# Service difficulty reports: N161US, cancelled Oct 30, 2002 A list on [N161US, cancelled Oct 30, 2002](https://openairdocs.org/deregistered/N161US-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 0200811161](https://openairdocs.org/sdr/0200811161.md): Projector · Mar 14, 2002 · N161US · Doug DC1040 · Entertainment System > During cruise electrical odor noticed around door 3 area when overhead projector on. Flight continued to DTW and landed without incident. Maintenance replaced overhead projector.See Logpage 6991285.No previous history in last 30 days. - [SDR 9904381161](https://openairdocs.org/sdr/9904381161.md): Slide · malfunctioned · Oct 15, 1999 · N161US · Doug DC1040 · Escape Slide > DURING CRUISE DOOR 1L EMERGENCY EVACUATION SLIDE PARTIALLY INFLATED AND BROKE OUT OF THE COVER. THE SLIDE WAS PUNCTURED TO DEFLATE AND MOVED OUT OF GALLEY AREA. FLIGHT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE SLIDE, COVER, AND - [SDR 9901341161](https://openairdocs.org/sdr/9901341161.md): Longeron · corroded · Feb 18, 1999 · N161US · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING M-CHECK, FOUND CORROSION ON LONGERON 27R WEB STRUCTURE AT FS 1522 TO 1540. REPAIRED PER EA 11-162951. - [SDR 9900991161](https://openairdocs.org/sdr/9900991161.md): Longeron · corroded · Feb 17, 1999 · N161US · Doug DC1040 · Fuselage Main, Longeron/Stringer > DURING M-CHECK, FOUND CORROSION ON LONGERON 44R FROM FS 1009 TO 1039. REPAIRED PER EA 11-164772. REPAIRED PER EA 11-164772. - [SDR 9901181161](https://openairdocs.org/sdr/9901181161.md): Floorbeam · cracked · Feb 16, 1999 · N161US · Doug DC1040 · Fuselage Main, Floor Beam > DURING M-CHECK, FOUND CRACK ON FLOOR I BEAM AT FS 791, LBL 18 TO RBL 18. REPAIRED PER EA 11-162954. - [SDR 9900981161](https://openairdocs.org/sdr/9900981161.md): Seat Track · corroded · Feb 12, 1999 · N161US · Doug DC1040 · Fuselage, Seat/Cargo Attach Fittings > DURING M-CHECK, FOUND GOUGING AND CORROSION ON THE OUTBOARD AFT CABIN SEAT TRACK LBL 108 AT FS 1661 TO 1700. REPAIRED PER EA 11-164769. - [SDR 9901191161](https://openairdocs.org/sdr/9901191161.md): Frame · cracked · Feb 5, 1999 · N161US · Doug DC1040 · Fuselage Main, Frame > DURING M-CHECK, FOUND CRACK IN FORWARD CARGO FLOOR FRAME AT FS 1099 AT LBL 38. REPAIRED PER EA 11-158134. - [SDR 9811261161](https://openairdocs.org/sdr/9811261161.md): Power Supply · inop · Sep 30, 1998 · N161US · Doug DC1040 · Emergency Lighting > DURING LINE CHECK, FOUND EMERGENCY LIGHTS WOULD NOT TEST. REPLACED OVERWING POWER SUPPLY. OPERATIONAL CHECK OK. - [SDR 9811251161](https://openairdocs.org/sdr/9811251161.md): Power Supply · inop · Sep 22, 1998 · N161US · Doug DC1040 · Emergency Lighting > DURING LINE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING FROM DOOR 3L AND 3R TO ROW 32 INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY AND CONTROL UNIT. OPERATIONAL CHECK OK. - [SDR 9811271161](https://openairdocs.org/sdr/9811271161.md): Battery Pack · discharged · Sep 18, 1998 · N161US · Doug DC1040 · Emergency Lighting > DURING LINE CHECK, FOUND EMERGENCY FLOOR LIGHTING INOPERATIVE FROM DOOR 3L AND 3R TO ROW 32. REPLACED BATTERY PACK ABOVE DOOR 3L. OPERATIONAL CHECK OK. - [SDR 9804391161](https://openairdocs.org/sdr/9804391161.md): Cadc · failed · Mar 14, 1998 · N161US · Doug DC1040 · Air Data Computer > ON TAKEOFF ROLL, CAPTAIN'S AIRSPEED INDICATOR INDICATED 20 KTS BELOW FIRST