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.
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
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 ASAA2016101318428Attach Angle · crackedFWD CARGO BAY UNDER TRANSITION PANEL, ATTACH ANGLE AT FWD END OF FRAME, CRACKED BS 500H, STRINGERS 24-25R. ACFT GROUNDED. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-05, 51-40-02, AND DWG 143A7505.SDR ASAA2016101318427Attach Angle · crackedFWD CARGO BAY, UNDER TRANSITION PANEL, RIGHT ATTACH ANGLE, FWD SIDE OF FRAME, CRACKED BS 500G, STRINGERS 24-25R. ACFT GROUNDED. REMOVED AND REPLACED THE ATTACH ANGLE IAW SRM 51-40-02, SRM 51-40-05, AND DWG 143A7505.SDR ASAA2016101318420Transition Panel · corrodedAFT CARGO BAY, RIGHT TRANSITION PANEL FROM BS 727 TO 727H+3 HAS SEVERAL AREAS WITH CORROSION AND BARE METAL. ACFT GROUNDED. BLENDED THE TRANSITION PANEL IAW DWG BAC1496-377. FOUND TO BE WITHIN LIMITS IAW SRM 53-00-53-1A-2,SDR ASAA2016101118483Skin · crackedRIGHT HORIZONTAL STAB LOWER SKIN HAS A CRACK INDICATION HSS 129.5. ACFT GROUNDED. REMOVED DAMAGE AND ACCOMPLISHED REPAIR IAW SRM 55-10-01-2R-11 REPAIR II.SDR ASAA2016100118165Valve · failedDURING CLIMB OUT, WITH ENGINE ANTI-ICE ON. RECEIVED A AMBER ANTI-ICE LIGHT ON NR 1 ENG. FOLLOWED QRH PROCEDURES AND REDUCED THRUST ON THE NR. 1 ENGINE AND THE LIGHT EXTINGUISHED WITH APPROXIMATELY A 5% REDUCTION IN N1. ADVANCED THRUST IN CLIMB OUT AND THE LIGHSDR ASAA2016091918071Control Panel · failedF/O'S COURSE INDICATOR NOT ILLUMINATED. GROUNDED - YES. REMOVED AND REPLACED MCP, IAW AMM 22-11-34, OPS CHECK NORMAL. ACCOMPLISHED MCP LWMP CHECKS, REF LWMP CHECKLIST IAW AMM 22-00-01, ALL TESTS PASSED. ACFT REMAINS CATIIIA AUTOLAND & HGS, VERIFIED STATUS SCRESDR ASAA2016090517936Unknown · unknownELECTRIC LIGHT ON. ACFT GROUNDED. ELECTRICAL PANEL LOGGED AUXILIARY BATTERY CHARGER FAULT, FAULT CLEARED. GVI OF AUXILIARY BATTERY CHARGER, NO DEFECTS NOTED. AUXILIARY BATTERY CHARGER, OPS NORMAL IAW AMM 24-31-31-710-801.SDR ASAA2016080617619Lens · detachedFAS REPORT OVERWING EXIT LIGHT FELL OFF OVER SEAT 16F. ACFT GROUNDED. REPLACED RT FWD OVERWING EMERGENCY EXIT LIGHT COVER, REF AMM 33-51-01.SDR ASAA2016070817311Lens · missingLENS MISSING ON FWD SIDE OF CENTER AISLE OVERHEAD EMERGENCY EXIT SIGN AT ROW 16/17. ACFT GROUNDED. INSTALLED NEW LENS & VERIFIED OPERATION OF OVERHEAD EXIT LIGHTS IAW AMM 33-51-00. OPS CHECKED GOOD.SDR ASAA2016070717297Control Valve · failedLEFT PACK LIGHT ILLUMINATED ON RECALL, EXTINGUISHES ON MASTER CAUTION RESET. ACFT GROUNDED. PERFORMED PACK ZONE TEMPERATURE CONTROLLER BITE IAW AMM 21-61-00-700-806-002, FAULTED LT PACK TEMPERATURE CONTROL VALVE (TCV). REMOVED LT PACK THE CONTROL VALVE IAWSDR ASAA2016063017206Shim · wornNR 2 ENGINE TREND DATA SHOWS VIBRATION LEVELS FROM THE LOW PRESSURE