Service difficulty report · Case · Dhav DHC8102

Difficulty date
May 8, 1997
Submitted
March 26, 2000
Operation
Air carrier
Aircraft
N926HA
Make and model
Dhav DHC8102
Aircraft serial
114
Engine
Pwa PW120A
Part
Case
Condition
Cracked
Location
Trubine Section
Stage of operation
IN
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

THE SUBSEQUENT INVESTIGATION AT PWA HAS REVEALED THAT THE CRACKING OF THE TURBINE SUPPORT CASE OUTER SKIRT WAS DUE TO MULTI-ORIGIN LOW CYCLE FATIGUE ALONG THE WELD HEAT AFFECTED ZONE. THE MODIFIED MICRO-STRUCTURE OBSERVED IN THE WELD HEAT AFFECTED ZONE CLOSE TO THE FRACTURE SURFACE WAS A CONTRIBUTING FACTOR AND MAY HAVE BEEN CAUSED BY HEAT TREATMENT OR ENGINE OPERATION. REFERENCE HNAA9792609. (M)