# Service difficulty reports: N141US, cancelled Jun 18, 2002

A list on [N141US, cancelled Jun 18, 2002](https://openairdocs.org/deregistered/N141US-2002-06-18.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR 0101241141](https://openairdocs.org/sdr/0101241141.md): Skin · cracked · Mar 1, 2001 · N141US · Doug DC1040 · Fuselage Main, Plate/Skin
  > DURING LINE CHECK, FOUND CRACK IN NOSE LANDING GEAR CUTOUT RT FORWARD CORNER SKIN AT BS 464. REPAIRED PER EA 11-182711.
- [SDR 0004231141](https://openairdocs.org/sdr/0004231141.md): Pump · failed · Nov 9, 2000 · N141US · Doug DC1040 · Hydraulic Pump (Electric/Engine), Main
  > DURING CRUISE, NR 1 SYSTEM HYDRAULIC QUANTITY DECREASED. FOLLOWED COM PROCEDURE, DEPRESSURIZED AND ISOLATED NR 1 SYSTEM. QUANTITY STABILIZED AT 3.5 GALLONS. UPON APPROACH TO HNL, RESTARTED NR 1 SYSTEM AND QUANTITY WENT TO ZERO. REQUESTED EMERGENCY EQUIPMEN
- [SDR 9900831141](https://openairdocs.org/sdr/9900831141.md): Longeron · corroded · Jan 7, 1999 · N141US · Doug DC1040 · Fuselage Main, Longeron/Stringer
  > DURING M-CHECK, FOUND CORROSION BETWEEN FS 1741 AND 1771 ON LONGERON 50L. REPAIRED PER EA 11-162749.
- [SDR 9900651141](https://openairdocs.org/sdr/9900651141.md): Longeron · corroded · Jan 7, 1999 · N141US · Doug DC1040 · Fuselage Main, Longeron/Stringer
  > DURING M-CHECK, FOUND CORROSION AT FS 1738 ON LONGERON 50L. REPAIRED PER EA 11-162749.
- [SDR 9900641141](https://openairdocs.org/sdr/9900641141.md): Lever · corroded · Jan 7, 1999 · N141US · Doug DC1040 · Wing, Landing Gear Attach Fittings
  > DURING M-CHECK, FOUND CORROSION UNDER AND AROUND PIVOT BEARING SUPPORT BUSHING ON INBOARD FLAP DRIVE LEVER. REPAIRED PER EA 11-162743.
- [SDR 9811481141](https://openairdocs.org/sdr/9811481141.md): Frame · cracked · Dec 17, 1998 · N141US · Doug DC1040 · Fuselage Main, Frame
  > DURING M-CHECK, FOUND FUSELAGE FRAME CRACKED AT FS 1921 AT ATTACH TO LEFT CARGO TRACK. REPAIRED PER EA 11-162429.
- [SDR 9809561141](https://openairdocs.org/sdr/9809561141.md): Fuel Line · cracked · Jun 16, 1998 · N141US · Doug DC1040 · Engine Fuel Distribution
  > WHILE AT CRUISE FL330, THE NR 2 ENGINE COMPRESSOR STALLED. ALL NR 2 PARAMETERS ROLLED BACK TO FLIGHT IDLE. THE ENGINE DID NOT RESPOND TO POWER LEVER INPUTS AND WAS SHUT DOWN. THE AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. THE CREW DID ATTEMPT ON
- [SDR 9808921141](https://openairdocs.org/sdr/9808921141.md): Compressor · stalled · May 7, 1998 · N141US · Doug DC1040 · Turbine Engine Compressor Section
  > DURING THE LANDING ROLLOUT, THE NR 3 ENGINE COMPRESSOR STALLED WHILE IN REVERSE THRUST. THE EGT REACHED 970C BEFORE THE ENGINE WAS SHUT DOWN. MAINTENANCE PERFORMED A BORESCOPE INSPECTION AND FOUND DAMAGE TO THE HIGH PRESSURE COMPRESSOR. THE AIRCRAFT WAS REMO
- [SDR 9806531141](https://openairdocs.org/sdr/9806531141.md): Cylinder · failed · Apr 14, 1998 · N141US · Doug DC1040 · Steering Unit
  > DURING TAKEOFF ROLL, LOST NR 1 HYDRAULIC SYSTEM. ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE FOUND THE LEFT NOSE WHEEL STEERING CYLINDER LEAKING. REPLACED THE STEERING CYLINDER, CHECKED FILTERS, AND REFILLED SYSTEM. LEAK AND OPERATIONAL CHECK OK.