OFFICER'S. ABORTED TAKEOFF AT 140 KTS AND RETURNED TO THE GATE. REPLACED THE NR 1 CADC, OPERATIONAL CHECK OK. - [SDR 9723131161](https://openairdocs.org/sdr/9723131161.md): Start Valve · malfunctioned · Dec 4, 1997 · N161US · Doug DC1040 · Engine Start Valves/Controls > DURING CRUISE, THE NR 1 ENGINE START VALVE OPEN LIGHT ILLIMINATED. CREW FOLLOWED COM PROCEDURE AND THEN DIVERTED TO BOS FOR MAINTENANCE. START VALVE WAS FOUND IN THE CLOSED POSITION WHEN AIRCRAFT ARRIVED BUT WAS CHANGED PRECAUTIONARY. START VALVE INDICATION - [SDR 9717151161](https://openairdocs.org/sdr/9717151161.md): Cadc · failed · Sep 10, 1997 · N161US · Doug DC1040 · Air Data Computer > DURING CRUISE, THE NR 2 AIR DATA COMPUTER FAILED, (NR 3 CADC WAS ON PREVIOUS MEL). FLIGHT DIVERTED INTO BOS. MAINTENANCE REPLACED NR 2 CADC. - [SDR 9715571161](https://openairdocs.org/sdr/9715571161.md): Engine · failed · Aug 14, 1997 · N161US · Doug DC1040 · Engine (Turbine/Turboprop) > WHILE CLIMBING THRU 2000 FEET AFTER TAKEOFF, THE NBR 2 ENGINE EGT WENT OFF SCALE HIGH AND EPR DROPPED. ENGINE WAS SHUT DOWN AND 55,000 LBS OF FUEL WAS DUMPED. AIRCRAFT RETURNED TO DEPARTURE AIRPORT WITHOUT INCIDENT. MAINTENANCE INSPECTED ENGINE WITH NO DEFE - [SDR 9710391161](https://openairdocs.org/sdr/9710391161.md): Transducer · seized · May 25, 1997 · N161US · Doug DC1040 · Stall Warning System > DURING FLAP RETRACTION AFTER TAKEOFF, STICK SHAKER ACTIVATED, SLAT DISAGREE LIGHT AND RESET LIGHT ILLUMINATED AND COULD NOT GET SLATS TO RETRACT. DUMPED 10,000 LBS OF FUEL AND RETURNED TO SFO. MAINTENANCE REPLACED THE STALL TRANSDUCER, OPERATIONAL CHECK OK. - [SDR 9707441161](https://openairdocs.org/sdr/9707441161.md): Prox Control · failed · Apr 11, 1997 · N161US · Doug DC1040 · Landing Gear Position and Warning > DURING GEAR RETRACTION, ALL LANDING GEAR UNSAFE LIGHTS ILLUMINATED WITH GEAR HANDLE UP. RECYCLED GEAR, NO HELP. GEAR VISULALY CHECKED UP. MAINTENANCE REPLACED MAIN LANDING GEAR PROXIMITY CONTROL. - [SDR 9623541161](https://openairdocs.org/sdr/9623541161.md): Fitting · corroded · Oct 28, 1996 · N161US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING L-CHECK, FOUND THE LONGERON 48L, 49L, AND 48R END FITTINGS CORRODED FROM FS 1509 - 1521. REPLACED BOTH FITTINGS. - [SDR 9623521161](https://openairdocs.org/sdr/9623521161.md): Skin · cracked · Oct 27, 1996 · N161US · Doug DC1040 · Fuselage Main, Plate/Skin > DURING L-CHECK, FOUND A CRACK IN THE FUSELAGE SKIN AT THE LEFT AIR CYCLE MACHINE DOOR JAMB UPPER AFT CORNER, FS 587. REPAIRED SKIN (P/N ACA 3108) PER EA 11-110287. - [SDR 9623501161](https://openairdocs.org/sdr/9623501161.md): Skin · cracked · Oct 25, 1996 · N161US · Doug DC1040 · Wing, Plate/Skin > DURING L-CHECK, FOUND A 1.6258 INCH CRACK IN THE RIGHT WING LOWER LEADING EDGE SKIN AT XOS 611. REPAIRED SKIN (P/N ARB2887-502) PER EA 11-110210. - [SDR 9621511161](https://openairdocs.org/sdr/9621511161.md): Compressor · stalled · Oct 8, 1996 · N161US · Doug DC1040 · Turbine Engine Compressor Section > DURING APPLICATION OF POWER FOR TAKEOFF, THE NR 3 ENGINE EXPERIENCED COMPRESSOR STALL. CREW ABORTED THE TAKEOFF AS EGT CLIMBED TO 990 DEGREES WITHIN ONE SECOND. AIRCRAFT RETURNED TO THE GATE AND VISUAL INSPECTION REVEALED NO DISCREPANCIES. BORESCOPE INSPECT - [SDR 9615301161](https://openairdocs.org/sdr/9615301161.md): Skin · cracked · Jun 27, 1996 · N161US · Doug DC1040 · Ailerons > DURING LINE CHECK, FOUND