Service difficulty report · Turbine Blades

Difficulty date
August 27, 2004
Submitted
March 3, 2005
Operation
General aviation
Engine
Pwa JT15D1A
Part
Turbine Blades
Condition
Failed
Location
Engine
Stage of operation
IN
How discovered
9
Nature of condition
O
Precautionary procedure
K

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

DISCOVERED HPT BLADE DAMAGE. CONFIRMED HPT BLADES DAMAGED WITH 1 BLADE MISSING ENTIRE TIP SECT. GAS GEN DEFLECTOR SEG FOUND MISSING SECTIONS & SIGNIFICANT NR OF RIVETS. EXAM OF FRACTURED BLADE SHOWED HIGH STRESS RAPID YIELD FRACTURE WITH NO EVIDENCE OF FATIGUE. FRONT SECT OF BLADE CONVEX SIDE (SUCTION SURFACE) ADJACENT TO FRACTURE BENT TOWARDS PRESSURE SURFACE AWAY FROM DIRECTION OF ROTATION AS WOULD OCCUR IF BLADE SUSTAINED A SIGNIFICANT IMPACT. BLADE NOT PRIMARY FAILURE & 2NDRY DAMAGE CAUSED FROM LIBERATED MATERIAL. MATERIAL BECAME DISLODGED & ENTERED THROUGH COMBUSTION CHAMBER LINER & TRAVELLED THROUGH GAS PATH CAUSING SEVERE HPT BLADE DAMAGE, AND MINOR IMPACT DAMAGE ON DOWNSTREAM COMPONENTS.