This paper investigates robustness of permanently mounted transducers used in airborne
structural health monitoring systems, when exposed to the operational environment. Typical
airliners operate in a range of conditions, hence SHM transducer robustness and integrity must
be demonstrated for these environments. A set of extreme temperature, altitude and vibration
environment test profiles are developed using the existing RTCA/DO-160 test methods. Commercially
available transducers and manufactured versions bonded to CFRP composite materials are tested. It
was found that the DuraAct transducer is robust to environmental conditions tested, while the other
transducer types degrade under the same conditions.