N787TA
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.
4 reports on file, 2000-12-11 – 2007-04-06.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 6,196 hrs · 5,205 cycles
DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION THE RIGHT INBOARD HORIZONTAL STABILIZER, THE LT AND RT RIBS WERE FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUÃ' NR 70. BOTH RIBS WERE REPLACED.
Part: RIB — CRACKED (HORIZ STAB) · airframe 5,530 hrs · 4,630 cycles
DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION AS PART OF THE A LEVEL INSPECTION THE LT IB HORIZONTAL STABILIZER NOSE RIB STRUCTURE WAS FOUND CRACKED NEXT TO THE SIDE ROLLER BRACKET. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE NR 70.
Part: FUSE — FAILED (EMER BUSS)
FLIGHT CREW REPORTED NO BATTERY VOLTAGE INDICATION ON VOLTMETER WITH ALL DC BUSSES POWERED. TROUBLESHOOTING FOUND AIRCRAFT WOULD NOT GO INTO EMERGENCY POWER OR PERFORMED FEEDER FAULT TEST. FOUND 5A MICROFUSE F105 CONNECTED TO K005 EMERGENCY BUSS POWER RELAY OPEN. REPLACED F105 FUSE, ALL DC POWER FUNCTIONS NORMAL, NO FAULTS NOTED. (K)
Part: CONTACTOR — FAILED (TAIL DEICE CNTRL)
THIS CONTACTOR, PN 128-384054-5, WHEN INSTALLED IN THE K-251 POSITION OF THE HORIZONTAL STABILIZER DEICE SYSTEM CAUSES THE SYSTEM TO FAIL WHEN THE AIRCRAFT IS AT AN ALTITUDE THAT A MINUS 10 DEGREES OR COLDER RAM AIR TEMPERATURE IS ACHIEVED. (X)