N418EA, cancelled Mar 25, 2013

Service difficulty reports · 27

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 = 'N418EA' AND deregistration_id = 'N418EA-2013-03-25'
  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 TWAA9909503Longeron · damagedDURING CHECK-C MAINTENANCE, THE AFT CANTED BELT RING AT STA 1243, LONGERON 3L, HAD ELONGATED HOLES AT ATTACH POINTS. REPAIRED LONGERON SECTION PER SRM 53-02, PAGE 53.Jul 7, 1999 · N418EA · Doug DC951 · Fuselage Main, Longeron/StringerSDR TWAA9909502Longeron · damagedDURING CHECK-C MAINTENANCE, THE CANTED BELT RING AT STA 1243, LONGERON 4L, HAD ELONGATED HOLES AT THE BELT RING ATTACH POINTS. INSTALLED A SECTION OF LONGERON PER SRM 53-02, FIG 18.Jul 1, 1999 · N418EA · Doug DC951 · Fuselage Main, Longeron/StringerSDR TWAA9902703Slide · air leakTHE FWD LT CABIN DOOR ESCAPE SLIDE WAS FOUND WITH LOW AIR BOTTLE PRESSURE. REPLACED THE SLIDE PER MC82501. CHECK-C 3-30-98 STL.Feb 20, 1999 · N418EA · Doug DC951 · Escape SlideSDR TWAA9819502Coalescer · contaminatedAFTER SOME TIME IN CRUISE FLIGHT AN OFFENSIVE ODOR WAS REPORTED IN THE FRONT PART OF THE CABIN. THERE WERE SOME REPORTS OF THROAT IRRITATION. REPLACED BOTH WATER SEPARATORS AND RAN THE PACKS ON FULL HOT FOR TWO HOURS. CHECK-C 3-30-98 STL.Dec 8, 1998 · N418EA · Doug DC951 · Humidity Control SystemSDR TWAA9819501Coalescer · contaminatedAN OFFENSIVE ODOR WAS REPORTED IN THE GALLEY AND FRONT PORTION OF THE AIRPLANE. SOME THROAT AND EYE IRRITATION. CLEANED THE ENTRANCE AND GALLEY FLOORS, OVERHEAD BAG COMPARTMENTS, AND PSU'S IN AREA. REPLACED BOTH AIR CONDITIONING WATER SEPARATORS. CHECK-C 3Dec 8, 1998 · N418EA · Doug DC951 · Humidity Control SystemSDR TWAA9809101Skin · delaminatedSTL - DURING OP 9 MAINTENANCE CHECK, FOUND DELAMINATION IN RT WING UPPER PANEL JUST FWD OF AILERON. REMOVED AND REPLACED UPPER WING PANEL JUST FWD OF AILERON. REF SRM 51-30-2 AND 20-30-0. (M)Mar 20, 1998 · N418EA · Doug DC951 · Wing, Plate/SkinSDR TWAA9808905Support · crackedSTL - DURING OP 9 MAINTENANCE CHECK, FOUND CRACK IN LOWER ANGLE ON RT SIDE OF LOWER RADAR SUPPORT BRACKET INSIDE NOSE WHEEL WELL. FABRICATED NEW ANGLE PER SRM 51-10-02. INSTALLED ANGLE PER SRM 51-30-02. (X)Mar 20, 1998 · N418EA · Doug DC951 · Fuselage Miscellaneous StructureSDR TWAA9809404Support · crackedMCI - DURING OP 9 MAINTENANCE CHECK, FOUND ONE INCH CRACK IN CENTER OF CENTER SUPPORT IN BIRD CAGE. REPAIRED CRACK IN CENTER SUPPORT IN BIRD CAGE PER SRM 53-01 PAGE 10. (X)Mar 18, 1998 · N418EA · Doug DC951 · Fuselage Miscellaneous StructureSDR TWAA9808904Support · crackedSTL - DURING OP 9 MAINTENANCE CHECK, FOUND .0312 INCH IN CRACK IN UPPER ANGLE ON RT SIDE OF LOWER RADAR SUPPORT BRACKET, INSIDE NOSE WHEEL WELL. CLEANED UP CRACK AND BLENDED TO SRM LIMITS PER SRM 53-01, PAGE 4, FIG 1. (X)Mar 18, 1998 · N418EA · Doug DC951 · Fuselage Miscellaneous StructureSDR TWAA9715301Retract Mech · malfunctionedSTL - FLT 407 - NOSE GEAR DOOR VIBRATION AFTER GEAR RETRACTED ON TAKEOFF. CYCLED GEAR, NO HELP. UPON RETURN TO GATE FOUND LEFT NOSE GEAR DOOR DOWN. CLOSED GEAR DOOR AND PERFORMED GEAR DOOR PULL CHECK. CHECKED NORMAL. (M)Dec 29, 1997 · N418EA · Doug DC951 · Landing Gear Door Retract SectionSDR TWAA9762002Retract Mech · malfunctionedDFW - FLT 374 - AFTER TAKEOFF, LEFT NOSE GEAR DOOR DID NOT CLOSE FOLLOWING GEAR RETRACTION. INSPECTED NOSE GEAR DOOR LINKAGE AND MECHANISM AND PROPERLY LOCK GEAR DOOR IN UP POSITION. (M)May 21, 1997 · N418EA · Doug DC951 · Landing Gear Door Retract SectionSDR TWAA9751001Coffeemaker · failedSTL - FLT 619 - DURING CRUISE, COFFEEMAKER EMITTED SMOKE. REMOVED AND REPLACED WORN COFFEEMAKER, MFG P/N 50198A, MANUFACTURED BY NORDSKOG INDUSTRIES, INC. OPERATIONAL CHECK NORMAL. (M)Apr 18, 1997 · N418EA · Doug DC951 · Buffet/GalleysSDR 96ZZZX4916Power Supply · inoperativeSTL - FLT 517 - DURING GROUND OPERATION CHECK, OVERWING EXIT LIGHTS REMAINED ILLUMINATED. FOUND BATTERY PACK WEAK, MFG P/N 41B030CF00101, AND POWER SUPPLY MALFUNCTIONING, MFG P/N 60-1177-5. REPLACED BATTERY PACK AND POWER SUPPLY AND OVERWING EXIT LIGHT OPERASep 8, 1996 · N418EA · Doug DC951 · Emergency LightingSDR 96ZZZX4915Battery Pack · dischargedSTL - FLT 517 - DURING GROUND OPERATION CHECK, OVERWING EXIT LIGHTS REMAINED ILLUMINATED. FOUND BATTERY PACK WEAK, MFG P/N 41B030CF00101, AND POWER SUPPLY MALFUNCTIONING, MFG P/N 60-1177-5. REPLACED BATTERY PACK AND POWER SUPPLY AND OVERWING EXIT LIGHT OPERASep 8, 1996 · N418EA · Doug DC951 · Emergency LightingSDR 96ZZZM629Filter Clog Ind · malfunctionedBNA - DURING DESCENT NR 2 ENGINE OIL FILTER CLOG LIGHT ILLUMINATED. REMOVED AND REPLACED OIL FILTER. PLACARDED FILTER CLOG INDICATOR LIGHT. (M)Mar 4, 1996 · N418EA · Doug DC951 · Engine Oil Indicating SystemSDR 95ZZZM684Floor Beam · crackedSTL - DURING C-CHECK, FOUND A TWO INCH CRACK IN FLOOR BEAM AT CENTER AISLE AREA, STATION 239. REPAIRED PER ARA 8749.Oct 6, 1995 · N418EA · Doug DC951 · Fuselage Main, Floor BeamSDR 95ZZZM542Control Cable · failedSTL - DURING CLIMB AFTER LANDING GEAR RETRACTION, HAD SEVERE VIBRATION FROM NOSE GEAR AREA. CYCLED LANDING GEAR AND VIBRATION CONTINUED. FOUND LEFT NOSE LANDING GEAR