# Service difficulty reports: N144JC, cancelled Nov 22, 2004 A list on [N144JC, cancelled Nov 22, 2004](https://openairdocs.org/deregistered/N144JC-2004-11-22.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 9902191144](https://openairdocs.org/sdr/9902191144.md): Longeron · corroded · May 18, 1999 · N144JC · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING M CHECK, FOUND CORROSION ON LONGERON 48R UPPER AND LOWER SURFACE FROM FS 1119 - FS 1139. REPAIRED PER EA 11-166880. - [SDR 9902221144](https://openairdocs.org/sdr/9902221144.md): Frame · cracked · May 17, 1999 · N144JC · Doug DC1040 · Fuselage Main, Frame > DURING M CHECK, FOUND CRACK IN TRANSVERSE FRAME BELOW DOOR 3R THRESHOLD AT FS 1256, RBL 110. REPAIRED PER EA 11-166446. - [SDR 9902231144](https://openairdocs.org/sdr/9902231144.md): Spar · corroded · May 14, 1999 · N144JC · Doug DC1040 · Wing Spar > DURING M CHECK, FOUND CORROSION ON CHORD AT UPPER CENTER TANK FORWARD SPAR AT FS 1236, RBL 70 TO RBL 75. REPAIRED PER EA 11-167439. - [SDR 9902211144](https://openairdocs.org/sdr/9902211144.md): Floorbeam · cracked · Apr 20, 1999 · N144JC · Doug DC1040 · Fuselage Main, Floor Beam > DURING M CHECK, FOUND CRACK IN FLOOR I BEAM SUPPORT AT FS 879 AT BL 0. REPAIRED PER EA 11-167434. - [SDR 9902201144](https://openairdocs.org/sdr/9902201144.md): Skin · corroded · Apr 20, 1999 · N144JC · Doug DC1040 · Fuselage Main, Plate/Skin > DURING M CHECK, FOUND CORROSION ON BELLY SKIN AT FS 1356 BETWEEN LBL 51 AND LBL 52. REPAIRED PER EA 11-166595. - [SDR 9901961144](https://openairdocs.org/sdr/9901961144.md): Longeron · corroded · Apr 20, 1999 · N144JC · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING M CHECK, FOUND CORROSION ON BELLY SKIN AT FS 1353 - 1365 AND LONGERON 51L - 52L. REPAIRED PER EA 11-166595. - [SDR 9810271144](https://openairdocs.org/sdr/9810271144.md): Line · failed · Oct 13, 1998 · N144JC · Doug DC1040 · Hydraulic System, Main > ON DEPARTURE FROM HNL, LOST ALL HYDRAULIC FLUID IN NR 3 SYSTEM. FOLLOWED COM PROCEDURE AND RETURNED TO HNL. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NR 4 BRAKE LINE CHAFED THROUGH. REPLACED BRAKE LINE AND SERVICED SYSTEM. OPERATIONAL CHECK OK. - [SDR 9806751144](https://openairdocs.org/sdr/9806751144.md): Compressor · stalled · Apr 15, 1998 · N144JC · Doug DC1040 · Turbine Engine Compressor Section > AFTER LANDING WHILE CREW WAS ATTEMPTING TO RESTOW THE NR 3 ENGINE THRUST REVERSER, THE NR 3 ENGINE COMPRESSOR STALLED. EGT CLIMBED TO 820C AND THE ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED THE ENGINE PER THE TAFI MANUAL WITH NO DEFECTS NOTED. THE ENGINE WA - [SDR 9803131144](https://openairdocs.org/sdr/9803131144.md): Compressor · stalled · Feb 22, 1998 · N144JC · Doug DC1040 · Turbine Engine Compressor Section > DURING CRUISE AT FL370, THE NR 2 ENGINE COMPRESSOR STALLED, EGT ROSE TO 940C AND THE ENGINE WAS SHUT DOWN. A RESTART ATTEMPT AT FL330 WAS SUCCESSFUL AND THE ENGINE OPERATION WAS NORMAL FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE INSPECTED THE ENGINE PER TAF - [SDR 9722521144](https://openairdocs.org/sdr/9722521144.md): Tr Unit · malfunctioned · Dec 1, 1997 · N144JC · Doug DC1040 · Engine Thrust Reverser > DURING TAKEOFF ROLL, THE NR 3 