- [SDR 9723231141](https://openairdocs.org/sdr/9723231141.md): Engine · failed · Dec 15, 1997 · N141US · Doug DC1040 · Engine (Turbine/Turboprop)
  > DURING CLIMB, THE CREW OBSERVED SPARKS EXITING FROM THE REAR OF THE NR 3 ENGINE EVERY 15 TO 20 SECONDS. ALL ENGINE INSTRUMENTS INDICATED NORMAL AND NO VIBRATION WAS NOTICED. THE FLIGHT RETURNED TO BOS. MAINTENANCE FOUND MOLTEN METAL ON THE BLEED SCREEN AND
- [SDR 9723111141](https://openairdocs.org/sdr/9723111141.md): Apu · smoking · Dec 12, 1997 · N141US · Doug DC1040 · APU Core Engine
  > DURING TAXI AS PACKS NR 2 AND NR 3 WERE BROUGHT ON LINE, SMOKE BEGAN TO ENTER THE CABIN AREA. AIRCRAFT RETURNED TO THE GATE AND PASSENGERS DEPLANED THROUGH THE JETWAY. MAINTENANCE FOUND OIL CONTAMINATION FROM THE APU WAS THE SOUCE OF SMOKE. PACK/DUCTING BUR
- [SDR 9721301141](https://openairdocs.org/sdr/9721301141.md): Fitting · corroded · Nov 10, 1997 · N141US · Doug DC1040 · Fuselage Miscellaneous Structure
  > DURING L-CHECK, FOUND CORROSION ON LONGERON 44R END FITTING AT FS 1701. REPLACED FITTING EPR SRM 51-00-00.
- [SDR 9719831141](https://openairdocs.org/sdr/9719831141.md): Fuel Control · malfunctioned · Oct 21, 1997 · N141US · Doug DC1040 · Fuel Control/Turbine Engines
  > WHILE DESCENDING THRU FL350, THE NR 3 ENGINE EGT ROSE TO 880C. THE ENGINE WAS SHUT DOWN. THE SECOND RESTART ATTEMPT WAS SUCCESSFUL WITH NORMAL OPERATION FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE BORESCOPED THE ENGINE WITH NO DEFECTS NOTES. THE FUEL CONT
- [SDR 9719081141](https://openairdocs.org/sdr/9719081141.md): Wire · broken · Oct 13, 1997 · N141US · Doug DC1040 · Light System Wiring
  > DURING LIGHT INSPECTION FOUND THE EMERGENCY FLOOR LIGHT INOPERATIVE IN LEFT SIDE IN B-ZONE. MAINTENANCE REPAIRED A BROKEN WIRE IN THE TRACK WIRING.
- [SDR 9718111141](https://openairdocs.org/sdr/9718111141.md): Tach Ind · failed · Sep 28, 1997 · N141US · Doug DC1040 · Engine RPM Indicating System
  > ON TAKEOFF ROLL, THE NR 3 ENGINE N1 INDICATION SPIKED WHILE AT MAXIMUM POWER. THE TAKEOFF WAS ABORTED AT APPROXIMATELY 40 KNOTS. ALL OTHER PARAMETERS WERE NORMAL. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE DEFERRED THE N1 INDICATION UNDER MEL 77-1B
- [SDR 9717941141](https://openairdocs.org/sdr/9717941141.md): Power Supply · inoperative · Sep 23, 1997 · N141US · Doug DC1040 · Emergency Lighting
  > DURING LINE INSPECTION, FOUND THE EMERGENCY ESCAPE PATH LIGHT INOPERATIVE AFT OF DOOR 2L. MAINTENANCE REPLACED POWER SUPPLY.
