N271
Service difficulty reports · 25
Newest first, from January 9, 1978, when the mark’s previous registration was cancelled.
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 = 'N271' AND difficulty_date > DATE '1978-01-09' 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 = 'N271' AND difficulty_date > DATE '1978-01-09' 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 WRLA2006038Switch · inoperativeRCH964/10 EDDR/OKBK SH0RTLY AFTER ARRIVAL NOTICED SMOKE SMELL IN FORWARD GALLEY. PULLED C/B'S AND DEACTIVATED NR 3 OVEN. FOUND NR 3 OVEN SW VERY HOT, WITH AIRCRAFT POWER ON CB POPPED. ISOLATED PROBLEM TO THE SWITCH. PULLED CB'S, PLACED ITEM ON DMI AND INSTALLSDR WRLA2006008Fire Loop · defectiveAPPROXIMATELY ONE HOUR AFTER TAKEOFF FROM KWI, ENGINE-2 FIRE DETECTOR FAIL ALERT INTERMITTENTLY APPEARED ON THE SD. (NOTE SYSTEM 2-B FIRE DETECTION SYSTEM PREVIOUSLY ON MEL). FLIGHT CREW FOLLOWED PROCEDURES AND RETURNED TO KWI. EXPECTED FIX: REPLACE DEFECTSDR WRLA2006007Actuator · malfunctionedAFTER TAKEOFF FROM SNN AND DURING CLIMB, WHEN FLAPS/SLATS WERE RETRACTED, A DEFLECTED AILERON DISAGREE ALERT MESSAGE WAS DISPLAYED ON THE SD ALONG WITH LEFT OUTBOARD AILERON INDICATING DEFLECTED. FLIGHT CREW FOLLOWED PROCEDURES AND RETURNED TO SNN, WHERE THE SDR WRLA2006001Wire Harness · burnedREADING LIGHTS WENT OUT AFTER TAKEOFF, PAX SAW SPARKS, BURNING SMELL. FOUND OVERHEAD DECODER AND ONE WIRING HARNESS BURNED. REMOVED DECODER AND HARNESS RUNNING FORWARD TO READING LIGHTS, DEFERRED ITEM TO DMI M25JA1806-131 PER MEL 25-22-1 AND COLLARED CIRCUITSDR WRLA2005002A/C Pack · smokeDURING START OF TAXI, SMOKE FROM AIR CONDITIONING DUCT IN COCKPIT. NR 1 AIR CONDITIONING PACK WAS SELECTED OFF. NO FURTHER CREW ACTION TAKEN. AIRCRAFT RETURNED TO BLOCKS. ENTERED IN DMI M21JA0405-13 PER MEL 21-51-1, NR 1 PACK INOP.SDR WLDA2004121Solenoid · overheatedSMOKE IN COCKPIT WHEN TAXI FOR TAKEOFF, RETURNED TO BLOCKS. FOUND DOOR SOLENOID VERY HOT AND SMOKING. DISCONNECTED AND TAPED WIRES BACK. C/B PULLED AND TRANSFERRED TO DMI M52DE2604-134 PER MEL 52-54-2 CAT "A".SDR WLDA2004108Warning Light · illuminatedAED/ODN COCKPIT DOOR LOCK OVERHEATED INFLIGHT. CABIN CREW SMELLED SMOKE, PULLED DOOR C/B, HEAT AND SMELL DISSIPATED. ENTERED IN DMI M52DE0604-35 CAT-A PER MEL 52-54-2.SDR WLDA2004105Sensor · seizedFRA/KWI ABORTED TAKEOFF AT 130 KTS DUE TO LEVEL II TIRE FAILURE AURAL & VISUAL ALERT. FOUND NR 2 TIRE PRESS SENSING UNIT SEIZED. DEACTIVATED SENSING UNIT AND ENTERED IN DMI M32NO2504-138 PER MEL 32-46-3 CAT-C. PERFORMED RTO INSPECTION AS PER WO CARD 0259 NISDR WLDA2004120Skin · crackedDURING 2C+12A CHECK, FOUND LT WING NR 2 SLAT OUTBOARD SIDE ANGLE/UPPER SKIN PANEL CRACK AT XIS 360. REPAIRED LT WING NR 2 SLAT OUTBOARD SIDE ANGLE/UPPER SKIN PANEL CRACK PER EGAT EI W2004A57B-592 REV.00 (MD-11 SRM VOL.I 57-10-00 FIG 33 AND FIG 10). PERFORMEDSDR WLDA2004119Skin Panel · nickedDURING C2+12A CHECK, FOUND NICK ON RT WING INBOARD FLAP ON STA XIFH 152WITH D=0.039" AND L=3/8". REPAIRED NICK ON RT WING INBOARD FLAP UPPER SKIN AT XIFH 152 PER EGAT EI W2004A57B-585 REV.00 (MD-11 SRM VOL.I 57-10-00 FIG 34 SHEET 3). CONDITION CHECK SATISFACSDR WLDA2004118Support Fitting · corrodedDURING 2C+12A CHECK, FOUND CORROSION IN CENTER WING W/W RT/LT SUPPORT FITTING AT STA Y=1481 X=-31.5 AND X=31.5. REPAIRED