# Service difficulty reports: N152US, cancelled Oct 30, 2002 A list on [N152US, cancelled Oct 30, 2002](https://openairdocs.org/deregistered/N152US-2002-10-30.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 0100061152](https://openairdocs.org/sdr/0100061152.md): Door · unsecure · Jan 4, 2001 · N152US · Doug DC1040 · Accessory Compartment Doors > AIRCRAFT WOULD NOT PRESSURIZE DURING CLIMBOUT OF MCO. FLIGHT RETURNED TO MCO AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CENTER ACCESSORY DOOR UNSECURED. ACCESSORY DOOR WARNING SWITCH INOPERATIVE DUE TO BROKEN WIRE. REPAIRED BROKEN WIRE AND SECURED ACCE - [SDR 0000991152](https://openairdocs.org/sdr/0000991152.md): Engine · stalled · Mar 22, 2000 · N152US · Doug DC1040 · Engine (Turbine/Turboprop) > DURING TAKEOFF ROLL AT 125 KTS, THE NR 2 ENGINE AUDIBLY AND VISIBLY COMPRESSOR STALLED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE ENGINE PER TAFI INCLUDING A BOROSCOPE INSPECTION WITH NO DEFECTS NOTED. AN ENGIN - [SDR 9903411152](https://openairdocs.org/sdr/9903411152.md): Frame · cracked · Jul 30, 1999 · N152US · Doug DC1040 · Fuselage Main, Frame > DURING M-CHECK, FOUND CRACK ON VERTICAL LEG OF CARGO FLOOR FRAME AT FS 879, RBL 33. REPAIRED PER EA 11-169416. - [SDR 9903241152](https://openairdocs.org/sdr/9903241152.md): Fitting · corroded · Jul 22, 1999 · N152US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING M-CHECK, FOUND CORROSION ON ANGLE FITTING FROM FS 420 - 460. REPAIRED PER EA 11-168628. - [SDR 9903421152](https://openairdocs.org/sdr/9903421152.md): Beam · cracked · Jul 13, 1999 · N152US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING M-CHECK, FOUND CRACK IN I-BEAM SUPPORT AT FS 791, BL 0. REPAIRED PER EA 11-168291. - [SDR 9806981152](https://openairdocs.org/sdr/9806981152.md): Compressor · stalled · Apr 20, 1998 · N152US · Doug DC1040 · Turbine Engine Compressor Section > DURING LANDING ROLLOUT WHILE IN REVERSE THRUST, THE NR 1 ENGINE COMPRESSOR STALLED. THE ENGINE WAS SHUT DOWN WITH THE EGT REACHING A MAXIMUM OF 940C. MAINTENANCE INSPECTED THE ENGINE WITH NO DEFECTS NOTED AND THE AIRCRAFT WAS RETURNED TO SERVICE. - [SDR 9807481152](https://openairdocs.org/sdr/9807481152.md): Skin · corroded · Mar 11, 1998 · N152US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING L CHECK, FOUND CORROSION ON EXTERIOR SKIN AT FASTENERS FS 1801-1821, LONGERON 43R. REPAIRED PER EA 11-155549. - [SDR 9805531152](https://openairdocs.org/sdr/9805531152.md): Frame · cracked · Mar 11, 1998 · N152US · Doug DC1040 · Fuselage Main, Frame > DURING L-CHECK, FOUND CRACK IN FRAME AT FS 459, LBL 62 IN THE FORWARD AVIONICS COMPARTMENT. REPAIRED PER EA 11-150785. - [SDR 9805501152](https://openairdocs.org/sdr/9805501152.md): Frame · cracked · Mar 10, 1998 · N152US · Doug DC1040 · Fuselage Main, Frame > DURING L-CHECK, FOUND CRACK IN FRAME AT FS 459, RBL 62 IN FORWARD AVIONICS COMPARTMENT. REPAIRED PER EA 11-150785. - [SDR 9805521152](https://openairdocs.org/sdr/9805521152.md): Web · cracked · Mar 1, 1998 · N152US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING L-CHECK, FOUND A CRACK IN THE NOSE GEAR SUPPORT BEAM RIGHT WEB AT FS 476. REPAIRED PER EA 11-156156. - [SDR 9805511152](https://openairdocs.org/sdr/9805511152.md): Frame · cracked · Mar 1, 1998 · N152US · Doug DC1040 · Fuselage Main, Frame > DURING L-CHECK, FOUND CRACK IN FORWARD CARGO DOOR JAMB FS 895. REPAIRED PER EA 11-154993. - [SDR 9801691152](https://openairdocs.org/sdr/9801691152.md): Compressor · stalled · Jan 27, 1998 · N152US · Doug DC1040 · Turbine Engine Compressor Section > DURING LANDING ROLLOUT, THE NR 3 ENGINE COMPRESSOR STALLED. THE EGT REACHED 670C AND THE ENGINE WAS SHUT DOWN. THE CREW RESTARTED THE ENGINE WHILE TAXIING WITH ALL PARAMETERS NORMAL. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE ENGINE AND AN OPERATIONAL - [SDR 9801101152](https://openairdocs.org/sdr/9801101152.md): Compressor · stalled · Jan 18, 1998 · N152US · Doug DC1040 · Turbine Engine Compressor Section > AT TOP OF DESCENT WITH POWER REDUCTION, THE NR 1 ENGINE AUDIBLY COMPRESSOR STALLED. THERE WAS A SLIGHT VIBRATION AND RISING EGT. THE ENGINE WAS SHUT DOWN WITH A MAXIMUM EGT OF 690C. RESTART ATTEMPT WAS SUCCESSFUL AND THE ENGINE OPERATION WAS NORMAL FOR THE - [SDR 9717691152](https://openairdocs.org/sdr/9717691152.md): Power Supply · inoperative · Sep 17, 1997 · N152US · Doug DC1040 · Emergency Lighting > DURING LINE INSPECTION, FOUND THE EMERGENCY ESCAPE LIGHTS INOPERATIVE AT DOORS 3L AND 3R AND ROWS 22-27 (BOTH AISLES). MAINTENANCE REPLACED THE POWER SUPPLY, BATTERY PACK, AND REPAIRED THE CANNON PLUG. - [SDR 9713141152](https://openairdocs.org/sdr/9713141152.md): Battery Pack · discharged · Jul 5, 1997 · N152US · Doug DC1040 · Emergency Lighting > DURING LINE INSPECTION, MID CABIN EMERGENCY LIGHT BATTERY FAILED BITE TEST. MAINTENANCE REPLACED BATTERY PACK. - [SDR 9711781152](https://openairdocs.org/sdr/9711781152.md): Altimeter · failed · Jun 16, 1997 · N152US · Doug DC1040 · Altimeter, Barometric/Encoder > DURING CRUISE, FIRST OFFICER'S ALTIMETER OFF FLAG CAME INTO VIEW AND SMOKE COMING FROM THE UNIT. PULLED CIRCUIT BREAKERS AND RETURNED TO HNL. MAINTENANCE REPLACED THE ALTIMETER INDICATOR. - [SDR 9710681152](https://openairdocs.org/sdr/9710681152.md): Prbc · failed · Jun 3, 1997 · N152US · Doug DC1040 · Compressor Bleed Valve > DURING DESCENT, THE NR 2 ENGINE COMPRESSOR STALLED WITH RISING EGT. ENGINE WAS SHUT DOWN AT MAX EGT OF 650C. NR 2 ENGINE RESTART AND SUBSEQUENT OPERATION WERE NORMAL. MAINTENANCE REPLACED THE PRBC AND RAN ENGINE TO TAKEOFF POWER. ALL PARAMETERS WERE NORMAL - [SDR 9709461152](https://openairdocs.org/sdr/9709461152.md): Skin · corroded · May 7, 1997 · N152US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING LINE CHECK, FOUND CORROSION ON FUSELAGE SKIN UNDER LEFT BODY FAIRING FS 1741 - 1761. REPAIRED PER EA 11-124146. - [SDR 9702811152](https://openairdocs.org/sdr/9702811152.md): Fire Warning · illuminated · Feb 9, 1997 · N152US · Doug DC1040 · Fire Detection > DURING CLIMB, THE NR 3 ENIGNE FIRE INDICATION ILLUMINATED. SHUT DOWN ENGINE AND FIRE BOTTLE DISCHARGED. DUMPED 16,800 LBS AND RETURNED TO LAX. AIRCRAFT TO BE FERRIED TO MSP. - [SDR 9620671152](https://openairdocs.org/sdr/9620671152.md): Fitting · corroded · Sep 24, 1996 · N152US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING T-CHECK, FOUND CORROSION ON LONGERON 52 AT THE CENTER WHEEL WELL AFT SHELF FS 1509 TO 1521. REPLACED FITTING (P/N AYB 7063-501) PER SRM 51-00-00. - [SDR 