- FAA-PMA approved - logbook entry.
- Internally cored for all wiring.
- Premium powder coat finishing.
- Removable switch plates on both grips.
- Electric trim switch plate option.
- Each grip has multiple switch positions.
- Solid heat treated aluminum.
- PMA and installation instructions included.
- Weight 2.9 lbs per wheel
- FAA approved alternate method of compliance (AMOC) for AD-64-0606 and other ADs.
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These FAA-PMA approved replacement Piper control yokes are a direct replacement for original
Piper 'bow tie' and 'rams horn' control yokes. They are installed in the same manner as the original Piper yokes with bolts and are
supplied with all installation hardware. Pre-1967 Pipers typically have a 3/4" diameter torque tube (shaft). Later models typically
have a 1.125" diameter tube.
The cast aluminum wheel is cored for internal cables, which can be routed through the torque tube or alternatively with a 'coiled
cord' to the panel.
These control yokes are FAA-PMA approved replacements for the original equipment Piper P/N 62818 yokes
and others, which are subject to Airworthiness Directive AD 64-06-06.
Avion replacement yokes are an approved alternate method of compliance for several Piper control
yokes AD's.
Avion recommends Otto Mil-Spec switches, Otto P7-5A1122 normally open with black actuator for PTT and Otto P7-5A1121
normally closed red actuator for A/P Disconnect
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- Installation time approximately two hours.
- Includes all the necessary hardware.
- Both grips cored for internal for wiring.
- Electric trim switch plate available.
- Switch plates easily removed for wiring access.
- Mounts onto either 3/4" or 1.125" original Piper shaft.
- The original attach rivets are removed and replaced with with
machine screws and nuts.
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Download Installation Manual and Model Applicability List
