What was found
DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE LT FWD SPAR CAP ANGLE, RADIATES FROM THE UPPER FWD TASTENER UPWARD TO EDGE OF SPAR CAP, .375" IN LENGTH. MX REPAIRED THE AFFECTED AREA IAW FR-CO-02586, STEP 1. MAJOR REPAIR
- Difficulty date
- December 4, 2012
- Submitted
- December 4, 2012
- Operation
- Air carrier
- Aircraft
- N210GL
- Make and model
- Beech 1900D
- Aircraft serial
- UE210
- Aircraft time
- 34,135 hours, 41,734 cycles
- System (JASC)
- 5511 · Horizontal Stabilizer, Spar/Rib
- Part
- Spar Cap
- Condition
- Cracked
- Location
- Horizontal Stab
- 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.