N563AS
Service difficulty reports · 561
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 = 'N563AS' 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 = 'N563AS' 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 ASAA2018082725888Indicator · inoperativeNR 2 REFUELING PANEL, QTY GAUGE WAS INOPERATIVE. ACFT GROUNDED.SDR ASAA2018082125890Unknown · unknownCAPTAIN`S CDU WENT BLANK DURING CRUISE, MOMENTARILY AND RETURNED TO NORMAL OPS. ACFT GROUNDED. PERFORMED FIM 34-61 TASK 804. OPS CHECK OK.SDR ASAA2018081425765Indicator · intermittentLEFT MAIN TANK REFUEL PANEL QUANTITY INDICATOR WAS INTERMITTENT. ACFT GROUNDED. REPLACED THE FUEL PANEL NR 1 INDICATOR IAW AMM 28-41-61.SDR ASAA2018071225345Transceiver · intermittentNR 2 HF RADIO SHOWS FAIL/FAIL WHEN SELECTED, WHEN THE FREQ. TRANSFER SWITCH IS PUSHED, THE RADIOS WORK NORMALLY, BUT THEN SHOW FAIL. GROUNDED - YES. ACCOMPLISHED FIM TASK 23-11 TASK 801 BITE TEST PASS. PRECAUTIONARY CHANGED HF TRANSCEIVER NR 2 LRU REF AMM 23-SDR ASAA2018070425283Unknown · malfunctionedHGS AIII AND AUTOLAND FAILED. ON LOC CAP, BOTH AUTOPILOTS DISCONNECTED. MOMENTARY FMC DISAGREE ON FO'S SIDE ILLUMINATED. MOMENTARY RA FAIL FLAG AT 5000' / FO'S FD DROPPED OFF. IN THE FLARE USING HGS ONLY, THE FLIGHT PATH CUE DISAPPEARED. GROUNDED - YES. RESET SDR ASAA2018070125266Fitting · detachedR1 DOOR GIRT BAR CLIP, LEFT SIDE IS HALF DETACHED -SWINGS SIDEWAYS WHEN BAR IS NOT CLIPPED IN. GROUNDED - YES. REMOVED SLIDE FROM DOOR, OPENED SLIDE SHROUD TO REMOVE SHEARED FASTENER, REMOVED FASTENER AND INSTALLED NEW, REINSTALLED SLIDE ON R1 DOOR REF SRM 51-SDR ASAA2018062520167Autothrottle Sys · malfunctionedAUTOTHROTTLE WILL NOT ARM. ACFT GROUNDED. ACCOMPLISHED FIM 22-31, TASK 801. NO FAULTS IN CURRENT STATUS OR IN FLIGHT FAULTS. ACCOMPLISHED AUTOTHROTTLE SYSTEM OPS TEST IAW AMM 22-31-00-710-801. OPS CHECKED NORMAL.SDR ASAA2018060862958Bulb · failedTEMPERATURE INDICATION NOT CORRECT FOR THE RIGHT PACK, ALL SUPPLY & PASSENGER TEMPS APPEAR NORMAL. LEFT PACK TEMP WAS NORMAL. ACFT GROUNDED. REMOVED AND REPLACED THE PACK TEMPERATURE BULB T489 IAW AMM 21-51-60. OPS CHECKED GOOD.SDR ASAA2018052524817Unknown · malfunctionedON PREFLIGHT FOUND HF NR 2 FAIL LIGHTS ILLUMINATED. GROUNDED - YES. REF FIM 23-11 TASK 801. PERFORMED NR 2 HF SYSTEM BITE. CYCLED BREAKER SYSTEM RESTORED. BITE CHECK OPS NORMAL. NO FAULT FOUND NO HISTORY PAST 30 DAYS. OK TO CONTINUE SERVICE.SDR ASAA2018051424645Indicator · failedFUELER REPORTED THE NR 1 TANK INDICATOR ON REFUEL PANEL HAS A DIGIT BURNT OUT. FLT DECK GAUGE READS NORMAL. ACFT GROUNDED. REMOVED AND REPLACED THE NR 1 TANK REFUEL INDICATOR IAW AMM 28-41-61. OPS CHECKED GOOD.SDR ASAA201805144588Control Valve · faultedLEFT PACK LIGHT ILLUMINATED DURING MASTER CAUTION RECALL. EXTINGUISHED WHEN MASTER CAUTION SYSTEM WAS RESET. ACFT GROUNDED. PERFORMED A NR 1 PZTC BITE IAW AMM 21-51-00. FOUND LEFT PACK TCV FAULT. REMOVED AND REPLACED THE LT TEMP CONTROL VALVE IAW AMM 21-SDR ASAA2018041924293Connector · dirtyDIAGNOSTICS REPORTED THE NR 1 ENGINE TREND DATA SHOWS A SHIFT IN EGT HOT DAY MARGIN ALL OTHER PARAMETERS NORMAL. EGT INDICATION ERRORS ARE SUSPECT PRI 2 ETOPS SIGNIFICANT SYSTEM. ACFT GROUNDED. ACCOMPLISHED EGT INDICATION SYSTEM TROUBLESHOOTING AND CONNECTSDR ASAA2020021143142Vane · crackedREPEAT BOROSCOPE INSPECTION ON #1 ENGINE WITH ONE LPT STAGE 1 NOZZLE VANE WITH FULL CRACK AND MISSING MATERIAL LESS THAN .039 SQ IN AT 3 O'CLOCK ALF PER B737-800 AMM 72-00-00-200-811-F00 FOUND RADIAL CRACKS FROM HOLE HAS PROGRESS, BUT REMAINS IN LIMITS. BURNEDSDR ASAA2018011823202Warning Light · false activationDURING CLIMB OUT, LEFT PACK ILLUMINATED, COMPLIED WITH QRH, TURNED LEFT PACK SWITCH TO OFF, CLOSED ISOLATION VALVE. PRESSURIZATION NORMAL AT CRUISE. ACFT GROUNDED. VERBAL FROM CREW LEFT PACK WOULD NOT RESET LIGHT ILLUMINATED WITH NO ASSOCIATED PACK OR M/CSDR ASAA2018010623106Transfer Valve · malfunctionedFUEL IMBALANCE. ACFT GROUNDED. ACCOMPLISHED CROSSFEED VALVE ALIGNMENT IAW AMM 28-22-21-820-801. REMOVED AND REPLACED THE ENGINE FUEL CROSSFEED VALVE BODY IAW AMM 28-22-21-000-803, AND AMM 28-22-21-400-803. COMPLETED ALL OPS AND LEAK CHECKS. NO UNWANTED FUELSDR ASAA2017121422902Control Panel · faulted"DISCHARGE" LIGHT ON CARGO FIRE PANEL CAME ON AND OFF IN FLIGHT. GROUNDED - YES. REMOVED, REPLACED CARGO FIRE CONTROL PANEL PER B737-800 AMM 26-00-02-400-801 OPS NML PER AMM 26-23-00-730-802. REMOVED & REPLACED CARGO FIRE BOTTLE #1 REF ASA T/C 78226001. OPS CHSDR ASAA2017121222883Warning Light · illuminatedON PREFLIGHT NOTED DISCHARGE LIGHT ON CARGO FIRE PANEL. GROUNDED - YES. VERIFIED DISCHARGE LIGHT ILLUMINATED, WENT OUT ON ITS OWN WITH - NO - ACTION BY FLIGHT CREW. REMOVED #1 & #2 CARGO FIRE BOTTLES PER TASK CARD # 78226001. INSTALLED #1 & #2 CARGO FIRE BOTTLSDR ASAA2017112822740Exciter · failedAPU FAULT LIGHT ILLUMINATED DURING APU START. APU DID NOT START. GROUNDED - YES. VERIFIED APU WILL NOT ACCELERATE PAST 12% DURING START. REMOVED & REPLACED APU IGNITION EXCITER. OPS CHECK NORMAL, REF B737-800 FIM 49-40 TASK 805 & AMM 49-41-31-000-801, 49-41-31SDR ASAA2017112222672Sensor · dirtyTHE CONTROL CABIN TEMPERATURE SELECTOR ON THE AIR CONDITIONING PANEL DOES NOT FUNCTION PROPERLY. WHEN POSITIONED TO FULL WARM OR OFF THE FLIGHT DECK IS ESTIMATED TO BE 50 DEG F OR LESS. THIS CONDITION BECAME NOTICEABLE 4 HOURS INTO FLIGHT AT 36,000 FT AND OUTSSDR ASAA2017100122091Fmc · malfunctionedNR 1 FMC FAILED AFTER LANDING, REBOOTED AFTER ONE MINUTE. ACFT GROUNDED. NO HISTORY LAST 