# Service difficulty reports: N155US, cancelled Jul 18, 2002 A list on [N155US, cancelled Jul 18, 2002](https://openairdocs.org/deregistered/N155US-2002-07-18.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR 0101881155](https://openairdocs.org/sdr/0101881155.md): A/C Pack · contaminated · May 17, 2001 · N155US · Doug DC1040 · Cabin Cooling System > DURING CLIMB, FLIGHT ATTENDANTS REPORTED FUMES AND FINE MIST IN CABIN. FOLLOWED COM PROCEDURE. SMOKE DISSIPATED AFTER NR 1 PACK TURNED OFF. FLIGHT CONTINUED TO MCO FOR AN UNEVENTFUL LANDING. MAINTENANCE FOUND NR 1 PACK CONTAMINATED WITH OIL. REPLACED ALL - [SDR 0101871155](https://openairdocs.org/sdr/0101871155.md): Harness · burned · May 16, 2001 · N155US · Doug DC1040 · Buffet/Galleys > DURING CLIMBOUT OF MSP, CABIN CREW REPORTED SMOKE AND ODOR IN MID CABIN. FOLLOWED COM PROCEDURE WITH NO NOTICEABLE CHANGE IN CONDITION. FLIGHT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE DRAINED GEARBOX AND RESERVICED. CHANGED SOCKS AND BURNED - [SDR 0002651155](https://openairdocs.org/sdr/0002651155.md): Unknown · odor · Jul 27, 2000 · N155US · Doug DC1040 · Air Distribution System > AFTER TAKEOFF, FLIGHT ATTENDANT REPORTED PUNGENT SMELL IN AFT CABIN. AFTER VERIFICATION BY SECOND OFFICER, FLIGHT DIVERTED TO PSM AND LANDED WITHOUT INCIDENT. MAINTENANCE CHECKED SYSTEM PER MAINTENANCE MANUAL AND FOUND ALL NORMAL. AIRCRAFT RETURNED TO SERVI - [SDR 9810001155](https://openairdocs.org/sdr/9810001155.md): Web · cracked · Aug 27, 1998 · N155US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING M-CHECK, FOUND CRACK IN WEB UPPER STRUCTURE IN LOWER RADIUS. REPLACED WEB DOUBLER PER EA 11-159807. - [SDR 9810021155](https://openairdocs.org/sdr/9810021155.md): Bracket · corroded · Aug 25, 1998 · N155US · Doug DC1040 · Rudder Structure > DURING M-CHECK, FOUND CORROSION IN UPPER FASTENER BRACKET IN RUDDER. REPAIRED PER EA 11-160285. - [SDR 9810041155](https://openairdocs.org/sdr/9810041155.md): Angle · corroded · Jul 14, 1998 · N155US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING M-CHECK, FOUND LOWER CHORD ANGLE CORRODED ON INBOARD END. REPAIRED PER EA 11-158027. - [SDR 9809961155](https://openairdocs.org/sdr/9809961155.md): Skin · corroded · Jul 1, 1998 · N155US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING M-CHECK, FOUND CORROSION ON OUTER SKIN FROM FS 1510 TO 1531, STR 45R TO 45L. REPAIRED PER EA 11-158670. - [SDR 9809951155](https://openairdocs.org/sdr/9809951155.md): Skin · cracked · Jun 19, 1998 · N155US · Doug DC1040 · Wing, Plate/Skin > DURING M-CHECK, FOUND TWO INCH CRACK IN INBOARD EDGE OF LEADING EDGE FLEX SKIN. REPAIRED PER EA 11-155651. - [SDR 9806761155](https://openairdocs.org/sdr/9806761155.md): Compressor · stalled · Apr 15, 1998 · N155US · Doug DC1040 · Turbine Engine Compressor Section > WHILE CLIMBING THRU 9500 FEET, THE NR 1 ENGINE COMPRESSOR STALLED. THE ENGINE WAS SHUT DOWN PER COM AND THE AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE PER MAINTENANCE AND TAFI MANUALS INCLUDING A BORESCOPE WITH NO - [SDR 9806391155](https://openairdocs.org/sdr/9806391155.md): Compressor · stalled · Apr 8, 1998 · N155US · Doug DC1040 · Turbine Engine Compressor Section > AT TOP OF DESCENT, THE NR 3 ENGINE COMPRESSOR STALLED WHEN THE POWER LEVER WAS RETARDED. THE ENGINE ROLLED BACK AND THE EGT BEGAN TO RISE. EGT CLIMBED TO 810C AND THE ENGINE WAS SHUT DOWN. THE COM PROCEDURE WAS FOLLOWED AND A SUCCESSFUL RESTART WAS ACCOMPLI - [SDR 9800521155](https://openairdocs.org/sdr/9800521155.md): Compressor · stalled · Jan 11, 1998 · N155US · Doug DC1040 · Turbine Engine Compressor Section > AFTER STARTING DESCENT FROM FL330, THE NR 2 ENGINE COMPRESSOR STALLED. POWER WAS REDUCED TO IDLE AND AFTER EGT REACHING 820C THE ENGINE RECOVERED. WHILE DESCENDING FROM FL290, THE NR 2 ENGINE STALLED AGAIN WITH MAX EGT OF 760. THE CREW FOLLOWED COM PROCEDUR - [SDR 9800201155](https://openairdocs.org/sdr/9800201155.md): Compressor · stalled · Jan 4, 1998 · N155US · Doug DC1040 · Turbine Engine Compressor Section > DURING DESCENT, THE NR 3 ENGINE COMPRESSOR STALLED AND EXPERIENCED A FLAME-OUT. MAXIMUM EGT REACHED WAS 830C. THE CREW FOLLOWED COM PROCEDURES AND RESTART WAS SUCCESSFUL. THE ENGINE OPERATED NORMALLY FOR THE REMAINDER OF THE FLIGHT. MAINTENANCE INSPECTED T - [SDR 9716201155](https://openairdocs.org/sdr/9716201155.md): Ins Connector · broken · Aug 22, 1997 · N155US · Doug DC1040 · Inertial Guidance System > DURING TAKEOFF ROLL, THE NR 2 INS FAILED WITH THE NR 3 INS ON MEL. FLIGHT RETURNED TO MSP. MAINTENANCE REPAIRED CANNON PLUGS ON BOTH NR 2 AND NR 3 INS SYSTEMS. - [SDR 9709631155](https://openairdocs.org/sdr/9709631155.md): Tr Unit · malfunctioned · May 1, 1997 · N155US · Doug DC1040 · Engine Thrust Reverser > WHEN POWER PUSHED UP TO TAKEOFF LEVEL, THE NR 3 ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED. AIRCRAFT RETURNED TO THE GATE AND MAINTENANCE DEFERRED NR 3 THRUST REVERSER PER MEL 78-1A. SPECIFIC PART CAUSING PROBLEM TO BE DETERMINED. - [SDR 9701241155](https://openairdocs.org/sdr/9701241155.md): Compressor · stalled · Jan 22, 1997 · N155US · Doug DC1040 · Turbine Engine Compressor Section > DURING TOP OF DESCENT FROM 33,000 FEET, NR 2 ENGINE STALLED. FLIGHT CREW NOTICED EGT RISE AND ELECTED TO SHUTDOWN NR 2 ENGINE. A SUCCESSFUL RELIGHT WAS ACCOMPLISHED BUT THE ENGINE WAS SHUTDOWN AGAIN DUE TO HIGH EGT. AN UNEVENTFUL LANDING WAS PERFORMED AT DE - [SDR 9700581155](https://openairdocs.org/sdr/9700581155.md): Turbine · damaged · Jan 10, 1997 · N155US · Doug DC1040 · Turbine Section > DURING DESCENT, THE NR 2 ENGINE EXPERIENCED A STALL AND POWER LOSS. PILOT ELECTED TO SHUT DOWN AND THEN RESTART NR 2 ENGINE. AN UNEVENTFUL LANDING FOLLOWED. MAINTENANCE BORESCOPE INSPECTION REVEALED TURBINE SECTION DAMAGE. REPLACED NR 2 ENGINE. - [SDR 9627681155](https://openairdocs.org/sdr/9627681155.md): Frame · cracked · Nov 27, 1996 · N155US · Doug DC1040 · Fuselage Main, Frame > DURING L-CHECK, A CRACK WAS FOUND ON THE LOWER NOSE FUSELAGE FRAME AT STA 459 AND X=61. REPAIRED PER EA 11-12013, (P/N ABA7348-3). - [SDR 9611291155](https://openairdocs.org/sdr/9611291155.md): Tr Unit · malfunctioned · May 20, 1996 · N155US · Doug DC1040 · Engine Thrust Reverser > DURING TAKEOFF ROLLOUT, THE NR 3 ENGINE REVERSER UNLOCK LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE NR 3 REVERSER AND FOUND IT TO BE NORMAL. DURING REVERSER OPERATION WITH GROUND AIR, REVERSER DEPL - [SDR 9611221155](https://openairdocs.org/sdr/9611221155.md): Compressor · stalled · May 20, 1996 · N155US · Doug DC1040 · Turbine Engine Compressor Section > DURING LANDING ROLLOUT, THE NR 1 AND NR 3 ENGINES EXPERIENCED COMPRESSOR STALLS IN REVERSE. MAXIMUM TEMPERATURE WAS AT 700 DEGRESS CELSIUS FOR BOTH ENGINES. BOTH ENGINES WERE SHUT DOWN AND RESTARTED. CREW FOLLOWED COCKPIT PROCEDURE AND TAXIED TO THE GATE WI - [SDR 9610411155](https://openairdocs.org/sdr/9610411155.md): Engine · malfunctioned · May 9, 1996 · N155US · Doug DC1040 · Engine (Turbine/Turboprop) > DURING LANDING ROLLOUT, THE NR 3 ENGINE EXPERIENCED REVERSE STALL WITH A SUBSEQUENT TAILPIPE FLAME WHICH WAS REPORTED BY THE CONTROL TOWER. THE NR 3 ENGINE WAS SHUTDOWN AND FIRE BOTTLE DISCHARGED AS EGT CLIMBED TO 915 DEGREES CELSIUS. HOWEVER, THERE WAS NO F - [SDR 9609111155](https://openairdocs.org/sdr/9609111155.md): Bleed Valve · malfunctioned · Apr 21, 1996 · N155US · Doug DC1040 · Compressor Bleed Valve > AT TOP OF DESCENT, THE NR 2 ENGINE EXPERIENCED COMPRESSOR STALL. THE EGT ROSE TO 800 DEGREES AND BACK TO NORMAL WITHIN A MINUTE. ALSO, WITH LOW FUEL FLOW N1 AND N2 WOULD NOT RESPOND TO THROTTLE MOVEMENTS. CREW FOLLOWED COCKPIT OPERATING MANUAL AND CONTINUED - [SDR 9513561155](https://openairdocs.org/sdr/9513561155.md): Fuel Control · malfunctioned · Sep 3, 1995 · N155US · Doug DC1040 · Fuel Control/Turbine Engines > TOP OF DESCENT, NR 2 ENGINE COMPRESSOR STALLED. SHUTDOWN ENGINE AND CONTINUED LANDING. BORESCOPED, PERFORMED PRECISION TRIM AND REPLACED ENGINE CONTROL. - [SDR 9511641155](https://openairdocs.org/sdr/9511641155.md): Skin · corroded · Jul 24, 1995 · N155US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING PERIODIC CHECK, FOUND CORROSION ON THE UNDERWING BARREL SKIN FS 1510 - 1531, LONGERON 51L - 51R. REPAIRED SKIN (P/N AYB 7065) PER EA 11-82926. - [SDR 