N458MC

Service difficulty reports not matched to an aircraft · 18

They name N458MC, 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 = 'N458MC' 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 UIEA2015050500255Relay · faultyLEFT CDU INTERMITTENT UPPER EICAS BLANK. R & R STDBY POWER TRANSFORMER RELAY R7227 IAW AMM 24-29-03 401. OPERATIONS CHECKED OK.May 5, 2015 · N458MC · Boeing 747446 · AC Generation SystemSDR UIEA2014120200624Autopilot Sys · malfunctionedDESCENDING ACFT ABRUPTLY PITCHED UP & STARTED TO CLIMB ON AUTOPILOT. DISCONNECT AUTOPILOT & RE-ENGAGED LATER & OPERATIONS WERE NORMAL. VERIFIED NO CMC ACTIVE FAULTS. PERFORMED AUTO LAND UNIQUE TEST & PASSED IAW AMM 27-00-00.Dec 1, 2014 · N458MC · Boeing 747446 · Autopilot SystemSDR UIEA2013061100325Lamp · burned outEMERGENCY LIGHT IN STAIRWELL TO UPPER DECK DOES NOT ILLUMINATE. RELAMPED EMERGENCY LIGHT IN STAIRWELL TO UPPER DECK IAW AMM 33-51-07-962-001. TEST GOOD.Jun 10, 2013 · N458MC · Boeing 747446 · Emergency LightingSDR UIEA2013022500105Structure · chafedLT WING L/E NR 9 L/C FLAP BULLNOSE INBD EDGE FOUND CHAFED. LT WING L/E NR 9 L/C FLAP BULLNOSE INBD EDGE REPAIRED IAW R1-57-44-16155, REV A.Feb 25, 2013 · N458MC · Boeing 747446 · Trailing Edge FlapsSDR UIEA2013022500104Stiffener · crackedLEFT WING OTBD REFUELING PANEL, ATTACH STIFFENING ANGLE OTBD CORNER FOUND CRACKED. LT WING OTBD REFUELING PANEL, ATTACH STIFFENING ANGLE REPLACED IAW R1-52-49-10154, REV A.Feb 23, 2013 · N458MC · Boeing 747446 · Wing Miscellaneous StructureSDR UIEA2013022500103Structure · chafedLT WING L/E NR 10 L/C FLAP BULL NOSE OTBD EDGE FOUND CHAFED. LT WING L/E NR 10 L/C FLAP BULL NOSE OTBD EDGE REPAIRED IAW R1-57-44-10156, REV A.Feb 21, 2013 · N458MC · Boeing 747446 · Trailing Edge FlapsSDR UIEA2012070300294Stowage Box · damagedCREW OXYGEN WAS FOUND TO BE LOW. ON INSPECTION AND LEAK CHECK AFTER BOTTLE REPLACEMENT IAW AMM 12-15-08, THE CAPTAIN'S OXYGEN MASK STOWAGE BOX WAS FOUND TO BE DAMAGED AND LEAKING. THE CAPTAIN'S OXYGEN MASK STOWAGE BOX WAS REPLACED IAW AMM 35-11-18. LEAK AND Jul 3, 2012 · N458MC · Boeing 747446 · Crew Oxygen SystemSDR UIEA2012022300057Structure · damagedDURING MX WALKAROUND, FOUND DAMAGE TO THE NR 2 ENGINE THRUST REVERSER CORE COWL AFT EXTRUSION.Feb 22, 2012 · N458MC · Boeing 747446 · Engine Thrust ReverserSDR UIEA2011122100726Seal · puncturedDURING A-3 CHECK AT BFM, MX FOUND DAMAGE TO THE LT INBD T/E MID FLAP-RUBBING SHEET/STRIP (PN 65B08436-35) OF THE COMPRESSION SEAL AT WBL 129.30, MEASURING 2.3 INCHES WIDE; X 15" LONG. A PUNCTURE DAMAGE (0.5 " WIDE X 0.8 " LONG) WAS ALSO FOUND ON THE BODY RIB Dec 20, 2011 · N458MC · Boeing 747446 · Trailing Edge FlapsSDR UIEA2011103100633Insulation · delaminatedDURING WALKAROUND, MX FOUND THE NR 4 RT T/R INSULATION DAMAGE AS FOLLOWS (REF FIG 1) DELAMINATIONS AND PUNCTURE OF INSULATION FROM HONEYCOMB STRUCTURE IS AS FOLLOWS: DELAMINATED AREA IS 19.0" FROM FRAME TO FRAME AND 35.0" TOP TO