# Service difficulty reports: N133JC, cancelled May 3, 2007 A list on [N133JC, cancelled May 3, 2007](https://openairdocs.org/deregistered/N133JC-2007-05-03.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 0000231143](https://openairdocs.org/sdr/0000231143.md): Engine · malfunctioned · Jan 27, 2000 · N133JC · Doug DC1040 · Engine Pressure Ratio (EPR) > AT 110 KTS ON TAKEOFF ROLL, THE CREW ABORTED TAKEOFF FOR LOW EPR INDICATION ON THE NR 2 ENGINE. THE EPR DID NOT EXCEED 1.2 WITH THE POWER LEVER NEAR THE MECHANICAL STOP. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE DEFERRED THE NR 2 EPR INDICATION UNDER M - [SDR 9806431143](https://openairdocs.org/sdr/9806431143.md): Compressor · stalled · Apr 9, 1998 · N133JC · Doug DC1040 · Turbine Engine Compressor Section > DURING LANDING ROLLOUT WHILE IN REVERSE THRUST, THE NR 3 ENGINE COMPRESSOR STALLED. THE EGT ROSE TO 980C FOR THREE SECONDS BEFORE THE ENGINE WAS SHUT DOWN. A BORESCOPE WAS PERFORMED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS REMOVED FROM SERVICE AND FERRIED TO - [SDR 9806421143](https://openairdocs.org/sdr/9806421143.md): Compressor · stalled · Apr 9, 1998 · N133JC · Doug DC1040 · Turbine Engine Compressor Section > DURING LANDING ROLLOUT WHILE IN REVERSE THRUST, THE NR 1 ENGINE COMPRESSOR STALLED. THE EGT ROSE TO 980C FOR THREE SECONDS BEFORE THE ENGINE WAS SHUT DOWN. A BORESCOPE WAS PERFORMED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS REMOVED FROM SERVICE AND FERRIED TO - [SDR 9804841143](https://openairdocs.org/sdr/9804841143.md): Engine · failed · Mar 20, 1998 · N133JC · Doug DC1040 · Engine (Turbine/Turboprop) > APPROXIMATELY 30 MINUTES AFTER TAKEOFF, THE NR 1 ENGINE OIL CLOG LIGHT ILLUMINATED. THE CREW FOLLOWED COM PROCEDURE AND SHUT DOWN THE ENGINE. FUEL WAS DUMPED AND THE AIRCRAFT RETURNED TO MSP WITHOUT DIFFICULTY. MAINTENANCE INSPECTED THE ENGINE AND THE AIRCR - [SDR 9801951143](https://openairdocs.org/sdr/9801951143.md): Engine · malfunctioned · Jan 30, 1998 · N133JC · Doug DC1040 · Engine (Turbine/Turboprop) > DURING LANDING ROLLOUT AND WHILE IN REVERSE THRUST, THE NR 1 ENGINE EGT ROSE RAPIDLY TOWARD THE RED LINE LIMIT. THE ENGINE WAS SHUT DOWN BEFORE EXCEEDING ANY LIMITATIONS. MAINTENANCE INSPECTED THE ENGINE WITH NO DEFECTS NOTED. - [SDR 9724111143](https://openairdocs.org/sdr/9724111143.md): Seal · failed · Dec 19, 1997 · N133JC · Doug DC1040 · Passenger/Crew Doors > PASSING FL280, A LOUD SQUEAL NOISE AND A LOUD FLUTTER NOISE WAS HEARD FROM DOOR 1R. VIBRATION WAS FELT UPPER RIGHT SIDE OF DOOR 1R. FLIGHT RETURNED TO HNL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND SEAL OUT ON UPPER AFT CORNER OF LEFT DOOR, REINSTALLED - [SDR 9723141143](https://openairdocs.org/sdr/9723141143.md): Compressor · stalled · Dec 11, 1997 · N133JC · Doug DC1040 · Turbine Engine Compressor Section > DURING THE APPLICATION OF TAKEOFF THRUST, THE NR 3 ENGINE COMPRESSOR STALLED. MAX EGT WAS 880C AND THE TAKEOFF WAS ABORTED. MAINTENANCE INSPECTED THE ENGINE PER MM 71-00-00 WITH NO DEFECTS NOTED. THE BOROSCOPE WAS DEFERRED. SUBSEQUENT ENGINE RUN WAS NORMAL - [SDR 9722961143](https://openairdocs.org/sdr/9722961143.md): Compressor · stalled · Dec 7, 1997 · N133JC · Doug DC1040 · Turbine Engine Compressor Section > WHILE DESCENDING THRU FL350 AND REDUCING POWER, THE NR 3 ENGINE COMPRESSOR STALLED. THE EGT ROSE RAPIDLY TO 700C AND THE ENGINE WAS SHUT DOWN. ALL OTHER ENGINE INDICATIONS WERE NORMAL AND A SUCCESSFUL RESTART WAS ACCOMPISHED. MAINTENANCE BORESCOPED THE ENGI - [SDR 9718781143](https://openairdocs.org/sdr/9718781143.md): Compressor · stalled · Oct 5, 1997 · N133JC · Doug DC1040 · Turbine Engine Compressor Section > AT TOP OF DESCENT FL280, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL WITH EGT RISING TO 900C. THE ENGINE WAS SHUT DOWN AND TWO RESTART ATTEMPTS WERE UNSUCCESSFUL. MAINTENANCE INSPECTED THE ENGINE PER MM 71-00-00 FOR TOP OF DESCENT STALL WITH NO DEFECTS N - [SDR 9710211143](https://openairdocs.org/sdr/9710211143.md): Engine · malfunctioned · May 24, 1997 · N133JC · Doug DC1040 · Engine (Turbine/Turboprop) > NR 1 ENGINE EGT ROSE RAPIDLY AFTER THE REVERSER WAS STOWED. ENGINE WAS SHUTDOWN, EGT PEAKED AT 780 CELSIUS. MAINTENANCE RAN NR 1 ENGINE, OPERATED REVERSER AND ALL INDICATIONS WERE NORMAL. - [SDR 9702071143](https://openairdocs.org/sdr/9702071143.md): Prox Control · failed · Feb 2, 1997 · N133JC · Doug DC1040 · Landing Gear Position and Warning > DURING TAKEOFF, THE GEAR WARNING HORN SOUNDED WITH THE STRUT EXTENSION, THE 4 RED GEAR UNSAFE LIGHTS ILLUMINATED. RECYCLED GEAR AND LIGHTS REMAINED ILLUMINATED. FLIGHT RETURNED TO MSP. MAINTENANCE REPLACED THE MAIN LANDING GEAR PROXIMITY CONTROL. - [SDR 9620341143](https://openairdocs.org/sdr/9620341143.md): Evc · malfunctioned · Sep 22, 1996 · N133JC · Doug DC1040 · Compressor Bleed Control > EN ROUTE, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL DURING DESCENT. THE ENGINE WAS SHUT DOWN AND RESTARTED. CREW FOLLOWED COM PROCEDURES AND CONTINUED FLIGHT TO MSP WITHOUT FURTHER INCIDENT. ENGINE BORESCOPE WAS ACCOMPLISHED AND NO DISCREPANCIES WERE F - [SDR 9615471143](https://openairdocs.org/sdr/9615471143.md): Engine · stalled · Jul 16, 1996 · N133JC · Doug DC1040 · Turbine Engine Compressor Section > EN ROUTE LAX-HNL, THE NR 2 ENGINE EXPERIENCED TOP OF DESCENT STALL WHEN POWER WAS RETARDED. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND FLIGHT CONTINUED TO HNL WITHOUT FURTHER INCIDENT. VISUAL INSPECTION OF THE NR 2 ENGINE REVEALED NO DISCREPANCIES. BORES - [SDR 9609321143](https://openairdocs.org/sdr/9609321143.md): Compressor · stalled · Apr 28, 1996 · N133JC · Doug DC1040 · Turbine Engine Compressor Section > AT TOP OF DESCENT, THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL. THE ENGINE WAS SHUTDOWN AND A HIGH ALTITUDE RAPID RESTART WAS ATTEMPTED BUT DID NOT START. A SECOND RESTART WAS SUCCESSFUL AND FLIGHT CONTINUED TO MCO WITHOUT FURTHER INCIDENT. MAINTENANCE P - [SDR 9609301143](https://openairdocs.org/sdr/9609301143.md): Air Data Comp · failed · Apr 28, 1996 · N133JC · Doug DC1040 · Air Data Computer > DURING TAKEOFF ROLL, THE CAPTAIN'S AIRSPEED READ 20 KNOTS HIGHER THAN THE FIRST OFFICER'S AIRSPEED INDICATOR. ABORTED TAKEOFF AND RETURED TO THE GATE. DURING TAXI THE CAPTAIN'S ALTIMETER READ 120 FEET HIGHER THAN THE FIRST OFFICER'S ALTIMETER. REPLACED THE - [SDR 9603331143](https://openairdocs.org/sdr/9603331143.md): Compressor · stalled · Feb 8, 1996 · N133JC · Doug DC1040 · Turbine Engine Compressor Section > DURING DESCENT, THE NR 2 ENGINE COMPRESSOR STALLED. THE ENGINE WAS SHUTDOWN AND RESTARTED. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND CONTINUED TO LAX WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED NR 2 ENGINE AND CHECK WAS NORMAL. - [SDR 9514591143](https://openairdocs.org/sdr/9514591143.md): Antenna Mt Rings · corroded · Sep 5, 1995 · N133JC · Doug DC1040 · Fuselage Miscellaneous Structure > DURING PERIODIC CHECK, FOUND CORROSION ON BOTH PAIRS OF RADIO ALTIMETER ANTENNA MOUNTING RINGS. REPAIRED RINGS (AYB 7022, AYB 7053), PER EA 11-98920. - [SDR 9513981143](https://openairdocs.org/sdr/9513981143.md): Skin · corroded · Sep 5, 1995 · N133JC · Doug DC1040 · Fuselage Main, Plate/Skin > DURING PERIODIC CHECK, FOUND CORROSION ON THE FUSELAGE SKIN FS 1721 TO 1741, LONGERONS 51R TO 52 AT THE VHF ANTENNA. REPAIRED SKIN PER EA 11-67705. - [SDR 9513951143](https://openairdocs.org/sdr/9513951143.md): Skin · corroded · Sep 4, 1995 · N133JC · Doug DC1040 · Fuselage Main, Plate/Skin > DURING PERIODIC CHECK, FOUND CORROSION ON THE FUSELAGE SKIN AT FS 1661 TO 1681, LONGERON 51L TO 51R AT THE ANTI-COLLISION LIGHT. REPAIRED SKIN PER EA 11-98921. - [SDR 9511351143](https://openairdocs.org/sdr/9511351143.md): Web · cracked · Jul 20, 1995 · N133JC · Doug DC1040 · Fuselage Miscellaneous Structure > DURING LINE CHECK, FOUND TWO CRACKS IN THE NOSE LANDING GEAR WHEELWELL VERTICAL PANEL PRESSURE WEB BS 495, LEFT SIDE AT Z-63 AND RIGHT SIDE AT Z-62. REPAIRED PER EA 11-98587. - [SDR 9509151143](https://openairdocs.org/sdr/9509151143.md): Fitting · cracked · Jun 3, 1995 · N133JC · Doug DC1040 · Fuselage Miscellaneous Structure > DURING LINE CHECK, FOUND A CRACK IN THE FORWARD CARGO DOOR ACTUATOR SUPPORT FITTING. REPLACED FITTING. ## 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 = 'N133JC' AND deregistration_id = 'N133JC-2007-05-03' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N133JC-2007-05-03/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.