If the cadmium is deposited by an electroplating process, then yes, hydrogen embrittlement becomes a concern. The conventional practice is to perform a baking operation after plating but before chromating to relieve the fasteners from hydrogen embrittlement. SAE-USCAR 5
Avoidance of Hydrogen Embrittlement of Steel has the following requirements:
320 HV < core hardness < 380 HV: bake minimum of 4 hours at 200 +/- 5 C within one hour plating and before chromate treatment.
350 HV < surface hardness < 400 HV: same as above.
core hardness > 380 HV or surface hardness > 400 HV: bake minimum of 8 hours at 200 +/- 5 C within one hour of plating and before chromate treatment.
Since you did not list a fastener standard, I do not know what "hi tensile" means regarding the proper embrittlement relief. If the steel has been tempered at a temperature less than 200 C in order to attain the necessary mechanical properties, then the fasteners should be baked for a minimum of 8 hours at 115 +/- 5 C.
I would not recommend using cadmium plated bolts manufactured from medium carbon alloy steel for this type of application, especially if they are not produced to a proper fastener standard (ASTM, ISO, etc.). Nickel alloy or multiphase alloys (nickel-cobalt-chromium-molybdenum) perform much better in this type of environment, and with a suitable combination of cold working and heat treatment, can attain the necessary mechanical properties. I recommend you read the following article on multiphase fastener alloys from SPS:
They also have an excellent booklet on these alloys called
Superalloys Developed by SPS Technologies for Aerospace Fasteners which you can obtain by clicking on the following link: