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 ASAA2016112618819Battery Pack · dischargedALL OVERWING EXIT & L2 & R2 EMERGENCY EXIT EXTERIOR LIGHTS INOP. GROUNDED - YES. EMERGENCY BATTERY PACKS IS FULLY CHARGED FOR SEVEN HOURS PER REF AMM 33-51-06. BATTERY TIME NECESSARY TO CHARGE IS 90 MINUTES. ACCOMPLISHED EMERGENCY LIGHTS TEST REF AMM 33-51-00.SDR ASAA2016110618581Lens · detachedFA REPORTS EMERGENCY LIGHT COVER AT L1 NOT ATTACHED. ACFT GROUNDED. REMOVED & REPLACED L1 EXIT SIGN EMERGENCY LIGHT ASSY WITH CORRECT LENS, IAW AMM TASK 33-51-01-960-802, OPS CHECKED NORMAL.SDR ASAA2016103018520Trim Panel · unsecureFA REPORTS EXIT SIGN AT MID-CABIN HAS TRIM FALLING LOOSE EXPOSING WIRING. GROUNDED, YES. SECURED MID-CABIN EXIT SIGN TRIM. A/C OK FOR CONTINUED SERVICE.SDR ASAA2016102918504Valve · failedANTI-SKID LIGHT ILLUMINATED AFTER LIFT-OFF AND FLICKERED THROUGHOUT REMAINDER OF FLIGHT. ACFT GROUNDED. AIR TURNBACK - PERFORMED AACU BITE B737-800 FIM 32-42 TASK 801. FOUND FAULT LOGGED "VLV 4". PERFORMED BITE AGAIN AFTER CLEARING FAULT. FOUND BOX 1-4 LOGGESDR ASAA2016102518510Probe · failedFOUND ECONOMIC FAULT FOR NR 2 ENGINE 77-20862. THE BOTTOM LEFT EGT SIGNAL (T495S3) IS OUT OF RANGE. ACFT GROUNDED. PERFORMED INPUT MONITORING OF T49.5 CONTROL TEMPS. FOUND S3 TEMP WAS DASHES. CONTINUED TO TROUBLESHOT IAW FIM REF 77-21 TASK 803. INSPECTED ANSDR ASAA2016102118445Anti-Ice Valve · failedLEFT ENGINE ANTI-ICE BLUE LIGHT REMAINS BRIGHT BLUE WHEN SELECTED ON. ALTERNATE DEACTIVATION PROCEDURES CH 5-07-01, TABLE 3 ITEMS 3, 4, 5, 9, & 10. GROUNDED - YES. REMOVED AND REPLACED NR 1 ENG COWL TAI VALVE REF B737-800 AMM 30-21-11. OPS CHECK GOOD REF B737-SDR ASAA2016092018120Probe · shortedAFTER SHUTTING DOWN NR 2 ENGINE, EGT INSTRUMENT HAD A RED RECTANGLE SHOW UP. 27K POWER TAKEOFF OUT OF SAN DIEGO. NEITHER PILOT NOTICED ANY EGT EXCEEDANCE. ACFT GROUNDED. ALL EGT CONNECTIONS CLEANED AND ACCOMPLISHED RETENTION CHECK AND RESISTANCE CHECKS. FOUNSDR ASAA2016090417899Control Panel · faultedAUTOPILOT B DISENGAGED TWICE DURING CRUISE FLIGHT, AT FL 340 FT AND AT 10,000 FT DURING DESCENT. ACFT GROUNDED. PERFORMED DFCS BITE BOTH A & B SHOWED FAULTS IN FLT 1. R & R MCP IAW AMM 22-11-34 ALL TEST PASSED.SDR ASAA2016080317601Unknown · unknownA AUTOPILOT DISENGAGED AT FL360 DURING CRUISE. ACFT GROUNDED. ACCOMPLISHED DFCS BITE FLT FAULT, LAST LEG MSG 22-11607 FAULTED 3 TIMES AT FL360, REF B737-800, FIM 22-11-00. ACCOMPLISHED FIM 22-11-803, MCP TESTS. ALL TESTS PASSED. ACCOMPLISHED FCC A OPS LRUSDR ASAA2016080317600Warning System · false activationDURING LAND VERIFY SPOILER 4 FAULTED MSG 22-11157 A SENSOR AND MSG 22-11158 