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 ASAA2013040894398Valve · intermittentFUEL CROSSFEED VALVE LIGHT ILLUMINATED INTERMITTENTLY DURING FLIGHT WITHOUT SELECTING THE OPEN POSITION. WHEN THE LIGHT IS ILLUMINATED, IT IS IN THE BRIGHT MODE. LIGHT CYCLES FROM BRIGHT TO OFF THROUGHOUT THE FLIGHT. ACFT GROUNDED. INBOUND CREW REPORTS FUELSDR ASAA2013032394238Control Module · inoperativeON THE PRESSURIZATION CONTROL PANEL,THE FLIGHT ALTITUDE DISPLAY IS INOPERATIVE, ONLY RANDOM LINE SEGMENTS ARE ILLUMINATED. R & R CABIN PRESSURE CONTROL MODULE REF 21-31-02-400-801, OPS CK OK, GROUND VERIFICATION CK OK.SDR ASAA2013032294249Satcom · malfunctionedSATCOM, THERE IS NO SAT PROMPT AVAILABLE AT 4L ON THE MCDU. ACCOMPLISHED SATCOM COMMUNICATION SYS TEST IAW AMM TASK 23-15-00-730-801. VERIFIED OUTGOING CALL AND INCOMING CALL VOICE TEST GOOD WITH DISPATCH-A IN DIRECTORY.SDR ASAA2013031994202Valve · failedENGINE ANTI ICE NR 1 COWL VALVE OPEN LIGHT REMAIN BRIGHT BLUE. WHEN SELECTED TO ON. SELECTION AT FL260, BRIGHT BLUE, DURING DESCENT WENT DIM AT FL180. AT 10000 FT WENT BRIGHT AGAIN WHILE IN CLOUDS. REMAINED BRIGHT BLUE UNTIL LANDING. REPLACED NR 1 ENG TAI VASDR ASAA2013031494175Control Valve · faultedLT PACK LIGHT ILLUM AFTER START DURING SYS RECALL. ACFT GROUNDED. REPLACED LT PACK TEMP CONTROL VALVE REF MM 21-51-10. OP CHECK GOOD. BITE CHECKED LT PACK TO VERIFY FAULT CLEARED REF MM 21-61-00 BITE CHECK GOOD. RESET PACK CONTROLLER, OK FOR SERVICE.SDR ASAA2013030394082Unknown · unknownSATCOMM PROMPT IS NOT AVAILABLE IN THE MCDU. ACFT GROUNDED. UNABLE TO DUPLICATE DEFECT, ALL LIGHTS WERE GREEN. R & R SATCOM TRANSCEIVER, REF MM 23-15-00, OPS CHECK NORMAL.SDR ASAA2013030194032Satcom · malfunctionedNO SATCOM PROMPT ON MCDU MENU PAGE. SATCOM PROMPT ON MCDU ILLUMINATED AFTER TRANSCEIVER FROM EXTERNAL POWER TO APU ELECT POWER SATCOM, OPS NORMAL IAW 23-15-00-730-801. GROUND VERIFICATION TEST SUCCESSFUL.SDR ASAA2013022694008Actuator · leakingON PDC WALKAROUND, FOUND FUEL LEAKING UNDER NR 2 ENGINE. REMOVED NR 2 VSV ACTUATOR IAW MM 75-31-01-00-8025. A-F. INSTALLED NR 2 ENG VSV ACTUATOR IAW AMM 75-31-01-400 LEAK AND ACTUATORS TEST GOOD IAW AMM 71-00-00-700.SDR ASAA2013010993645Warning Light · false activationFMC DISAGREE ILLUMINATED DURING TAXI. CLEARED IAW QRH PROCEDURE.SDR ASAA2013010593611Warning Light · intermittentWHEN PRESSING MASTER RECALL, LT PACK LIGHT ILLUMINATES. WHEN PRESSED AGAIN, PACK LIGHT EXTINGUISHES, REF CHECKLIST. PERFORMED PACK ZONE TEMP CONTROLLER BITE REF MM 21-62, TASK 801. BITE CHECKED OK. RAN LT PACK THEN REACCOMPLISHED BITE, BITE PASSES, INTERMITTSDR ASAA2012122893574Ignition Unit · faultedDURING MX TROUBLESHOOTING, CSS FAILED, FAULT LIGHT. FOUND FAULT CODE 49-41011. NO FLAME SHUTDOWN. MADE 2 START ATTEMPTS WITH NO EGT RISE NOTED, FAULT LT ILLUM AND FAULT CODE 349-41011. LATCHED ON EACH ATTEMPT. ACCOMP. FIM TASK 49-40, TASK 802, FOR MAINT. SDR ASAA2012122493535Shutoff Valve · failedLEFT DUCT PRESSURE BELOW 18 PSI (AT 16PSI) WITH IDLE POWER DURING HIGH STAGE CROSSOVER CHK. ACFT GROUNDED. R & R NR 1 ENG PRSOV AND LEAK AND OPS CHECKED GOOD IAW MM 36-11-04 ACP ENG BLEED AIR CROSSOVER OPS TEST IAW MM 36-11-00 TEST GOOD.SDR ASAA2012120693543Floorbeam · corrodedMAIN CABIN, TOPSIDE OF FLOORBEAM CORRODED AT BS 312, RBL 12. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW REO-G15772, REV B. PERFORMED FPI ON NEW UPPER CHORD IAW SOPM 20-20-02, ACCOMPLISHED HFEC INSPECTION OF CUTOUT IAW SRM 53-10-51 AND 737 NDT MASDR ASAA2012120693478Floor Panel · corrodedMAIN CABIN, FLOOR STRUCTURE CORRODED ON TOP AT BS 322, LBL. 12. GROUNDED. REMOVED FLOOR PANEL IAW SRM 51-40-02. LOCATED AND DRILLED NEW FLOOR PANEL IAW SRM 51-40-02 AND DWG 141A5410. REV -. INSTALLED NEW FLOOR PANEL IAW SRM 51-40-02.SDR ASAA2012120693477Intercostal · crackedMAIN CABIN INTERCOSTAL AT BS 394 AND BL 0 IS CRACKED AT FASTENER HOLE. ACFT GROUNDED. R & R INTERCOSTAL UPPER ANGLE AT BS 394, BL 0 IAW SRM 51-40-02.SDR ASAA2012120693476Intercostal · crackedMAIN CABIN INTERCOSTAL AT BS 394 AND RBL 10 IS CRACKED AT FASTENER HOLE. R & R INTERCOSTAL UPPER ANGLE BS 394RBL10 IAW SRM 51-40-02.SDR ASAA2012120693475Floor Panel · corrodedMAIN CABIN, FLOOR STRUCTURE CORRODED ON TOP AT BS 340 LBL 12. REMOVED OLD PANEL BREAK IAW SRM 51-40-02. LOCATED AND DRILLED NEW PANEL BREAK IAW SRM 51-40-02 AND DWG 141A5410, REV -INSTALLED NEW PANEL BREAK IAW SRM 51-40-02.SDR ASAA2012120293567Windshield · crackedR1 WINDOW REMOVED DUE TO SCRATCHES AND FOUND LOWER WINDSHIELD GLASS CRACKED ADJACENT TO FASTENER LOCATIONS. R & R R-1 WINDOW ASSY IAW MM 56-11-11-400-801. LEAK AND OPS CHECKED GOOD.SDR ASAA2012111193269Warning Light · false activationAUTO FAIL AND ALTERNATE ILLUMINATED ON PRESSURIZATION CONTROL PANEL. PERFORMED DCPC BITE REF FIM 21-31, TASK 801. NO EXISTING FAULTS DCPC 1 AND 2. DCPC 2 SHOWS FAULT HISTORY LEG 00 FC 001. INITIAL EVAL NO EXISTING FAULTS (TASK 804). NO HISTORY 30 DAYS. AUTOSDR ASAA2012110193226Unknown · unknownWHEN RT ENGINE ANTI-ICE IS TURNED ON, COWL VALVE OPEN LIGHT COMES ON, THEN AFTER A FEW SECONDS FLICKER BETWEEN BRIGHT TO DIM OR STEADY BRIGHT. THIS TAI INDICATES GREEN. PERFORMED GROUND VERIFICATION OPS TEST 30-21-00-710-801. ALL TESTS SUCCESSFUL. ACFT GOSDR ASAA2012103093215Indicator · activatedNR 1 ENG IDG DPI EXTENDED. VERIFIED NR 1 ENG IDG DPI EXTENDED THIRD EXTENSION DECAL REFLECTS THE SAME. R & R FILTERS AND OIL, CHECKED GOOD IAW FIM TASK 24-11-803 LEAK CHECKED GOOD IAW AMM 24-11-00-700-802.SDR ASAA2012100493016Warning Light · false activationON RECALL, LT PACK LIGHT ILLUMINATED. BITE SHOWS TEMP CONTROL VALVE FAULT ON NR 1 ZONE TEMP CONTROLLER. RAN BITE REF AMM 2-61-00, FAULT CLEARS AND OPS NORMAL.SDR ASAA2012092292925Drive Unit · failedON TAXI OUT TURNED WEATHER RADAR TO WX-T. PWS AND WEATHER RADAR INOPERATIVE. OPS TEST IAW MM TASK 34-43-00-710-802-001 SHOWS PWS AND WEAHTER RADAR INOPERATIVE FAULTING ANTENNA. R & R WEATHER RADAR ANTENNA DRIVE UNIT IAW MM 34-43-11-000-802. OPS TEST NORMAL ISDR ASAA2012091192869Hose · leakingDURING REMOVAL AND REPLACEMENT OF (TIME CHANGE UNIT) NR 2 ENG PRECOOLER CONTROL VALVE FAILED INSTALLATION TEST IAW AMM 36-12-02 (PART G) VALVE IS OPENING HALFWAY. ACFT GROUNDED. PERFORMED LEAK CHECK OF NR 2 ENG BLEED AIR SYS SENSE LINES IAW AMM 36-11-00. FSDR ASAA2012080892682Antenna · failedAFTER POWER UP, GRINDING NOISE HEARD FROM NOSE CONE AREA. WEATHER RADAR FAIL RT AND PWS FAIL MESSAGES SHOWN ON ND DISPLAY. ACFT GROUNDED. CONFIRMED WEATHER RADAR FAIL RT AND PWS FAIL MESSAGE ON ND. REPLACED WEATHER RADAR ANTENNA FLAT PLATE IAW 34-43-11-000SDR ASAA2012082092754Computer · malfunctionedON TAXI OUT, FMC DISAGREE MESSAGE. ACFT GROUNDED. CYCLED FMCS COMPUTER NR1 CB AND FMCS COMPUTER NR2 CB, IAW QRH 11.2- OPS CHECK NORMAL.SDR ASAA2012072492598Transceiver · failedDURING CRUISE FLIGHT WHILE USING RADAR GOT AMBER WEATHER RADAR FAIL WARNING ON NAV DISPLAY. SHUT RADAR OFF. WEATHER RADAR SYSTEM TEST PASSED. R & R WEATHER RADAR TRANSCEIVER IAW MM 34-43-41, GROUND VERIFICATION TEST PASSED.SDR ASAA2012072292582Transceiver · dirtyON DESCENT, TURNED WEATHER RADAR ON, WX FAIL APPEARED ON MFD. TURNED OFF THEN ON RECEIVED WEATHER RADAR FAIL & NO PWS, TURNED OFF AND AS EXPECTED NO PWS REAPPEARED BELOW 1600. ACFT GROUNDED. ACCOMPLISHED GVI OF WEATHER RADAR TRANSCEIVER, FOUND TO COVERED INSDR ASAA2012071992567Filter · cloggedFOUND NR 1 ENGINE IDG DPI POPPED DURING S/C. ACFT GROUNDED. PERFORMED FIM TASK 24-11-00-810-803. REPLACED FILTER AND RESET DPI. DPI DIDN`T POP AGAIN. THIS WAS THE FIRST TIME POPPED AND WAS MARKED ACCORDINGLY ON DECAL.SDR ASAA2012071992564Controller · malfunctionedON PREFLIGHT, FOUND AUTO FAIL ILLUMINATED WITH SWITCH IN AUTO MANUAL LIGHT WAS ALSO ILLUMINATED. GROUNDED