# Service difficulty reports: N148US, cancelled Dec 14, 2001 A list on [N148US, cancelled Dec 14, 2001](https://openairdocs.org/deregistered/N148US-2001-12-14.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 0100721148](https://openairdocs.org/sdr/0100721148.md): Coalescer Bag · dirty · Feb 17, 2001 · N148US · Doug DC1040 · Humidity Control System > AFTER TAKEOFF, AIR CONDITIONING PACKS PRODUCED A BLUE CLOUD OF BILLOWING SMOKE. FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. FOUND NR 2 AND NR 3 COALESCER BAGS DIRTY. REPLACED COALESCER BAGS AND PERFORMED PACK BURNOUT PROCEDURE. REPLACED AIR CYCLE M - [SDR 9806911148](https://openairdocs.org/sdr/9806911148.md): Tr Unit · malfunctioned · Apr 16, 1998 · N148US · Doug DC1040 · Engine Thrust Reverser > DURING TAKEOFF ROLL, THE NR 2 ENGINE REVERSER UNLOCKED LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PLACED THE REVERSER ON MEL 78-1A. - [SDR 9806411148](https://openairdocs.org/sdr/9806411148.md): Tr Unit · malfunctioned · Apr 9, 1998 · N148US · Doug DC1040 · Engine Thrust Reverser > WHEN ENGINE POWER WAS ADVANCED TO THE TAKEOFF SETTING, THE NR 2 ENGINE THRUST REVERESER UNLOCK INDICATION ILLUMINATED. THE TAKEOFF WAS ABORTED AT APPROXIMATELY 30 KTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PLACED THE REVERSER ON MEL 78-1A. - [SDR 9804851148](https://openairdocs.org/sdr/9804851148.md): Compressor · stalled · Mar 20, 1998 · N148US · Doug DC1040 · Fuel Controlling System > DURING THE LANDING ROLLOUT WHILE IN REVERSE THRUST AT 85 KTS, THE NR 3 ENGINE COMPRESSOR STALLED. THE EGT ROSE TO 900C BEFORE THE ENGINE WAS SHUT DOWN. MAINTENANCE INSPECTED THE ENGINE WITH NO DEFECTS NOTED. THE REVERSER WAS PLACED ON MEL 78-1A DUE TO LACK - [SDR 9802721148](https://openairdocs.org/sdr/9802721148.md): Power Supply · inoperative · Feb 14, 1998 · N148US · Doug DC1040 · Emergency Lighting > DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE FROM DOOR 2 TO DOOR 3. REPLACED POWER SUPPLY AND BATTERY, OPERATIONAL CHECK OK. - [SDR 9803051148](https://openairdocs.org/sdr/9803051148.md): Pressure Panel · corroded · Feb 7, 1998 · N148US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING PERIODIC CHECK, FOUND CORROSION ON THE AFT PRESSURE BULKHEAD IN THE CENTER WHEEL WELL AT FS 1368. REPAIRED PER EA 11-154567. - [SDR 9803921148](https://openairdocs.org/sdr/9803921148.md): Skin · corroded · Feb 2, 1998 · N148US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING PERIODIC CHECK, FOUND CORROSION ON FUSELAGE EXTERNAL SKIN AT FS 1521 TO 1532, LBL 5 TO RBL 3, LONGERON 48L AND 48R. REPAIRED PER EA 11-154367. - [SDR 9803061148](https://openairdocs.org/sdr/9803061148.md): Longeron · corroded · Jan 29, 1998 · N148US · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING PERIODIC CHECK, FOUND CORROSION ON LONGERON 48R AT FS 1099. REPAIRED PER EA 11-155274. - [SDR 9803931148](https://openairdocs.org/sdr/9803931148.md): Pressure Web · cracked · Jan 16, 1998 · N148US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING PERIODIC CHECK, FOUND CRACK IN NOSE LANDING GEAR WHEEL WELL RIGHT PRESSURE PANEL WEB FS 495. REPAIRED PER EA 11-153941. - [SDR 9719781148](https://openairdocs.org/sdr/9719781148.md): Prox Box · malfunctioned · Oct 22, 1997 · N148US · Doug DC1040 · Landing Gear Position and Warning > DURING APPROACH, THE SAFE AND UNSAFE GEAR INDICATION LIGHTS DID NOT ILLUMINATE. APPROACH WAS ABORTED. DUE TO WEATHER AND FUEL CONCERNS FLIGHT PROCEEDED TO CDG. RECYCLED GEAR AND INDICATION NORMAL. MAINTENANCE RESEATED LANDING GEAR PROXIMITY BOX, NO FAULTS - [SDR 9716051148](https://openairdocs.org/sdr/9716051148.md): Tr Cable · out of adjust · Aug 21, 