What was found
RIGHT FUSELAGE - TO - VERTICAL STAB FORWARD DRAG ANGLE POSSIBLE CRACK IN THE RADIUS AREA. REPAIRED RT FUSELAGE - TO - VERTICAL STAB FORWARD DRAG ANGLE IAW SRM 55-31-00-201-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.
- Difficulty date
- April 21, 2026
- Submitted
- July 3, 2026
- Operation
- Air carrier
- Aircraft
- N770SK
- Make and model
- Cndair CL6002C10
- Aircraft serial
- 10243
- Aircraft time
- 49,503 hours, 33,314 cycles
- System (JASC)
- 5342 · Fuselage, Stabilizer Attach Fittings
- Part
- Drag Angle
- Condition
- Cracked
- Location
- Zone 300
- Stage of operation
- IN
- How discovered
- V
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.