N576F
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, 2005-03-28 – 2005-04-10.
Part: PANEL — CORRODED (HORIZONTAL STAB) · airframe 44,668 hrs · 9,069 cycles
LT HORIZONTAL STABILIZER UPPER BARREL NUT NR 02 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 02 LT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 43, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100.
Part: SKIN PANEL — CORRODED (HORIZ STAB) · airframe 44,668 hrs · 9,069 cycles
LEFT HORIZONTAL STABILIZER UPPER BARREL NUT NR 11 HAS BORE CORROSION EXCEEDING LIMIT. HOLE AT BARREL NUT BORE NR 11 LT FURTHER REAMED TO 1.002 INCH DIA, SMOOTHED AND FOUND CLEAN HOLE CONDITION AND IS WITHIN LIMITS AS PER EO E1-5510-7-5000D. STABILIZER HORIZONTAL INSPECT / REPAIR HORIZONTAL STABILIZER BARREL NUT HOLE AND SB/MD11 55-023.
Part: PANEL — CORRODED (HORIZONTAL STAB) · airframe 44,668 hrs · 9,069 cycles
RIGHT HORIZONTAL STABILIZER UPPER BARREL NUT NR 06 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 06 RIGHT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 11, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100.
Part: PANEL — CORRODED (HORIZONTAL STAB) · airframe 44,668 hrs · 9,069 cycles
RIGHT HORIZONTAL STABILIZER UPPER BARREL NUT NR 08 HAS BORE CORROSION EXCEEDING LIMITS. BARREL NUT BORE NR 08 RIGHT REPAIRED IAW EA 1-5510-78133 ATTACHMENT 12, HORIZONTAL STABILIZER BARREL NUT BORE REWORK/ REPAIR AD 2003-22-08. MAJOR REPAIR AS PER GMM 6-2-100.