B SENSOR BOTH WERE AT -0.5VAC. ACFT GROUNDED. COULD NOT DUPLICATE. ACCOMPLISHED DFCS LAND VERIFY TEST IAW AMM 22-11-00/201, TEST PASSED. VERIFIED NR 4 SPOILER POSITION SENSOR CORRESDR ASAA2016080117585Probe · out of limitsWHILE PERFORMING T/C 78273000, FOUND NR 2 ENGINE ECONOMIC FAULT MSG 77-20862. THE BOTTOM LT EGT SIGNAL, T495S3 IS OUT OF RANGE. ACFT GROUNDED. IAW TSR908147. ACCOMPLISHED T/C 78273000, FOUND MSG 77-20862 THE BOTTOM LT EGT SIGNAL, T495S3 IS OUT OF RANGE OSDR ASAA2016073117565Control Panel · failedMCP AUTOPILOT B ENGAGE SWITCH INTERNAL LIGHT PARTIALLY INOPERATIVE. ACFT GROUNDED. REMOVED AND INSTALLED NEW MCP. PERFORMED MCP OPS TEST, IAW AMM 22-11-34/501. SYSTEM CHECKS NORMAL.SDR ASAA2016072617523Plenum · delaminatedWHILE WORKING T/C 78121000, HEAT EXCHANGER CLEANING FOUND THE RT AFT PLENUM DELAMINATED MIG-2C 40-0012871, 40-0012872 INITIALIZED. ACFT GROUNDED. RT AFT HEAT EXCHANGER & PLENUM REMOVED, IAW AMM 21-51-03-000-805-002. INSTALLED NEW RH AFT PLENUM WITH HEAT EXCSDR ASAA2016072417482Controller · failedCANNOT ADJUST FLT ALTITUDE ON PRESSURIZATION CONTROLLER. ACFT GROUNDED. REMOVED AND REPLACED CABIN PRESSURE CONTROL MODULE, IAW AMM 21-31-02-400. CONTROL MODULE CHECKS OK, IAW AMM 21-31-00-700-802 & 21-31-00-710-801.SDR ASAA2016070917318Nut Plate · brokenNR 2 ENGINE AFT ACOUSTICAL PANEL FWD NUTPLATE BROKEN APPROXIMATELY 3 O'CLOCK. ACFT GROUNDED. REMOVED AND REPLACED BAD NUTPLATE IAW SRM 51-40-02.SDR ASAA2016070117231Anti-Ice Valve · failedNR 1 ANTI-ICE VALVE STUCK IN OPEN POSITION WHEN ENGINE OPERATING . LIGHT EXTINGUISHED WHEN ENGINE IS OFF. ACFT GROUNDED. REMOVED AND REPLACED NR 1 ENGINE COWL TAI VALVE. OPS NORMAL IAW AMM 30-21-11-000-801.SDR ASAA2016062317145Sign · unsecureEXIT SIGN FELL OFF OF WALL NEXT TO FORWARD F/A JUMPSEAT. BETWEEN F/A JUMPSEAT AND L1 DOOR. ACFT GROUNDED. RESECURED EXIT SIGN IN BETWEEN F/A JUMPSEAT AND L1 DOOR.SDR ASAA2016051216731Module · malfunctionedFLT ALT AND LAND ALT DISPLAYS ON THE PRESSURIZATION CONTROL PANEL ARE FLICKERING. ACFT GROUNDED. ACCOMPLISHED FIM 21-31, TASK 803, CPC MODULE DISPLAY FAULTS, OPS CHECK NORMAL. R & R CABIN PRESSURE CONTROL MODULE IAW AMM 21-31-02.SDR ASAA2016051016686Connector · dirtyDIAGNOSTIC REPORTS NR 2 ENGINE TREND DATA SHOWS A SHIFT IN DELTA CRUISE AND TAKEOFF MARGIN INDICATIVE OF EGT INDICATION ERRORS. ACFT GROUNDED. ELECTRONIC ENGINE CONTROL FAULT HISTORY SHOWED 5 FLT LEGS OF EGT OUT OF RANGE FAULT. CHECKED EGT CONTROL TEMPS ANDSDR ASAA2016041916467Warning Message · false activationHF 1 FAIL MESSAGE ON COMM RADIO. ACFT GROUNDED. PERFORMED FIM 23-11, TASK 801, NR 1 & NR 2 HF TRANSCEIVERS BITE CHECK NORMAL, NO