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AT 70 KTS WITH THE INDICATION EXTINGUISHING WITH POWER REDUCTION. MAINTENANCE PLACED THE REVERSER ON MEL 78-1A AND THE AIRCRAFT RETURNED TO SERVICE. - [SDR 9717361144](https://openairdocs.org/sdr/9717361144.md): Handle · lack of lube · Sep 11, 1997 · N144JC · Doug DC1040 · Landing Gear Selector > DURING APPROACH, UNABLE TO GET ALL GREEN LIGHTS ON THE LANDING POSITION. RECYCLED GEAR TWICE WITH NO HELP. USED ALTERNATE GEAR EXTENSION AND ALL GREEN LIGHTS ILLUMINATED. MAINTENANCE FOUND LANDING GEAR HANDLE STICKING. LUBED GEAR HANDLE. - [SDR 9716251144](https://openairdocs.org/sdr/9716251144.md): Tr Light · illuminated · Aug 25, 1997 · N144JC · Doug DC1040 · Engine Thrust Reverser > ON TAKEOFF ROLL, THE NR 3 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AT 100 KNOTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE DEFERRED THE REVERSER INDICATION SYSTEM UNDER MEL 78-2A WITH THE REVERSER STOWED AND LOCKED. E - [SDR 9713601144](https://openairdocs.org/sdr/9713601144.md): Roll Computer · failed · Jun 29, 1997 · N144JC · Doug DC1040 · Autopilot Computer > DURING CRUISE, COULD NOT ENGAGE AUTO PILOTS WITHOUT ENCOUNTERING ROLLING INPUT TO THE AILERONS. AIRCRAFT DIVERTED TO LGW. MAINTENANCE REPLACED BOTH ROLL COMPUTERS (11-2211-9-0001, S/N 90034 AND 56026) AND THE DIRECTIONAL CONTROL PANEL (11-2216-9-00005, S/N 9 - [SDR 9709911144](https://openairdocs.org/sdr/9709911144.md): Switch · sticking · May 12, 1997 · N144JC · Doug DC1040 · Landing Gear Position and Warning > DURING LANDING, LOWERED LANDING GEAR HANDLE AND RED UNSAFE LIGHT ILLUMINATED AND DID NOT GO OUT. RECYCLED GEAR AND OPERATION WAS NORMAL. MAINTENANCE CLEANED AND LUBED GEAR HANDLE SWITCH. - [SDR 9706051144](https://openairdocs.org/sdr/9706051144.md): Battery · discharged · Mar 23, 1997 · N144JC · Doug DC1040 · Emergency Lighting > DURING LINE INSPECTION, FOUND THE EMERGENCY LIGHT IN MID CABIN FLOOR AND CEILING INOPERATIVE. REPLACED BATTERY PACK. - [SDR 9613851144](https://openairdocs.org/sdr/9613851144.md): Power Supply · inoperative · Jun 20, 1996 · N144JC · Doug DC1040 · Emergency Lighting > DURING LINE INSPECTION, FOUND THE OVERWING EMERGENCY LIGHT POWER SUPPLY FAULTED. MAINTENANCE REPLACED THE OVERWING EMERGENCY POWER SUPPLY AND BATTERY. - [SDR 9613581144](https://openairdocs.org/sdr/9613581144.md): Bulkhead · corroded · Jun 11, 1996 · N144JC · Doug DC1040 · Fuselage Main, Bulkhead > DURING T-CHECK, FOUND CORROSION ON THE PRESSURE BULKHEAD CAP FS 1369 IN THE CENTER MAIN LANDING GEAR WHEEL WELL. REPAIRED CAP (P/N AYB 7080-5) PER EA 11-105427. - [SDR 9613571144](https://openairdocs.org/sdr/9613571144.md): Frame · corrosion · Jun 9, 1996 · N144JC · Doug DC1040 · Fuselage Main, Frame > DURING T-CHECK, FOUND CORROSION ON THE FS 1360 FRAME FROM LONGERON 51L TO 51R. REPAIRED FRAME (P/N AYB 7031-3) PER EA 11-105407. - [SDR 9613561144](https://openairdocs.org/sdr/9613561144.md): Frame · cracked · Jun 6, 1996 · N144JC · Doug DC1040 · Fuselage Main, Frame > DURING T-CHECK, FOUND A 4.625 INCH CRACK IN THE FS 1561 FRAME SPLICE AT LONGERON 44L. REPAIRED SPLICE (P/N AEA 7296-11) PER EA 11-102166. - [SDR 9613551144](https://openairdocs.org/sdr/9613551144.md): Frame · corroded · Jun 