N473AS, cancelled Mar 18, 2008
Service difficulty reports · 38
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 = 'N473AS' AND deregistration_id = 'N473AS-2008-03-18' 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 = 'N473AS' AND deregistration_id = 'N473AS-2008-03-18' 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 XN0A1358Hose · failedUPON LANDING, LOST GREEN HYDRAULIC SYSTEM QUANTITY AND PRESSURE. LEVEL LOW AND PRESSURE LOW LIGHTS ON. FOUND LEFT GEAR SIDE BRACE LOCK ACTUATOR AFT HOSE FAILED. INSTALLED NEW HOSE, SERVICED GREEN HYDRAULIC SYSTEM. PRESSURE AND LEAK CHECKS NORMAL IAW A300 ASDR XN0A1347Engine · unknownFLIGHT LEVEL 290 MACH .75 COULD NOT MAINTAIN SPEED OR FLIGHT LEVEL, ENGINE AI WAS ON. AC SHOULD BE ABLE TO MAINTAIN MACH .78 WITH N1 OF 98.4 FLIGHT LEVEL 280 M72. TAT 05 SAT-31. LOOKED OUT BOTH OVERWING WINDOWS AND NO ICE NOTED. PERFORMED ENGINE IDLE RUN NR 1SDR XN0A1345Line · looseNR 2 BLEED REGULATOR FAULT 90 DEGREE CELSIUS, 0 PSI, COULD NOT PRESSURIZE. NR 1 BLEED OVER TEMP, COULD NOT PRESSURIZE, USED APU FOR PRESSURIZATION, LIMIT 15000 FT, RETURNED TO VHH. FOUND LOOSE SENSE LINE, SECURED LINE OPS CHECK NORMAL IAW A300 AMM CHAPTER 36SDR XN0A1346Line · leakingON GEAR DOWN LOST ALL GREEN HYDRAULIC FLUID AND NOSE WHEEL STEERING. REPLACED FAILED HYDRAULIC LINE AT LT MLG STRUT IAW A300 AMM CHAPTER 20-23-11, SERVICED HYDRUALICS TO FULL IAW A300 AMM CHAPTER 12-12-29. NO LEAKS NOTED AT THIS TIME. TEMPORARY FLEX LINE ENTSDR XN0A1339Control Box · faultyDURING TAXI ALL ANTI SKID RELEASE LIGHTS ON WITH ANTI SKID SWITCH IN NORM OR ALT POSITION. REMOVED AND REPLACED ANTI SKID CONTROL BOX IAW A300 AMM CHAPTER 32-42-72 GROUND FUNCTIONAL CHECK NORMAL.SDR XN0A1324Warning Light · illuminatedDURING CLIMBOUT NR 1 BLEED LIGHT ON, NO PRESSURIZATION ACCOMPANIED BY REGULATOR FAULT LIGHT. NR 2 BLEED HIGH TEMP LIGHT ACCOMPANIED BY BLEED FAULT LIGHT. REMOVED AND REPLACED NR 1 ENGINE IAW ENA EO 008-08 AND A300 AMM CHAPTER 71-00-00 PAGES 401 THRU 448. GRSDR XN0A1318Bleed Valve · malfunctionedENGINE NR 2 BLEED AIR TEMP HI LIGHT ILLUMINATED AFTER TAKEOFF. REGUL FAULT LIGHT ALSO ILLUMINATED. REMOVED AND REPLACED FAN AIR VALVE IAW A300 AMM CHAPTER 36-11-16 AND REMOVED AND REPLACED HIGH PRESSURE BLEED VALVE IAW A300 AMM CHAPTER 36-11-12. PERFORMED ESDR XN0A1317Control Box · malfunctionedON TAXI OUT BRAKE CHECK RT BRAKES WERE GRABBING IN BOTH NORMAL AND ALTERNATE BRAKE SYSTEMS. REMOVED AND REPLACED BRAKE SYSTEM CONTROL BOX IAW A300 AMM CHAPTER 32-42-72. BLED NR 3, 4, 7 AND 8 BRAKE SYSTEMS BOTH YELLOW AND GREEN SYSTEMS AT BRAKE UNITS AS