# N160BS: 1994 Mcdonnell Douglas DC-9-83(MD-83), registration cancelled 2009-08-19 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 19, 2009 - Exported to: Mali - Status when cancelled: Triennial form not returned - Airframe: [Mcdonnell Douglas DC-9-83(MD-83)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83) (registry code 3022083) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 53463 - Year built: 1994 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: August 15, 2005 - Certificate issued: July 21, 2005 - Last registry action: August 19, 2008 - Mode S code: A0F1D8 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N160BS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=160BS - Page: https://openairdocs.org/deregistered/N160BS-2009-08-19 From the FAA registry file of October 31, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Mcdonnell Douglas DC-9-83(MD-83): https://openairdocs.org/model/mcdonnell-douglas-dc-9-83-md-83.md ## Service difficulty reports (14) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ANCF2009012700034](https://openairdocs.org/sdr/ANCF2009012700034), Jan 27, 2009: TRANSDUCER. MALFUNCTIONED. DURING TAKE-OFF WHEEL NOT TURNING LIGHT CAME ON REJECTED TAKE-OFF WAS PERFORMED AT LOW SPEED RAMP RETURN. IAW AMM: 20-50-00 AND 32-43-02 IT WAS REPLACED CONNECT - [SDR MU12008F00000](https://openairdocs.org/sdr/MU12008F00000), Oct 9, 2008: WHEEL. VIBRATION. REJECTED TAKE OFF. DURING TAKE OFF ROLL AFTER A/T ENGAGE AND TO POWER WAS ADJUSTED (EPR 2.04) REACHING 60 KTS THERE WAS A VERY STRONG VIBRATION, LOW SPEED REJEC - [SDR 2008FA0000476](https://openairdocs.org/sdr/2008FA0000476), Jun 17, 2008: WHEEL. LOOSE. REJECTED TAKEOFF, DURING T/O ROLL, THERE WAS AND ABNORMAL AND ABRUPT VIBRATION IN THE NOSE SECTION. IAW AMM 32-21-04, PAGE 201/210 WAS CHECKED TORQUE LINKS ASSY - [SDR ANCF200800001](https://openairdocs.org/sdr/ANCF200800001), Jan 23, 2008: FILTER. CLOGGED. R OIL STRAINER CLOG ANNUNCIATION DISPLAYED ON EOAP DURING CRZ AT FL 350, ENG WAS OPERATED AT IDLE THRUST UNTIL LANDING; NO REVERSE WAS USED ON ENGINE. AS PER AM - [SDR ANCF200700034](https://openairdocs.org/sdr/ANCF200700034), Dec 28, 2007: WIRE. BURNED. DURING CRUISE STRONG BURNING ODOR IN COCKPIT DUE TO PREVIOUS REPORTS ON RT PACK THE PACK WAS TURNED OFF AND THE ODOR DISSIPATED. THE ODOR WAS IN COCKPIT. IAW WD - [SDR ANCF200700033](https://openairdocs.org/sdr/ANCF200700033), Dec 20, 2007: SWITCH. OUT OF ADJUST. DURING T/O ROLL, T/O CONFIGURATION FLAP WAS PRESENTED AT SPEED 105 KTS 110.500 LBS. THE FLAP STAT HANDLE POSITION SWITCHES WERE ADJUSTED. IAW AMM 27-80-07 PAG 2 - [SDR ANCF200600045](https://openairdocs.org/sdr/ANCF200600045), Feb 2, 2007: ENGINE. MALFUNCTIONED. ON TAKEOFF LT ENGINE PARAMETER DROOPED & EGT RAISED UP TO 610. POWER REDUCED AND EPR 1.61 N1 57 PERCENT N2 62 PERCENT ADVANCING LT THROTTLE THERE WAS NO REACTIO - [SDR ANCF200600030](https://openairdocs.org/sdr/ANCF200600030), Aug 18, 2006: PROXIMITY SENSOR. DEFECTIVE. DURING LANDING GEAR EXTENSION, LT MAIN GEAR GREEN LIGHT DID NOT COME ON WITH RED LIGHT ON PROCEDURE ACCOMPLISHED. PLEASE CHECK FOR INDICATION IAW AMM 32-60-05 P - [SDR ANCF200600024](https://openairdocs.org/sdr/ANCF200600024), Jun 17, 2006: ENGINE. MALFUNCTIONED. PILOT REPORT: DURING CRUISE AT FLIGHT LEVEL OF 300, LEFT OIL TEMPERATURE START TO RAISE ABOVE NORMAL RANGE (BETWEEN 135C TO 162C) WAS NECESSARY TO INCREASE POWE - [SDR ANCF200600018](https://openairdocs.org/sdr/ANCF200600018), May 7, 2006: A/C PACK. OUT OF ADJUST. DURING CLIMB CABIN ALTITUDE WARNING LIGHT WITH CABIN AURAL SOUND CAME ON, ABNORMAL PROCEDURE WERE MADE AND CABIN ALTITUDE CONTINUED CLIMBING UNTIL 13000FT WITH - [SDR ANCF200600005](https://openairdocs.org/sdr/ANCF200600005), Jan 22, 2006: ODOR. DETECTED. PILOT REPORT, FLIGHT ATTENDANTS REPORT A SMELL OF BURNED RUBBER IN THE REAR OF THE AIRCRAFT. AS PER AMM 21-21-00 AIR CONDITIONING PACKS AND WAVES OF REAR GALLEY - [SDR ANCF200600006](https://openairdocs.org/sdr/ANCF200600006), Jan 20, 2006: RELAY. FAILED. AFTER LT ENGINE START THE GENERATOR DID NOT COME INTO THE LINE- RESET WAS UNSUCCESSFUL. IAW MEL, CONTINUED WITH THE FLIGHT AND REACHING CRUISE ALTITUDE APU FAIL - [SDR ANCF200600004](https://openairdocs.org/sdr/ANCF200600004), Jan 14, 2006: CONTROLLER. FAILED. AT FLIGHT LEVEL 230, AUTOMATIC PRESSURIZATION SYSTEM FAIL TO PRESSURIZE AIRPLANE. TRANSFER LOCKOUT AND STAND BY LIGHT. CHECK LIST WAS PERFORMED AND AUTO PRESSUR - [SDR ANCF200600002](https://openairdocs.org/sdr/ANCF200600002), Jan 11, 2006: CABIN PRESSURE. MALFUNCTIONED. AT FL330, 50MM BEFORE KIKAS, FLOW LIGHT CAME ON AND CABIN CLIMB INCREASE TO 1500 FT (CLIMB) AND CABIN ALTITUDE ALSO. FLIGHT ATTENDANT REPORTED STRONG NOISE AFT ## Other aircraft with N160BS - [Registered now](https://openairdocs.org/aircraft/N160BS): Learjet 60, S/N 112, built 1997 --- 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.