N557AS
Service difficulty reports · 525
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 = 'N557AS' 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 = 'N557AS' 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 ASAA2019080863335Pump · failedNR 2 ENGINE HYD PUMP LOW PRESSURE ILLUMINATED DURING CRUISE. RAN QRH, TURNED OFF PUMP. B SYSTEM QUANITY 85% PRESSURE 3020. GROUNDED - YES. FOUND THE NR 2 ENGINE EDP FAILED. REMOVED AND REPLACED THE PUMP IAW AMM 29-11-11.SDR ASAA2019080230273Autopilot Sys · malfunctionedWHILE ATTEMPTING A HGS AIII AUTOLAND, AUTOPILOT DISCONNECTED AT ABOUT 2100' MSL AND ABOUT 6 MILES ON FINAL APPROACH. AMBER "NO AIII" ILLUMINATED FOR ABOUT FIVE SECONDS SHORTLY BEFORE THE DISCONNECT BUT HAD RETURNED TO GREEN "AIII" . NEVER GOT AN "APCH WARN". GSDR ASAA2019070729945Blower · inoperativeWEATHER RADAR R/T FAN IS INOP. GROUNDED - YES. REMOVED WEATHER RADAR R/T MOUNT BLOWER REF AMM 34-43-51-000-801. INSTALLED NEW BLOWER REF AMM 34-43-51-400-801. REMOVED AND REINSTALLED WEATHER RADAR R/T REF AMM 34-43-41-000-801 AND 34-43-41-400-801. C/W OPS TESTSDR ASAA2019062429800Plug · missingON DEPARTURE FROM SEATTLE THE LEFT DUCT PRESSURE INDICATED 80 PSI AND RIGHT DUCT PRESSURE INDICATED 42 PSI. CONSULTED WITH FODO AND MAINT CONTROL VIA SAT BECAUSE AT LIMITATION EXCEEDANCE. DURING CLIMBOUT TO FLT 370 LEFT DUCT STARTED TO DROP AND ONCE LEVELING ASDR ASAA2019051829371Warning System · false activationAUTO FAIL AND ALTN LIGHTS ON ON PRESSURIZATION PANEL. GROUNDED - YES. PERFORMED RESET PER FIM 21-31-00-810-827, OPS CHECK GOOD, AUTO FAIL AND ALTN LIGHT EXTINGUISHED, NO DEFECTS NOTED.SDR ASAA2019042729188Pressure Switch · failed#1 COWL ANTI-ICE CAUTION LIGHT ON PRIOR TO TAKEOFF. GROUNDED - YES. REMOVED AND REPLACED ENG #1 ENG COWL TAI VALVE PER B737-800 AMM 30-21-11. REPLACED ENGINE #1 ANTI-ICE PRESSURE SWITCH PER AMM 30-21-21. SYSTEM OPS CHECK NORMAL. ETOPS GROUND VERIFICATION IS SUSDR ASAA201904229084Wire Harness · inoperativeEEC CHANNEL A ON #1 ENGINE IS INOP. GROUNDED - YES. FOUND MW0301 HARNESS FAULTY. REMOVED AND REPLACED MW0301 HARNESS IAW B737-800 AMM 71-51-03. EEC TEST PASS IAW AMM 73-21-00-700-804-F00. ACTUATORS TEST PASS REF AMM 71-51-03, 73-21-00.SDR ASAA2019031628641Fmc · malfunctionedAFTER LANDING BOTH FMC'S DUMPED, LOST ALL DATA, HAD "VTK" ON BOTH SIDES. GROUNDED - YES. PERFORMED FIM 34-61 TASK 801 FOUND LT FMC WITH PROGRAM FAULT. PERFORMED FIM 34-61 TASK 807, NO FAULTS PRESENT AT THIS TIME.SDR ASAA2019030228427Anti-Ice Valve · failedCLIMBING THROUGH FL 230 NR 1 COWL ANTI-ICE LIGHT ILLUMINATED