ROTOR TO GREATER THAN EXPECTED. DATA SCATTER INDICATES FAN LUBE REQUIRED. PER T/C 7847200 NR 2 ENGINE FAN BLADE SHIMS EXHIBIT MORE THAN 25% MOLYDAG COATING LOSS PER AMM 72-21-02-801 STEP L (1)SDR ASAA2016062017099Unknown · malfunctionedELECTRIC LIGHT ILLUMINATED. ACFT GROUNDED. PERFORMED BITE CHECK P5-13, PANEL IAW FIM 24-31-801. SHOW FAULT OK, BATTERY CHARGER INOPERATIVE. RESET PANEL FAULT CLEARED. ACFT OK TO CONTINUED SERVICE.SDR ASAA2016061217017Display · failedCAPTAINS FMC BRIGHT KNOB DOESNT STOP, FLICKERS. ACFT GROUNDED. REPLACED CAPTAIN'S MCDU, OPS NORMAL, REF AMM TASK 34-61-01-400-802. OPS NORMAL. REF AMM TASK 34-61-00-750-802 FOR SOFTWARE VERIFICATION.SDR ASAA2016052916878Warning Light · false activationDURING CLIMB THROUGH 9000, COWL ANTI-ICE AND MASTER CAUTION LIGHTS ILLUMINATED ON THE NR 1 ENGINE. CYCLED ENGINE ANTI-ICE SWITCHES OFF. LIGHT EXTINGUISHED. ACCOMPLISHED QRH PROCEDURE, CLIMBING OUT OF 15000, TURNED ENGINE ANTI-ICE ON. OPERATED NORMAL. NO WARNSDR ASAA2016041016340Panel · delaminatedREF T/C 78472000, NR 1 ENGINE INLET AND FAN BLADES. DETAILED INSPECTION FOUND NR 5 FAN STRUT PANEL 5 O'CLOCK POSITION HAS 1 FASTENER INSERT DELAMINATED FROM PANEL, AFT OTBD FASTENER. ACFT GROUNDED. REPLACED NR 5 FAN STRUT PANEL AT 5 O'CLOCK POSITION, REF AMSDR ASAA2016032916146Satcom · lockedSATCOM LOCKUP DURING POWER TRANSFER. ACFT GROUNDED. ACCOMPLISHED SATCOM RESET PROCEDURES IAW QRH. SATCOM OPS NORMAL.SDR ASAA2016032516092Valve · failedRIGHT "COWL VALVE OPEN" LIGHT ILLUMINATES INTERMITTENTLY. RIGHT ENGINE N1 AND EGT STAY STEADY. (NO VARIATION). ACFT GROUNDED. R & R NR 2 ENGINE "TAI" VALVE IAW AMM 30-21-11-400-801. OPS AND LEAK CHECK NORMAL.SDR ASAA2016030815835Lens · detachedEMERGENCY EXIT SIGN FELL OFF. ACFT GROUNDED. RE-ATTACHED EXIT SIGN, OK FOR SERVICE.SDR ASAA2016020615304Satcom · lockedSATCOM LOCKUP ON POWER TRANSFER. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. SATCOM RESTORED NORMAL.SDR ASAA2016020215273Lens · detachedF/A REPORTS OVERHEAD EXIT SIGN AT EXIT ROW FELL FROM CEILING. ACFT GROUNDED. REINSTALLED EXIT SIGN PLASTIC FACE.SDR ASAA2016011614836Sensor · failedBLEED TRIP OFF LT PACK IN FIRST HOUR, IN CRUISE 41,000 FT. RESET SUCCESSFUL FOLLOWED BY SECOND BLEED TRIP LT SIDE IN 20 MIN LATER. RESET SUCCESS 2ND TIME. ACFT GROUNDED. ON DEFERRAL, R & R 450 SENSOR, REF AMM 36-11-05 AND PRE COOLER CONTROL VALVE SENSOR REFSDR ASAA2016011114729Wire Harness · damagedREF T/C N8420000, FOUND BROKEN CLAMP AND HARNESS DAMAGE ON HARNESS MW0326 AT THE LEFT CORE DETECTOR, B2. ACFT GROUNDED. R & R MW0326 CORE FIRE DETECTION HARNESS. REF AMM 26-11-02-000-802. HARNESS REQUIRES SECURING AND TIGHTENING. COMPLETED INSTALL OF MW0326 SDR ASAA2016011014717Lens · looseEXIT SIGN FROM WING EMERGENCY EXITS NEEDS TO BE RE-SECURED. ACFT GROUNDED.