WELL SDR XN0A1305Switch · contaminatedJAM LIGHT ILLUMINATED FOR BLUE SERVO CONTROLS. TRANSFERRED TO DMI 6202 IAW MEL 27-82-01 CAT C PLACARD INSTALLED. INSPECTED RUDDER SERVOS FOUND ALL TO BE WORKING NORMAL IAW A300 AMM CHAPTER 27-24-00. INSPECTED JAMMING DETECTION SWITCHES IAW A300AMM CHAPTER 2SDR XN0A1281Unknown · vibrationON TAKEOFF ROLL AT APPROXIMATELY 135K - SEVERE VIBRATION FELT AND SUSPECT BLOWN TIRE, NORMAL LANDING ACCOMPLISHED. ON POST-FLIGHT INSPECTION FOUND NR 8 TIRE BLOWN. REMOVED AND REPLACED NR 8 AND NR 7 WHEEL AND TIRE ASSY IAW A300 AMM CHAPTER 12-37-32. PERFORMSDR XN0A1280Exciter · faultyNO LIGHT UP ON NR1 ENGINE ON (B) IGNITION. FOR T/S TRIED (A) IGNITION BUT NO LIGHT-UP. ABNORMAL PROCEDURES CARRIED OUT IAW QUICK REFERENCE HANDBOOK. REPAIRED (B) SYSTEM IGNITION EXCITER IAW AMM 74-11-01 OPS CK GOOD. PLACED (A) SYSTEM ON DMI LOG NR 5959 IAWSDR XN0A1279Control Unit · failedNR 2 YAW DAMPER WILL NOT ENGAGE. TRANSFERRED TO DMI LOG 5951 IAW ENA MEL REFERENCE 22-21-01 CAT-A. REMOVED AND REPLACED YAW DAMPER ENGAGE UNIT, OPS CHECK OK IAW A300 AMM 22-11-12. THIS CLEARS DMI 5951. PLACARDS REMOVED.SDR XN0A1275Brake · malfunctionedGREEN BRAKE INOP ON TAXI. YELLOW SYS PRESSURE SHOW ON BRAKE GAGE. INSPECTED BRAKES THROUGH 8, FOUND NO DEFECTS, PERFORMED OPERATIONAL CHECK OF GREEN AND YELLOW BRAKE SYTEMS. OPS CHECK GOOD. CLEANED AND RESEATED BRAKE, CONTROL BOX AND CONNECTION. ALL SYSTEMS OSDR XN0A1256Access Panel · inflt separationLEFT ACCESS PANEL (AC) DEPARTED AIRCRAFT ON T/O. ATC REPORTED SEEING PANEL FULL, TURNED BACK. PERFORMED L INSPECTION OF WHEEL WELL AREA, LOWER SURFACE WINES, FUSELAGE EMPENNAGE, NO DAMAGE NOTED. INSPECTED LT & RT MLG, NO DAMAGE NOTED. INSTALLED SERVICEABLESDR XN0A1228Coupler · defectiveNR 1 COMPASS FLUCTUATING + - 20 DEGREES. REPLACED NR 1 COMPASS COUPLER, OP'S GOOD IAW A300MM 34-21-34.SDR XNOA1217Connector · damagedCAPT'S DG FAILED IN FLIGHT. REMOVED, CONNECTOR & REINSTALLED NR 1 DG OPS, CHECKED GOOD. SWAPPED NR 1 DG & NR 3 DG PENDING FURTHER TROUBLESHOOTING, OPS CHECKED NR 1, NR 2, & NR 3 SYSTEMS OPS CHECKED GOOD IAW A300AMM 34-25-34 & 34-25-00.SDR XNOA1181Generator · inoperativeAT PUSHBACK IN SCK NR 2 GEN NO VOLT'S AND FREQ'S. SHUT DOWN ENG AND RETURNED TO THE GATE. R&R NR 2 GENERATOR CONTROL UNIT IAW A300 AMM 24-21-12 OPS CHECK GOOD. (STATUS:SUPP/CLOSED)SDR XNOA1176Damper · failedBTB DUE BOTH YAW DAMPERS FAILED DURING TAXI OUT. PART INSTALLED FOR YAW DAMPER AUTO STAB CONT. REPLACED WITH ORIGINAL UNIT. TRANSFERRED TO DMI 4053, ORIGINAL DMI CONTINUES. NEW AUTO STAB FAILED, BAD FROM STOCK, IAW A-300 AMM 