1997 · N148US · Doug DC1040 · Engine Thrust Reverser > WHILE ADVANCING THROTTLES TO TAKEOFF POWER, THE NR 2 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE LOCKED OUT THE NR 2 THRUST REVERSER AND PLACED IT ON MEL 78-1A. AIRCRAFT THEN DE - [SDR 09712131148](https://openairdocs.org/sdr/09712131148.md): Engine · malfunctioned · Jun 22, 1997 · N148US · Doug DC1040 · Engine (Turbine/Turboprop) > CREW ABORTED TAKEOFF AT 110 KNOTS WHEN THE NR 1 ENGINE WOULD NOT REACH TAKEOFF EPR. TAKEOFF EPR WAS SET TO 1.51, BUT NR 1 ENGINE ONLY REACHED 1.45. ALL OTHER ENGINE INDICATIONS WERE NORMAL. CREW RAN ENGINE TO TAKEOFF EPR OF 1.51 AND PERFORMED BLEED CHECK PE - [SDR 9709171148](https://openairdocs.org/sdr/9709171148.md): Compressor · stalled · May 7, 1997 · N148US · Doug DC1040 · Turbine Engine Compressor Section > DURING TAKEOFF ROLL WITH POWER APPLICATION, THE NR 3 ENGINE COMPRESSOR STALLED. TAKEOFF WAS ABORTED WITH NO ENGINE LIMITS EXCEEDED. SECOND TAKEOFF WITH SLOWER POWER APPLICATION WAS NORMAL. MAINTENANCE VISUALLY INSPECTED ENGINE PER MM 71-00-00. NO DEFECTS W - [SDR 9707401148](https://openairdocs.org/sdr/9707401148.md): Air Data Comp · failed · Apr 10, 1997 · N148US · Doug DC1040 · Air Data Computer > DURING TAKEOFF ROLL, THE CAPTAIN'S AIRSPEED INDICATOR READ ZERO WHILE THE COPILOT'S READ 120. ABORTED TAKEOFF. MAINTENANCE REPLACED THE AIR DATA COMPUTER. - [SDR 9704941148](https://openairdocs.org/sdr/9704941148.md): Skin · cracked · Feb 25, 1997 · N148US · Doug DC1040 · Wing, Plate/Skin > DURING L-CHECK, FOUND CRACK IN WING SKIN AT FORWARD INBOARD CORNER OF REFUELING DOOR AT STA XORS506. REPAIRED PER EA 11-121770. - [SDR 9614331148](https://openairdocs.org/sdr/9614331148.md): Switch · broken · Jun 30, 1996 · N148US · Doug DC1040 · Landing Gear Position and Warning > DURING CLIMB, PLACED THE GEAR HANDLE IN THE UP POSITION. THE 4 UNSAFE LIGHTS REMAINED ILLUMINATED. FOLLOWED COM 2.32.16 AND VERIFIED GEAR UP. MAINTENANCE REPLACED THE S1-342 SWITCH. - [SDR 9601461148](https://openairdocs.org/sdr/9601461148.md): Solenoid · failed · Jan 19, 1996 · N148US · Doug DC1040 · Compressor Bleed Valve > DURING LANDING, THE NR 1 ENGINE EXPERIENCED COMPRESSOR STALL. EGT INCREASED TO TOP OF SCALE. CREW FOLLOWED COCKPIT OPERATING PROCEDURE, SHUT NR 1 ENGINE DOWN AND MOTORED UNTIL EGT IS BELOW 100C. BORESCOPED NR 1 ENGINE AND INSPECTED PER MM 71-00-00. REPLACE - [SDR 9515231148](https://openairdocs.org/sdr/9515231148.md): De-Oiler Shaft · failed · Oct 6, 1995 · N148US · Doug DC1040 · Turbine Engine Oil System > DURING CRUISE, THE NR 3 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED, OIL QUANTITY WENT TO ZERO AND THE ENGINE WAS SHUTDOWN. THE AIRCRAFT DIVERTED TO BOS WHERE AN UNEVENTFUL TWO ENGINE LANDING WAS ACCOMPLISHED, NO FUEL WAS DUMPED. THE DE-OILER SHAFT WAS FOUND S - [SDR 9503211149](https://openairdocs.org/sdr/9503211149.md): Pwr Lever Cable · lack of lube · Feb 23, 1995 · N148US · Doug DC1040 · Power Lever > DURING LANDING (AMS), THE NR 2 ENGINE POWER LEVER COULD NOT BE RETARDED AND THE ENGINE WAS SHUT DOWN DURING ROLLOUT. THE POWER LEVER CABLE WAS CLEANED, LUBRICATED, AND OPERATION CHECKED OK. - [SDR 9502751148](https://openairdocs.org/sdr/9502751148.md): Transmitter · failed · Feb 20, 1995 · N148US · Doug DC1040 · Engine RPM Indicating System > DURING TAKEOFF, THE NR 1 ENGINE FAIL LIGHT ILLUMINATED AND THE TAKEOFF WAS ABORTED. REPLACED THE NR 1 ENGINE N1 TRANSMITTER. ## 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 = 'N148US' AND deregistration_id = 'N148US-2001-12-14' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N148US-2001-12-14/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.