ACFT. FOUND CABIN PRESSURE CONTROL FAULT TO BE A RECOVERABLE FAULT REF MEL 21-14C.SDR ASAA2012061892375Fmc · failedNR 2 FMC SINGLE OPS, F/OS PFD HAS VTK AND MAP FLAGS. ACFT GROUNDED. REMOVED NR 2 FMCS COMPUTER IAW AMM 34-61-02-000-801. INSTALLED NR 2 FMCS COMPUTER IAW AMM 34-61-02-400-801. LOADED SOFTWARE INTO LT AND RT FMCS COMPUTERS IAW 34-61-00-470-805. PERFORMED SSDR ASAA2012061792358Seal · unbondedNR 1 ENGINE, PLATFORM AT BLADE NR 4 HAS ELASTOMER SEAL UNBONDED. ACFT GROUNDED. R & R NR 4 & NR 16 BLADE PLATFORM IAW T/C 78472002, STEP 46. C/W ENG NR 1, TEST 7, VIBRATION SURVEY IAW T/C 78472002, STEP 53. VIBRATION SURVEY WITHIN LIMITS.SDR ASAA2012061792357Shim · wornNR 1 ENGINE FAN BLADE SHIMS WORN, ACFT GROUNDED. R & R NR 1 ENG FAN BLADE SHIMS, REF T/C 78472002, STEP 44.SDR ASAA12511614Seal · missingWHILE PERFORMING FAN BLADE LUBE TASK CARD 78472002. FOUND NR 16 PLATFORM MISSING RUBBER SEALS. ACFT GROUNDED. R & R NR 16 PLATFORM IAW TASK CARD NR 7847002. NR 2 ENG REQUIRES TEST 7. VIBRATION SUEVEY REF AMM 71-00-00, PB 501. COMPLETED NR 2 ENG ENGINE RUNSDR ASAA12511613Control Panel · arcedDURING SERVICE CHECK, FOUND MCP VERTICAL SPEED LCD WINDOW HAS A WHITE ARC DISPLAY. ACFT GROUNDED. R & R DFCS MCP REF AMM TASK 22-11-34/401. ACCOMPLISHED DFCS LRU INTERFACE MCP TEST GP32 REF AMM TASK 22-11-34/501 AND LAND VERIFY TEST GP49 REF AMM TASK 22-11-SDR ASAA12511543Position Switch · faultedDURING ACCOMPLISHEMENT OF APU INTERROGATION, CURRENT STATUS FAULTED 49-15218, INLET DOOR DID NOT CLOSE. ACFT GROUNDED. R & R AIR INLET DOOR POSITION SWITCH IAW AMM TASK 49-15-41-000-801 AND 49-15-41-400-801.SDR ASAA1251528Filter · cloggedF/A REPORTS ABOUT CABIN TEMPERATURE, SUGGEST THAT "FWD CABIN" AND "AFT CABIN" CONTROL KNOBS ARE PRODUCING ERRATIC SUPPLY TEMPS THAT ARE INCONSISTENT WITH KNOB POSITION. FOR INSTANCE "FWD CAB" AT 11 O'CLOCK PRODUCES 20 DEG SUPPLY TEMP CONT FROM FLIGHT DECK DIFSDR ASAA12511431Actuator · failedAIR CONDITIONER ON RECALL AND "PACK" LT ILLUMINATED. EXTINGUISH ON RESET. GROUNDED, YES. PERFORMED BITE TEST TO VERIFY THE FAULT. FOUND RAM AIR ACTUATOR TO BE INOPERATIVE. R & R LT RAM AIR ACTUATOR IAW AMM 21 51 21. PERFORMED BITE CHECK IAW AMM 21 51 21. CHSDR ASAA12511369Warning Light · illuminatedON LANDING RECALL "AIR COND" LIGHT ILLUMINATED WITH LEFT PACK LIGHT. LEFT PACK LT WENT OUT DURING RESET. RAN PACK / ZONE TEMP CONTROLLER BITE FOR NR 2 PACK. OPS CHECKED GOOD. INITIALLY THE "RAM AIR ACT" IS WHAT FAULTED BUT AFTER RESET AND TESTING SEVERAL SDR ASAA12511125Warning Light · illuminated"FMC DISAGREE" ANNUNCIATION ILLUMINATED