30 DAYS. PERFORMED FIM 34-61, TASK 836, & FMC OPS CHECKED GOOD. GROUND FUNCTIONAL TEST PASSED.SDR ASAA2017092322020Actuator · leakingDURING A LEAK CHECK FOR T/C 78472040, FUEL WAS LEAKING OUT OF THE NR 1 ENGINE RIGHT VSV DRAIN. ACFT GROUNDED. REMOVED AND REPLACED RT VSV ACTUATOR IAW AMM 75-31-01-400-802-F00. ACTUATOR LEAK TEST PERFORMED IAW AMM 75-31-01-790-801-F00.SDR ASAA2017082321702Terminal · brokenNR 2 FIRE BOTTLE DISCHARGE HANDLE WILL NOT LIGHT UP DURING TEST. ACFT GROUNDED. REPLACED CORE FIRE LOOP HARNESS MW326 DUE TO BROKEN TERMINALS TO RIGHT CORE FIRE DETECT ASSEMBLY. OPS NORMAL IAW AMM 26-11-02.SDR ASAA2017073121502Idg · leakingFOUND THE NR 2 IDG WITH NO OIL VISIBLE IN SIGHT GLASS WINDOW. ACFT GROUNDED. FOUND OIL LEAKING AROUND IDG SEAL ON THE CASE SECTIONS OF IDG, DUE TO EXCESSIVE OIL SERVICING IN HISTORY REMOVED AND REPLACED THE NR 2 IDG ASSY IAW AMM 24-11-11. FOUND NO OIL CONTAMISDR ASAA2017072521461Guide Vane · crackedWHILE ACCOMPLISHING HPT BLADE BOROSCOPE IAW T/C 78472022 ON THE NR 2 ENGINE, FOUND 2 LPT STAGE 1 NOZZLE GUIDE VANES WITH AN AXIAL CRACK .075 INCH, 14 VANE SEGMENTS IN FROM S17, VIEWING CONCAVE SIDE OF LPT VANES. ACFT GROUNDED.SDR ASAA2017071521373Actuator · faultedLEFT PACK RAM DOOR FULL OPEN LIGHT REMAINED ILLUMINATED IN CRUISE AT FL380. ACFT GROUNDED. PERFORMED PACK/ZONE TEMP CONTROL NR 1 BITE IAW FIM 21-62 TASK 801. TEST SHOWED FAULT FOR RAM AIR ACTUATOR AND FAULT FOR RAM AIR SENSOR. FOR THE RAM AIR ACTUATOR FAULSDR ASAA2017071321372Actuator · faultedON RECALL NR 1 PACK LIGHT ILLUMINATED RESETS WITH CAUTION LIGHT RESET. ACFT GROUNDED. REVERSED CONFIGURATION CHANGE FOR MEL 21-5C AND PERFORMED PACK/ZONE TEMP CONTROL 1 BITE IAW FIM 21-62, TASK 801. VERIFY TEST SHOWED FAULT FOR RAM AIR ACTUATOR AND FAULT FORSDR ASAA2017071121335Warning Message · intermittentLEFT PACK LIGHT ILLUMINATED ON RECALL, RESETS WITH MASTER CAUTION RESET. ACFT GROUNDED. LEFT PACK/ZONE TEMP CONTROLLER BITE SHOWED NO CURRENT FAULTS, BUT PREV FLT SHOWED FAULT FOR LEFT PACK RAM AIR TEMP SENSOR. VERIFY TEST DID NOT CONFIRM FAULT. DUE TO HISTORSDR ASAA2017070721309Hose · severedEXCESSIVE AIR NOISE IN COCKPIT AT HIGH POWER SETTINGS. COCKPIT TO ATC AND PILOT TO PILOT COMMUNICATIONS WERE AFFECTED. ACFT GROUNDED. DIVERTED, RAN ENGINES AT HIGH POWER SETTINGS IAW AMM 71-00-00, NO AIR NOISE NOTED. ACCOMPLISHED ON TSR 818575. FOUND Y HOSSDR ASAA2017070521283Warning Light · illuminatedLEFT PACK LIGHT ILLUMINATED ON RECALL. GOES AWAY DURING RESET. ACFT GROUNDED. OPENSDR ASAA2017070321257Warning Light · false activationLEFT PACK LIGHT ILLUMINATED ON RECALL. GOES OUT WITH MASTER CAUTION RESET. ACFT GROUNDED. PERFORMED PACK/ZONE TEMP CONTROLLER BITE TEST IAW AMM 21-51-00-700-803. NO FAULTS INDICATED.SDR