Used to remove and install the pinion nut and specified throughout the AMM and CRO manuals. Comes with all shown attachments and tool pouch. Reference P/N AN8515-1 | Bell

This is our substitute for the necessary OEM P/N: XW20509 / 02314-0023-0001 tool called out in the maintenance manuals of Bell and other aircraft. We have seen some middle-man suppliers try to charge over $2000 for these, which is ridiculous. We offer it at a reasonably low price.

Used to disassemble the main rotor yoke, trunnion, and the pillow block. Reference P/N 1124 | Bell

Used to remove the transmission oil pump assembly. Reference P/N 518 | Bell

Built using the OE specifications, this puller will also work to pull any fuel cartridge with 7/16-20 threads. Reference P/N E2-10-1 | Airborne | Parker

Built using the OE specifications, this adapter is used for some disassembly of the fuel pump. Reference P/N E2-14-1 | Airborne | Parker

Built as per BHT-212-CR&O-4. Lead time is 4-6 weeks.

So, you’re into doing things right, with the best of the best equipment. With this complete package, you will be able to bleed rotor brakes faster, by yourself, and if using our Hydra-Pro, less frequently. This is due to the Hydra-Pro’s filtered fluid prolonging the life of the hydraulic internals. What’s included? A Bell 205 / 206 / 212 / 407 / UH1 rotor brake servicing bleed adapter, Hydra-Pro servicing pump (10 micron), and 10’ hose with quick disconnect couplers that meet MIL-C-4109. The unique adapter has a push button bleed valve, and an anti-emulsification tube that also acts as a volumetric spacer to prevent over-servicing, and the resulting mess when removing it from the master cylinder. This enables one person to bleed the brake and leave the master cylinder serviced to “full” without any mess. It will work with any 125 max psi pump, but was designed to be used with our Hydra-Pro (Included).