N565AS

Service difficulty reports · 509

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 = 'N565AS' 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 ASAA2015082312874Warning Light · false activationON SHORT FINAL RT PACK LIGHT ILLUMINATED. LIGHT EXTINGUISHED WHEN MASTER CAUTION RESET. ACFT GROUNDED. ACCOMPLISHED BITE OF THE PACK/ZONE TEMP. CONTROLLER, REF FIM 21-62, TASK 801. FOUND THE FAULT ON THE NR 2 CONTROLLER FOR THE RAM AIR ACTUATOR FAULT CLEARAug 23, 2015 · N565AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2015081812907Battery Pack · failed4 EA EMERGENCY LIGHTS FAILED. ACFT GROUNDED. REPLACED 2 EA BATTERY PACKS.Aug 18, 2015 · N565AS · Boeing 737890 · Emergency LightingSDR ASAA2015072912632Terminal · looseLEFT SIDE WINDOW OVERHEAT LIGHT ILLUMINATED. FOLLOW QRH CHECKLIST 3.3 LIGHT RE-ILLUMINATE. SWITCH NOW IN OFF POSITION. ACFT GROUNDED. FOUND TERMINALS ON THE SENSOR AT THE WINDOW TO BE LOOSE ENOUGH TO BREAK CONNECTION. MEASURED RESISTANCE WHILE SHAKING DOWJul 29, 2015 · N565AS · Boeing 737890 · Ice/Rain Protection System WiringSDR ASAA2015072612593Shutoff Valve · no testNR 2 ENGINE PRSOV AND PRECOOLER CONTROL VALVE FAIL CONTROL PRESSURE CHECK, REF T/C NG-36WC-00001. FOUND BRAIDED LINE LEAKING ON NR 2 ENGINE. ACFT GROUNDED. REPLACED NR 2 ENGINE PRSOV REF MM 36-11-04. REPLACED NR 2 ENG PRECOOLER CONTROL VALVE, REF MM 36-12-Jul 26, 2015 · N565AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2015072112534Warning Message · false activationFMC DISAGREE ON TAXI. ACFT GROUNDED. QRH PROCEDURE CORRECTED ISSUE.Jul 21, 2015 · N565AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015072112533Lens · detachedOVERWING EMERGENCY EXIT SIGN COVER FELL OFF. ACFT GROUNDED. RE-INSTALLED LENS COVER.Jul 21, 2015 · N565AS · Boeing 737890 · Emergency LightingSDR ASAA2015071712468Satcom · lockedSATCOM LOCK-UP OCCURRED DURING POWER TRANSFER. ACFT GROUNDED. RESET SUCCESSFUL IAW QRH.Jul 17, 2015 · N565AS · Boeing 737890 · Communications SystemSDR ASAA2015071012389Fmc · malfunctionedF/O FMC INOPERATIVE. "MAP" & "VTK" ON NAV DISPLAY. ACFT GROUNDED. ACCOMPLISHED FIM 34-61, TASK 807. RESET SYSTEM, SYS OPS CHECKS NORMAL IAW AMM 34-61-00, GROUND VERIFICATION SUCCESSFUL. NO HISTORY 90 DAYS.Jul 10, 2015 · N565AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015062612231Warning Light · false activationELECTRONIC AMBER CAUTION LIGHT ILLUMINATED. ACFT GROUNDED. ACCOMPLISHED FIM 34-31, TASK 801. AUXILIARY BATTERY CHARGER INOPERATIVE FAULT. ACCOMPLISHED FIM 34-31, TASK 825. FAULT CLEARED & AUXILIARY BATTERY CHARGER OPS NORMAL. NO PREVIOUS HISTORY. GROUND VJun 26, 2015 · N565AS · Boeing 737890 · Electrical Power SystemSDR ASAA2015060411982Satcom · malfunctionedNO SATCOM PROMPT ON THE GROUND. ACFT GROUNDED. PERFORMED SATCOM LOCKOUT PROCEDURE, SATCOM CAPABILITY RESTORED.Jun 4, 2015 · N565AS · Boeing 737890 · Communications SystemSDR ASAA2015052411826Valve · failedON DESCENT, AT 10,000 FT, THE BLUE NR 2 "COWL VALVE OPEN" LIGHT ILLUMINATED WITH THE NR 2 ENGINE ANTI-ICE SWITCH IN THE OFF POSITION. THE LIGHT APPEARED