- [SDR 9717701141](https://openairdocs.org/sdr/9717701141.md): Battery Pack · discharged · Sep 15, 1997 · N141US · Doug DC1040 · Emergency Lighting
  > DURING LINE INSPECTION, FOUND THE FLOOR EMERGENCY LIGHT BETWEEN DOORS 2L AND 2R INOPERATIVE. REPLACED BATTERY PACK.
- [SDR 9709471143](https://openairdocs.org/sdr/9709471143.md): Skin · cracked · Apr 19, 1997 · N141US · Doug DC1040 · Wing, Plate/Skin
  > DURING 'M' CHECK, FOUND CRACKS IN LEADING EDGE SKIN AT EXTINGUISHER BOTTLE ACCESS INBOARD AND OUTBOARD FORWARD CORNER. REPAIRED PER EA 11-122890.
- [SDR 9708001143](https://openairdocs.org/sdr/9708001143.md): Frame · cracked · Apr 19, 1997 · N141US · Doug DC1040 · Fuselage Main, Frame
  > DURING M-CHECK, FOUND CRACK IN FRAME AT FS 1851, LONGERON 11R. REPAIRED PER EA 11-098840.
- [SDR 9709491143](https://openairdocs.org/sdr/9709491143.md): Doubler · cracked · Apr 18, 1997 · N141US · Doug DC1040 · Fuselage Miscellaneous Structure
  > DURING 'M' CHECK, FOUND CRACK IN DOUBLER BETWEEN LONGERON 4R AND 5R, FS 1129. REPAIRED PER EA 11-122888.
- [SDR 9708661143](https://openairdocs.org/sdr/9708661143.md): Frame · cracked · Apr 18, 1997 · N141US · Doug DC1040 · Fuselage Main, Frame
  > DURING M-CHECK, FOUND CRACK IN FRAME AT FS 1851 AT LONGERON 10L TO 11L. REPAIRED PER EA 11-098839.
- [SDR 9708021143](https://openairdocs.org/sdr/9708021143.md): Frame · cracked · Apr 18, 1997 · N141US · Doug DC1040 · Fuselage Main, Frame
  > DURING M-CHECK, FOUND CRACK IN FRAME AT FS 1841 JUST BELOW LONGERON 12L. REPAIRED PER EA 11-123994.
- [SDR 9708011143](https://openairdocs.org/sdr/9708011143.md): Frame · cracked · Apr 18, 1997 · N141US · Doug DC1040 · Fuselage Main, Frame
  > DURING M-CHECK, FOUND CRACK IN FRAME AT FS 1851 AT LONGERON 10R. REPAIRED PER EA 11-098840.
- [SDR 9709481143](https://openairdocs.org/sdr/9709481143.md): Frame · corroded · Apr 17, 1997 · N141US · Doug DC1040 · Fuselage Main, Frame
  > DURING 'M' CHECK, FOUND CORROSION LOWER AFT SKIN ATTACH ANGLE IN SILL ACCESS FS 1708, RBL 70. REPAIRED PER EA 11-124021.
- [SDR 9708161143](https://openairdocs.org/sdr/9708161143.md): Bracket · corroded · Apr 16, 1997 · N141US · Doug DC1040 · Fuselage Miscellaneous Structure
  > DURING M-CHECK, FOUND CORROSION ON AFT SHEAR TIE AT FS 945 BETWEEN LONGERONS 45R TO 46R. REPAIRED PER EA 11-122908.
- [SDR 9708101143](https://openairdocs.org/sdr/9708101143.md): Spar Chord · cracked · Apr 16, 1997 · N141US · Doug DC1040 · Wing Spar
  > DURING M-CHECK, FOUND CRACK IN RADIUS AT AFT UPPER SPAR CHORD WING STA XW 948-946 LEFT WING. REPAIRED PER EA 11-123995.