6, 1996 · N144JC · Doug DC1040 · Fuselage Main, Frame > DURING T-CHECK, FOUND CORROSION ON LONGERON 43R AT FS 1561. REPAIRED LONGERON (P/N AFA 7070-1) PER EA 11-105418. - [SDR 9613541144](https://openairdocs.org/sdr/9613541144.md): Skin · cracked · Jun 6, 1996 · N144JC · Doug DC1040 · Wing, Plate/Skin > DURING T-CHECK, FOUND CRACKS IN BOTH THE LEFT AND RIGHT WING LEADING EDGE SKIN XOS 290 AND 330. REPAIRED SKIN (P/N ARB 2984-501, -502) PER EA 11-105409. - [SDR 9613971144](https://openairdocs.org/sdr/9613971144.md): Frame · corroded · Jun 4, 1996 · N144JC · Doug DC1040 · Fuselage Main, Frame > DURING T-CHECK, FOUND CORROSION ON THE FORWARD CARGO DOOR JAMB FRAME AT THE LOWER FORWARD CORNER FS 895, LONGERON 41R. REPAIRED FRAME (P/N ADA 0233) PER EA 11-105379. - [SDR 9613521144](https://openairdocs.org/sdr/9613521144.md): Skin · cracked · Jun 4, 1996 · N144JC · Doug DC1040 · Wing, Plate/Skin > DURING T-CHECK, FOUND A.9 INCH CRACK IN THE RIGHT WING LEADING EDGE SKIN AT XOS 603. REPAIRED SKIN (P/N ARB 2887-502) PER EA 11-105398. - [SDR 9613511144](https://openairdocs.org/sdr/9613511144.md): Bulkhead · corroded · Jun 4, 1996 · N144JC · Doug DC1040 · Fuselage Main, Bulkhead > DURING T-CHECK, FOUND CORROSION ON THE CENTER ACCESSORY PRESSURE BULKHEAD WEB AT FS 1156, LBL 9. REPAIRED WEB (P/N NPB 6280-3) PER EA 11-105414. - [SDR 9613501144](https://openairdocs.org/sdr/9613501144.md): Frame · cracked · Jun 4, 1996 · N144JC · Doug DC1040 · Fuselage Main, Frame > DURING T-CHECK, FOUND A 3.625 INCH CRACK IN THE FS 1841 FRAME BETWEEN LONGERON 12L TO 13L EXTENDING COMPLETELY THROUGH THE INBOARD FLANGE AND 2.25 INCH INTO THE FRAME WEB. REPAIRED FRAME (P/N AGA 3783-501) PER EA 11-105412. - [SDR 9612861144](https://openairdocs.org/sdr/9612861144.md): Fitting · corroded · Jun 4, 1996 · N144JC · Doug DC1040 · Fuselage Miscellaneous Structure > DURING T-CHECK, FOUND CORROSION ON THE SPLICE FITTING JUST INBOARD OF THE LOWER FORWARD CORNER OF THE FORWARD CARGO DOOR JAMB. REPLACED FITTING (P/N ADA 7109-501). - [SDR 9612581144](https://openairdocs.org/sdr/9612581144.md): Fitting · cracked · Jun 1, 1996 · N144JC · Doug DC1040 · Wing, Landing Gear Attach Fittings > DURING T-CHECK, FOUND A CRACK IN THE LEFT WHEEL WELL GEAR SUPPORT FITTING AT THE REAR SPAR XORS 240. REPLACED FITTING (P/N ARB198-501). - [SDR 9605011144](https://openairdocs.org/sdr/9605011144.md): Compressor · stalled · Mar 1, 1996 · N144JC · Doug DC1040 · Turbine Engine Compressor Section > DURING LANDING ROLLOUT, THE NR 3 ENGINE EXPERIENCED REVERSE STALL. CREW FOLLOWED COCKPIT OPERATING PROCEDURE AND NR 3 ENGINE SHUTDOWN WAS ACCOMPLISHED WITHOUT FURTHER INCIDENT. BORESCOPE INSPECTION OF NR 3 ENGINE HPC 13TH AND 15TH STATOR STAGES REVEALED NO D - [SDR 9510491144](https://openairdocs.org/sdr/9510491144.md): Fuel/Oil Cooler · leaking · Jul 8, 1995 · N144JC · Doug DC1040 · Engine Fuel/Oil Cooler > DURING CRUISE, STRONG SMELL AND SOME SMOKE AND FUMES WERE PRESENT IN THE CABIN. RETURNED TO MSP. REPLACED THE NR 2 ENGINE FUEL/OIL COOLER AND AIR CONDITIONING SOCKS. - [SDR 9509951144](https://openairdocs.org/sdr/9509951144.md): Ins Computer · unreliable · Jun 26, 1995 · N144JC · Doug DC1040 · Inertial Guidance System > DURING CRUISE, THE NR 2 INS BECAME