N125GH
Registered owner: TVPX AIRCRAFT SOLUTIONS INC TRUSTEE, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Wing Aviation Charter Services LLC (Y9PA) | Certificate holder | — | Matched by certificate designator |
| Y. L. HALLQUIST | Operator | on 1982-07-25 | Operator named in NTSB report |
Accident & incident history
Operated by Y. L. HALLQUIST (per NTSB report)
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, 2021-03-17.
Part: TORQUE TUBE — CORRODED (RUDDER) · airframe 10,752 hrs · 3,417 cycles
POST CORROSION REMOVAL AND EVALUATION, ENGINEERING DETERMINED THAT THE REMAINING MATERIAL THICKNESS ON THE RUDDER TORQL'E TUBE ATI ACH EARS DOES NOT MEET AIRWORTHINESS REQUIREMENTS.
Part: FLANGE — CORRODED (VERTICAL STAB) · airframe 10,752 hrs · 3,417 cycles
CORROSION WAS IDENTIFIED ON BOTH SIDES OF VERTICAL STABILIZER REBATE FLANGES. REMOVED 64 NUTPLATE, CLEANED CORROSION FROM BELOW THE 64 REMOVED NUTPLATES, INSTALLED NUT PLATES ON THE VERTICAL STABILIZER REBATE FLANGES IN ACCORDANCE WITH GV SRM CH 51-42-00.
Part: SKIN — CORRODED (LT WING) · airframe 10,752 hrs · 3,981 cycles
LH AND RH WING PLANK AT TRAILING EDGE OF AILERON AREAS. HAVE CORROSION ON THE PLANKS AROUND NUTPLATES FOR CLOSEOUT PANELS, TO INCLUDE OUTBOARD TRAILING EDGE OF BOX AREA BETWEEN AILERONS AND WINGLETS.
Part: ACCESS DOOR — CORRODED (APU BAY) · airframe 10,752 hrs · 3,981 cycles
CORROSION FOUND ON STRUCTURE WHERE EXTERNAL APU ACCESS DOOR MATES TO THE FUSELAGE.
Part: FLANGE — CORRODED (FUSELAGE) · airframe 10,752 hrs · 3,417 cycles
EXFOLIATION CORROSION ON THE RIGHT FORWARD-CENTER WING BOX REBATE FLANGE, JUST OUTBOARD OF SINGLE POINT.