RE-SECURED EXIT SIGN AS REQUIRED.SDR ASAA2016010914708Indicator · trippedWHILE PERFORMING TSR817378 FOUND ENGINE NR 2 SUPPLY OIL FILTER POP-OUT INDICATOR EXTENDED. ACFT GROUNDED. PERFORMED OIL SUPPLY FILTER POP-OUT INDICATOR INSPECTION. NO CONTAMINATION FOUND ON SUPPLY OIL FILTER FOR ENGINE NR 2. REF AMM 79-00-00-200-805-F00. PERSDR ASAA2016010914688Oil Cooler · leakingNR 2 IDG FREQUENT SERVICING, ACFT GROUNDED. FOUND IDG NR 2 LEVEL NOT PRESENT IN SIGHT GLASS. FOUND IDG AIR/OIL COOLER EXTERNAL LEAK WITH EVIDENCE DRIPPING FROM THRUST REVERSER SLEEVE. CLEANED ALL OIL FROM THRUST REVERSER AND ALL EFFECTED AREAS. R & R ENGINE NSDR ASAA2016010814695Warning Message · false activationFMC DISAGREE ON GROUND. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. FMCS RESTORED NORMAL.SDR ASAA2015122514472Sensor · faultedNR 1 ENGINE LONG TERM FAULT NR 77-21171, THE N1 SIGNAL IS OUT OF RANGE. ACFT GROUNDED. ACCOMPLISHED FIM 77-11, TASK 801, FAULT MSG PRESENT ON FLT LEGS 1 THROUGH 10, BUT NOT ON LEG 0. RESISTANCE CHECKED AT N1 SENSOR 58.9 OHM COMPARED TO 58.4 FOR CH A. RESISTASDR ASAA2015122414454Oil Cooler · leakingNR 2 ENGINE, IDG AIR/OIL COOLER LEAKING IN THE MATRIX. C-DUCT WET WITH OIL. ACFT GROUNDED. REPLACED NR 2 ENGINE, IDG AIR/OIL COOLER. LEAK CHECK OK. REF MM 24-11-21.SDR ASAA2015120713968Idg · failedNR 2 ENGINE IDG FREQUENT OIL SERVICING. ACFT GROUNDED. R & R NR 2 ENGINE IDG. OPS CHECK, LEAK CHECK GOOD, REF AMM 24-11-11-000-801, 24-11-11-400-801, 24-11-00-700-803.SDR ASAA2015120214074Actuator · failedLEFT PACK LIGHT ILLUMINATES DURING RECALL. ACFT GROUNDED. R & R NR 1 RAM AIR EXHAUST ACTUATOR IAW AMM 21-51-21. PERFORMED TASKS AMM 32-09-00 FOR AIR MODE AND GROUND MODE FOR INSTALLATION. PERFORMED PACK TEMP CONTROLLER BITE TEST AMM TASK 21-61-00. OPS TESSDR ASAA2015111913824Anti-Ice Valve · failedR 2 ENGINE COWL TAI VALVE LIGHT STAYING ON. ACFT GROUNDED. R & R NR 2 ENGINE TAI VALVE, REF AMM 30-21-11. OPS CHECK NORMAL.SDR ASAA2015111813850Anti-Ice Valve · failedNR 2 ENGINE COWL VALVE OPEN LIGHT ILLUMINATED, ACFT GROUNDED. R & R NR 2 ENGINE TAI VALVE REF AMM 30-21-11. OPS CHECK NORMAL.SDR ASAA2015111613736Valve · failedNR 2 IDG FREQUENT