TO FLICKER AND ILLUMINATE STEADY. REMAINED FOR ABOUT 3 MINS WITH AND WITHOUT POWER FROM NR 2 ENGINE. ACFMay 24, 2015 · N565AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR ASAA2015051411745Warning Light · false activationJUST PRIOR TO TAKE OFF, NOTICED THE NR 2 ENGINE ANTI ICE BLUE LIGHT FLICKER DIM BLUE, CYCLED THE SWITCH ON AND OFF AND THE LIGHTS AND VALVES REACTED NORMALLY. WHEN THRUST LEVERS WENT TO IDLE ON DESCENT THE LIGHT WENT OUT, NO FLICKERING. ACFT GROUNDED. VERIFIEMay 14, 2015 · N565AS · Boeing 737890 · Air Intake Anti/De-Ice SystemSDR ASAA2015042811569Display · failedF/O MCDU SCREEN BRIGHTNESS INOPERATIVE AND OCCASIONALLY FLICKERS BETWEEN DIM AND BRIGHT. ACFT GROUNDED. REPLACED F/O'S MCDU REF AMM 34-61-01-000-802. GROUND VERIFICATION TEST GOOD. ETOPS NOTIFIED, P/N VERIFIED.Apr 28, 2015 · N565AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015042711548Display · malfunctionedF/O MCDU STAYS DIM AND WILL NOT BRIGHTEN. OCCASIONALLY SCREEN FLICKERS. ACFT GROUNDED. RESET POWER FOR F/O, REF FIM 34-61, TASK 803, MCDU NOW DIMS AND BRIGHTENS NORMALLY. NO FLICKERS, GROUND VERIFICATION, OPS CHECK OK.Apr 27, 2015 · N565AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015042511524Warning Message · false activation"FMC DISAGREE" PROMPT ON GROUND. ACFT GROUNDED. RESET NORMALLY VIA QRH PROCEDURES.Apr 25, 2015 · N565AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015041111295Fmc · failedUPON TOUCHDOWN F/O'S FMC SCREEN FLICKERS WITH A LINE THROUGH SCREEN AS WELL; SCREEN SEEMS TO BE FAILING. ACFT GROUNDED. CONFIRMED FAULT, F/O FMC CDU DISPLAY INTERMITTENT. R & R F/O FMC CDU REF AMM 34-61-01, OPS CK NORMAL. ALSO, ACCOMPLISHED CDU SOFTWARE CONApr 11, 2015 · N565AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015041011296Valve · failedNR 1 BLEED TRIP OFF LIGHT ILLUMINATED DESCENDING THROUGH 380. ACCOMPLISHED BLEED TRIP OFF CHECKLIST. LIGHT REMAINED ILLUMINATED. ACFT GROUNDED. ACCOMPLISHED T/C NG-36WC-00001. FOUND PCU VALVE & PRSOV FAILED. R & R PRECOOLER CONTROL VALVE REF AMM 36-12-02 OApr 10, 2015 · N565AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2015032511121Warning Message · false activationON TAXI "FMC DISAGREE" CAME ON. ACFT GROUNDED. PERFORMED PROCEDURE FROM QRH. OPS NORMAL.Mar 25, 2015 · N565AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015032311087Idg · contaminatedDEBRIS FOUND IN NR 2 ENGINE IDG SIGHT GLASS. ACFT GROUNDED. REMOVED NR 2 ENGINE IDG SIGHT GLASS , FOUND DEBRIS TO BE DISLODGED DEPOSITS CONTAINED WITHIN SIGHT GLASS CAVITY. CLEANED CAVITY OF REMAINING DEPOSITS, REINSTALLED SIGHT GLASS IAW CMM 24-11-85 P.715.Mar 23, 2015 · N565AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2015020510604Channel · puncturedAFT CARGO BAY, RT SIDEPLATE CHANNEL IS PUNCTURED AT APPROXIMATELY STA 727H+15. ACFT GROUNDED. REMOVED DAMAGE SECTION IAW SRM 51-40-02 FABED SECTION AND SPLICE REPAIR IAW SRM 53-00-53-2R-5, INSTALLED NEW SECTION AND SPLICE REPAIR IAW SRM 53-00-53-2R-5 AND SRMFeb 5, 2015 · N565AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015013010618Skin · crackedRIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STA 129 , 26" AFT FROM FRONT SPAR. ACFT GROUNDED. REPAIRED THE SKIN IAW SRM 55-10-01-2R-11.Jan 30, 2015 · N565AS · Boeing 737890 · Horizontal Stabilizer, Plate/SkinSDR ASAA2015012910606Support Angle · corrodedFWD CARGO BAY AFT BULKHEAD LOWER SUPPORT ANGLE IS CORRODED. ACFT GROUNDED. R & R AFT BULKHEAD LOWER SUPPORT ANGLE IAW SRM 51-40-02, AND 51-10-02, PARA 9, ANGLE EXFOLIATED, 100 PERCENT MATERIAL LOSS.Jan 29, 2015 · N565AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015012910611Attach Angle · corrodedFWD CARGO BAY, AFT LT BULKHEAD TO FLOOR SUPPORT ATTACH ANGLE IS CORRODED. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2. R & R THE ATTACH ANGLE IAW AMM 25-52-06.Jan 29, 2015 · N565AS · Boeing 737890 · Fuselage Main, Attach FittingsSDR ASAA2015012910603Attach Angle · corrodedFWD CARGO BAY AFT RT BULKHEAD TO FLOOR SUPPORT ATTACH ANGLE IS CORRODED. ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS OF 10 PERCENT MAX IAW SRM 53-00-53-11-2. R & R THE ATTACH ANGLE IAW SRM 51-40-02 AND 51-10-02, PARA 9.Jan 29, 2015 · N565AS · Boeing 737890 · Fuselage Main, Attach FittingsSDR ASAA2015012910594Strip · corrodedFWD CARGO BAY LT AFT CAP STRIP IS CORRODED. ACFT GROUNDED. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2. REPLACED CAP STRIP IAW SRM 51-10-02, PARA 9.Jan 29, 2015 · N565AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015012910524Channel · corrodedFWD CARGO BAY RT FLOOR SUPPORT SIDEPLATE IS CORRODED. BS 500H+8 - 500". ACFT GROUNDED. REMOVED CORROSION AND FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-00-53-1A-2, FIG 103, DETAIL D. ORIGINAL MATERIAL THICKNESS WAS 0.040 IN IAW SRM 53-30-53-0I-2, MATERIAL THIJan 29, 2015 · N565AS · Boeing 737890 · Fuselage Miscellaneous StructureSDR ASAA2015012510416Fmc · failedRIGHT FMC FAILED IN FLIGHT. ACCOMPLISHED QRH PROCEDURE AND FMC NOT RESTORED. ACFT GROUNDED. REMOVED AND INSTALLED NEW RT FMC COMPARTMENT REF 34-61-02. PERFORMED INSTALL TEST, STEP E REF 34-61-00-710-801. STEP F 1, 2, AND 3. SYS CKS NORMAL.Jan 25, 2015 · N565AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2015012310390Valve · failedRIGHT PACK ZONE TEMP CONTROLLER FAULTED: RT PACK TCV. ACFT GROUNDED. R & R RT PACK TCV IAW AMM 21-51-10, ZONE TEMP CONTROL NR 2 BITE CHECKED GOOD. IAW AMM 21-61-00. LEAK CHECKED GOOD.Jan 23, 2015 · N565AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2015012110345Valve · malfunctionedLEFT PACK LIGHT CAME ON WITH RECALL DURING LANDING CHECK. LIGHT WENT OUT ON MASTER CAUTION RESET. ACFT GROUNDED. INTERROGATED NR 1 ZONE TEMP CONTROLLER: FAULTED TCV THIS PACK & OTHER PACK. REPLACED LT PACK TCV. REF'S: 21-61-00 & 21-51-10. R & R RT PACK TCJan 21, 2015 · N565AS · Boeing 737890 · Cabin Cooling SystemSDR ASAA2015011910291Controller · malfunctionedCONTROL CABINE TEMP CONTROLLER NOT WORKING PROPERLY. IN COLDEST SETTING STILL BLOWS OUT HOT AIR. DUCT TEMP HOVERS AROUND 40C REGARDLESS OF KNOB POSITION. ACFT GROUNDED. PERFORMED BITE CHECK ON RT & LT PACK CONTROLLERS IAW PLACARD. NO