Service difficulty reports · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ANCF2009012700034Transducer · malfunctionedDURING 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 CONNECTOR OF TRANSDUCER NR 2.SDR MU12008F00000Wheel · vibrationREJECTED 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 REJECTED TAKE OFF WAS PERFORMED. DURING VIBRATION BRAKES DID NOT WORK UNTIL REACHING 30 TO 49 KTS. TOGSDR 2008FA0000476Wheel · looseREJECTED 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 BY LOOSE AND ADJUSTMENT ALSO WERE CHECK BOTH NOSE WHEELS, IAW AMM 32-40-02 PAGE 201, PRESS IN BOTHSDR ANCF200800001Filter · cloggedR 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 AMM 79-20-06 REMOVED AND REPLACED ENG OIL FILTER AND ENG OIL CHANGE PER AMM 12-12-04. PERFORMED ENG SDR ANCF200700034Wire · burnedDURING 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 WDM AND AMM 33-22-07/525 AND 20-50-01 /201 IN LT UPPER SIDE WALL LIGHTING TRANSFORMER LINE IL 1701F1SDR ANCF200700033Switch · out of adjustDURING 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 205 TEST SATISFACTORY.SDR ANCF200600045Engine · malfunctionedON 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 REACTION AND ENGINE WAS SHUTDOWN. 2 MINUTES BEFORE LANDING, OIL PRESSURE NORMAL, OIL TEMP NORMAL. IAW AMSDR ANCF200600030Proximity Sensor · defectiveDURING 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 PAGE 201 TO 205 AND 32-30-00 PAGE 1. LT MAIN LANDING GEAR DOWN PIN LOCK PROXIMITY SENSOR SWITCH WASSDR ANCF200600024Engine · malfunctionedPILOT 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 POWER IN LT ENGINE TO MAINTAIN OIL TEMPERATURE BELOW 165C, CHECK LIST WAS ACCOMPLISHED UNSUCCESFULLY, FUSDR ANCF200600018A/C Pack · out of adjustDURING CLIMB CABIN ALTITUDE WARNING LIGHT WITH CABIN AURAL SOUND CAME ON, ABNORMAL PROCEDURE WERE MADE AND CABIN ALTITUDE CONTINUED CLIMBING UNTIL 13000FT WITH MANUAL PRESURIZATION CONTROL. IAW 21-00-00/501 PERFORMED OPERATIONAL TEST AT AIR CONDITIONING SYSTESDR ANCF200600005Odor · detectedPILOT 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 WERE INSPECTED BY EVIDENCE OF BURNED RUBBER. NO FAULT FOUND.SDR ANCF200600006Relay · failedAFTER 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. IAW AMM 24-20-06 PAGE 201 THE LT AC CONTROL RELAY (R2-33) WAS REPLACED. OK. APU TEST ACCOMPSDR ANCF200600004Controller · failedAT FLIGHT LEVEL 230, AUTOMATIC PRESSURIZATION SYSTEM FAIL TO PRESSURIZE AIRPLANE. TRANSFER LOCKOUT AND STAND BY LIGHT. CHECK LIST WAS PERFORMED AND AUTO PRESSURIZATION WAS RECOVERED AND FAIL TO PRESSURIZE AGAIN AT LOW THRUST DURING APPROACH. AS PER AMM 21-32SDR ANCF200600002Cabin Pressure · malfunctionedAT 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 OF THE AIRCRAFT. CHECK LIST WAS ACCOMPLISHED. CABIN ALTITUDE REACHED 13,500 FT AND COULD NOT BE M
Other aircraft with N160BS · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. N160BS is registered now to the first aircraft listed.