PERFORMED QRH NR 1 ENG IDLE, LIGHT REMAINED ILLUMINATED. GROUNDED - YES. REMOVED & REPLACED NR 1 ENG COWL TAI VALVE REF AMM 30-21-11, LEAK & OPS CHECK GOOD. GROUND VERIFICATION SUCCESSFUL.SDR ASAA2019022728382Blade · damagedDURING ACCOMP T/C 78472010 FOUND NR 12 BLADE CU-NI COATING MISSING OUT OF LIMITS NR 1 ENG. GROUNDED - YES. REMOVED AND REPLACED NR 12 BLADE AND NR 24 BLADE , REQUIRES ENGINE VIBRATION SURVEY REF TASK CARD 78472010 FOR SURVEY.SDR ASAA2019022728381Platform · wornENGINE PLATFORMS AT POSITIONS 4,15, 19 WORN BEYOND LIMITS. GROUNDED - YES. REMOVED AND REPLACED AIRCRAFT ENGINE NR 1 PLATFORMS AT POSTION 4,15, 19 REF TASK CARD 78472010.SDR ASAA2019022728379Spinner · unserviceableDURING ACCOMP OF T/C 78412010 FOUND PAINT MISSING ON FRONT SPINNER CONE. GROUNDED - YES. REMOVED AND REPLACED FRONT SPINNER CONE REF T/C 78472010.SDR ASAA2019022628439Warning System · false activationWHILE PERFORMING TASK CARD FOUND MAINT MSG NR 73-31371 FOR NR 1 ENGINE. GROUNDED - YES. EEC BITE DONE FOR ENGINE NR 1: NO FAULTS FOUND. NO ACTIVE FAULTS, NO FAULTS IN HISTORY. T49.5 PROBE TEMPERATURES ARE WITHIN TOLERANCE REF AMM 77-21-00-140-801 STEP 8. THIS SDR ASAA2018122637559Cover · detachedBOTH EMERGENCY EXIT LIGHT COVERS LOCATED OVER AISLE AT WING EXIT LOCATION FELL OFF ON TAKE OFF AND NOT SECURED. GROUNDED - YES. RESECURED BOTH EMERGENCY EXIT LIGHT COVERS LOCATED IN MIDDLE WALKWAY ON THE CEILING IN AISLE 16.SDR ASAA2018120527215Not Reported · unknownCREW REPORTS CTR TANK AT 1200 POUNDS, LIGHTS FOR CTR PUMPS OFF IN ON POS. FUEL STARTED BURNING FROM WING TANKS. GROUNDED - YES. PERFORMED FUEL QTX OPS CK PER AMM 28-41-00-710/801. NO CURRENT OR INFLIGHT FAULTS OPS NORMAL. TRANSFERRED FUEL PER AMM 28-26-00, PUMSDR ASAA2018120427216Lens · detachedEXIT SIGN FROM CENTER AISLE FELL OFF. GROUNDED - YES. REINSTALLED LENS TO THE CENTER AISLE EXIT SIGN AS REQUIRED LIGHT TESTED GOOD REF AMM 33-51-01-01-960-801.SDR ASAA2018103026676Control Module · failedLANDING ALTITUDE WINDOW IN PRESSURIZATION PANEL WOULD NOT RESET AFTER LANDING ( READS ONLY 50 FEET OR 0). GROUNDED - YES. CONFIRMED. REPLACED CABIN PRESS CTRL MODULE REF AMM 21-31-02. GND VERIFICATION GOOD.SDR ASAA2018102426579Switch · defectiveNR 1 COWL ANTI ICE LIGHT ILLUMINATED ON POWER UP TO TAXI FOR DEPARTURE. GROUNDED - YES. R & R ENG COWL TAI VALVE PER AMM 30-21-11. VALVE OPS CK NORMAL. BUT AMBER LIGHT NOW ILLUMINATES DIMLY ALL THE TIME. PERFORMED FIM 30-21 TASK 801. FOUND CONTINUITY BETWEEN PSDR ASAA2018100526361Turbine Blades · damagedREF. T/C 78472002 NR 2 ENGINE (SDI) HPT BLADES