Text in force at CS29-12: from CS29-0, effective 14 Nov 2003.
For reciprocating engine powered rotorcraft the following apply:
(a) Each exhaust heat exchanger must be constructed and installed to with stand th e vibration, i nertia, and ot her l oads t o whi ch i t would be subjected in operation. In addition:
(1) Each exchanger must be suitable for continued operat ion at hi gh t emperatures and resistant to corrosion from exhaust gases;
(2) There must be m eans for inspecting the critical parts of each exchanger;
(3) Each exchanger m ust have cool ing provisions wherever it is subject to contact with exhaust gases; and
(4) No exhaust heat exchanger or m uff may have st agnant areas or l iquid t raps that would in crease th e p robability o f ig nition o f flammable fluids or vapours t hat m ight be present in case of t he failure or m alfunction of components carrying flammable fluids.
(b) If an exhaust heat exchanger is used for heating ventilating air used by personnel –
(1) There m ust be a secondary heat exchanger between the pri mary exhaust gas heat ex changer an d th e v entilating air system; or
(2) Other m eans m ust be used to prevent harm ful cont amination of t he ventilating air.
ED Decision 2003/016/RM · Source