N202TT
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
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.
5 reports on file, 2013-04-07 – 2015-06-19.
Part: ENGINE — FLAMED OUT (NR 2) · airframe 3,379 hrs · 2,499 cycles
WHILE ENROUTE, THE NR 2 ENGINE FLAMED OUT AT APPROXIMATELY FL380. THE ACFT, DIVERTING FOR A LARGE CELL DEPICTED ON THE RADAR, THE CELL WAS DEPICTED OVER DESTINATION. THE ACFT HAD EXPERIENCED 3 TO 4 SUSPECTED LIGHTNING STRIKES AND WAS DESCENDING THROUGH FL380 FOR FL340 WHEN THE NR 2 ENGINE EXPERIENCED A ROLLBACK TO A FLAMEOUT. NO SECONDARY MALIFICIENT INDICATIONS WERE NOTED. AN EMERGENCY WAS DECLARED WITH ATC AND THE APPROPRIATE CHECKLISTS WERE RUN. THE CREW NOTED THAT THE NR 2 ENGINE WAS WINDMILLING AND NO BAD INDICATIONS WERE NOTED SO A RESTART WAS ATTEMPTED. THE RESTART WAS SUCCESSFUL AND ATC WAS NOTIFIED AND EMERGENCY STATUS WAS REQUESTED TO BE REPEALED. THE CREW MADE AN UNEVENTFUL 2 ENGINE NORMAL LANDING.
Part: WHEEL — OUT OF BALANCE (NLG) · airframe 2,712 hrs · 2,010 cycles
PILOT REPORTED THAT THE NOSE WHEEL VIBRATED BADLY DURING TAKEOFF. THE NOSE WHEEL ASSEMBLY WAS REMOVED, NO VISUAL DEFECTS WERE NOTED, IT WAS FOUND THAT THE WHEEL ASSEMBLY WAS WAY OUT OF BALANCE. THE UNIT WAS REBALANCED & THEN REINSTALLED. THE NOSE WHEEL ASSEMBLY HAD BEEN OVERHAULED A LITTLE OVER A MONTH PREVIOUSLY, 51.5 HRS & 33 CYCLES OF USE.
Part: ACTUATOR — FAULTY (TRIM TAB) · airframe 2,650 hrs · 1,969 cycles
FLIGHT CREW REPORTED THAT THE HORIZONTAL STABILIZER TRIM FAILED PREFLIGHT TRIM CHECKS. STAB TRIM DID NOT CONSISTANTLY TRIM (UP OR DOWN) WHEN THE PRIMARY OR EMERGENCY TRIM SWITCHES WERE DEPRESSED. THE TRIM MOTOR WAS AUDIBLE BUT INTERMITTENT STAB MOVEMENT WAS NOTED. FULL DOWN TRIM COULD NOT BE ACHIEVED. MX REMOVED THE DEFECTIVE HORIZONTAL STABILIZER ACTUATOR PN 45AS61023-143, SN 061102. AN O/H UNIT WAS INSTALLED, OPS CHECKS WERE SATISFACTORY. TRIM INDICATIONS WERE WITHIN LIMITS. REF MM 27-40-00. A TEARDOWN REPORT WAS REQUESTED FOR THE REMOVED UNIT.
Part: SWITCH — DEFECTIVE (COCKPIT) · airframe 2,630 hrs · 1,955 cycles
IT WAS REPORTED THAT THE RT ENG FAILED TO START. TROUBLESHOOTING IDENTIFIED THE START SWITCH WAS DEFECTIVE. THE DEFECTIVE SWITCH WAS REMOVED PN 45AS88822-003 & A NEW SWITCH WAS INSTALLED. OPERATIONS CHECKED SATISFACTORY. THE ACFT WAS RETURNED TO SERVICE.
Part: ACTUATOR — DEFECTIVE (PITCH TRIM) · airframe 2,355 hrs · 1,737 cycles
CREW REPORTED STAB PITCH TRIM FAILS IN FLIGHT. TROUBLESHOOTING INDENTIFIED THAT THE STAB TRIM ACTUATOR DEFECTIVE. REMOVED ACTUATOR. INSTALLED REPAIRED ACTUATOR. FUNCTIONAL CHECKED SATISFACTORY.