N061FE
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.
5 reports on file, 1997-01-20 – 2001-08-11.
Part: LIGHT — ILLUMINATED (COCKPIT) · airframe 31,216 hrs · 9,958 cycles
NR 3 MANIFOLD FAIL LIGHT ILLUM. RED TABS ACCOMPLISHED.
Part: STRUT — CORRODED (LT MLG)
NR 466 - LEFT MLG HAS CORROSION ON EXT INSIDE OF BEAR STRUT AT O-RING GROOVE. REMOVED AND REPLACED MLG EXT AND TORQUED BOLTS AS PER MM 32-11-04. SERV STRUT PER MM 32-11-01.
Part: STRUT — CORRODED (LT MLG)
NR 470 - UPPER SURFACE OF LEFT MLG AFT OF PLUG HAS SURFACE CORROSION. REMOVED CORROSION MAIN GEAR STRUT COMPLIED WITH EA 8-3211-40488.
Part: BOLT — SHEARED (BS 118-115)
FOUND 3 BOLTS SHEARED AT BS XCW 118 TO XCW 115 RT AFT SPAR TOP SURFACE. *S/D* REMOVED AND REPLACED BOLT AND TORQUED. INSP AND NDT, MEASURE BOLT HOLE, SPOT FACE AREA.
Part: BRACKET — CRACKED (NR 2 ENGINE)
FOUND BRACKET FOR AFT SUPPORT ROD ON NR 2 ENGINE COWL ANTI-ICE S/O VALVE BROKEN WHERE IT ATTACHES TO FAN CASE FLANGE. ROD AND PORTION OF FREE BRACKET THEN ARE ALLOWED TO CHAFE AGAINST UPPER FAN CASE FLANGE. SEE IPC 36-14-25-01-FDX ITEM 475 OR 470. MATERIAL THICKNESS OF BRACKET NEEDS TO BE INCREASED WHERE SUPPORT ROD AND FAN CASE ATTACHMENT ARE MADE. *S/D* REMOVED AND REPLACED BRACKET ASSY FOR AFT SUPPORT ROD OF A/I S/O VALVE, COMPONENT SECURE.