ASAA2017052820887Warning Light · false activationELECTRIC LIGHT ILLUMINATED. ACFT GROUNDED. VERIFIED DEFECT. ACCOMPLISHED FIM 24-31 TASK 801, ALL FAULTS CLEARED. REACCOMPLISHED BITE TEST, NO FAULTS. NO HISTORY PAST 30 DAYS.SDR ASAA2017042421297Bulkhead · crackedRT WHEEL WELL FWD BULKHEAD CRACK NOTED BELOW CEILING PANEL AT RBL 43. GROUNDED - YES. REPAIRED WING CENTER SECTION REAR SPAR VERTICAL PRESSURE DECK WEB AT BS 663, RBL 25 - RBL 48 IAW SRM 57-10-10-2R-3 REPAIR 3 ALTERNATIVE 2. WORK ACCOMPLISHED ON TASK CARD 7675SDR ASAA2017031520182Window · malfunctionedACARS AND VERBAL FROM CAPTAIN`S R1 WINDOW HEAT, ON LEFT THIRD. INOPERATIVE DURING CRUISE AND ICED UP. RIGHT 2/3 WINDOW HEAT FEELS NORMAL. ACFT GROUNDED. ACCOMPLISHED WINDOW HEAT SYSTEM OPERATIONAL TEST IAW AMM 30-41-00-710-801, R1 WINDOW OPERATED NORMAL. ACCSDR ASAA2017022819967Actuator · faultedDURING DESCENT RECALL CHECK, MASTER CAUTION, AIR CONDITIONER, RT PACK LIGHT ILLUMINATED. RESET AND ALL LIGHTS EXTINGUISHED. ACFT GROUNDED. PERFORMED NR 2 PACK ZONE TEMP CONTROL BITE IAW AMM 21-61-00. FOUND RT RAM AIR DOOR ACTUATOR FAULTED IN CURRENT HISTORYSDR ASAA2017022419920Warning Light · false activationRT PACK LIGHT ILLUMINATED ON RECALL. GOES OUT WITH MC RESET. GROUNDED - YES. PERFORMED CONTROLLER BITE IAW FIM 21-62 TASK 801. FAULT ON NR 2 RAM AIR ACTUATORON BITE, UNABLE TO VERIFY.SDR ASAA2017011319377Nut Plate · brokenLT FWD OVERWING EMERGENCY EXIT LIGHT LENS COVER HAS 2EA SPINNING FASTENERS. NUTPLATES ARE BROKEN. ACFT GROUNDED. REPAIRED IAW AMM 33-51-04-960-802 PARAGRAPH F(3) THROUGH (9). COMPLETED STEP F(10) THROUGH G(1). LIGHT OPS TEST GOOD, IAW AMM 33-61-04.SDR ASAA2017011219383Starter Gen · failedAPU GENERATOR NO FREQ OR VOLTS-GENERATOR FAILED. GROUNDED - YES. REMOVED AND REPLACED APU STARTER GENERATOR, REF AMM 49-41-21. OPS TEST GOOD, BITE TEST NO FAULTS FOUND. THIS CLEARS MEL 49-1B.SDR ASAA2017011219353Door · damagedRT RAM AIR INLET ACTUATOR DEFLECTOR DOOR SPONGY. ACFT GROUNDED. PERFORMED BITE TEST AMM TASK 21-61-00-700-806-002, NO DEFECTS NOTED. DEFLECTOR DOOR OPS NORMAL AND SECURE IN DEPLOYED POSITION. OK FOR CONTINUED SERVICE.SDR ASAA2017010619259Compensator · no testDURING ACCOMPLISHMENT OF TASK CARD NG-28FCD-18088-1. FOUND A TOTAL SEVEN BAD FUEL PROBES, F15, F1, F2, F3, F7, F8 AND F10. ACFT GROUNDED. NR 1 TANK IS SUMPED AND NR 1 BUSSING PLUG IS DISCONNECTED. REPLACED THE NR 1 TANK COMPENSATOR F15 AND PROBES F1, F2, SDR ASAA2017010619258Probe · no testDURING ACCOMPLISHMENT OF TASK CARD NG-28FCD-18090-1. FUEL QTY INDICATION SYSTEM NR 2 TANK AND COMPENSATOR UNITS TESTING. FOUND SIX FUEL PROBES OUT OF TOLERANCE F1, F2, F3, F4, F6 AND F8. ACFT GROUNDED. 