SERVICING, ACFT GROUNDED. PERFORMED IDG STATIC LEAK CHECK, CHECK GOOD, REF MM 24-11-00. BAGGED IDG DRAIN AND RUN ENGINE AT IDLE FOR 10 MIN FOUND NO OIL IN THE BAG FROM THE DRAIN. CHECK FOR LEAKS FROM ALL IDG CONNECTIONS PLUMBING LUBE LINES,SDR ASAA2015111313767Warning Message · false activationNR 2 "COWL VALVE OPEN" LIGHT ON. ACFT GROUNDED. RAN NR 2 ENGINE AND CYCLED NR 2 COWL VALVE 3 TIMES. OPS NORMAL.SDR ASAA2015111014235Lens · detachedMID CABIN EXIT SIGN OVER AISLE FELL DOWN. ACFT GROUNDED. REINSTALLED EXIT SIGN LENS, NO DAMAGE NOTED. EXIT SIGN OPS CK GOOD. AMM 33-51-01.SDR ASAA2015110513672Warning Light · false activationON GROUND, RT ANTI-ICE ENGINE COWL VALVE LIGHT REMAINED ON. ACFT GROUNDED. RAN NR 2 ENGINE PERFORMED NR 2 ENGINE COWL ANTI-ICING OPS TEST IAW AMM 30-21-00-710-801, STEP 5(B) . TESTED SEVERAL TIMES. LIGHT WENT OUT. OPERATES NORMALLY IN ALL CONDITIONS. NO DESDR ASAA2015103013567Bolt · missing2EA BOLTS & ATTACHING HARDWARE MISSING FROM NR 1 ENGINE INNER FLANGE OF THE TURBINE REAR FRAME AT 7 O`CLOCK POSITION. ACFT GROUNDED. REMOVED PRIMARY PLUG ASSY & TURBINE REAR FRAME OIL INLET COVER. ACCOMPLISHED BOLT INSTALLATION IAW EA 800-72EA-16004 ON NR 1SDR ASAA2015102113489Connector · unsecureDURING ELECTRONIC ENGINE CONTROL TEST 73-21-700-800-F00, FOUND 3 MAINTENANCE MESSAGES. 73-10752, 75-10892 AND 73-20762. ACFT GROUNDED. FOUND PIN ON NR 2 ENGINE ID PLUG NOT SEATED. SEATED PIN IAW MM 73-21-61-800, ELECTRONIC ENGINE CONTROL TEST PASSED.SDR ASAA2015102113445Engine · making metalNON-MAGNETIC METAL PARTICLES FOUND IN NR 2 ENGINE AFT CHIP DETECTOR. ACFT GROUNDED. IAW MM 79-00-00-200-804, STEP 7H, 7, L, 27H, REMOVED NR 2 OIL SCAVENGE FILTER FOR ANALYSIS. INSTALLED NEW FILTER IAW MM 79-21-05. LEAK CHECK GOOD. ELECTRONIC ENGINE CONTROL SDR ASAA2015101113457Warning Light · false activationLEFT PACK LIGHT ILLUMINATED ON LANDING, CHECK RECALL. ACFT GROUNDED. VERIFIED LT PACK LIGHT ON RECALL, EXTINGUISHED ON RESET. PERFORMED CONTROLLER BITE NR 1 CONTROLLER SHOWED RAM AIR ACTUATOR FAULT. FAULT CLEARED. NO HISTORY 30 DAYS, IAW FIM 21-53/803. OPSDR ASAA2015100513339Actuator · failedRT PACK LIGHT ILLUMINATED ON LANDING CHECKLIST RECALL. LIGHT