N29YV
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
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.
3 reports on file, 1997-07-14 – 1998-04-11.
Part: SKIN — CRACKED (FUSELAGE)
DURING ROUTINE MAINTENANCE, DISCOVERED A SKIN CRACK APPROXIMTELY 1.5 INCHES LONG AT FORWARD OUTBOARD LEFT SIDE OF NR 2 VHF ANTENNA. COMPLETED REPAIR BY STOP DRILLING CRACK AND INSTALLING A REINFORCEMENT DOUBLER TO SKIN CRACK IAW BEECHCRAFT STRUCTUAL REPAIR MANUAL CHAPTER 53-90-00 PP 10-11. REFERENCE RO NR B1900D-53-0005 JAX. (M)
Part: SKIN — CRACKED (FUSELAGE)
DURING ROUTINE MAINTENANCE, DISCOVERED SKIN CRACK APPROXIMATELY 2 INCHES LONG ON LOWER RIGHT FUSELAGE IN SPAR AREA. REPAIR WAS COMPLETED BY STOP DRILLING CRACK AND INSTALLING REINFORCEMENT DOUBLER TO AFFECTED AREA IAW BEECH STRUCTURAL REPAIR MANUAL CHAPTER 53-00-06, PP 40-41. REFERENCE RO NR B1900D-53-0006 JAX. INSPECTED FOR HIDDEN DAMAGE, FOUND NO DISCREPANCIES. (M)
Part: HINGE — CORRODED (LT ELEVATOR)
DURING A FLEET CAMPAIGN DIRECTIVE INSPECTION, THE LEFT OUTBOARD ELEVATOR HINGE ASSEMBLY WAS FOUND TO HAVE HEAVY CORROSION. REMOVED AND REPLACED LEFT OUTBOARD ELEVATOR HINGE ASSEMBLY. INSPECTION OF THE RIGHT OUTBOARD ELEVATOR HINGE ASSEMBLY REVEALED SURFACE CORROSION. CLEANED AND TREATED HINGE ASSEMBLY PER BEECH SRM. (X)