N5112
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
10 reports on file, 1995-08-25 – 2004-02-18.
Part: HOSE — LEAKING (HYD SYSTEM)
DURING WALK-AROUND AFTER PARKIGN CREW NOTICED HYDRAULIC FLUID ON TAIL AND MADE WRITE UP ON SHUT DOWN AT LAS HYDRAULIC FLUID WAS POURING OUT OF THE LEFT ELEVATOR HINGE POINT CLOSEST TO THE VERTICAL STAB. MAINTENANCE FOUND ELEVATOR ACTUATOR HOSE HAD BEEN RUBBED THROUGH BY ELEV PCU. ACTUATOR HOSE WAS REPLACED, SYSTEM BLEED AND SERVICED. OPS AND LEAK CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LIMITER — DAMAGED (RUDDER)
CREW REPORTED A 'FAILED RUDDER LIMITER B' MESSAGE ON THE CAS. THE LOWER RUDDER LIMITER LINEAR ACTUATOR B-CHANNEL, FAILED AT 25 PERCENT. REPLACED RUDDER LIMITER ACTUATOR 'B' IAW CHAPTER 27-23-00 OF CESSNA MM, OPERAITON CHECK GOOD OK FOR SERVICE. (M)
Part: SWITCH — BROKEN (BRAKE SYSTEM)
DURING TAXI TO TAKEOFF, THE NO TAKEOFF CAUTION APPEARED ON THE EICAS. SIMULTANEOUSLY, THE PARK BRAKE PRESS LOW MESSAGE WAS ILLUMINATED. THE CREW TAXIED BACK TO GM BASE AND ANOTHER AIRCRAFT WAS UTILIZED FOR THE FLIGHT. UPON TROUBLESHOOTING, THE PARK BRAKE SWITCH WAS FOUND TO BE FAULTY. THE CONTACT PLUNGER HAD DETERIORATED, THUS NO ACTUATING THE CONTACTS. SWITCH WAS REPLCED AND OPERATION WAS NORMAL. (M)
Part: SWITCH — BROKEN (PARKING BRAKE)
DURING TAXI TO TAKEOFF, THE NO TAKEOFF CAUTION APPEARED ON THE EICAS. SIMULATNEOUSLY, THE PARK BRAKE PRESS LOW MESSAGE WAS ILLUMINATED. THE CREW TAXIED BACK TO GM BASE AND ANOTHER AIRCRAFT WAS UTILIZED FOR THE FLIGHT. UPON TROUBLESHOOTING, THE PARK BRAKE SWITCH WAS FOUND TO BE FAULTY. THE CONTACT PLUNGER HAD DETERIORATED, THUS NOT ACTUATING THE CONTACTS. SWITCH HAS BEEN REQUESTED. (M)
Part: CONTROL MODULE — MALFUNCTIONED (RUDDER)
SHORTLY AFTER TAKEOFF THE (RUDDER LIMIT FAIL) CAS MESSAGE ILLUMINATED. PERFORMED RUDDER CONTROL LIMITER TEST IAW MM. NO FAULTS DURING 3 HOURS OF TESTING. RESET RUDDER LIMIT CONTROL MODULE NK123. PERFORMED OPERATIONAL CHECK FLIGHT. NO PROBLEMS WERE ENCOUNTERED AND THE AIRCRAFT WAS RETURNED TO SERVICE.
Part: FLAP TRACK — CONTAMINATED (LT AND RT)
AFTER SELECTING FLAPS UP, AMBER FLAPS FALL LIGHT CAME ON. UNABLE TO RESET. RETURN TO DTW. SLATS OK. ZERO FLAPS. ICE, WATER AND SAND FOUND IN THE LT AND RT INBOARD FLAP WELLS AND FLAP TRACKS. CAUSED FLAP MOTOR OVERCURRENT DURING FLAP ACTUATION.
Part: DISPLAY — MALFUNCTIONED (COCKPIT)
AFTER TAXIING FROM RAMP, RETURNED TO PARKING RAMP WITH EICAS YELLOW CAUTION MESSAGE FOR THE NR 5 COCKPIT DISPLAY UNIT. MESSAGE CREATED IN WRAP AROUND CIRCUIT BETWEEN THE NR 1 AND NR 5 DISPLAY UNITS. CYCLED AVIONICS MASTER SWITCH OFF THEN BACK ON. SYSTEM OPERATION WAS NORMAL. SYSTEM SERVICEABLE.
Part: SWITCH — FAILED (AILERON)
DUE TO A NO TAKEOFF WARNING ILLUMINATING AT 90 KNOTS, THE CREW REJECTED TAKEOFF. MAINTENANCE DISCOVERED A LOOSE PROXIMITY SWITCH AT THE AILERON/SPOILER DISCONNECT HANDLE. ADJUSTED PROXIMITY SWITCH AND PERFORMED OPS CHECK. MAINTENANCE RETURNED AIRCRAFT TO SERVICE.
Part: PITOT MAST — OBSTRUCTED (NR 1 LT)
AT EIGHTY KNOTS, THE NR 1 ADC (AIR DATA COMPUTER) FAILED AND THE FLIGHT CREW ABORTED TAKEOFF. THE AIRCRAFT RETURNED TO THE RAMP AND MAINTENANCE CONFIRMED THE NR 1 PITOT TUBE WAS OBSTRUCTED. REPLACED THE PITOT TUBE MAST.
Part: BLADE — SHROUD MISSING (NR 3 LPT)
ONE BLADE TIP SHROUD FOUND MISSING DURING POST-FLIGHT ON NR 3 LOW PRESSURE TURBINE.