22-21-00. R&R RATE GYRO OPS CKSDR XNOA01153Control Cable · lack of lubeFLIGHT CONTROLS LOCKED TO LEFT ON TAKEOFF ROLL. ABORTED TAKEOFF AT 60 KTS. INSPECTED AIL CABLES AND TENSION REG. LUBED TENSION REG. OPS CHECK NORMAL IAW A300 MM 27-11-00. INSP. AIL HYD ACT. SYS IAW A300 MM 27-14-00. NO DEFECTS NOTED.SDR XNOA01146Radio · inoperativeNR 1 VHF RADIO WILL NOT TRANSMIT OR RECEIVE. NR 2 VHF WILL ONLY TRANSMIT ON 121.9. DISCONNECTED AND RECONNECTED THE CAPTAINS FREQUENCY SELECT PANEL AND AUDIO SELECT PANEL. PERFORMED OPERATIONAL CHECKOUT OF THE NR 1 VHF COMM.SYS. ON FREQUENIES 129.07 AND 121.9SDR XNOA01137B-Nut · looseLOST GREEN HYD FLUID AND PRESSURE. MOTOR DUMPED FUEL TO MAX LANDING AND RETURNED TO SJU. ACTION TAKEN: TIGHTENED LOOSE AND LEAKING B-NUT ON LEFT MLG DRAG BRACE CYLINDER. LEAK CHECK GOOD AND SERVICED GREEN HYD IAW A300 MM 12-12-29.SDR XNOA01135Tire · failedAFTER T/O TOWER SAID LT MLG TRAILING SMOKE-NO ABNORMAL INDS ON BRAKE TEMP GUAGES. THEN TWR ADVISED THEY FOUND TIRE DEBRIS ON RWY-HAD NOT RETRACTED GEAR AS PRECAUTION. PHONE PATCH WITH CO. THEY REQUESTED US TO RETURN TO CLT. JETTISONED 15000 KILOS OF FUEL. REMOSDR XNOA01110Engine · malfunctionedENGINE 1 N1 114 EGT 410 DEGREE C N2 47 PERCENT FF 2300. ACTED LIKE A HUNG START AT 50 SEC. WE REJECTED TAKE OFF. PERFORMED ENG RUN. ALL PARAMETERS NORMAL IAW A300 MM 72-00. INSPECTED NR 1 ENG. NO DEFECTS NOTED.SDR XNOA01102Engine · malfunctionedON TAKEOFF, POWER APPLICATION NR 2 ENG N2 INDICATED LOW. TAKEOFF REJECTED (NO HIGH ENERGY STOP). AS PER MAINTENANCE CONTROL INLET & EXHAUST INSPECTED. NO DEFECT NOTED. ACCOMPLISHED POWER RUN TO 70 PERCENT. FOUND FUEL FLOW N2 & EGT IN PARAMETERS. DEFERRESDR XNOA01099Landing Gear · malfunctionedDURING FINAL APPROACH TO DAY MLG WOULD NOT EXTEND. MANUAL EXTENSION PROCEDURE WAS USED. REMOVED & REPLACED ELECTRO VALVE IAW A300 MM 32-31-12. PERFORMED INSPECTION CHECK IAW 32-31-12. NO DEFECTS NOTED. PERFORMED GEAR SWING IAW A300 MM 32-30-00 TO SYS 1 & SDR XNOA01086Proximity Sensor · malfunctionedUNABLE TO RETRACT LANDING GEAR WITH EITHER SYSTEM. REMOVED & REPLACED RT MLG BOAGIE TRIM PROXIMITY SENSORS 8GA IAW A300 MM 32-00-00. REMOVED & REPLACED LANDING GEAR EXTEND & RETRACT SWITCH IAW A300 MM 32-31-11. PERFORMED LANDING GEAR EXTENSION & RETRACTION FOSDR XNOA01081Line · cloggedNO AIRSPEED ON FO'S AIRSPEED INDICATOR ON TAKEOFF. ABORTED AT 90 KTS. ACTION TAKEN: FLUSHED NR 2 AIR DATA COMP. LINE. OPS CHECK GOOD IAW A300 MM 34-11-10.SDR XNOA01067Hydraulic System · dirtyNR 1 EDP INOP (GREEN SYSTEM). CLEANED AND RESECURED CONNECTION AT BYPASS. SOL SYS CHECKED