Connecting Rods / Rocker Arms

Connecting Rods / Rocker Arms

Each piece is degreased, cleaned and magnetic particle inspected. Connecting rods undergo a dimensional inspection, alignment check, as well as a twist and bore check. They are re-bushed and precision bored to new dimensional limits and alignment. Each part receives a final inspection to ensure it is like-new and an FAA 8130 maintenance release is issued for return to service.


Connecting Rods

Complete Repair/Recondition $100.00
Exchange RFQ
Lycoming Tongue & Groove (LW10646, 13422, 19332) $175.00
Exchange Tongue & Groove (LW10646, 13422, 77450, 19332) RFQ
Modify Per S.I. 1183 $33.00
Modify Per S.I. 1359 $100.00
IO-520 Exchange Wide for Narrow,  (Includes workup less bushing) $219.00
Balance a Set of 4 $62.00
Balance a Set of 6 $103.00
Balance a Set of 8 $146.00


Rocker Arms

Complete Repair/Recondition Lycoming Style $53.00
Complete Repair/Recondition Continental $53.00
Clean and Dimensional Inspection Only $24.00
Drill Oil Supply Hole in Continental Old Style  $24.00
Modify To Accept One Piece Bushing (Complies with S.B. M93-7)  RFQ


Prices listed above are “per item” and do not include parts, except where noted. All prices USD.
Five day turnaround is normally available upon request for all items above except crankshafts requiring re-nitriding. 
Certain items may be issued a Dual Release (FAA/EASA). Prices are subject to change without notice.




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Disclaimer: While reasonable efforts have been made to ensure all information on this website is accurate, Aircraft Specialties Services does not assume responsibility for any errors or omissions. All specifications, illustrations, data and prices are subject to change without notice. Applications and interchangeability information depicted on this website is strictly for reference only. Installers must consult the engine/airframe IPC for the manufacturer’s approved data. All prices "each" unless specified. Images represent attributes, not quantity. Application information is provided for reference only. Make sure to refer to the applicable airframe/engine manufacturer's manual for exact application information.