9620461152](https://openairdocs.org/sdr/9620461152.md): Fitting · corroded · Sep 21, 1996 · N152US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING T-CHECK, FOUND CORROSION ON THE LONGERON 48R ATTACH FITTING AT FS 1509 TO 1521. REPLACED FITTING (P/N AYB 7061-1). - [SDR 9620641152](https://openairdocs.org/sdr/9620641152.md): Longeron · corroded · Sep 20, 1996 · N152US · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING T-CHECK, FOUND CORROSION ON THE OVERWING EXTERNAL LONGERONS 29R AND 30R FROM FS 1432 TO 1501. REPAIRED LONGERONS PER EA 11-110221. - [SDR 9621191152](https://openairdocs.org/sdr/9621191152.md): Floor Beam · cracked · Sep 19, 1996 · N152US · Doug DC1040 · Fuselage Main, Floor Beam > DURING T-CHECK, FOUND A CRACK IN THE FORWARD CARGO FLOOR BEAM AT FS 1099, LBL 58. REPAIRED BEAM (P/N ADA 0039-5) PER EA 11-110248. - [SDR 9621171152](https://openairdocs.org/sdr/9621171152.md): Longeron · corroded · Sep 18, 1996 · N152US · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING T-CHECK, FOUND CORROSION ON LONGERON 46R FROM FS 1754 - 1812. REPAIRED LONGERON (P/N AFA 7098-1) PER EA 11-110220. - [SDR 9621161152](https://openairdocs.org/sdr/9621161152.md): Longeron · corroded · Sep 17, 1996 · N152US · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING T-CHECK, FOUND CORROSION ON LONGERON 48R FROM FS 1964 - 1970. REPAIRED LONGERON (P/N AGA 7047-501) PER EA 11-110251. - [SDR 9620621152](https://openairdocs.org/sdr/9620621152.md): Seat Track · corroded · Sep 17, 1996 · N152US · Doug DC1040 · Fuselage, Seat/Cargo Attach Fittings > DURING T-CHECK, FOUND CORROSION ON THE RBL 65 SEAT TRACK AT FS 1841. REPAIRED TRACK (P/N NFA 6222-39) PER EA 11-110225. - [SDR 9619841152](https://openairdocs.org/sdr/9619841152.md): Fitting · corroded · Sep 15, 1996 · N152US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING T-CHECK, FOUND CORROSION ON THE LONGERON 52 END FITTING AT FS 1521. REPLACED FITTING PER SRM 53-00-01. - [SDR 9620611152](https://openairdocs.org/sdr/9620611152.md): Door Jamb · cracked · Sep 12, 1996 · N152US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING T-CHECK, FOUND TWO CRACKS IN THE NR 3R DOOR JAMB FORWARD WEB FS 1250 TO 1256 AT THE FLOOR LEVEL. REPAIRED WEB (P/N AEA 0155-2) PER EA 11-110246. - [SDR 9619821152](https://openairdocs.org/sdr/9619821152.md): Skin · corroded · Sep 11, 1996 · N152US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING T-CHECK, FOUND CORROSION AND A SHEARED BOLT IN THE 4L DOOR CUTOUT SPLICE FS 1851 AT LONGERON 15L. REPLACED BOLT PER SRM 51-31-01. - [SDR 9613631152](https://openairdocs.org/sdr/9613631152.md): Oil Fill Line · loose · Jun 18, 1996 · N152US · Doug DC1040 · Turbine Engine Oil System > THE NR 1 ENGINE OIL QUANTITY BEGAN TO DECREASE AND AT FIVE GALLONS, THE ENGINE WAS SHUT DOWN. CREW FOLLOWED COM PROCEDURE AND RETURNED TO HNL. ALSO, ON TAXIING TO GATE, APU FIRE WARNING LIGHT ILLUMINATED. CREW FOLLOWED COM PROCEDURE AND FIRED BOTTLE. INSPE - [SDR 9608171152](https://openairdocs.org/sdr/9608171152.md): Battery Pack · discharged · Mar 22, 1996 · N152US · Doug DC1040 · Emergency Lighting > DURING INSPECTION, FOUND THE EMERGENCY LIGHTS IN THE FORWARD CABIN FAILED THE SELF-TEST. REPLACED THE BATTERY PACK. - [SDR 