N513NA

Service difficulty reports not matched to an aircraft · 28

They name N513NA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N513NA' AND registry_match IS NULL
  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.

SDR ANCF200800032Landing Gear · malfunctionedAIR TURN BACK, EICAS MSG GEAR DISAGREE AND GEAR DOORS DISPLAYED WITH GEAR HANDLE UP. LT GEAR LIGHT, GEAR AMBER LIGHT AND DOORS AMBER LIGHT ILLUMINATE. IAW AMM 32-20-09 FIM PROCEDURE THE PSBU BITE TEST WAS PERFOMED AND NO FAULT CODE AND MAIN NLG PINS WERE REMOJan 4, 2009 · N513NA · Boeing 7572T7 · Main Landing GearSDR ANCF200800008Warning Light · illuminatedFLAP LEVER UP, FLAP POINTERS UP, EICAS MSG LE SLAT ASYM, LEADING EDGE LIGHT ON DURING CLIMB, RUDDER TRIM 3-4 UNITS TO THE RIGHT TO CENTER COLUMN. FIM PROCEDURE 27-81-00 FIG 105 WAS ACCOMPLISHED. IN ACCORDANCE AMM 27-51-01/201 FLAP SLAT ELECTRONIC UNIT NR 1 AApr 13, 2008 · N513NA · Boeing 7572T7 · Trailing Edge Flap Control SystemSDR ANCF200800004Air Duct · leakingEICAS MESSAGE "L ENG OVHT" DISPLAYED, WITH "ENG OVHT" LIGHT ILLUM. LIGHT REMAINED ILLUM AFTER THRUST REDUCTION, ENGINE WAS SHUTDOWN , (LIGHT EXTINGUISHED INITIALLY AFTER THRUST REDUCTION BUT AFTER FEW SECONDS IT ILLUMINATED AGAIN). PERFORM FIM 26-11-00 AND FFeb 8, 2008 · N513NA · Boeing 7572T7 · Pneumatic Distribution SystemSDR ANCF200700015Filter · dirtyDURING CLIMB CROSSING FL 300 ASC TO FL 370, HAD SMOKE COMING FROM THE PEDALS IN THE COCKPIT. CHECK LIST WAS PERFORMED AND THEN DECIDED GOING TO MIA BECAUSE OF THE SMOKE AND ALSO THE CABIN CREW TOLD US THAT THERE WAS A LOT OF SMOKE IN THE PASSENGER CABIN. WHEJun 6, 2007 · N513NA · Boeing 7572T7 · Air Distribution SystemSDR ANCF200600046Engine · failedLT ENGIINE SURGED DURING CONSTANT POWER DURING CLIMB AT 6.000 FT. ENGINE OPS NORMAL AFTER SURGE AT LOW THRUST. BOROSCOPE INSPECTION ACCOMPLISHED TO INTERMEDIATE PRESSURE COMPRESOR, HIGH PRESSURE COMPRESOR, COMBUSTION CHAMBER, HIGH PRESSURE TURBINE BLADES, LOMar 12, 2007 · N513NA · Boeing 7572T7 · Engine (Turbine/Turboprop)SDR ANCF200600034Access Panel · loosePILOT REPORT: RT ENG COVER UPPER SIDE SEPARATE DURING TAKE OFF. RT ENG INSPECTED. NO VISIBLE DAMAGE FOUND INTERNAL WING, EMPENNAGE AND FUSELAGE SKIN WERE INSPECTED NO FINDINGS, IAW AMM 05-51-18 PAG 204. THE PANEL 442AL WAS INSTALLED IAW AMM 54-52-01 PAG 401.Sep 23, 2006 · N513NA · Boeing 7572T7 · Nacelle/Pylon, Plate/SkinSDR 513NA0011Warning Light · illuminatedABORTED TAKEOFF DUE TO SPOILER MASTER CAUTION LIGHT. PERFORMED BITE PROCEDURE, RESET SYSTEM BY FIM 27-61-00. OPERATIONAL CHECK OK. NEXT FLIGHT: SPOILER OVERHEAD LIGHT AND EICAS MESSAGE CAME ON IN FLIGHT. NO ADVERSE FLIGHT CONTROLS NOTICED. ACCOMPLISHED BITDec 12, 2004 · N513NA · Boeing 7572T7 · Drag Control SystemSDR 513NA0010Gearbox · vibrationON TAXI OUT, HAD EICAS MESSAGE: LT OIL FILTER. FOUND METAL ON CHIP DETECTOR FOR HIGH SPEED GEAR BOX. REPLACED MAIN OIL FILTER AND SCAVENGE FILTER AND RAN ENGINE. LT ENGINE HAD VIBRATION DURING POWER RUN. SENT MECHANICS. 