ESN 894103 SUBTASK 72-00-00-210-053-F00,STEP (1) (J) MORE THAN 10 BLADES HAVE BURNING OR MELTING TRAILING EDGES ON AREA "B". GROUNDED - YES. REPLACED NR 2 ENGINE.SDR ASAA2018092546241Wire Harness · intermittentPERFORMED T/C 78273000, FOUND FAULT CODE 77-20862 (THE BOTTOM LEFT EGT SIGNAL (T495S3) IS OUT OF RANGE) REQUIRES 50 HR RE-CHECK. GROUNDED - YES. PERFORMED #2 ENGINE CURRENT FAULT CHECK. FOUND S3 PROBE SHOWING DASHES. ACCOMPLISHED B737-800 FIM 77-21 TASK 803. TSDR ASAA2018091726149Acoustic Panel · damagedNR 1 ENG AT NR 3 ROTATION ACOUSTIC PANEL DAMAGED. GROUNDED - YES. REPLACED ACOUSTIC PANEL PER AMM 72-23-02-400-801-F00.SDR ASAA2018090726042Control Panel · malfunctionedMCP PANEL- FO COURSE DISPLAY BLANKED OUT INOP. GROUNDED - YES. REMOVED AND REPLACED DFCS MODE CONTROL PANEL, OPS NML REF AMM 22-11-34-740-801. ACCOMPLISHED DFCS MCP LRU REPLACEMENT TEST, GRP BITE 32, ALL TEST PASSED REF AMM 22-11-34/501. ACCOMPLISHED DFCS LANDSDR ASAA2018080225628Sensor · dirtyFOUND NR 2 ENGINE ECONOMIC FAULT 77-20862 "THE BOTTOM LEFT EGT SIGNAL IS OUT OF RANGE". GROUNDED - YES. ACCOMPLISHED EGT CLEANING PROCEDURES, BEFORE CLEAN TEMP READS: S1- 126.50, S2- 70.25, S3, S4- 123.12. AFTER CLEAN, TEMPERATURES READS: S1- 65.37, S2- 35.00,SDR ASAA2018062195137Valve · faultedCONTROL CABIN ZONE TEMP LIGHT ILLUMINATED ON MASTER CAUTION RECALL. ACFT GROUNDED. ACCOMPLISHED CONTROLLER BITE IAW 21-61-00-700-806-002. FOUND FLT DECK TRIM VALVE FAULTED. RESET SUCCESSFUL. OPS GOOD IAW AMM 21-01-00-700-807-002. NO HISTORY LAST 90 DAYS.SDR ASAA2018061125033Spinner · damagedNR 2 ENGINE FRONT SPINNER CONE HAS DAMAGED THREADED INSERT AND TOOLING MARKS. GROUNDED - YES. REMOVED AND REPLACED FRONT SPINNER CONE REF TASK CARD 78472002.SDR ASAA201806114992Warning Message · false activationNR 2 HF FAIL ON BOTH ACTIVE AND STANDBY. ACFT GROUNDED. PERFORMED FIM 23-11, TASK 801, BITE CHECK OF THE NR 2 HF, MESSAGE CLEARED, OPS CHECKED GOOD, AND THE NR 2 HF OPERATED NORMAL, NO DEFECTS NOTED.SDR ASAA2018060224890Warning Message · unknownCAT II APPROACH AUTOLAND FAILED. AT 20-30 FEET APPROACH WARNING ANNUNCIATED, ON SPEED 138 KIAS ON GLIDESLOPE AND LOC, FLAPS 40 DEG VFR CONDITION. GROUNDED - YES. ACCOMPLISHED FLT FAULT REVIEW, GRP BITE 10, NO FAULTS REF B737-800 FIM 22-11 TASK 801. ACCOMPLISHESDR ASAA2018052524833Connector · dirtyWHILE PERFORMING T/C 78273000 FOUND ENG NR 2 FAULT 77-20862 THE BOTTOM LEFT EGT SIGNAL (T495S3) IS OUT OF RANGE, ECONOMIC FAULT. DEFERRED PER T/C 78273000. GROUNDED - YES. T495 PRE CLEANING TEMPS: S1-198C, S2-163C, S3-159C, S4-195C. CLEANED