Engine Mount Bolts

Scott Swing let me know that the engine mount for a TCM IO-550 is 24″ wide at the bottom, and that the bolts penetrate the firewall just above the fuselage floor. I had previously cut down my header tank to make more room in this area, and I was relieved to find that there appears to be sufficient space to accommodate the bolts and the large washers. The 12″ mark is aligned with the fuselage centerline, and the tape measure shows the approximate location where the holes will be.

Hydraulic Pump and Lines

The landing gear hydraulic pump was mounted onto the MLG bulkhead with a thick aluminum backing plate. Bolts enter from the aft side, pass through the backing plate, and then screw into the hydraulic pump body. The pump reservoir is about 2 cm off the floor of the fuselage.

After making a couple of flexible hydraulic lines that run from the pump to the fittings on the MLG hydraulic cylinder, I started to worry about the hydraulic lines fouling the MLG retraction cables. One solution would’ve been to fabricate rigid hydraulic lines, but I decided to separate the keel space vertically into an upper deck and a lower deck. The brake lines, which are rigid tubing, and the MLG cables will occupy the lower deck, an the aileron torque tube, hydraulic lines, and wiring will be on the upper deck. A thin layup was made with 2x BID on aircraft plywood, and this was shaped to be the divider. An aluminum tunnel was made to cover the aft end of the gear cables, and to provide a transition for the hydraulic lines to enter the keel.

Aft Battery Tray

An aft battery tray was fabricated as a layup of 1x triax and 2x BID on divinylcell foam. The layup was done directly on a glass plate to get a smooth top finish. The tray and the legs were cut out with a jigsaw, and the legs were contoured until the tray sat level in the aft area between the whale tail and the MLG bulkhead. An aluminum battery bracket is being fabricated to retain the battery to the tray and to the MLG bulkhead.

Drilling Aileron Torque Tube

The aileron torque tube sections, the universal joint, and the rear torque tube bell crank have to be drilled so that the sections and parts will mate together tightly and in proper alignment. I used the wing spar and firewall as a table and clamp plate, respectively, to hold the assembled torque tube in position for drilling the last hole through the torque tube bell crank. The torque tube bell crank and the forward side-stick bell crank have to both be aligned vertically when attached. Its a kluge, but it worked OK. The holes were drilled slightly undersized, and then reamed for an interference fit for the AN-3 bolt. Slop is unacceptable.

Landing Gear Dump Valve

I decided to put the landing gear hydraulic dump valve inside the keel, where it will be accessed by opening a door just under the pilot’s right elbow. I plan to also put the main fuel shutoff knob here. This location is above the aileron torque tube, and should not interfere with other stuff in the keel.

An aluminum bracket was made to hold the valve itself, and a drilled aluminum backing plate was glassed onto the exterior wall of the keel to be a hard point for the valve.

Landing Gear Retraction Test

With the main landing gear filled and primed, and with the brake lines attached to the gear legs, I did a retraction test to make sure that there was still no interference with the MLG cutouts in the fuselage (which had to be widened slightly), and the aluminum tubing for the header tank vent and drain. The trusty nitrogen cylinder was used to do the retraction, and all was successful.

Brake Lines and Brake Calipers

The routing of the brake lines needs to be such that there is adequate length to accommodate the retraction of the gear, and that the excess stays out of the way of the gear leg during the MLG movement into the down position.  The flexible brake hose was routed close to the gear leg pivot axle, and from there, terminates at an AN bulkhead elbow fitting through the landing gear bulkhead.  Hard aluminum tubing will run to the front of the aircraft from these fittings.

A significant portion of the landing gear door holder plate had to be removed to prevent interference with the brake caliper.  I want to be able to remove the brake caliper without having to remove the gear axle, so this was a necessity.  I will find alternate ways to hold the gear doors when that time comes.  Finally, a 3/8″ thick brass bushing was used during assembly of the MLG over-center mechanism to hold the mechanism forward and prevent interference with the header tank fittings.