10/10/2004: REPLACED HIGH SPEED GOct 4, 2004 · N513NA · Boeing 7572T7 · Turbine Engine Accessory DriveSDR 513NA0009Bulb · burned outEMERGENCY LIGHT OVER 11 DEF INOP. PLACED ON MEL 33-51-1. RELAMPED AND OPS CHECKED OK PER MM 33-50.Jul 30, 2004 · N513NA · Boeing 7572T7 · Emergency LightingSDR 513NA0008Bolt · missingDURING WALK-AROUND, FOUND NR 7 MAIN WHEEL ASSEMBLY TIE BOLT MISSING. REPLACED NR 7 MAIN WHEEL ASSEMBLY PER MM 32-45-01.Jun 28, 2004 · N513NA · Boeing 7572T7 · FastenersSDR 513NA0007Indicator · malfunctionedON DESCENT INTO KSFB, NO AUTO LAND DISPLAYED ON AUTO LAND STATUS INDICATOR. RESET RIGHT FCC AND RAN MCDP TEST PER MM 22-10-00. ALL AUTO PILOT ENGAGE AND FCC CHECKS GOOD.Jun 7, 2004 · N513NA · Boeing 7572T7 · Autopilot SystemSDR 513NA0006Bolt · missingNR 2 MAIN LANDING GEAR TIRE HAS TWO WHEEL BOLTS MISSING. REPLACED NO. TWO MAIN LANDING GEAR WHEEL/TIRE ASSEMBLY PER MM 32-45-01.May 6, 2004 · N513NA · Boeing 7572T7 · Wheel/Ski/FloatSDR 513NA0005Bolt · missingTHREE TIE BOLTS MISSING ON THE NR 5 MAIN WHEEL ASSEMBLY. REPLACED LEFT OUTBOARD TIRE ASSEMBLY PER MM 32-45-01.Apr 15, 2004 · N513NA · Boeing 7572T7 · FastenersSDR 513NA0004Battery Pack · inoperativeMID CABIN FLOOR ILLUMINATION LIGHTS AND R3 DOOR AND OVERWING EMERGENCY LIGHTS INOP. REPLACED M734 EMERGENCY LIGHT BATTERY PACK PER MM 33-51-0.Apr 6, 2004 · N513NA · Boeing 7572T7 · Emergency LightingSDR 513NA0003Bolt · missingNR 7 TIRE ASEMBLY MISSING 3 BOLTS. REPLACED NR 7 MAIN TIRE PER MM 32-45-01.Apr 1, 2004 · N513NA · Boeing 7572T7 · Wheel/Ski/FloatSDR 513NA0002Bolt · missingMAIN WHEEL BOLTS MISSING. REPLACED NR 8 MAIN TIRE (WHEEL ASSEMBLY) PER MM 32-45-01.Feb 29, 2004 · N513NA · Boeing 7572T7 · FastenersSDR 513NA0001Window · crackedLEFT FWD WINDOW CRACKED. REPLACED NR 1 FWD WINDOW PER MM 56-11-01 AND REPLACED WINDOW HEAT CONTROLLER PER MM 30-41-01. OPS CHECKS GOOD.Jul 24, 2003 · N513NA · Boeing 7572T7 · Flight Compartment WindowsSDR HN62003F00000Cable · chafedNR 2 ENGINE GENERATOR FEEDER CABLES ARE CHAFING ON NR 6 SLAT INBOARD AUXILLARY TRACK. MOUNT PLATE FOR CLAMP IS MISPOSITIONED BELOW AUXILLARY TRACK. THERE ARE 2 POSITIONS FOR THE MOUNT PLATE, IN THE UPPER POSITION THE AUXILLARY TRACK CHAFES THE FEEDER CABLE. Jan 20, 2003 · N513NA · Boeing 7572T7 · Electrical Power System WiringSDR 02090901Hydraulic Line · burstJust prior to takeoff, the "R Hyd Press" EICAS Msg. came on and right hyd qty had dropped to "0.45RF". Aircraft returned to the gate. further investigation revealed the right aft outboard (#8) Brake flex line had ruptured. Line was removed and replaced as per Sep 5, 2002 · N513NA · Boeing 7572T7 · Brake Anti-Skid SectionSDR 02062501WindowDuring climb out at 25,000 ft., heard a loud bang from back. Flt attendants said window at Row 1D cracked, Aircraft returned to base, an uneventful landing was accomplished.Jun 22, 2002 · N513NA · Boeing 7572T7 · Passenger Compartment WindowsSDR 2002F00241Duct · leakingDURING CLIMB, PASSING THROUGH 8,000 FT MSL, LT ENGINE OVERHEAT EICAS' MESSAFE CAME ON. SECURED BLEED VALVE, RETARDED THRUST. MESSAGE EXTINGUISHED. INVESTIGATION REVEALED HP6 DUCT LEAKING. REPLACED HP6 DUCT, LEAK CHECKED GOOD. (M)Feb 23, 2002 · N513NA · Boeing 7572T7 · Engine Bleed Air SystemSDR 02022502Duct · leakingDURING CLIMB, PASSING THROUGH 8,000 FT MSL, LENG OVERHEAT EICAS MESSAGE CAME ON. SECURED BLEED VALVE, RETARDED THRUST; MESSAGE EXTINGUISHED. INVESTIGATION REVEALED HP6 DUCT LEAKING. REPLACED HP6 DUCT, LEAK CHECKED GOOD.Feb 23, 2002 · N513NA · Boeing 7572T7 · Pneumatic Distribution SystemSDR 2001F00746Oil System · lowDURING CRUISE, APU OIL ADD LIGHT CAME ON, APU SHUT DOWN. ATTEMPTED RESTART TWICE WITH NO SUCCESS. RIGHT IDG PREVIOUSLY PLACED ON MEL. ACCOMPLISHED UNEVENTFUL, UNSCHEDULED LANDING. SERVICE APU WITH 3 QUARTS OF OIL, CHECKED CHIP DETECTORS. PERFORMED APU BITNov 8, 2001 · N513NA · Boeing 7572T7 · APU Oil SystemSDR 20010430AP006Warning System · activatedON APPROACH, IN LANDING CONFIGURATION, LE SLAT DISAGREE AND TE FLAP DISAGREE EICAS MESSAGE ILLUMINATED. EXTENDED USING ALTERNATE EXTENSION. ACCOMPLISHED OPERATIONAL CHECK OF THE FLAP AND SLAT SYSTEM. NO FAULTS FOUND BITE CHECK OF FSEU. NO FAULTS FOUND. NOMar 28, 2001 · N513NA · Boeing 757200 · Central WarningSDR 20010425AP007Power Supply · inoperativeNUMEROUS ESCAPE PATH LIGHTING LIGHTS ON SEATS NOT WORKING. REPAIRED WIRING AT POWER SUPPLY AND REPLACED POWER SUPPLY. (M)Mar 8, 2001 · N513NA · Boeing 757200 · Lighting SystemSDR 20010112SG037Control Cable · out of rigON TAKEOFF, HEADING EDGE SLATS STOPPED IN INTERMEDIATE POSITION AND A SLAT DISAGREE MESSAGE WAS RECEIVED. INVESTIGATION REVEALED CABLE TO LEFT PDU OUT OF RIG. RIGGED PER AMM, OPS CHECKED GOOD. (M)Nov 13, 2000 · N513NA · Boeing 757200 · Leading Edge Slat Control SystemSDR 20010108AP002Pressure Switch · failedON DESCENT, ENGINE NR 1 ROLLED BACK AND FLAMED OUT. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. UPON INVESTIGATION TRANCIENT PRESSURE UNIT (TPU) BITE WAS ACCOMPLISHED REVEALING INTERNAL FAILURE CODES FOR THE TPU. TPU AND BUCU WERE REPLACED, ENGINE RUN AND FLIGHOct 5, 2000 · N513NA · Boeing 757200 · Engine Bleed Air SystemSDR 20010425AP001Power Supply · inoperativeNUMEROUS ESCAPE PATH LIGHTING LIGHTS ON SEATS NOT WORKING. REPAIRED WIRING AT POWER SUPPLY AND REPLACED POWER SUPPLY. (M)Aug 8, 2000 · N513NA · Boeing 757200 · Emergency Lighting
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