OhioStatePilot
Well-Known Member
You got it, that was fast too! I don't think I'm terribly good at making these yet...
EPIC fail - Scholls Chipmunk was NOT Ranger powered.
ENGINE CONVERSION: Fitment of a six cylinder inline Ranger 6-440C-5 engine of 200 hp and strengthening of the bulkhead area to cope with greater engine torque – with this engine the standard Chipmunk cowlings were retained with just small vents or humps for clearance being added. The nose cowling cooling inlet for the original Gipsy Major engine on the port side was faired over and converted to the starboard side. As the Ranger engine had no electrical starter unit a hand cranking facility was incorporated on the port side immediately aft of the cowling and a Kopper Aeromatic variable pitch propeller converted the power.
Yes it was...
ADDITIONAL MODIFICATIONS: The installation of a flat-opposed 6 cylinder Lycoming G0-435-C2 of 260 hp.@ 3400 rpm. with a new engine mount giving1½º downthrust and with 0º offset and a completely redesigned one piece cowling which fitted over the nose and required the removal of the prop to service the engine. The standard Chipmunk with Gipsy Major 145hp engine was never fitted with an inverted fuel system so a flop tube was installed in the starboard rubber bag tank of twelve gallon capacity, a Bendix PS-5BD ‘all attitudes’ pressure carburetor and an inverted Christen oil system completed this part of the conversion. Once again an Aeromatic air controlled wooden bladed propeller was used with an overall diameter of 150” with modified pitch settings. With the closely cowled engine there was no room to fit an oil cooler and this was installed in the fuselage behind the rear seat and cooling ducts fitted in the fuselage. The centre section of the fuselage also received attention with beefed-up spars (7075-T6 material and specification 4130 steel plates) and a modified (flatter) dihedral angle in order to help with inverted flight - the centre section control box area in the cockpit which had proven liable to cracking with harsh aerobatic use was also beefed-up with additional plates.
Further down the same page.ADDITIONAL MODIFICATIONS: The installation of a flat-opposed 6 cylinder Lycoming G0-435-C2 of 260 hp.@ 3400 rpm.