A CRACK IN THE LEFT OUTBOARD AILERON UPPER SKIN AT THE NR 5 RIB. REPAIRED PER EA 11-105126. - [SDR 9608541161](https://openairdocs.org/sdr/9608541161.md): Tach Generator · malfunctioned · Apr 13, 1996 · N161US · Doug DC1040 · Engine RPM Indicating System > DURING CLIMBOUT, THE NR 3 ENGINE N1, N2 AND NR 3 EPR BECAME ERRATIC, ALL OTHER INDICATIONS NORMAL. CREW FOLLOWED COCKPIT OPERATING PROCEDURES AND RETURNED TO DTW WITHOUT FURTHER INCIDENT. REPLACED THE N1 AND N2 INDICATORS. ALSO, REPLACED THE NR 3 N2 TACH GE - [SDR 9603531161](https://openairdocs.org/sdr/9603531161.md): Power Supply · inoperative · Feb 10, 1996 · N161US · Doug DC1040 · Emergency Lighting > DURING LINE CHECK, THE EMERGENCY LIGHT TEST LIGHT WOULD NOT ILLUMINATE. REPLACED POWER SUPPLY AND BATTERY. - [SDR 9601141161](https://openairdocs.org/sdr/9601141161.md): Controller · failed · Jan 19, 1996 · N161US · Doug DC1040 · Aircraft Fuel Distribution System > DURING CRUISE, THE TANK OVER FILLED LIGHT ILLUMINATED AND FUEL WAS STREAMING FROM THE LEFT DUMP NOZZLE. DUMPED 92,500 LBS OF FUEL AND RETURNED TO DTW. REPLACED FUEL CONTROLLER. - [SDR 9516921161](https://openairdocs.org/sdr/9516921161.md): Slat Sensor · malfunctioned · Oct 28, 1995 · N161US · Doug DC1040 · Leading Edge Slat Position Indicating System > DURING TAKEOFF, THE SLAT DISAGREE LIGHT AND THE TAKEOFF WARNING HORN SOUNDED. ABORTED TAKEOFF AND RETURNED TO GATE. ADJUSTED SLAT SENSORS AND REPLACED THE MAIN LANDING GEAR PROXIMITY CONTROL BOX. - [SDR 9512641161](https://openairdocs.org/sdr/9512641161.md): Floorbeam · cracked · Aug 10, 1995 · N161US · Doug DC1040 · Fuselage Main, Floor Beam > DURING T-CHECK, CRACKS WERE FOUND AT THE NUTPLATE HOLES ON THE FS 1887 FLOORBEAM UPPER CHORD FLANGE AT RBL 26. REMOVED DAMAGED AREA AND INSTALLED REPAIR ANGLES PER EA 11-99176, MFG PART NUMBER AGA 3793-19. - [SDR 9512611161](https://openairdocs.org/sdr/9512611161.md): Bulkhead · cracked · Aug 3, 1995 · N161US · Doug DC1040 · Fuselage Main, Bulkhead > DURING PERIODIC INSPECTION, A CRACK WAS FOUND ON THE BULKHEAD AT FS 515, STR 27R AND LONGERON 27L. REPLACED WEB PER EA 11-98526 AND INSTALLED DOUBLER PER EA 11-98525. - [SDR 9512621161](https://openairdocs.org/sdr/9512621161.md): Support · cracked · Aug 2, 1995 · N161US · Doug DC1040 · Fuselage Miscellaneous Structure > DURING T-CHECK, A CRACK WAS FOUND ON THE FLOOR SUPPORT AT FS 495 RBL 24 TO 26. INSTALLED REPAIR STRAP PER EA 11-99021, MFG PART NUMBER 0048-33. - [SDR 9512631161](https://openairdocs.org/sdr/9512631161.md): Spar Cap · cracked · Jul 28, 1995 · N161US · Doug DC1040 · Horizontal Stabilizer, Spar/Rib > DURING INSPECTION OF THE RIGHT HORIZONTAL SPAR CAP, A CRACK WAS FOUND AT THE FORWARD FLANGE AT STA XFS 82. INSTALLED REPAIR PER EM 5511-01014 AND EA 11-99036. - [SDR 9501121161](https://openairdocs.org/sdr/9501121161.md): Evc · malfunctioned · Jan 17, 1995 · N161US · Doug DC1040 · Compressor Bleed Control > DURING TAKEOFF ROLL (AMS), THE NR 3 ENGINE EXPERIENCED A COMPRESSOR STALL WITH RISING EGT AND WAS SHUT DOWN. THE TAKEOFF WAS ABORTED. THE ENGINE WAS INSPECTED AND BOROSCOPED. THE EVC WAS REPLACED AND A PRECISION TRIM WAS ACCOMPLISHED. GROUND RUN-UP CONFIRM ## 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 = 'N161US' AND deregistration_id = 'N161US-2002-10-30' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N161US-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.