ON TAXI OUT. ACCOMPLISHED QRH PROCEDURE. ANNUNCIATOR REMAINED OFF.SDR ASAA12511120Warning Light · false activationRT PACK LIGHT ILLUMINATED AFTER START RESETS WITH MASTER CAUTION. REMOVED AND REPLACED RT PACK TEMPERATURE CONTROL VALVE. TEMP CONTROLLER BITE TEST COMPLIED WITH. CHECKED GOOD, NO FAULTS IAW AMM 21-51-10-000-801.SDR ASAA12511119Warning Light · false activationRT PACK LIGHT ILLUMINATES ON MASTER CAUTION RECALL. THE LIGHT GOES ON MASTER CAUTION RESET. ACCOMPLISHED BITE ON NR 2 PACK ZONE TEMP CONT PER FIM TASK 21-62-00, OPS CHECKED NORMAL. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2012021411108Warning Light · false activationON PRESSING RECALL AT EEP. FOR A SYSTEMS CHECK, THE RIGHT PACK AMBER LIGHT ILLUMINATED ON OVERHEAD PER DIRECTION OF QRH. LIGHT EXTINGUISHED ON MASTER CAUTION CLEAR. PER QRH NO FURTHER ACTION REQUIRED. PERFORMED PACK/ZONE TEMP CONTROLLER BITE TEST FOR RT PASDR ASAA12510989Unknown · malfunctionedRIGHT PACK COMES ON WHEN RECALL IS PUSHED GOES OUT WHEN RESET IS PUSHED. PERFORMED BITE CHECK ON NR 1 & NR 2 PACK ZONE TEMP CONTROLLERS PER FIM TASK 21 62 00 810 801 NR 2 PACK ZONE CONTROLLER HAD A PACK SENSOR FAULT RESET FAULT PER SAME REFERENCE. PERFORMED SDR ASAA11510860Drain Mast · crackedAPUR SHROUD AND HYD DRAIN MAST AFT OF LT W/W APPEARS CRACKED AT THE BASE ON THE T/E. VERFIED CRACK USING HFEC 2.0 IN ON OTBD SIDE AND 3.0 IN ON INBD SIDE PER BOEING NDT MANUAL 51 00 00 FIG 23 PART 6. REPLACED APU FUEL FEED LINE SHROUD DRAIN MAST REF MM 25 25SDR ASAA11510669Apu · making metalAPU WILL NOT START FAULT LIGHT ILLUMINATED. DURING T/S OF APU FAULT FOUND THE MAGNETIC DRAIN PLUG COVERED WITH MAGNETIC SILVER COLORED PARTICLES. IAW FIM TASK 49 91 81 200 801 APU REPLACEMENT IS REQUIRED. APU CHANGE COMPLETED. NO DEFECTS NOTED.SDR ASAA1150640Unknown · malfunctionedON TAXI GOT FMC DISAGREE WARNING. ACCOMPLISHED QRH PROCEDURE. OPS CHECK NORMAL.SDR ASAA11510479Battery Pack · dischargedWHILE PERFORMING MAINT IAW TC 78233001 BATTERY PACK AND POWER SUPPLY AT M1675 PERFORMED UN SAT. REPLACED BATTERY PACK AND POWER SUPPLY AT M1675 TESTS GOOD. REF AMM 33 51 06.SDR ASAA11510476Unknown · malfunctioned"SINGLE FMC OPERATION" MSG DISPLAYED ON BOTH FMC'S. FMC RETURNED TO NORMAL AFTER PWR SWITCHING. OPS NORMAL.SDR ASAA11510452Power Unit · faultyDURING APU START ON EXT PWR O/BS'D BATTERY DISCHARGE LT "ON". VIS INSP'D START CONVERTER & START POWER UNITS IN E & E. OBS'D APU START CONV UNIT C/B ON P91 115VAC TRANSFER BUS 1 OUT (A 11). REPLACED START POWER UNIT MM 49 41 71 000 801 & 400 801. APU START
Back to N563AS