N141WE

Service difficulty reports · 26

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 = 'N141WE' AND registry_match = 'registration'
  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 22AA20090203Indicator · inoperativeTAKEOFF ABORTED FROM MHLM AT 110 KTS. ON TAKEOFF ROLL ENGINE NR 2 EPR GAUGE FAILED AT 1.20 EPR. POINTER AND ANALOG DIGITS FAILED IN PLACED WITH NO FLAG IN VIEW. TRANSFERRED TO DMI 22467, PLACARD INSTALLED, PER MEL 77-3-2, PAGE 77-2. REMOVED AND REPLACED NRFeb 22, 2009 · N141WE · Doug DC1040F · Engine Pressure Ratio (EPR)SDR 2003F00115Cowling · delaminatedDURING SCHEDULED MAINTENANCE, NR 1 FAN COWL PREVIOUS REPAIR WAS FOUND DELAMINATED ON THE INBOARD LOWER CORNER. REPAIRED IAW AS11 DRAWING AS11476, DOUBLER REPAIR. AIRCRAFT RETURNED TO SERVICE. (M)Dec 4, 2002 · N141WE · Doug DC1040F · Engine Cowling SystemSDR 2003F00089Thrust Reverser · debondedDURING ROUTINE MAINTENANCE, THE NR 2 ENGINE THRUST REVERSER INNER SURFACE WAS FOUND DEBONDED. REMOVED DEBONDED AREA, FABRICATED DOUBLER REPAIR AND REPAIRED AREA IAW AS11 DRAWING AS11465, AND AN 8110-3 WAS ISSUED. RETURNED AIRCRAFT TO REVENUE SERVICE. (M)Nov 3, 2002 · N141WE · Doug DC1040F · Engine Thrust ReverserSDR 2002F00629Hydraulic System · malfunctionedFLT 558 - MSLP-KMIA - DURING CLIMB-OUT, LOST HYDRAULIC SYSTEMS ONE AND TWO. RETURNED TO MSLP AND A NORMAL LANDING WITHOUT INCIDENT WAS MADE. NR 1 TIRE MISSING A LARGE SECTION OF TREAD, NR 5 TIRE DAMAGED BY GROUND DEBRIS. BOTH NR 1 AND 5 WHEELS WERE INTACT. Apr 27, 2002 · N141WE · Doug DC1040F · Hydraulic System, MainSDR 2002F00334Thrust Reverser · damagedDURING C-CHECK, THE NR 2 ENGINE THRUST REVERSER LEFT COWL SKIN WAS FOUND DAMAGED ON LEADING EDGE. A DOUBLER WAS INSTALLED IAW REO-G08284. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M)Dec 1, 2001 · N141WE · Doug DC1040F · Engine Collector/Tailpipe/NozzleSDR 2002F00333Structure · corrodedDURING C-CHECK, THE FORWARD LT AIR CONDITIONING BAY CAP ANGLE AT STATION 595 BETWEEN LONGERON 47L AND 48L WAS CORRODED PAST SRM LIMITS. A REPAIR DOUBLER WAS INSTALLED ON THE EXTERIOR OF THE SKIN TO REINFORCE THE BLEND AREA. THE AIRCRAFT WAS RETURNED TO REVENDec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, StructureSDR 2002F00332Longeron · crackedDURING C-CHECK, LONGERON 13L WAS FOUND CRACKED BETWEEN FASTENER HOLES AT CANTED STATION Y2153. LONGERON 13L WAS REPAIRED. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M)Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, Longeron/StringerSDR 2002F00331Structure · corrodedDURING C-CHECK, THE LEFT NOSE WHEEL WELL CHORD VERTICAL LEG WAS FOUND CORRODED AND BLENDED JUST PAST SRM REPAIRABLE LIMITS. A REPAIR ANGLE WAS INSTALLED IAW TIMCO REO-G08344 REV IR AND REO G8336 REV IR. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M)Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, StructureSDR 2002F00330Thrust Reverser · damagedDURING C-CHECK, THE NR 2 ENGINE THRUST REVERSER LEFT COWL SKIN WAS FOUND DAMAGED ON LEADING EDGE. A DOUBLER WAS INSTALLED IAW REO-G08284 AND A 8110-3 WAS ISSUED, DER DERT-511032-CE FAR 145 REPAIR AGENCY NR TIPR833K. THE AIRCRAFT WAS RETURNED TO REVENUE SERVIDec 1, 2001 · N141WE · Doug DC1040F · Engine Thrust ReverserSDR 2002F00318Angle · corrodedDURING C-CHECK, THE FORWARD LEFT AIRCONDITIONING BAY CAP ANGLE AT STATION 595 BETWEEN LONGERON 47L AND 48L WAS CORRODED PAST SRM LIMITS. A REPAIR DOUBLER WAS INSTALLED ON THE EXTERIOR OF THE SKIN TO REINFORCE THE BLEND AREA IAW TIMCO REO-GO8333. A 8110-3 WASDec 1, 2001 · N141WE · Doug DC1040F · Fuselage Miscellaneous StructureSDR 2002F00317Longeron · crackedDURING C-CHECK, LONGERON 13L WAS FOUND CRACKED BETWEEN FASTENER HOLES AT CANTED STATION Y2153. LONGERON 13L WAS REPAIRED IAW TIMCO REO-GO8321 REV IR AND FAA FORM 8110-3 WAS ISSUED DER DERY 510314-CE FAR 145 REPAIR AGENCY NR TIPR833K. THE AIRCRAFT WAS RETURNDec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, Longeron/StringerSDR 2002F00316Frame · corrodedDURING C-CHECK, THE LT NOSE WHEEL WELL CHORD VERTICAL LEG WAS FOUND CORRODED AND BLENDED JUST PAST SRM REPAIRABLE LIMITS. A REPAIR ANGLE WAS INSTALLED IAW TIMCO REO-GO8344 REV IR AND REO G8336 REV IR A 8110-3 WAS ISSUED BY DER, DERY 510314-CE FAR 145 REPAIR Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, FrameSDR 2002F00025Frame · corrodedDURING C-CHECK, THE LEFT NOSE WHEEL WELL CHORD VERTICAL LEG WAS FOUND CORRODED AND BLENDED JUST PAST SRM REPAIRABLE LIMITS. A REPAIR ANGLE WAS INSTALLED IAW TIMCO REO-G08344 REV IR AND REO G8336 REV IR. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, FrameSDR 2002F00024Longeron · crackedDURING C-CHECK, LONGERON 13L WAS FOUND CRACKED BETWEEN FASTENER HOLES AT CANTED STATION Y2153. LONGERON 13L WAS REPAIRED IAW TIMCO REO-GO8321 REV IR AND FAA FORM 8110-3. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M)Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, Longeron/StringerSDR 2002F00023Angle · corrodedDURING C-CHECK, THE FORWARD LEFT AIR CONDITIONING BAY CAP ANGLE AT STATION 595 BETWEEN LONGERON 47L AND 48L WAS CORRODED PAST SRM LIMITS. A REPAIR DOUBLER WAS INSTALLED ON THE EXTERIOR OF THE SKIN TO REINFORCE THE BLEND AREA IAW TIMCO REO-G08333. THE AIRCRAFDec 1, 2001 · N141WE · Doug DC1040F · Fuselage Miscellaneous StructureSDR 2002F00022Thrust Reverser · damagedDURING C-CHECK, THE NR 2 ENGINE THRUST REVERSER LEFT COWL SKIN WAS FOUND DAMAGED ON LEADING EDGE. A DOUBLER WAS INSTALLED IAW REO-G08284 AND A 8110-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Dec 1, 2001 · N141WE · Doug DC1040F · Engine Thrust ReverserSDR 2002F00021Frame · corrodedDURING C-CHECK, THE LEFT NOSE WHEEL WELL CHORD VERTICAL LEG WAS FOUND CORRODED AND BLENDED JUST PAST SRM REPAIRABLE LIMITS. A REPAIR ANGLE WAS INSTALLED IAW TIMCO REO-G08344 REV IR AND REO G8336 REV IR. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M)Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, FrameSDR 2002F00020Longeron · crackedDURING C-CHECK, FOUND LONGERON 13L WAS FOUND CRACKED BETWEEN FASTENER HOLES AT CANTED STATION Y2153. LONGERON 13L WAS REPAIRED IAW TIMCO REO-G08321 REV IR AND FAA FORM 8110-3. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Dec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, Longeron/StringerSDR 2002F00019Skin · corrodedDURING C-CHECK, THE FORWARD LEFT AIR CONDITIONING BAY CAP ANGLE AT STATION 595 BETWEEN LONGERON 47L AND 47L WAS CORRODED PAST SRM LIMITS. A REPAIR DOUBLER WAS INSTALLED ON THE EXTERIOR OF THE SKIN TO REINFORCE THE BLEND AREA IAW TIMCO REO-G08333. THE AIRCRAFDec 1, 2001 · N141WE · Doug DC1040F · Fuselage Main, Plate/SkinSDR 2002F00018Thrust Reverser · damagedDURING C-CHECK, THE NR 2 ENGINE THRUST REVERSER LEFT COWL SKIN AS FOUND DAMAGED ON LEADING EDGE. A DOUBLER WAS INSTALLED IAW REO-GO8284 AND A 8110-3 WAS ISSUED. THE AIRCRAFT WAS RETURNED TO REVENUE SERVICE. (M)Dec 1, 2001 · N141WE · Doug DC1040F · Engine Thrust ReverserSDR 20001128AP001Spar Cap · corrodedDURING C-CHECK, FOUND CORROSION ON LT WING UPPER REAR SPAR CAP AFT FLANGE AT THREE LOCATIONS, STATIONS ORS 433, 451 AND 455. FOUND CORROSION WAS REMOVED AND FASTENERS WERE REPLACED IAW EO CH-00-007 AND BOEING TLX ALI-FCO 00-0244H DTD 10 APR 00. RELEASED AIRCJun 21, 2000 · N141WE · Doug DC1040 · Wing SparSDR 20001127AP015Skin · corrodedDURING C-CHECK, FOUND CORROSION ON THE LT WING TRAILING EDGE UPPER SKIN AT STATION XRS 230. CORROSION WAS REMOVED AND FASTENERS WERE REPLACED IAW EO CH-00-009 AND BOEING TLX CAC-FCO 00-00004H DTD 14 APR 00. RELEASED AIRCRAFT FOR REVENUE SERVICE. (M)Jun 21, 2000 · N141WE · Doug DC1040 · Wing, Plate/SkinSDR 20001127AP014Skin · corrodedDURING C-CHECK, FOUND CORROSION ON THE RIGHT WING FIXED LEADING EDGE AT STATION XOS 420-25. CORROSION WAS BLENDED OUT AND FASTENERS WERE REPLACED IAW EO CH-00-006 AND BOEING TLX CAC-FCO 00-00002H DTD 14 APR 00, AND SRM 57-10-00 VOL 1 FIG 15A SHEET 2. RELEASEJun 21, 2000 · N141WE · Doug DC1040 · Wing, Plate/SkinSDR 20001127AP013Spacer · corrodedDURING C-CHECK, THE RIGHT MLG UPPER SPACER IS CRACKED BY CORROSION AT STATION XW=212 TO XW=214. INTERIM REPAIR WAS MADE IAW EO CH-00-0010 AND BOEING TLX CAC-FCO 00-00007F DTD 18 APR 00. REPETITIVE INSPECTION ARE REQUIRED AT C-CHECK INSPECTIONS, NOT TO EXCEEDJun 21, 2000 · N141WE · Doug DC1040 · Landing Gear Retraction/Extension SystemSDR 20001127AP012Skin · corrodedDURING C-CHECK, FOUND CORROSIONI ON LT WING LOWER AFT SKIN AT STATION XORS 340.00. FOUND CORROSION BLENDED OUT AND SHOTPEENED IAW EO CH-00-0011 AND BOEING TLX TAU-FCO 00-00097H DTD 17 APR 00. RELEASED AIRCRAFT FOR REVENUE SERVICE. (M)Jun 21, 2000 · N141WE · Doug DC1040 · Wing, Plate/SkinSDR 20001127AP011Spar Cap · corrodedDURING C-CHECK, FOUND CORROSION ON RIGHT WING REAR SPAR CAP AFT TANG UPPER SURFACE BETWEEN STATION XORS 917 TO 885. FOUND CORROSION BLENDED OUT IAW EO CH-00-012 AND BOEING TLX CAC-FCO- 00-00006H DATED 17, APR 00, AND SRM VOL 2 CHAPTER 51-21-02. RELEASED AIRCJun 21, 2000 · N141WE · Doug DC1040 · Wing Spar
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