Kiddo's Driver
Pattern Altitude
Well, my Tampico's Lycoming O-320-D2A, configured for a fixed-pitch propeller, has finally given up the ghost. 6,000 hours TT, 34 years old, 1800+ SMOH, and 28+ years SMOH. It had a good run, but it's done now. Making a LOT of metal.
The good news is that I have a new-old-stock Lycoming O-320-D1A, configured for a constant speed propeller, sitting in the hangar.
The difference between the two engines is the configuration of the plugs in the hollow crankshaft and the thread size in the propeller flange bushings. It's an easy conversion.
Obviously, I will also need to remove the propeller governor, put a cover plate on the pad, remove the piping and fittings from the governor to the front of the engine for the CS prop, and then plug the holes.
The process for converting from CS to fixed pitch is covered in Lycoming SI1435, attached below. It includes what you need to do to mark the engine tag to indicate it has been modified, as well as what to do in the engine logbook.
Lycoming SI1304K states that they won't issue a new engine tag and provides guidance on marking the tag, making engine logbook entries, and submitting a 337, SI attached below.
I've called my local FSDO and talked to them.
Is it really as simple as making the CS-to-fixed-pitch changes, swapping the propeller flange inserts from 7/16" to 3/8", making the engine logbook entries, and then submitting a 337?
That is the guidance I got verbally from the FSDO, and it aligns with the SIs.
I've also attached the Lycoming Engine Designations SSP. D1A is at the bottom of the third page. D2A is at the top of the fourth page.
The good news is that I have a new-old-stock Lycoming O-320-D1A, configured for a constant speed propeller, sitting in the hangar.
The difference between the two engines is the configuration of the plugs in the hollow crankshaft and the thread size in the propeller flange bushings. It's an easy conversion.
Obviously, I will also need to remove the propeller governor, put a cover plate on the pad, remove the piping and fittings from the governor to the front of the engine for the CS prop, and then plug the holes.
The process for converting from CS to fixed pitch is covered in Lycoming SI1435, attached below. It includes what you need to do to mark the engine tag to indicate it has been modified, as well as what to do in the engine logbook.
Lycoming SI1304K states that they won't issue a new engine tag and provides guidance on marking the tag, making engine logbook entries, and submitting a 337, SI attached below.
I've called my local FSDO and talked to them.
Is it really as simple as making the CS-to-fixed-pitch changes, swapping the propeller flange inserts from 7/16" to 3/8", making the engine logbook entries, and then submitting a 337?
That is the guidance I got verbally from the FSDO, and it aligns with the SIs.
I've also attached the Lycoming Engine Designations SSP. D1A is at the bottom of the third page. D2A is at the top of the fourth page.
Attachments
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