9512171152](https://openairdocs.org/sdr/9512171152.md): Override Valve · malfunctioned · Aug 9, 1995 · N152US · Doug DC1040 · Compressor Bleed Control > DURING LANDING ROLL, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL WHILE IN REVERSE THRUST. THE EGT WENT TO 910 DEGREES AND THE ENGINE WAS SHUTDOWN. THE ENGINE WAS INSPECTED AND THE 3.0 BLEED OVERRIDE SOLENOID VALVE WAS REPLACED. GROUND RUNUP CONFIRMED PRO - [SDR 9508851152](https://openairdocs.org/sdr/9508851152.md): Compressor · stalled · Jun 3, 1995 · N152US · Doug DC1040 · Turbine Engine Compressor Section > DURING CRUISE WHILE TAKING WHITE LINE READINGS, THE NR 3 ENGINE EXPERIENCED A COMPRESSOR STALL AND WAS SHUTDOWN. THE AIRCRAFT CONTINUED TO MSP WHERE AN UNEVENTFUL TWO ENGINE LANDING WAS MADE, NO FUEL WAS DUMPED. THE ENGINE WAS REPLACED. - [SDR 9504731152](https://openairdocs.org/sdr/9504731152.md): Angle · corroded · Mar 25, 1995 · N152US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE 'J' ANGLE AT FS 1781, RBL 20 - LBL 15 BELOW THE SUMP FLOOR. REMOVED CORROSION AND INSTALLED DOUBLER. - [SDR 9504751152](https://openairdocs.org/sdr/9504751152.md): Bulkhead · corroded · Mar 24, 1995 · N152US · Doug DC1040 · Fuselage Main, Bulkhead > DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE BULKHEAD AT FS 1157, STR 51R AND 50R IN THE CENTER ACCESSORY COMPARTMENT. REMOVED CORROSION AND INSTALLED REPAIR DOUBLERS AND FILLERS PER EA 11-97898. - [SDR 9504741152](https://openairdocs.org/sdr/9504741152.md): Longeron · corroded · Mar 24, 1995 · N152US · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING PERIODIC CHECK, CORROSION WAS FOUND ON LONGERON 52 AT FS 1139 - 1156 IN CENTER ACCESSORY COMPARTMENT. REMOVED CORROSION AND INSTALLED REPAIR DOUBLERS PER EA 11-97898. - [SDR 9505191152](https://openairdocs.org/sdr/9505191152.md): Skin · corroded · Mar 23, 1995 · N152US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE FUSELAGE SKIN AND BULKHEAD AFT OF CENTER LANDING GEAR AT FS 1509 - 1531, LONGERONS 50L AND 50R. REMOVED CORROSION AND INSTALLED REPAIR DOUBLERS PER EA 11-97918. - [SDR 9504891152](https://openairdocs.org/sdr/9504891152.md): Bulkhead · corroded · Mar 21, 1995 · N152US · Doug DC1040 · Fuselage Main, Bulkhead > DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE CENTER WING PRESSURE BULKHEAD AND LONGERON 52 IN THE CENTER ACCESSORY COMPARTMENT. REPAIRED BULKHEAD PER EA N11-97898. - [SDR 9504481152](https://openairdocs.org/sdr/9504481152.md): Rib · damaged · Mar 21, 1995 · N152US · Doug DC1040 · Elevator, Spar/Rib > DURING PERIODIC CHECK, FOUND THE RIGHT DETACHABLE ELEVATOR RIB DAMAGED AT FS XE =67.226, 49.5 INCHES FROM TRAILING EDGE. REPAIRED PER SRM 55-20-00. - [SDR 9504471152](https://openairdocs.org/sdr/9504471152.md): Roller Tray · corroded · Mar 21, 1995 · N152US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING PERIODIC CHECK, CORROSION WAS FOUND ON THE ROLLER TRAY IN THE FORWARD CARGO COMPARTMENT AT FS 759, RBL 28. REMOVED CORROSION AND INSTALLED DOUBLER AND FILLER PER EA 11-97896. ## 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 = 'N152US' AND deregistration_id = 'N152US-2002-10-30' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N152US-2002-10-30/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.