9511631155](https://openairdocs.org/sdr/9511631155.md): Floor Beam · cracked · Jul 22, 1995 · N155US · Doug DC1040 · Fuselage Main, Floor Beam > DURING PERIODIC CHECK, FOUND A CRACK IN THE FS 1178 FLOOR BEAM AT RBL 104. REPAIRED BEAM (P/N AEA 0361) PER EA 11-99038. - [SDR 9511621155](https://openairdocs.org/sdr/9511621155.md): Skin · corroded · Jul 22, 1995 · N155US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING PERIODIC CHECK, FOUND CORROSION ON THE FUSELAGE SKIN AND FINGER DOUBLERS FS 1129 AT LONGERON 48R. REPAIRED PER EA 11-98907. - [SDR 9511951155](https://openairdocs.org/sdr/9511951155.md): Clip · corroded · Jul 21, 1995 · N155US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING PERIODIC CHECK, FOUND CORROSION ON THE T-CLIP AT FS 979 BETWEEN LONGERONS 44R AND 45R. REPAIRED CLIP (P/N ADA 0252-7), PER EA 11-98910. - [SDR 9511611155](https://openairdocs.org/sdr/9511611155.md): Skin · corroded · Jul 19, 1995 · N155US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING PERIODIC CHECK, FOUND CORROSION ON THE FUSELAGE SKIN AT FS 1139, LONGERON 43L - 47L. REPAIRED SKIN (P/N AYB 7065-1) PER EA 11-99040. - [SDR 9511601155](https://openairdocs.org/sdr/9511601155.md): Skin · corroded · Jul 15, 1995 · N155US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING PERIODIC CHECK, FOUND CORROSION ON THE FORWARD RADIO ALTIMETER MOUNTING RINGS. REPAIRED BOTH PER EA 11-98579. - [SDR 9511591155](https://openairdocs.org/sdr/9511591155.md): Floor Beam · cracked · Jul 14, 1995 · N155US · Doug DC1040 · Fuselage Main, Floor Beam > DURING PERIODIC CHECK, FOUND CRACKS AND CORROSION ON THE FS 791 FLOOR BEAM AT X16, X14. REPAIRED BEAM (P/N ADA 7226-13) PER EA 11-99045. - [SDR 9511581155](https://openairdocs.org/sdr/9511581155.md): Track · corroded · Jul 11, 1995 · N155US · Doug DC1040 · Fuselage, Seat/Cargo Attach Fittings > DURING PERIODIC CHECK, FOUND CORROSION ON THE LBL 27.5 SEAT TRACK AT FS 435 - 450. REPAIRED TRACK (P/N ABA 7684-503) PER EA 11-82931. - [SDR 9508151155](https://openairdocs.org/sdr/9508151155.md): Skin · torn · May 17, 1995 · N155US · Doug DC1040 · Wing, Plate/Skin > DURING LINE CHECK, FOUND A 21 BY 8 SECTION OF TRAILING EDGE SKIN TORN FROM THE LEFT WING OUTBOARD OF THE OUTBOARD AILERON. REPAIRED PER EA 11-98538, MFG PART NUMBER ARC0550-1. - [SDR 9506511155](https://openairdocs.org/sdr/9506511155.md): Switch · lack of lube · Apr 24, 1995 · N155US · Doug DC1040 · Central Warning > DURING TAKEOFF, THE TAKEOFF WARNING HORN SOUNDED. TAKEOFF WAS ABORTED. LUBED AND CYCLED SPEED BRAKE HANDLE SWITCH MECHANISM. ## 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 = 'N155US' AND deregistration_id = 'N155US-2002-07-18' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N155US-2002-07-18/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.