N16203
Registered owner: WOODBURN THOMAS J, VA (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.
7 reports on file, 1995-02-03 – 2017-03-23.
Part: FRAME — CRACKED (BS 130) · airframe 20,933 hrs
THE LT BS 130 FRAME WAS FOUND CRACKED DURING A PHASE VISUAL INSPECTION. THE CRACK EXTENDED OUTBOARD 5.0 INCH FROM THE INBOARD FLANGE FREE EDGE AT LBL 67. THE FRAME WAS REPLACED.
Part: FRAME — CRACKED (BS 130) · airframe 21,500 hrs
THE RT BS 130 FRAME WAS FOUND CRACKED DURING A PHASE VISUAL INSPECTION. THE CRACK EXTENDED OUTBOARD 5.0 INCHES FROM THE INBOARD FLANGE FREE EDGE AT RBL 67. THE FRAME WAS REPLACED.
Part: SKIN — CRACKED (FWD GALLEY DOOR)
GSO - INSPECTION FOUND A .25 INCH CRACK IN SKIN AT FORWARD GALLEY DOOR UPPER HINGE. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5330-02315. (M)
Part: WEB — CORRODED (LT TE FLAP)
31J - CORROSION WAS FOUND ON THE LT OUTBOARD MID-FLAP WEB AND DOUBLER AT THE FOREFLAP ATTACH POINT. THE CORRODED AREA WAS REMOVED AND REPAIR WAS INSTALLED IAW SRM 51-10-6, 51-40-6, 51-10-3, AND 57-52-00. (X)
Part: SLAT — CRACKED (LT NR 3 LE FLAP)
31J - INSPECTION FOUND A 1 INCH CRACK IN THE LEFT LEADING EDGE NR 3 SLAT NR 1 HINGE DOOR AREA. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 51-10-2, 57-30-4, AND 51-30-2. (X)
Part: SKIN — CRACKED (LT EMER EXIT DR.)
31J - A 1 INCH CRACK WAS FOUND ON THE OUTER SKIN OF THE LEFT FORWARD EMERGENCY EXIT DOOR. THE CRACK WAS STOP DRILLED, ROUGH EDGES WERE BLENDED OUT, AND A REPAIR WAS INSTALLED IAW SRM 52-00-2. (X)
Part: FLOOR BEAM — CRACKED (BS 716.0)
31J - A 2 INCH CRACK WAS FOUND IN THE FLOOR BEAM AND RUNNING UNDER THE RADIUS AT BS 716.0 AND BL 0. A REPAIR WAS FABRICATD AND INSTALLED IAW SRM 53-10-9. (X)