FAULTS FOUND. NO FAULJan 19, 2015 · N565AS · Boeing 737890 · Cabin Temperature Control SystemSDR ASAA2014121910023Regulator · failedNR 1 ENGINE HIGH STAGE REGULATOR FAILED REVERSE FLOW DIAPHRAM TEST DURING ENGINE BLEED AIR HEALTH CHECK TASK CARD. ACFT GROUNDED. REPLACED NR 1 ENGINE HIGH STAGE REGULATOR. LEAK/OPS CHECK OK, REF MM 36-11-07.Dec 19, 2014 · N565AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2014121910015Warning Light · false activationAFTER ENGINE START, ELECTRIC LIGHT WAS ILLUMINATED ON OVERHEAD PANEL. ACFT GROUNDED. ACCOMPLISHED FIM ELECTRICAL LIGHT BITE 24-31, TASK 801, AUX BATTERY CHARGER INOP I FAULT. VERIFIED AUX BATTERY CHARGER, C/B P91 WAS SET AND LIGHTS ON AUX BATTERY CHARGER WEDec 19, 2014 · N565AS · Boeing 737890 · DC Generating SystemSDR ASAA2014121909998Regulator · no testNR 1 ENGINE HIGH STAGE REGULATOR FAILED REVERSE FLOW DIAPHRAM TEST DURING ENGINE BLEED AIR HEALTH CHECK TASK CARD. ACFT GROUNDED. REPLACED NR 1 ENGINE HIGH STAGE REGULATOR. LEAK, OPS CHECK OK, REF MM 36-11-07.Dec 19, 2014 · N565AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2014121109927Fire Detector · failedNR 1 ENGINE LOOP B FIRE DETECTOR INOPERATIVE. ACFT GROUNDED. PERFORMED ENGINE FIRE DETECTOR BITE CHECK IAW FIM 26-10, TASK 801. FOUND HIGH RESISTANCE OF FIRE DETECTOR LOOP. REPLACED FIRE CORE ELEMENT ASSY IAW MM 26-11-01. OPS CHECKED NORMAL.Dec 11, 2014 · N565AS · Boeing 737890 · Fire DetectionSDR ASAA2014111209654Warning Message · activatedFOUND LONG TERM FAULT CODE 77-21171, N1 SIGNAL OUT OF RANGE ON NR 1 ENGINE. ACFT GROUNDED.Nov 12, 2014 · N565AS · Boeing 737890 · Engine (Turbine/Turboprop)SDR ASAA2014110509598Valve · failedAFTER TAKE OFF, OBSERVED SPLIT IN DUCT PRESSURE INDICATION. DURING CLIMBOUT, RT AT 15 PSI LT AT 41PSI. CRUISE RT AT 19 PSI LT AT 43 PSI. RT AT 20PSI LT AT40 PSI. DESCENT: RT AT 16 PSI LT AT 26 PSI. ACFT GROUNDED. DURING WRENCH CHECK FOUND HIGH STAGE VALVENov 5, 2014 · N565AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2014100809330Warning Message · false activationON GROUND, FMC DISAGREE. ACFT GROUNDED. RAN QRH, SYS RESTORED. OPS NORMAL.Oct 8, 2014 · N565AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014091609141Control Valve · malfunctionedCLIMBING OUT OF 16,000 FT, OBSERVED NR 1 ENGINE BLEED TRIP OFF LIGHT ILLUMINATE. PERFORMED QRH PROCEDURES AND NORMAL OPERATIONS RESTORED. ACFT GROUNDED. COMPLETED TASK CARD, NG36WC-00001. FOUND PCV AND HIGH STAGE REG REQUIRED CHANGING. REPLACED HIGH STAGESep 16, 2014 · N565AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2014091409129Valve · failedLEFT ENGINE BLEED TRIP CAME ON AT 100 FT . CHECKLIST PROCEDURE CLEARED LIGHT AND RESTORED OPS. ACFT GROUNDED. DIVERTED BACK TO DEPARTURE. ACCOMPLISHED FIM TASK 36-10, TASK 801. FOUND HIGH STAGE VALVE STICKING & RATCHETING WHILE MANUALLY OPERATING IT. R &Sep 14, 2014 · N565AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2014080508771Warning Message · activatedFOUND LONG TERM FAULT CODE 77-21171 ON ENGINE. N1 SIGNAL OUT OF RANGE. ACFT GROUNDED. FAULT IS NOT ACTIVE. NO ACTIVE