Abstract: A jet pipe liner for a gas turbine engine comprises of an inner skin consisting of a multiplicity of longitudinally extending sections arranged edge-to-edge in a circumferential direction and suspended along their edges by a multiplicity of longitudinally extending A-frame members. The supporting members are attached to the inside of the jet pipe and the inner skin sections are clamped along their long edges by double-skinned distal ends of the links of the A-frame members.