CORROSION ON LT/RT FWD TRUNNION FITTING BOOT STRAP OF CENTER MLG PER EGAT EI W2004A53B-590 REV.00 (FAA 8110-3 FORM DATED OCT/04/2004). CONSDR WLDA2004117Web · crackedDURING 2C+12A CHECK, FOUND CRACK AT CENTER CARGO COMPARTMENT STA 1841 L-50 RT WEB. REPAIRED CRACK ON FUSELAGE FRAME WEB STA 1841 L-50 RT PER EGAT EI W2004A53B-559 REV.00 (FAA 8110-3 FORM DATED SEP/23/2004). CONDITION CHECK SATISFACTORY.SDR WLDA2004116Seat Track · corrodedDURING 2C+12A CHECK, FOUND CABIN SEAT TRACK CORRODED AT STA Y=959 X=-8.5. REPAIRED DAMAGED SEAT TRACK PER MD-11 SRM VOL.I 53-70-00, CONDITION CHECK SATISFACTORY.SDR WLDA2004115Skin Panel · scratchedITEM: DURING 2C+12A CHECK, FOUND 3 EA SCRATCH ON EXTERNAL SKIN ON LT HST L/E BETWEEN XFS 275.410 AND XFS 263.762. BLENDED REPAIR PER EGAT EI W2004A 55B-575 REV 00 (1-PGVIM WITH FAA 811-3 FORM DATED SEP/23/2004). CONDITION CHECK FOUND SATISFACTORY.SDR WLDA2004114Skin · dentedDURING 2C+12A CHECK, FOUND SHARP DENT ON LT WING NR 3 SLAT UPPER SKIN AND INNER RIB AT STA XOS 414. REPAIRED DAMAGE AREA PER EGAT EI W2004A 57B-581 REV 00(MD-11 SRM VOL.I 57-10-00 FIG 33). PERFORMED SLAT OPERATION AND CONDITION CHECK, FOUND SATISFACTORY.SDR WLDA2004113Skin Panel · dentedDURING 2C+12A CHECK, FOUND 2EA SHARP DENT ON LT WING NR 1 SLAT UPPER SKIN PANEL LOCATED AT STA XIS 240. REPAIRED DAMAGE AREA PER EGAT EI W2004A 57B-564 REV 00(MD-11 SRM VOL.I 57-10-00 FIG 33 SHEET 6 AND 7). SLAT OPERATION AND CONDITION CHECK SATISFACTORY.SDR WLDA2004112Skin Panel · puncturedDURING 2C+12A CHECK, FOUND LT WING NR 1 SLAT L/E AREA HOLE DAMAGE AT STA XIS 186. REPAIRED DAMAGE AREA PER EGAT EI W2004A 57B-560 REV 00 (MD-11 SRM VOL.I 57-10-00 FIG 33 SHEET 6 AND 7). PERFORMED SLAT OPERATION CHECK, FOUND NORMAL.SDR WLDA2004111Stringer · crackedDURING 2C+12A CHECK, FOUND RT WING FIXED L/E SKIN CRACK ABOUT 10" AND STRINGER DOUBLER CRACK AT STA XOS 906. REPAIRED CRACK ON RT WING FIXED L/E SKIN PANEL AND STRINGER DOUBLER AT STA XOS 906 PER EGAT EI W2004A57B-558 REV 00. (MD-11 SRM VOL.I 57-10-00 FIG 18 SDR WLDA200490Engine · leakingAIR TURNBACK DUE TO LOSS OF NR 2 ENGINE OIL QUANTITY. INDICATION BOXED "0", PERFORMED CHECKLIST NOTED OIL PRESSURE DECREASING; ENGINE WAS SHUTDOWN PERFORMED. REMOVED AND REPLACED NR 2 ENGINE PER WOA T/C 0105 AND MD-11 MM PROCEDURES. ACCOMPLISHED ENGINE RUN USDR WLDA200432Charger · defectiveFRA/NKT AIR TURNBACK DUE TO LEVEL I BATTERY CHARGING ALERT ILLUMINATED DURING NORMAL CRUISE FLIGHT. ELECTRIC SCHEMATIC SHOWED 40V. BATTERY APPEARED TO BE CONTINUOUSLY CHARGED WITH NO DRAW. REMOVED & REPLACED BATTERY CHARGER IAW MM PROCEDURES. PERFORMED EMESDR CHQ000130Compass · out of toleranceDURING CLIMBOUT RECEIVED AN AMBER HEADING MESSAGE ON BOTH PFD'S. PERFORMED COMPASS SWING AND FLUX DETECTOR TEST, OPS CHECK GOOD.SDR CHQ000127Smoke Warning · false activationBAGGAGE SMOKE WARNING AFTER T/O. CREW BLEW FIRE EXTINGUISHERS, NO EVIDENCE OF FIRE. COULD NOT DUPLICATE SMOKE WARNING AND DETECTION SYSTEM, OPS CHECK GOOD. FERRIED A/C TO CMH FOR FIRE BOTTLES.SDR CHQ000116Warning System · activatedOUTBOARD BRAKE FAIL MESSAGE ON EICAS.SDR CHQ00038Indicator · inoperativeNR 1 FUEL INDICATION INOP.SDR 20000710SH013Frame · crackedFRAME WAS FOUND CRACKED. REPAIRED PER AMERICAN EUROCOPTER REPAIR PROCEDURE. (X)
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