FAULTS NOTED, COMM HEAD FAIL MESSAGE EXTINGUISHED.SDR ASAA2016041516426Actuator · leakingDURING PRE-FLIGHT WALK AROUND, FOUND FLUID DRIPPING FROM RT ENGINE. ACFT GROUNDED. VERIFIED LEAK COMING FROM RT VSV DRAIN. ACCOMPLISH ENGINE RUN IAW AMM 71-71-00-200, LEAK CHECKED WITHIN THRESHOLD LIMITS. R & R NR 2 ENGINE RT VSV ACTUATOR IAW AMM 75-31-0SDR ASAA2016040716314Display · failedNR 2 MCDU FAILED 40 MINUTES AFTER TAKEOFF AT FL 360. ACFT GROUNDED. R & R F/O MCDU, IAW AMM 34-61-01.SDR ASAA2016040716309Valve · failedENGINE ANTI-ICE SWITCH 1 WHEN SWITCH MOVED TO ON THE COWL VALVE OPEN LIGHT STAYED BRIGHT AND TAI INDICATION ON UPPER DU WAS AMBER WHEN SWITCH MOVED TO OFF THE COWL VALVE OPEN LIGHT EXTINGUISHED. ACFT GROUNDED. R & R NR 1 ENGINE INLET COWL THERMAL ANTI-ICE VALVSDR ASAA2016040116211Warning Message · false activationFMC DISAGREE, ACFT GROUNDED. ACCOMPLISHED FMCS RESET PROCEDURES IAW QRH. FMCS OPS NORMAL.SDR ASAA2016033116196Coupler · failedHF 2 WILL NOT TUNE OR TRANSMIT. ACFT GROUNDED. REMOVED HF COUPLER NR 2 REF AMM 23-11-61-000-801. ACCOMPLISHED HF ANTENNA ELECTRICAL BOND CHECK REF AMM 23-11-51-760-801. BONDING CHECKS GOOD -2.6 MILLIOHMS AND 2.7 MILLIOHMS. INSTALLED NEW HF COUPLER REF AMM SDR ASAA2016031715995Autopilot Sys · malfunctionedON RECALL FLT CONTINUED AND SPEED TRIM FAIL LIGHT ILLUMINATE. AUTOPILOTS A AND B WILL NOT ENGAGE. ACFT GROUNDED. MOVED A/P STABILIZER TRIM CUTOUT SWITCH TO NORMAL. PERFORMED DFCS BITE REF FIM TASK 22-11, TASK 801. TEST PASSED. NO FURTHER FAULTS FOUND.SDR ASAA2016031615964Static Inverter · inoperativeAFTER ENGINES STARTED, RECEIVED AN ELECTRIC LIGHT. ACFT GROUNDED. ACCOMPLISHED FIM 24-31, TASK 801. FOUND 1 FAULT STATIC INVERTER INOPERATIVE. CLEARED FAULT DID NOT REAPPEAR. ALL INDICATIONS NORMAL.SDR ASAA2016031615962Sensor · faultedAFTER ENGINE START, RECEIVED A CONTROL CABIN "ZONE TEMP" LIGHT. ACFT GROUNDED. FOUND NR 2 TEMP CONTROLLER HAD A FLIGHT CONTROL TEMP SENSOR FAULT. CLEARED FAULT TEST GOOD IAW AMM 21-61-20-860-005.SDR ASAA2016031615961Control Panel · malfunctionedCABIN ALTITUDE CONTROL PANEL DOES NOT DIM AND OUTFLOW VALVE POSITION NEEDLE IS BLANK. PRESSURIZATION NORMAL. ACFT GROUNDED. UNABLE TO DUPLICATE, VERIFY ON ACFT POWER UP. PERFORMED FIM 21-31, TASK 803. FLIGHT ALT AND LAND ALT DISPLAYS DIM AND BRIGHTEN WITH SDR ASAA2016022915717Baffle · crackedFWD CARGO COMPARTMENT BAFFLE ASSY BETWEEN BS 500E AND 500F, LBL 21.0 IS CRACKED AT FASTENER HOLE. ACFT GROUNDED. R & R BAFFLE IAW SRM 51-40-02, 51-40-05 AND BAC DWG 143A7510, REV B.SDR ASAA2016022415689Baffle · crackedFWD CARGO COMPARTMENT BAFFLE ASSY BETWEEN BS 500D AND 500E, LBL 21.0 IS CRACKED. ACFT