SDR UIEA9502

Service difficulty report · Blade · Boeing 747230B

Difficulty date
November 10, 1995
Submitted
March 26, 2000
Operation
Air carrier
Aircraft
N509MC
Make and model
Boeing 747230B
Aircraft serial
21221
Engine
Ge CF650E2
Part
Blade
Part number
9299M30G09R
Condition
Fracture
Location
Hpt
Part time
24,031 hours
Stage of operation
CL
Nature of condition
A, E, K
Precautionary procedure
E, A, J, F

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

What was found

ENGINE, SN 455833, TEAR DOWN REVEALED CONSIDERABLE TURBINE DAMAGE. HPT STAGE 1 BLADES METALLURGICAL ANALYSIS FOR PRIMARY FAILURE MODE. ONE BLADE FOUND WITH FAILURE PATTERNS IN THE TRAILING EDGE AREA. BLADE, PN 9299M30G09R, SN KTWD2263, REPAIR HISTORY M1K-M2K-M3K-M4H, TSN/CSN, 24,031 HOURS/5,199 CYCLES. BLADES EXHIBITED 2 FAILURE MODES - 1 TRAILING EDGE CRACKING AND SEPARATION, 2 INTERGRANULAR OXIDATION (IGO) ON INNER PASSAGE WALLS. BLADE ANALYSIS REVEALED PRESENCE OF MISLOCATED COOLING HOLE ON BLADE CONVEX SIDE WITHOUT INTERSECTING BLADE INNER OR OUTER WALLS. THE PRIMARY BLADE FAILURE ATTRIBUTED MORE TO INTERGRANULAR OXIDATION DUE TO LACK OF INTERNAL COATING. (X)