The FIELD AVIATION APU removal STC for the DHC-8 provides the operator with a procedure for removing the OEM Installed Hamilton Sundstrand T-62T-40C7B Auxiliary Power Unit.
Please click on "Front sheet" link for a copy of our brochure.
Removal of APU for operations where it is not required providing additional payload capacity.
Up to a 250 lb weight savings.
Removal of the APU includes the following:
• Removal of the APU, Starter Generator and miscellaneous accessories
• Removal of the APU structural mounting provisions
• Removal of the associated ducting AFT of the pressure bulkhead
• Removal of the drain lines and welded drain mast and installation of blanking doublers
• Capping and stowing the associated electrical harnesses
• Draining, capping and stowing the APU fuel supply lines
• Removing the control heads for the APU system and installation of blanking provisions
• Temporary removal options are also available
TC and EASA STCs are also available.
Up to a 250 lb weight savings.