Piper PA-22 Tri-Pacer — Type Certificate
1 type certificate reference for the Piper PA-22 Tri-Pacer.
Overview
ARKUSZ DANYCH TECHNICZNYCH do Świadectwa Uznania Zdatności Nr UZ-BB-14/01 z dnia 06 września 2001 · 2001
This document is a Type Certificate Data Sheet (TCDS) for the Piper PA-22-160, commonly known as the Tri-Pacer. Issued by the General Inspectorate of Civil Aviation in Poland, it outlines the airworthiness approval conditions and limitations for the aircraft. The TCDS serves as an official record of the aircraft's compliance with safety and operational standards as set by the Federal Aviation Administration (FAA). It includes critical specifications such as engine type, fuel requirements, weight limits, and seating capacity, which are essential for pilots and operators to ensure safe operation of the aircraft.
- Aircraft Model: Piper PA-22-160 (Tri-Pacer)
- Maximum Takeoff Weight: 2000 lbs
- Baggage Weight Limit: 100 lbs
- Engine: Lycoming O-320-B2A or O-320-B2B
- Fuel Requirement: Aviation gasoline min. 91/96 octane
- Maximum Engine Speed: 2700 RPM
- Seating Capacity: 4 persons
1 document