- [SDR 9708651143](https://openairdocs.org/sdr/9708651143.md): Aft Shelf · corroded · Apr 14, 1997 · N141US · Doug DC1040 · Fuselage Miscellaneous Structure
  > DURING M-CHECK, FOUND CORROSION ON SKIN IN CENTER WHEEL WELL AFT SHELF INBOARD AND OUTBOARD OF RBL 27 'T' CHORD. REPAIRED PER EA 11-122905.
- [SDR 9708641143](https://openairdocs.org/sdr/9708641143.md): Jamb · cracked · Apr 4, 1997 · N141US · Doug DC1040 · Fuselage Miscellaneous Structure
  > DURING M-CHECK, FOUND CRACK IN DOOR JAMB FOR DOOR 3R IN THE FORWARD LOWER WEB AT THE LOWER LIGHTENING HOLE. REPAIRED PER EA 11-122885.
- [SDR 9708171143](https://openairdocs.org/sdr/9708171143.md): Bulkhead Channel · corroded · Mar 22, 1997 · N141US · Doug DC1040 · Fuselage Main, Bulkhead
  > DURING M-CHECK, FOUND CORROSION IN SEVERAL AREAS ON THE FOURTH AND FIFTH CHANNELS DOWN FROM THE TOP OF THE BS 2007 BULKHEAD. PRIMED AND INSTALLED REPAIR PER EA 11-122886.
- [SDR 9700861141](https://openairdocs.org/sdr/9700861141.md): Epr Indicator · malfunctioned · Jan 19, 1997 · N141US · Doug DC1040 · Engine Pressure Ratio (EPR)
  > DURING TAKEOFF ROLL, THE NR 3 ENGINE EPR WAS LOW. TAKEOFF WAS ABORTED AT 50 KNOTS. MAINTENANCE FOUND EPR INDICATOR FAULTY. REPLACED THE EPR INDICATOR.
- [SDR 9700961141](https://openairdocs.org/sdr/9700961141.md): Battery · discharged · Jan 16, 1997 · N141US · Doug DC1040 · Emergency Lighting
  > DURING INSPECTION, FOUND THE MID CABIN EMERGENCY FLOOR LIGHT ON THE LEFT SIDE INOPERATIVE. REPLACED MID CABIN EMERGENCY BATTERY.
- [SDR 9615861141](https://openairdocs.org/sdr/9615861141.md): Skin · cracked · Jul 3, 1996 · N141US · Doug DC1040 · Wing, Plate/Skin
  > DURING L-CHECK, FOUND A CRACK IN THE LEFT WING LEADING EDGE SKIN AT THE ANTI-ICE DUCT DOOR CUTOUT XOS 467. REPAIRED SKIN PER EA 11-105129.
- [SDR 9613321141](https://openairdocs.org/sdr/9613321141.md): Cables · worn · Jun 15, 1996 · N141US · Doug DC1040 · Door Warning System
  > DURING TAKEOFF, DOOR 1L ANNUNCIATOR LIGHT ILLUMINATED, ABORTED TAKEOFF. MAINTENANCE REPLACED BOTH TRANSLATOR CABLES.
- [SDR 9613111141](https://openairdocs.org/sdr/9613111141.md): Compressor · stalled · Jun 14, 1996 · N141US · Doug DC1040 · Turbine Engine Compressor Section
  > AT TOP OF DESCENT, THE NR 2 ENGINE COMPRESSOR STALLED WHEN THROTTLE WAS RETARDED. AT THE TIME OF STALL, TEMPERATURE REACHED 750 DEGREES CELSIUS. FLIGHT CONTINUED TO LGW WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED INSPECTION PER 71-00-00 AND NO DAMAGE WA
- [SDR 9602271141](https://openairdocs.org/sdr/9602271141.md): Compressor · stalled · Jan 26, 1996 · N141US · Doug DC1040 · Turbine Engine Compressor Section
  > DURING LANDING ROLL-OUT (CDG), THE NR 3 ENGINE EXPERIENCED A SLIGHT REVERSE STALL. CREW FOLLOWED COCKPIT OPERATING PROCEDURE BY SHUTTING THE ENGINE DOWN AND PROCEEDED WITH LANDING WITHOUT FURTHER INCIDENT. REPLACED THE NR 3 ENGINE AND CHECK WAS NORMAL.
