'S.Aug 4, 2016 · N596AS · Boeing 737890 · Auto Throttle SystemSDR ASAA2016072917553Satcom · lockedSATCOM LOCKUP. ACFT GROUNDED. ACCOMPLISHED SATCOM RESET PROCEDURE IAW QRH. SATCOM OPS RESTORED TO NORMAL.Jul 29, 2016 · N596AS · Boeing 737890 · Communications SystemSDR ASAA2016072217467Switch · malfunctionedFIRE, OVERHEAT TEST SHOWS FAULT LIGHT AND NO LIGHTS IN NR 2 ENGINE FIRE HANDLE. ACFT GROUNDED. REPLACED BROKEN TERMINAL IAW SWPM 20-30-11 AND WDM 26-11-21. OPS CHECKED OK. NR 2 ENGINE OVERHEAT DETECTOR SWITCH PLACED IN BOTH POSITION.Jul 22, 2016 · N596AS · Boeing 737890 · Overheat DetectionSDR ASAA2016071317362Actuator · failedON RECALL LEFT PACK LIGHT ILLUMINATED ON RESET LIGHT WENT OUT. ACFT GROUNDED. REMOVED AND REPLACED RAM AIR ACTUATOR NR 1 IAW AMM 21-51-21. PERFORMED NR 1 PACK ZONE TEMPERATURE CONTROLLER BITE TEST IAW AMM 21-61-00-700-806-002, NO FAULTS.Jul 13, 2016 · N596AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016070317278Shroud · wornNR 2 ENGINE, F/O NOTED SOME SCRAPING OF FAN BLADES AGAINST INNER SHROUD DURING WALKAROUND. ACFT GROUNDED. ACCOMPLISHED VISUAL INSPECTION OF GROOVES & CIRCUMFERENTIAL DAMAGE, DETERMINED TO BE FAN BLADE RUB & FOUND TO BE WITHIN LIMITS IAW AMM 72-24-02-200-801-Jul 3, 2016 · N596AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2016062317138Warning System · intermittentLEFT PACK LIGHT ILLUMINATED ON RECALL. PACK LIGHT OFF WITH MASTER CAUTION RESET. ACFT GROUNDED. PACK CONTROLLER 1 LOGGED ACT, RAM AIR, FAULT. FAULT RESET AND IS DEEMED AN INTERMITTENT FAULT IAW FIM 21-62, TASK 848. GROUND VERIFICATION SUCCESSFUL.Jun 23, 2016 · N596AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2016051516743Fmc · malfunctionedON GROUND WITH POWER TRANSFER LT FMC FAILED AND RESTORED INTERMITTENTLY "VTK". ACFT GROUNDED. ACCOMPLISHED FIM 34-61 NR 807, SYS RESTORED AND CKS NORMAL. GROUND VERIFICATION SUCCESSFUL.May 15, 2016 · N596AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2016050516638Sensor · failedRIGHT SIDE WINDOW OVERHEAT, UNABLE TO RESET VIA QRH. ACFT GROUNDED. PERFORMED WINDOW SENSOR RESISTANCE TEST IAW AMM 30-41-21, PRIMARY SENSOR FAILED, SWAPPED TO SECONDARY SENSOR IAW FIM 30-41, TASK 811, RESISTANCE WAS WITHIN LIMITS, R2 WINDOW HEAT OPS NORMAL IMay 5, 2016 · N596AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2016042316496Fmc · failedSINGLE FMC OPERATION MESSAGE & FMC FAIL LIGHT, RIGHT FMC, ON LANDING. ACCOMPLISHED FMC FAIL QRH PROCEDURES. FMC FAIL LIGHT EXTINGUISHED. ACFT GROUNDED. REF B737-800, FIM 34-61 TASK 801 COMPLETED. BITE SHOWS NO FAULTS.Apr 23, 2016 · N596AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2016040616264Blade · damagedWHILE ACCOMPLISHING NR 2 ENGINE FAN LUBE TC 78472002, ESN-894361 FOR TSR907910, FOUND RUBBER MISSING ON NR 4, NR 10, AND NR 7 PLATFORMS BOTH SIDES AND ALL SHIM COATINGS WORN. ACFT GROUNDED. R & R NR 2 ENGINE FAN BLADE PLATFORMS NR 4, NR 10, AND NR 7 AND ALL 2Apr 6, 2016 · N596AS · Boeing 737890 · Turbine Engine Air Inlet SectionSDR ASAA2016040216198Charger · failedELECTRIC LIGHT ILLUMINATED AFTER TOUCHDOWN. ACFT GROUNDED. BITE SHOWS AUX BATTERY CHARGER INOPERATIVE, CONFIRMED. R & R AUXILIARY BATTERY CHARGER IAW AMM 24-31-31. OPS CHECK GOOD.Apr 2, 2016 · N596AS · Boeing 737890 · Battery/Charger SystemSDR ASAA2016033016165Valve · failedRIGHT PACK LIGHT ILLUMINATED UPON RECALL, EXTINGUISHED WITH RESET. ACFT GROUNDED. PERFORMED PACK ZONE TEMP CONTROL BITE IAW FIM 21-62, TASK 801. RT CONTROLLER FAULTED THIS PACK TCV IAW FIM 21-62, TASK 831, FAULTS RT TCV. REMOVED RT PACK TEMP CONTROL VALVE IMar 30, 2016 · N596AS · Boeing 737890 · Cabin Cooling System
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