In addition to the 2 standards mentioned above, you should also refer to the American National Standard ANSI MH27.1, "Specifications for Patented Track Underhung Cranes and Monorail Systems". This standard (referenced by the ASME B30.11) is published by the Monorail Manufacturers Association, Inc., an affiliate of the Material Handling Industry (MHIA) out of Charlotte, NC. Their website can be found at
As opposed to the ASME B30.11 safety standard, the MH27.1 standard sets forth more "design guide" specifics, such as loading conditions, allowable stress, etc. In particular, the impact factor is specified as 0.5% of the rated load for each foot per minute of hoist speed, with a minimum value of 15% and a maximum value of 50%.
One glaring shortfall of this standard is the treatment of operating lateral load on the monorail beam or crane runway system. In this regard, the standard states that operating lateral load is to be "as specified by the purchaser or determined by the manufacturer..." (sounds to me like the committee couldn't agree on this issue).
In the case of an underhung crane runway where the load can travel perpendicular to the runway beam, I think you have to apply the AISC "20%" method for determining the side thrust as a minimum.
For a monorail beam with no lateral movement of the load, I would agree that prudence still dictates some consideration of side thrust. The 5 degree angle of lift mentioned above seems reasonably conservative in lieu of anything specified by the Owner, but I've never seen that value actually referenced in any standard.
Another way of looking at the side thrust value for a monorail beam is to apply the minimum specified horizontal load that CMAA No. 74 would use in the design of an underhung girder on a crane. At a minumum, this value would be 2.5% of the vertical load (specified by CMAA as the 'inertia forces' from the crane drive and dependent on the accel. or decel. rate of the crane). (An earlier edition of the CMAA standard specified this value as 5% of the vertical load, regardless of the accel. or decel. rate). In either case, the CMAA method would result in significantly less thrust than that produced from the 5 degree angle of lift.
Hope this helps.