N412
Registered owner: FIRST STATE AG AIR INC, DE (owner ≠ operator)
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.
6 reports on file, 2006-06-13 – 2008-01-10.
Part: SKIN — CRACKED (LT TE FLAP) · airframe 34,148 hrs · 5,146 cycles
LT INBD MID FLAP WITH MULTIPLE AREAS OF DAMAGE TO THE INBD L/E FAIRING ADJACENT TO THE CONCERTINA SEAL. THIS DAMAGE COMPRISES OF A HOLE 1.2" BY 0.9", WITH AN ASSOCIATED 8.0" CRACK RUNNING OUTBD. TOTAL SIZE OF DAMAGE IS 9.2" LONG.
Part: PANEL — CRACKED (RT WING) · airframe 34,148 hrs · 5,146 cycles
RT WING L/E FIXED UPPER PANEL WS426 CRACKED FROM THE L/E OF THE PANEL THROUGH TO THE FIRST RIVET HOLE. LOCATION IS 29" OUTBD OF INBD EDGE OF FIXED PANEL AT WS 426, 0.500" LONG. OUT OF LIMITS AS PER SRM 51-70-02.
Part: SKIN — DENTED (LT TE FLAP) · airframe 34,148 hrs · 5,146 cycles
SMALL DENT ON THE LT I/B AFT FLAP LOWER SURFACE I/B OF NR 4 CANOE. DENT 0.250" DIAMETER, PIN HOLE IN CENTER 0.060" IS NOT NEAR AN EDGE IS MIDSPAN AND IS COVERED UNDER ALLOWABLE DAMAGE SRM 57-53-01 PAGE 102, C, D, F.
Part: STRUCTURE — DAMAGED (TE FLAP) · airframe 33,000 hrs · 3,986 cycles
DAMAGE WAS FOUND TO THE I/B END OF THE LT O/B MID FLAP. THE DAMAGE IS DUE TO CONTACT OF THE MID FLAP WITH THE FIXED STRUCTURE ADJACENT TO THE I/B AILERON. REPAIRED IAW XEO 57-101507-1.
Part: PANEL — CRACKED (NR 1 PYLON) · airframe 26,492 hrs · 4,080 cycles
NR 1 PYLON STRUT FAIRING PANEL 4541R CRACKED.
Part: SLEEVE — CRACKED (THRUST REVERSER) · airframe 26,492 hrs · 4,080 cycles
INBOARD THRUST REVERSER TRANSLATING SLEEVE CRACKED.