UNRELIABLE. THE NR 3 INS WAS ALREADY ON MEL. FLIGHT DIVERTED TO BOS. REPLACED THE NR 2 INS COMPUTER. - [SDR 9508691144](https://openairdocs.org/sdr/9508691144.md): Engine · failed · May 28, 1995 · N144JC · Doug DC1040 · Engine (Turbine/Turboprop) > DURING CRUISE, THE NR 1 ENGINE OIL QUANTITY BEGAN TO DECREASE FOLLOWED BY DECREASE IN OIL PRESSURE. THE ENGINE WAS SHUT DOWN. APPROXIMATELY 85,000 POUNDS OF FUEL WAS DUMPED AND THE AIRCRAFT DIVERTED TO YUL WHERE AN UNEVENTFUL TWO ENGINE LANDING WAS MADE. TH - [SDR 9503701144](https://openairdocs.org/sdr/9503701144.md): Skin · crack · Mar 12, 1995 · N144JC · Doug DC1040 · Wing, Plate/Skin > DURING PERIODIC INSPECTION, A CRACK WAS FOUND ON THE LEFT WING LEADING EDGE SKIN AT THE FORWARD INBOARD CORNER OF FUELING ACCESS DOOR. STOP DRILLED CRACK AND INSTALLED DOUBLER PER EA 11-89870. - [SDR 9503691144](https://openairdocs.org/sdr/9503691144.md): Frame · corroded · Mar 12, 1995 · N144JC · Doug DC1040 · Fuselage Main, Frame > DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE LOWER CHORD OF FRAME AT FS 1099, STRINGER 51R AND 52R. REMOVED DAMAGED AREA AND INSTALLED SPLICES PER EA 11-97861. - [SDR 9504201144](https://openairdocs.org/sdr/9504201144.md): Skin · damaged · Mar 11, 1995 · N144JC · Doug DC1040 · Wing, Plate/Skin > DURING PERIODIC INSPECTION, DAMAGE WAS FOUND ON THE RIGHT DROOPED LEADING EDGE. REMOVED DAMAGE AND REPAIRED PER EA 11-96662. - [SDR 9503721144](https://openairdocs.org/sdr/9503721144.md): Frame · corroded · Mar 11, 1995 · N144JC · Doug DC1040 · Fuselage Main, Frame > DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON FRAME AT FS 1902 LONGERON 51R TO 50L AND FS 1997 LONGERON 51L TO 48R. REMOVED CORROSION AND INSTALLED DOUBLER PER EA 11-97827. - [SDR 9503711144](https://openairdocs.org/sdr/9503711144.md): Floorbeam · corroded · Mar 9, 1995 · N144JC · Doug DC1040 · Fuselage Main, Floor Beam > DURING PERIODIC INSPECTION, DAMAGE WAS FOUND ON THE FLOORBEAM AT FS 939 IN FORWARD CARGO COMPARTMENT. - [SDR 9504221144](https://openairdocs.org/sdr/9504221144.md): Bulkhead · cracked · Mar 7, 1995 · N144JC · Doug DC1040 · Fuselage Main, Bulkhead > DURING PERIODIC INSPECTION, A CRACK WAS FOUND ON THE LEFT AND RIGHT SIDE FUEL TANK BULKHEAD TEE AT FS 1159, X = 50. REMOVED CORROSION AND INSTALLED REPAIR ANGLES PER EA 11-97796. - [SDR 9504231144](https://openairdocs.org/sdr/9504231144.md): Longeron · corroded · Mar 6, 1995 · N144JC · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING PERIODIC INSPECTION, CORROSION WAS FOUND ON THE LEFT SIDE CENTER FUSELAGE EXTERNAL LONGERONS 30L-32L, FS 1386-1523. REMOVED CORROSION AND INSTALLED REPAIR ANGLES PER EA 11-96668. - [SDR 9504641144](https://openairdocs.org/sdr/9504641144.md): Longeron · cracked · Mar 2, 1995 · N144JC · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING PERIODIC INSPECTION, CRACKS WERE FOUND ON LONGERON 28L AT FS 514. LONGERON IS MADE FROM.050 INCH THICK 7075-T6 ALUMINUM. TRIMMED LONGERON AND INSTALLED DOUBLER PER EA11-96648. ## 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 = 'N144JC' AND deregistration_id = 'N144JC-2004-11-22' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N144JC-2004-11-22/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.