N710UP
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, 1996-01-03 – 1996-01-06.
Part: SKIN — CORROSION (WS 608-614)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, MODERATE CORROSION ON RT WING L/E BETWEEN XFS 608 TO XFS 614, LOWER SURFACE. REPLACED DOUBLER SECTION PER DOUGLAS PRINT 5769600.
Part: TE WEDGE — CORROSION (RT WING)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING T/E EDGE O/B WEDGE HAS CORROSION ON INNER LOWER SURFACE. REPAIRED PER 51-1-21.
Part: FLAP TRACK — CORROSION (RT TE FLAP)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, BOTH I/B AND O/B FLAP TRACK ASSYS HAVE CORROSION PITS, LOWER SIDE RT AFT I/B FLAP ASSY STA XW 98. REPLACED TRACKS PER MM 27-51-03.
Part: FRAME — CORROSION (FS 80)
WHILE IN FOR C-CHECK MAINTENANCE REPORTED, MODERATE CORROSION ON AFT SIDE OF BOLT FRAME FS 80, LONGERON 26R. REPAIRED BOLT FRAME PER SRM 53-2-0 FIG 2.