- [SDR 9509091141](https://openairdocs.org/sdr/9509091141.md): Longeron · corroded · May 26, 1995 · N141US · Doug DC1040 · Fuselage Main, Longeron/Stringer
  > DURING 'T' CHECK, FOUND CORROSION ON LONGERON 37R AT FS 850. REPAIRED PER EA 11-98559.
- [SDR 9509081141](https://openairdocs.org/sdr/9509081141.md): Longeron · corroded · May 26, 1995 · N141US · Doug DC1040 · Fuselage Main, Longeron/Stringer
  > DURING 'T' CHECK, FOUND CORROSION ON STR 52 FROM FS 1710 - 1781. REPAIRED PER EA 11-97970.
- [SDR 9509061141](https://openairdocs.org/sdr/9509061141.md): Frame · corroded · May 24, 1995 · N141US · Doug DC1040 · Fuselage Main, Frame
  > DURING 'T' CHECK, FOUND CORROSION ON THE FS 939 FORWARD CARGO FRAME AT LONGERON 51R. REPAIRED PER EA 11-98552.
- [SDR 9509051141](https://openairdocs.org/sdr/9509051141.md): Frame · corroded · May 24, 1995 · N141US · Doug DC1040 · Fuselage Main, Frame
  > DURING 'T' CHECK, FOUND CORROSION ON THE FORWARD CARGO FLOOR FRAME FS 979 AT LBL 29. REPAIRED PER EA 11-98545.
- [SDR 9509021141](https://openairdocs.org/sdr/9509021141.md): Le Skin · cracked · May 23, 1995 · N141US · Doug DC1040 · Wing Main, Frame Structure
  > DURING 'T' CHECK, FOUND CRACKS IN THE RIGHT WING FIXED LEADING EDGE SKIN, XOS 610.8; ARB 1137-4 WEB AND ARB 1137-9 TEE. REPAIRED ALL PER EA 11-98524.
- [SDR 9509011141](https://openairdocs.org/sdr/9509011141.md): Frame · corroded · May 23, 1995 · N141US · Doug DC1040 · Fuselage Main, Frame
  > DURING 'T' CHECK, FOUND CORROSION ON THE FS 879 FORWARD CARGO FLOOR FRAME AT LBL 38. REPAIRED PER EA 11-98535.
- [SDR 9508981141](https://openairdocs.org/sdr/9508981141.md): Frame · corroded · May 20, 1995 · N141US · Doug DC1040 · Fuselage Main, Frame
  > DURING 'T' CHECK, FOUND CORROSION ON THE FORWARD CARGO FLOOR FRAME FS 939, LBL 38. REPAIRED PER EA 11-98542.
- [SDR 9505141141](https://openairdocs.org/sdr/9505141141.md): Engine · malfunctioned · Mar 30, 1995 · N141US · Doug DC1040 · Engine (Turbine/Turboprop)
  > DURING DESCENT FL280 AT IDLE POWER, THE NR 1 ENGINE ENCOUNTERED WAKE TURBULENCE AND A SURGE FOLLOWED BY RISING EGT. THE ENGINE WAS SHUTDOWN, AND A RELIGHT WAS SUCCESSFUL. OPERATION WAS NORMAL THE REMAINDER OF THE FLIGHT. THE ENGINE WAS INSPECTED AND A BORES

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'N141US' AND deregistration_id = 'N141US-2002-06-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N141US-2002-06-18/reports

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