Tecnam P2002 JF - Page 964

2
nd
Edition - Rev 0
SUPPLEMENT S1
Chapter 3 – Airplane General Description
Page 1
CHAPTER 3 – AIRPLANE GENERAL DESCRIPTION
ENGINE
Manufacturer
Bombardier-Rotax GmbH
Model
912 S3
Certification Basis
FAR 33 Amendment 15
Austrian T.C. No.
TW 9-ACG dated 27th November 1998
Tipo di
4 cylinder horizontally-opposed twins with overall dis-
placement of 1352 c.c., mixed cooling, (water-cooled
heads and air-cooled cylinders), twin carburetors, inte-
grated reduction gear with torque damper.
Maximum rating
73.5kW (98.5hp) @5800rpm (max.5’)
69.0kW (92.5hp) @5500rpm (cont.)
PROPELLER
Manufacturer
Hoffmann Propeller
Certification Basis
Joint Airworthiness Requirements JAR-P
Propellers, Change 7 inclusive
Type Certificate No.
LBA TCDS 32.130/88 dated 20/08/2003
Model
HOV352F1/C170FQ+8
Number of blades
2
Diameter
1780 mm (no reduction allowed)
Type
Variable pitch – wood
GOVERNOR
Manufacturer
Jihostroj
Model
P-110-030/A
Type
Hydraulic