DOOR STOP CABLE, MFG P/N 3926528-1, TENSION LOW. RIGGED CABLE TENSION AND NOSE LANDING GEARSep 13, 1995 · N418EA · Doug DC951 · Landing Gear Door Retract SectionSDR 95ZZZX2348Longeron · crackedSTL - DURING SPECIAL CHECK, FOUND CRACK IN LONGERON 4L, STA 832. REPAIRED PER SRM 53-02, FIGURE 2. AIRCRAFT TOTAL TIME: 39,023 HOURS; 48,633 CYCLES.Apr 11, 1995 · N418EA · Doug DC951 · Fuselage Main, Longeron/StringerSDR 95ZZZX2344Longeron · crackedSTL - DURING SPECIAL CHECK, FOUND A .50 INCH CRACK IN LONGERON 3L, STA 794 AND STA 832. REPAIRED PER SRM 53-02, FIGURE 2. AIRCRAFT TOTAL TIME: 39,023 HOURS; 48,633 CYCLES.Apr 11, 1995 · N418EA · Doug DC951 · Fuselage Main, Longeron/StringerSDR 95ZZZW607Longeron · crackedSTL - DURING SPECIAL CHECK, FOUND A .5 INCH CRACK IN LONGERON 3L, STATION 794 AND STA 832. REPAIRED PER SRM 53-02, FIGURE 2.Apr 11, 1995 · N418EA · Doug DC951 · Fuselage Main, Longeron/StringerSDR 95ZZZW604Longeron · crackedSTL - DURING SPECIAL CHECK, FOUND A CRACK IN LONGERON 4L, STATION 832. REPAIRED PER SRM 53-02, FIGURE 2.Apr 11, 1995 · N418EA · Doug DC951 · Fuselage Main, Longeron/StringerSDR 95ZZZX2350Longeron · crackedSTL - DURING SPECIAL CHECK, FOUND A 1.50 INCH CRACK IN LONGERON 4L, STA 794. REPAIRED PER SRM 53-02, FIGURE 2. AIRCRAFT TOTAL TIME: 39,023 HOURS; 48,633 CYCLES.Apr 10, 1995 · N418EA · Doug DC951 · Fuselage Main, Longeron/StringerSDR 95ZZZX2347Longeron · crackedSTL - DURING SPECIAL CHECK, FOUND A ONE INCH CRACK IN LONGERON 2R, STA 832. REPAIRED PER SRM 53-02, FIGURE 2. AIRCRAFT TOTAL TIME: 39,023 HOURS; 48,633 CYCLES.Apr 10, 1995 · N418EA · Doug DC951 · Fuselage Main, Longeron/StringerSDR 95ZZZX2346Longeron · crackedSTL - DURING SPECIAL CHECK, FOUND .50 INCH CRACK IN LONGERON 3R, STA 734. REPAIRED PER SRM 53-02, FIGURE 2. AIRCRAFT TOTAL TIME: 39,023 HOURS; 48,633 CYCLES.Apr 10, 1995 · N418EA · Doug DC951 · Fuselage Main, Longeron/StringerSDR 95ZZZW609Longeron · crackedSTL - DURING SPECIAL CHECK, FOUND A 1.5 INCH CRACK IN LONGERON 4L, STA 794. REPAIRED PER SRM 53-02, FIGURE 2.Apr 10, 1995 · N418EA · Doug DC951 · Fuselage Main, Longeron/StringerSDR 95ZZZW606Longeron · crackedSTL - DURING SPECIAL CHECK, FOUND A .5 INCH CRACK IN LONGERON 3R, STATION 734. REPAIRED PER SRM 53-02, FIGURE 2.Apr 10, 1995 · N418EA · Doug DC951 · Fuselage Main, Longeron/StringerSDR 95ZZZW603Longeron · crackedSTL - DURING SPECIAL CHECK, FOUND A ONE INCH CRACK IN LONGERON 2R, STATION 832. REPAIRED PER SRM 53-02, FIGURE 2.Apr 10, 1995 · N418EA · Doug DC951 · Fuselage Main, Longeron/Stringer
Back to N418EA, cancelled Mar 25, 2013