GROUNDED. R & R CRACKED BUFFLE BETWEEN BS 500D-BS 500E IAW SRM 51-40-02, 51-40-05 AND BAC 143A7510. REV B.SDR ASAA2016022315705Door Frame · corrodedAFT CARGO COMPARTMENT CARGO DOOR SURROUND LOWER SILL WEB IS CORRODED. ACFT GROUNDED. ACCOMPLISHED BLENDOUT OF CORRODED AREA AT AFT CARGO COMPARTMENT CARGO DOOR SURROUND LOWER SILL WEB IAW SRM 51-10-02. ORIGINAL MATERIAL: .056", REMAINING MATERIAL: .035", MASDR ASAA2016022115692Web · gougedLOWER FUSELAGE ELECTRONIC EQUIPMENT COMPARTMENT DOOR CUTOUT, RT INTERCOSTAL WEB UPPER EDGE IS GOUGED. ACFT GROUNDED. R & R WEB, PN 141A8512-28, REF SRM 51-40-02, BAC DWG 141A8511. OPS CHECK GOOD. REMOVED DOT.SDR ASAA2016021915715Channel · corrodedAFT CARGO COMPARTMENT LT TRANSITION PANEL HAS SEVERAL AREAS OF CORROSION FROM BS 727D TO BS 807. ACFT GROUNDED. REMOVED CORROSION FROM AFT CARGO COMPARTMENT LT TRANSITION PANEL FROM BS 7270 TO BS 807 IAW SRM 51-10-02. ORIGINAL MATERIAL THICKNESS 0.040. MATESDR ASAA2016021915704Channel · corrodedFWD CARGO COMPARTMENT LT TRANSITION PANEL HAS SEVERAL AREAS OF CORROSION FROM BS 500D TO BS 500I. ACFT GROUNDED. REMOVED CORROSION IN FWD CARGO COMPARTMENT LEFT TRANSITION PANEL FROM BS 500D+10-500I IAW SRM 53-00-53 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53SDR ASAA2016021915687Channel · corrodedAFT CARGO COMPARTMENT RT TRANSITION PANEL HAS SEVERAL AREAS OF CORROSION FROM BS 727D TO BS 767. ACFT GROUNDED. REMOVED CORROSION FROM BS 727D-727H+10. ORIGINAL THICKNESS WAS .040, LOST .002, REMAINING .038 FOUND TO BE IN LIMITS IAW SRM 53-00-53-1A-2 ALODISDR ASAA2016021915686Channel · corrodedFWD CARGO COMPARTMENT RT TRANSITION PANEL HAS SEVERAL AREAS OF CORROSION FROM BS 500B TO BS 500I. ACFT GROUNDED. REMOVED CORROSION FROM BS 500B-500D IAW SRM 53-00-53. ORIGINAL MATERIAL THICKNESS .040, MATERIAL REMOVED .002, AND REMAING .038, FOUND TO BE WITHSDR ASAA2016021815734Tee Fitting · corrodedAFT CARGO COMPARTMENT FLOOR PANEL 140BF SPLICE TEE ASSY IS CORRODED. ACFT GROUNDED. R & R AFT CARGO COMPARTMENT FLOOR PANEL 140BF SPLICE TEST ASSY IAW AMM 25-52-10, PN 146A9401-4, PO 860175.1. REMOVED DOT.SDR ASAA2016021815733Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR PANEL 140AF SPLICE TEE ASSY IS CORRODED. ACFT GROUNDED. R & R AFT CARGO COMPARTMENT FLOOR PANEL 140AF SPLICE TEE ASSY IAW AMM 25-52-10, PN 146A9401-8, PO 860175.2, NO DOT.SDR ASAA2016011814873Hmu · failedDURING DESCENT, WHEN POWER LEVERS WERE BROUGHT TO IDLE FROM ABOUT 60 PERCENT N1, THE RT, N2 VALUE TOOK ABOUT 15 SECONDS LONGER TO REACH IDLE N1, N1 35 PERCENT, THEN THE NR1 ENGINE N1. REPEATED BY BRINGING THRUST TO ABOUT 60 PERCENT AND BACK TO IDLE, SAME RESSDR ASAA2016011114732Warning Message · false activationFMC DISAGREE. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. FMCS RESTORED NORMAL.SDR ASAA2016010714700Fmc · malfunctionedWHILE AT CRUISE FLIGHT, CAPTS ND SHOWED A "VTK" WITH A FAILURE OF THE MAP. BOTH CDU'S HAD NO "FMC" DISPLAYED. QRH ACCOMPLISHED. BEFORE MOVING THE FMC SELECT SWITCH, THE CAPTS SIDE WAS RESTORED BUT THE F/O SIDE LOST THE MAP DISPLAY. BOTH CDUS DISPLAYED AN "FMSDR ASAA2016010314631Warning Light · false activationVTK DISPLAYED ON CAPTAIN'S ND, NO FMC PROMPT DISPLAYED ON EITHER CDU. ACFT GROUNDED. T/S FOUND NO FAULTS ON NR 1 FMC IAW FIM 34-61, TASK 836.SDR ASAA2016010314630Warning Flag · false activationIN FLIGHT, CAPTAIN`S ND BRIEFLY SHOWED "VTK" AND "MAP" FLAGS BEFORE RETURNING TO NORMAL. SHORTLY THEREAFTER F/O'S ND SHOWED A "MAP" FLAG. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. FMC RESTORED NORMAL.SDR ASAA2016010314629Warning Message · false activationFMC DISAGREE MESSAGE ON GROUND AFTER PUSH. ACFT GROUNDED. ACCOMPLISHED RESET PROCEDURE IAW QRH. FMC RESTORED NORMAL.SDR ASAA2015122414452Transmitter · malfunctionedHF 2 WILL NOT TRANSMIT. ACFT GROUNDED. PERFORMED HF SYS BITE TEST REF FIM 23-11, TASK 801. NO FAULTS FOUND. SWAPPED HF TRANSMITTERS FROM 1 TO 2 POSITION AND 2 TO 1 POSITION BOTH HF 1 AND HF 2, OPS TEST NORMAL REF AMM 23-11-21-400-801. NO HISTORY PAST 30 SDR ASAA2015111613800Fire Detector · failedAPU DET INOPERATIVE ANNUNCIATOR ILLUMINATED IN FLIGHT. ACFT GROUNDED. PERFORMED ENGINE/APU FIRE DETECTION CONTROL MODULE BITE IAW FIM TASK 26-10, TASK 801. FOUND TAILPIPE DETECTOR RESISTANCE READING OUT OF TOLERANCE. R & R APU TAILPIPE OVERHEAT DETECTOR ASSDR ASAA2015110513657Control Valve · failedRIGHT PACK LIGHT COMES ON AT MASTER CAUTION RECALL. ACFT GROUNDED. PERFORMED PACK TEMP CONT BITE IAW FIM 21-62, TASK 801. RT PACK LOGGED TCV FAULT. R & R RT PACK TCV REF. AMM 21-51-10. LEAK CK GOOD. PERFORMED RT PACK TEMP CONTROL BITE TEST IAW AMM 21-61-SDR ASAA2015110413642Warning Light · illuminatedUPON RECALL, GOT MASTER CAUTION LIGHT RT PACK ILLUMINATED. CAUTION LIGHT GOES OUT UPON RESETTING MASTER CAUTION. ACFT GROUNDED. PERFORMED PACK TEMP CONT BITE REF FIM 21-62, TASK 801, RT PACK LOGGED TCV FAULT LAST FLT PERFORMED, FIM 21-62, TASK 831 & FAULT CLSDR ASAA2015101913441Warning Message · false activationCONTROL CABIN ZONE LIGHT ILLUMINATED, EXTINGUISHES ON RECALL. ACFT GROUNDED. ACCOMPLISHED BITE OF THE PACK/ZONE TEMP. CONTROLLERS, REF FIM 21-82, TASK 801 ON NR 2 CONTROLLER FLIGHT DECK TRIM VALVE, FAULT CLEARED. RAN APU & PACKS, FLIGHT DECK TEMP. WAS CONTR
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