GOOD PER A300 MM 29-11-32.SDR XNOA01037Damper · lowTHREE TRIES TO GET GEAR RETRACTED OUT OF DENVER. INSPECTED LANDING GEAR. FOUND PITCH DAMPERS NITROGEN CHARGE LOW ALL 4. SERVICED PITCH DAMPERS IAW A300 MM 12-12-32. RECHECKED PRESS AFTER 48 HRS. NO DEFECTS NOTED. LUBED LANDING GEAR IAW A300 MM 12-22-32. SDR XNOA01034Switch · looseON TAKEOFF GEAR WOULD NOT RETRACT. PERFORMED CHECK LIST. WOULD NOT RETRACT. OVERWEIGHT LANDING NOT FACTOR. CLEANED AND RESECURED NOSE GEAR CENTERING SWITCH. C/P OPS CHECK NORMAL ON GEAR SWING IAW A300 MM 32-30-00.SDR XN0A01030Pitot Tube · obstructedABORTED TAKEOFF DUE TO CPT AIRSPEED IND FAILURE. REMOVED DEBRIS FROM PILOT TUBE, FUNCTIONALLY. OPS CHECK GOOD IAW A300 MM 34-11-40.SDR XN0A01029Module · malfunctionedAFTER TAKEOFF AT GEAR RETRACT, GEAR HANDLE WOULD NOT GO PAST NEUTRAL. PERFORMED QRH L/G LEVER INTERLOCKED CHECK LIST. TRIED SYS 2 AND SAME AS SYS 1, GEAR HANDLE NEUTRAL. NO OTHER LIGHTS ONLY DOWN GREEN ARROWS. REMOVED AND REPLACED POSITION DETECTOR UNIT ANSDR XN0A01028Module · failedLANDING GEAR FAILED TO SELECT UP SYS 1 OR 2. LANDING PERFORMED AT 300 FT PER MINUTE. FOUND FAILED PROXIMITY MODULE UNIT. REMOVED AND REPLACED PROXIMITY DETECTOR MODULE UNIT IAW MM 32-61-12. OPS CHECK AND TEST NORMAL IAW 32-61-00.SDR XNA01015Jackscrew · lack of lubeDURING TAXI, NO SLATS INDICATION ON THE FCPI. SERVICED SLAT JACKSCREW AT LEFT WING ROOT. OPS CHECK GOOD IAW A300 MM 27-80.SDR XNA01013Warning Light · illuminatedCLIMBING THRU 13,000 FEET HEARD LOUD BANGING NOISE FROM CARGO SECTION FOLLOWED BY FLAPPING NOISE COMING FROM AIR CONDITIONING DUCTS. DOORS LIGHT CAME ON, ON MASTER WARNING PANEL ONLY. INSPECTED FREIGHT IN MAIN CARGO COMPARTMENT, FWD, MID AND BULK CARGO COMPASDR XNA01011AIndicator · faultyDURING CONTROL CHECK, LT&RT AIL INDICATORS SHOWED LESS THAN FULL THROW. MEASURED LT & RT LS & AS AILERONS FOR PROPER DEFLECTION UP AND DOWN. CHECKED NORMAL IAW A300 MM 27-11-00. REMOVED BIRD NESTS FROM LT AND RT LS AILERON ACCESS PANEL. REMOVED AND REPLACESDR XNA01008Indicator · inoperativeTAKEOFF ABORTED. NO AIRSPEED INDICATION ON CAPTAIN A/S INDICATOR. REMOVED AND REPLACED MACH/AIRSPEED INDICATOR. PERFORMED PITOT OPS AND LEAK CHECK. OPS AND LEAK CHECK NORMAL IAW A300 MM 34-11-40.SDR XNA01007Pitot Line · obstructedABORTED T/O AT 120 KTS. CAPTS AIRSPEED HAD NO INDICATION AT 70 KTS AND INDICATED APPROX 90 TO 100 KTS W/FO''S STBY AIRSPEED AT 120 KTS. AFTER ABORT W/FO''S INDICATING 70-80 KTS, CAPT''S WAS STUCK AT 100, THEN CAME DOWN BELOW 60 KTS. FLUSHED CAPT''S PITOT SY
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