EXTINGUISHED WITH MASTER CAUTION RESET. ACFT GROUNDED. REMOVED RT RAM AIR ACTUATOR REF AMM 21-51-21-000-801. INSTALLED RT RAM AIR ACTUATOR ACCOMPLISHED GROUND VERIFICATION CHECK PACK/ZONE TEMP NR SDR ASAA2015100313295Warning Message · false activationRIGHT PACK ANNUNCIATOR ILLUMINATED AND EXTINGUISHES WITH MASTER CAUTION RESET. ACFT GROUNDED. PERFORMED BITE ON PACK TEMP CONTROLLERS IAW 21-51-00. READS NR 2 CONTROLLER RAM AIR ACCT. RESET CONTROLLERS REPERFORMED BITE ALL PASS GO. NO HISTORY 30 DAYS. ACFTSDR ASAA2015092913282Bleed Valve · damagedRT BLEED TRIP OFF LIGHT ILLUMINATED IN FLIGHT, RESET TRIP, REILLUMINATED AT CRUISE 1, PSI AT 40, NR 2, PSI AT 10. ACFT GROUNDED. DIVERSION TIME-74 MINUTES. FOUND PRECOOLER VALVE INOPERATIVE. REPLACED PRECOOLER VALVE REF AMM 36-12-02-400-801. OPS CK, GROUSDR ASAA2015092813253Fmc · failedRIGHT FMC FAILED. THEN MAP ON F/O SIDE. SINGLE FMC MESSAGE IN SCRATCH PAD. QRH PROCEDURES FOLLOWED. ACFT GROUNDED. PILOT DOES NOT INDICATE IN DEFECT DESCRIPTION WHETHER OR NOT QRH PROCEDURES REMEDIED RT FMC PROBLEM. FOUND NUMEROUS FAULTS FROM LAST FLIGHT ISDR ASAA2015092813249Lens · detachedEMEGENCY EXIT SIGN COVER, MID-CABIN, FELL OFF. ACFT GROUNDED. RE-INSTALLED EMERGENCY EXIT SIGN COVER IN MID CABIN. OK FOR SERVICE.SDR ASAA2015091913104Warning Message · false activation"FMC DISSAGREE" MESSAGE ON BOTH CDU'S ON GROUND. ACFT GROUNDED. ACCOMPLISHED QRH PROCEDURES NO FURTHER ANOMILIES.SDR ASAA2015091013003Warning Message · false activationFMC DISAGREE ON GROUND. ACFT GROUNDED. AFTER FMC DISAGREE QRH CHECKLIST, FMC DISAGREE MESSAGE NO LONGER DISPLAYED.SDR ASAA2015090712971Warning Message · false activationFMC DISAGREE ON GROUND. ACFT GROUNDED. QRH PROCEDURE FIXED IT.SDR ASAA2015090612959Fault Code · activatedMAINTENANCE MESSAGE 77-21171, N1 SIGNAL IS OUT OF RANGE FOR ENGINE NR 1. THIS IS A LONG TERM FAULT WHICH MUST BE CORRECTED WITHIN 450 FLIGHT HOURS. ACFT GROUNDED. ON DEFERRAL.SDR ASAA2015090412941Warning Message · false activationFMC DISAGREE LIGHT ILLUMINATED DURING TAXI OUT. ACFT GROUNDED. QRH PROCEDURE SUCCESSFULLY RESOLVED THE ISSUE AND CLEARED THE DISAGREEMENT.
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