FAULTS LOGGED IN FLIGHT LEG 0 OR IN FAULT HISTORY, LAST 10 FLIGHTS. REF FIM TASK 77-11, TASK 801.Aug 5, 2014 · N565AS · Boeing 737890 · Engine Indicating SystemSDR ASAA2014072708687Relief Valve · failedDURING CLIMB DUCT PRESSURE WERE 45 ON LT AND 20 ON RT, AFTER LEVEL OFF AT FL380 DUCT PRESSURE WERE 35 ON LT 20 ON RT. ACFT GROUNDED. ACCOMPLISHED HEALTH CHECK FOR NR 2 BLEED AIR SYS IAW TC NG-36WC-0001. WRENCH CK PRSOV FAILED. R & R THE NR 2 ENG PRSOV IAW Jul 27, 2014 · N565AS · Boeing 737890 · Pneumatic Distribution SystemSDR ASAA2014071908601Fmc · malfunctionedFMC WILL NOT LOAD DATA. ACFT GROUNDED. CYCLED POWER. ALL SYS RETURNED TO NORMAL, REF AMM 34-61-00.Jul 19, 2014 · N565AS · Boeing 737890 · Flight Management Computing Hardware SystemSDR ASAA2014070908521Heater · overheatedOVERHEAT LIGHT ON FOR R2 WINDOW IN COCKPIT. ACFT GROUNDED. R & R RT SLIDING WINDOW AMM 56-12-11, OPS CHECK NORMAL AMM 30-41-00, SEAM C PAT FOR PARTS VERIFICATION THIS CLEARS MEL 30-11C. REMOVED PLACARD, SEAM C PAT NOTIFIED.Jul 9, 2014 · N565AS · Boeing 737890 · Windshield/Door Rain/Ice RemovalSDR ASAA2014070308438Idg · failedARRIVING, THE NR 1 ENGINE SOURCE AND DRIVE LIGHTS AMBER ILLUMINATED. QRH FOLLOWED AND LANDED WITHOUT INCIDENT. ACFT GROUNDED. REMOVED THE NR 1 IDG, REF MM 24-11-11-000-801. INSTALLED THE NR 1 IDG REF MM 24-11-11-400-801. OPS AND LEAK CKS GOOD, REF MM 24-11Jul 3, 2014 · N565AS · Boeing 737890 · AC Generator-AlternatorSDR ASAA2014070108417Warning Light · false activationON BLEEDS OFF 27K TO, AFTER PACKS RECONFIGURED, RT BLEED TRIP OFF OCCURRED. PERFORMED QRH PROCEDURE, TRIP RESET RT BLEED TRIP OFF LIGHT EXTINGUISHED. ACFT GROUNDED. OPS NORMAL IAW FIM 36-10-801.Jul 1, 2014 · N565AS · Boeing 737890 · Central WarningSDR ASAA2014062508356Warning Light · illuminatedAT 9000 FEET DURING APPROACH, THROTTLES BACK, NR 1 ENGINE START VALVE OPEN LIGHT ILLUMINATED FOR APPROXIMATELY 1 MINUTE, TURNED BOTH IGNITION SWITCHES FROM CONTINUOUS TO OFF, THEN BACK TO CONTINUOUS, MOVED BOTH THROTTLES UP, LIGHT EXTINGUISHED. ACFT GROUNDED.Jun 25, 2014 · N565AS · Boeing 737890 · Engine Start Valves/ControlsSDR ASAA2014051107770Igniter · faultedAPU FAULT LIGHT ILLUMINATED DURING START. ACFT GROUNDED. REPLACED IGNITER PLUG, IGNITER PLUG LEAD AND IGNITION UNIT REF AMM 49-41-51, AMM 49-41-52 & AMM 49-41-31. OPS CHECKED GOOD.May 11, 2014 · N565AS · Boeing 737890 · APU Start/Ignition SystemSDR ASAA2014030207047Chain · brokenNR 2 ENGINE OIL TANK CAP RETAINING CHAIN IS BROKEN. ACFT GROUNDED. INSTALLED NEW RETAINING CHAIN AT NR 2 ENGINE OIL TANK CAP.Mar 2, 2014 · N565AS · Boeing 737890 · Turbine Engine Oil SystemSDR ASAA2014022406976Satcom · malfunctionedSATCOM LOCKED UP ON GROUND DURING POWER TRANSFER. ACFT GROUNDED. FOLLOWED QRH PROCEDURE, RESTORED SATCOM.Feb 24, 2014 · N565AS · Boeing 737890 · Communications SystemSDR ASAA2014021906913A/C Pack · warning lightRT PACK LIGHT ILLUMINATED. WOULD NOT RESET, PACK TUTRNED OFF. ACFT GROUNDED.Feb 19, 2014 · N565AS · Boeing 737890 · Cabin Cooling System
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