ALL EGT CONNECTORS SDR ASAA2018041024194Transceiver · failedNR 1 HF FAIL INDICATION IN BOTH ACTIVE AND STANDBY WINDOWS. ACFT GROUNDED. FAIL DISPLAYED ON RADIO TUNING PANEL NR 1 HF. BITE SHOWS LRU FAILED ON NR 1 HF TRANSCEIVER IAW BITE IAW FIM 23-11/801. REPLACED THE NR 1 TRANSCEIVER IAW AMM 23-11-21. OPS CHECKED NOSDR ASAA2018040924192Warning Message · false activationNR 1 HF FAILED. ACFT GROUNDED. ACCOMPLISHED FIM 23-11 / 801. BITE CHECKED GOOD. NO DEFECTS NOTED. ACCOMPLISHED FIM 23-11 T806. NR 1 AND 2 HF TESTS PASSED. NO DEFECTS NOTED. GROUND VERIFICATION SUCCESSFUL. OK FOR CONTINUED SERVICE.SDR ASAA2018040224107Hf Comm · malfunctionedHF TRANSMISSION AND RECEPTION CHECKED ON GROUND. IN AIR APPROACHING GATEWAY FIX, TRANSMISSION WAS ATTEMPTED AND BOTH FAIL FLAGS APPEARED, NO SIDETONE WAS HEARD. DESCENDING THROUGH 8500, THE HF1 RADIOS STARTED WORKING AGAIN. ACFT GROUNDED. HF 1 SYSTEM TEST DOSDR ASAA2018031823962Lens · detachedMID CABIN CEILING EMERGENCY EXIT SIGN LENS DETACHED. ACFT GROUNDED. SECURED THE LENS IAW AMM 33-51-01.SDR ASAA2018031724025Terminal · looseNR 1 ENGINE, LOOP B OVERHEAT, HANDLE LIGHTS DO NOT ILLUMINATE ON OVERHEAT TEST. ACFT GROUNDED. MOVED THE NR 1 ENGINE OVERHEAT DETECTOR SWITCH TO NORMAL POSITION. PERFORMED ALT DEACTIVATION PROCEDURES IAW CHAP 5, TABLE 3. TERMINATED LOOSE TERMINALS ON THSDR ASAA2018031723934Fire Detector · failedFAULT IN THE NR 1 B LOOP. ACFT GROUNDED. CONFIRMED FAULT, NR 1 ENGINE B LOOP WILL NOT TEST. ENGINE, APU FIRE & OVHT DETECTION CONTROL MODULE BITE SHOWS UPPER FAN LOOP DEFECTIVE. ACCOMPLISHED DETECTOR LOOP RESISTANCE TEST IAW AMM 26-11-00-730-801, CONFIRMESDR ASAA2018031623982Connector · dirtyFOUND FAULTS FOR THE NR 2 ENGINE, 77-20862, BOTTOM LEFT EGT SIGNAL OUT OF RANGE. ACFT GROUNDED. TSR 701692 ACCOMPLISHED EGT INDICATION SYSTEM TROUBLESHOOTING AND CONNECTOR CLEANING IAW AMM 77-21-00-140-801. RAN ENGINE FOR 5 MINUTES. ALL READING WERE WELL SDR ASAA2018030123745Door · out of adjustL2 DOOR HANDLE REQUIRES TOO MUCH FORCE TO CLOSE. ACFT GROUNDED. ADJUSTED THE L2 DOOR AND PERFORMED OPERATIONAL CHECK, CHECKED GOOD, WITHIN LIMITS AND LIGHT CHECKED GOOD IAW AMM 52-13-00-820-801, AMM 52-13-31-400-802, AMM 25-66-01-400-803, AMM 52-71-11-710SDR ASAA2018021123628Attach Bracket · crackedFWD CARGO, ATTACH BRACKET CRACKED AT LT AFT SIDE OF FRAME BS 500H BELOW TRANSITION PANEL. ACFT GROUNDED. REMOVED AND REPLACED THE ATTACH BRACKET IAW SRM 51-40-02, DWG 143A7502, REV, AND DWG 143A7505, REV A.SDR ASAA2018020823521Transition Panel · corrodedAFT CARGO BAY, RIGHT TRANSITION PANEL HAS CORROSION, BS 767 AND 787, BETWEEN STRINGERS 25R AND 26R. