TECNAM P2008 JC — Systems Description
2 systems description references for the TECNAM P2008 JC.
Overview
TECNAM P2008 JC - Aircraft Flight Manual · 2018
The Aircraft Flight Manual for the Tecnam P2008 JC provides essential information for the safe and efficient operation of this light aircraft. It includes details on aircraft systems, limitations, emergency procedures, and performance specifications.
- Tecnam P2008 JC is a single-engine, two-seat aircraft.
- The aircraft features a strut-braced high wing and fixed landing gear.
- The manual must be carried in the aircraft at all times.
- It is approved for EASA CS-VLA certified airplanes.
- The maximum takeoff weight (MTOW) is 650 kg.
- The engine is a Bombardier-Rotax 912 S2 with a maximum power of 73.5 kW.
- The propeller is a fixed-pitch MT Propeller with a diameter of 1700 mm.
- The manual includes a record of revisions to maintain current operational data.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.
2 documents
TECNAM P2008 JC — Systems Description FAQ
How many Systems Description documents does Sprinkle have for the TECNAM P2008 JC?
Sprinkle has 2 Systems Description documents on file for the TECNAM P2008 JC.
What year is the TECNAM P2008 JC Systems Description?
The TECNAM P2008 JC Systems Description on file is dated 2018.