BOTTOM. THE PUNCTURE IN THE MOct 30, 2011 · N458MC · Boeing 747446 · Engine Thrust ReverserSDR UIEA2011041200245Landing Gear · misinstalledDURING D-CHECK AT SIN, LANDING GEARS WERE REPLACED; UPON OPS CHECKS, MX FOUND THE LT AMP; RT BODY GEARS- UPPER JURY STRUT PLATES MOUNTING BOLTS BEING INSTALLED TOO LONG, RESULTING IN RIDING CONDITION AGAINST THE DOWNLOCK SENSORS (REF FIGURE 1). (DISPOSITION WApr 12, 2011 · N458MC · Boeing 747446 · Main Landing GearSDR UIEA2011032800168Frame · unknownDURING SB 747-53A2507 INSP AT BS 1220, S8L LOCATION COMMON TO FRAME WEB, FRAME DOUBLER AND FRAME CHORD. (THE REPAIR WAS ACCOMPLISHED IAW RI NR N458MC-11-002 IAW REPAIR INSTRUCTIONS PROVIDED BY IN SR 1-1817615622. THE REPAIR WAS APPROVED BY FAA FORM 8100-9)Mar 28, 2011 · N458MC · Boeing 747446 · Fuselage Main, FrameSDR UIEA2011032500165Frame · crackedDURING D INSPECTION OF DATUM ACFT IAW EO 4453A197, CRACK WAS FOUND ON FRAME AT BS 1160 (RT AT STR 9). (THE DAMAGED FRAME WAS REPAIRED IAW PART 5 OF EO 4453A197, REV D (SRM 53-40-07, REPAIR 3). IAW PART 5 OF EO, THE FRAME CRACKS THAT CANNOT BE REMOVED BY DOINMar 25, 2011 · N458MC · Boeing 747446 · Fuselage Main, FrameSDR UIEA2011031800158Frame · crackedTHE LT NR 4 FAN REVERSER EXHIBITED A CRACK ON THE TORQUE BOX FWD FRAME. (IN THIS INSTANCE THE CRACK HAD BEEN STOP DRILLED AND REGULARLY INSPECTED BY THE PRIOR OPERATOR JAL. AS THE ACFT WAS IN HEAVY CHECK, SIAEC WAS ADVISED TO PERFORM A PERMANENT REPAIR IAW SMar 18, 2011 · N458MC · Boeing 747446 · Engine Thrust ReverserSDR UIEA2011030600154Skin · damagedTHE LIGHTNING STRIKE DAMAGE TO 65B07656-259 SKIN WAS DETECTED AT BS 385 AND S31AL. THE DEPTH OF LIGHTNING STRIKE DAMAGE WAS .015 INCHES AS RECORDED IAW SIAEC NRC 005380. (THE LIGHTNING STRIKE DAMAGED AREA WAS LOCALIZED IN 65B07656-259 SKIN ONLY. THE LIGHTNIMar 6, 2011 · N458MC · Boeing 747446 · Fuselage Main, Plate/SkinSDR UIEA2011022400178Skin · damagedFUSELAGE SKIN INSP DURING "D-CHECK", FOUND LIGHTNING STRIKE ON CROWN SKIN AT STA 345 BETWEEN STR 1R AND 2R (SOLID FASTENER REPAIR CARRIED OUT IAW B744SF SRM 53-00-01. REPAIR 9 SECTION I, PAR S.)Feb 24, 2011 · N458MC · Boeing 747446 · Fuselage Main, Plate/SkinSDR UIEA2011022400145Skin · damagedDURING D-CHECK OF THE DATUM AIRPLANE, A LIGHTNING STRIKE DAMAGE WAS FOUND ON RT FUSELAGE SKIN AT BS 345, S1R-2R . DAMAGE WAS FOUND TO BE BEYOND THE ALLOWABLE LIMIT IAW SRM 53-00-01, FIG 101. (THE DAMAGE WAS REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 9 AND IAFeb 24, 2011 · N458MC · Boeing 747446 · Fuselage Main, Plate/SkinSDR UIEA2011022300142Skin · damagedLIGHTNING STRIKE DAMAGE FOUND AT STA 385 LT, S-31A, DEPTH FOUND APPROX 0.015, LENGTH APPROX 1" TO C/OUT FUSELAGE SKIN EXTERNAL REPAIR IAW SRM 53-00-01. CAT B REPAIR CARRIED OUT IAW MSG SEP-TLS-11-0036-02B. EXTERNAL DOUBLER AND TRIPLER FABRICATED.Feb 23, 2011 · N458MC · Boeing 747446 · Fuselage Main, Plate/Skin
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