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. REMOVED AND REPLACED THE TRANSITION PANEL IAW SRM 51-40-02, SDR ASAA2018020823505Transition Panel · corrodedAFT CARGO TRANSITION PANEL HAS CORROSION BETWEEN BS 727H+10 AND 767, STRINGER 26R. ACFT GROUNDED. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. REPLACED THE TRANSITION PANEL IAW SRM 53-00-53-212-5.SDR ASAA2018020723661Attach Bracket · crackedFWD CARGO, INTERCOSTAL ATTACH BRACKET CRACKED AT FWD SIDE OF BS 500H, BELOW TRANSITION PANEL. ACFT GROUNDED. REMOVED AND REPLACED THE ATTACHED BRACKET IAW SRM 51-40-02, 51-40-05, DWG 143A7505, REV A, AND DWG 143A7502, REV A.SDR ASAA2018020723627Attach Bracket · crackedFWD CARGO, INTERCOSTAL ATTACH BRACKET CRACKED AT LT FWD SIDE OF FRAME, BS 500G BELOW TRANSITION PANEL. ACFT GROUNDED. REMOVED AND REPLACED THE ATTACH BRACKET IAW SRM 51-40-02.SDR ASAA2018020723626Attach Bracket · crackedFWD CARGO, INTERCOSTAL ATTACH BRACKET CRACKED BS 500H, BELOW TRANSITION PANEL. ACFT GROUNDED. REMOVED AND REPLACED THE ATTACH BRACKET IAW SRM 51-40-02, AND SRM 51-40-05.SDR ASAA2018020623519Floor Support · crackedMAIN CABIN FLOOR SUPPORT CRACKED, BS 380 - 400, BL 0. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-022.SDR ASAA2018020623518Floor Support · crackedMAIN CABIN FLOOR SUPPORT CRACKED, BS 380 - 400, LBL 13. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.SDR ASAA2018020623517Floor Support · crackedMAIN CABIN FLOOR SUPPORT CRACKED BS 380 - 400, RBL 10. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02.SDR ASAA2018020623502Floorbeam · crackedMAIN CABIN FLOORBEAM AT BS 540, BL 0 TO LBL 24 IS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-40-02, AND DWG 143A5240, REV A.SDR ASAA2018020623500Floorbeam · crackedMAIN CABIN FLOORBEAM AT BS 540, BL 0 TO RBL 24 IS CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE FLOORBEAM IAW DWG 143A0060, AND SRM 51-40-02.SDR ASAA2018020623499Skin · crackedRIGHT HORIZONTAL STAB LOWER SKIN CRACKED, HSS 175.5. ACFT GROUNDED. REPAIRED THE AREA IAW SRM 55-10-01-2R-11.SDR ASAA2018020523459Fitting · corrodedCORROSION FOUND ON THE L1 DOOR AFT GIRT BAR LATCH FITTING MOUNT. ACFT GROUNDED. REMOVED AND REPLACED THE FITTING IAW SRM 51-40-02, AND DWG 141A5220, REV A.SDR ASAA2018020523458Floor Support · damagedDAMAGE ON THE UPPER AND LOWER SURFACES OF THE BS 277 - 294, BL0, FLOOR SUPPORT. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW DWG 141A5400, AND SRM 51-40-02.
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