2 TANK IS SUMPED AND NR 2 BUSSING PLUG IS DISCONNECTESDR ASAA2017010419244Probe · failedAT PUSHBACK, FUEL TANKS READ LEFT 8.5, RIGHT 8.6, CENTER 25.9. DURING CRUISE, MAIN TANKS SLOWLY DECREASED TO LEFT 7.93, RIGHT 8.17 BY THE TIME THE CENTER TANK REACHED ZERO. OUTSIDE TEMP -64C. FUEL TEMP GOT TO -30C. ACFT GROUNDED. ACCOMPLISHED TASK CARDS NG-SDR ASAA2017010319240Lens · damagedEMERGENCY LIGHT EXIT LOCATOR SIGN AT RIGHT FORWARD OVERWING EXIT HAS DAMAGED LENS. GROUNDED - YES. REMOVED AND REPLACED LENS AND TESTED LIGHT ASSEMBLY PER AMM 33-51-01-960-801 - OPS NORMAL.SDR ASAA2016122219127Warning Light · false activationRIGHT PACK ANNUNICATED ON RECALL. EXTINGUISHED WHEN SYSTEM WAS RESET. ACFT GROUNDED. PERFORMED CONTROLLER BITE IAW FIM 21-62 TASK 801. FAULT ON RAM AIR ACTUATOR NR 2, UNABLE TO VERIFY, CLEARED AND RETESTED, NO FAULTS. INTERMITTENT, OK FOR SERVICE,SDR ASAA2016112318815Indicator · failedNR 1 FUEL INDICATOR IN WING FUELING PANEL INOP. GROUNDED - YES. REMOVED AND REPLACED NR 1 REFUEL QTY INDICATOR IAW AMM 28-41-61. INDICATORS OPS TESTED GOOD. FQIS BITE GND TESTED GOOD. REMOVED MEL 28-12B.SDR ASAA2016112218821Fmc · malfunctionedIN CRUISE THE LEFT FMC FAILED BRIEFLY THEN RECOVERED AUTOMATICALLY WITHOUT ANY PILOT INPUT. DURING THE INTERMITTENT FAILURE, THE FOLLOWING INDICATIONS WERE OBSERVED. THE FMC ALERT LIGHT ILLUMINATED, THE MENU PAGE APPEARED ON BOTH CDU'S, VTK APPEARED ON THE LEFSDR ASAA2016102018450Seal · out of positionON TAKE OFF RIGHT AFTER GEAR RETRACTION, FORWARD FLIGHT ATTENDANTS REPORTED L1 DOOR HAD A GAP WITH A LOT OF WIND NOISE, FLIGHT ATTENDANTS REPORTED SEEING DAYLIGHT. ACFT GROUNDED. AIR TURNBACK, FOUND LOWER ENTRY DOOR FLAPPER SEAL NOT SEATED PROPERLY TO L-1 DOOSDR ASAA2016101818393Warning Light · false activationAFTER TWO ENGINE STARTS, RECALL DISPLAYED ELEC ON OVERHEAD PANEL. RAN QRH, RETURNED TO GATE. ACFT GROUNDED. COMPLIED WITH FIM TASK 24-34 TASK 802. RAN BOTH ENGINES. BITE PROCEDURE FIM 24-31 TASK 801 PASSES. OPS CHECKED NORMAL.SDR ASAA2016101318336Autoland Sys · malfunctionedUNSUCCESFUL AUTOLAND. JUST PRIOR TO FLARE, RECEIVED A APPROACH WARNING WITH ROLLOUT CAUTION. TOWER CONFIRMED THE APPROACH AREA WAS PROTECTED. ACFT GROUNDED. PERFORMED LANDING DFCS BITE GROUP 20 FAULT REVIEW IAW FIM 22-11 TASK 801, NO FAULTS AND NO CURRENT FASDR ASAA2016100918249Fmc · malfunctionedDUAL FMC FAILURE DURING CRUISE. BOTH FMCS RESTORED THEMSELVES WITHIN TWO MINUTES. ACFT GROUNDED. PERFORMED FIM TASK 34-61 TASK 801. NO ACTIVE FAULTS NOTED. OPS CHECKED GOOD PER SAME.SDR ASAA2016091818064Intercostal · damagedFLOOR SUPPORT ANGLES BETWEEN STA 312 TO STA 294, BL 12L, LAV ANCHOR, TOP SURFACE HAS SCRIBE LINE FORWARD OF MOUNT. ACFT GROUNDED. R & R 141A569041 FLOOR SUPPORT INTERCOSTAL BETWEEN BS 294-BS 312, LBL12 IAW SRM 51-40-02 AND BAC DWG 141A5600, REV N. REMOVED AN
Back to N563AS