EasyManua.ls Logo

Tecnam P2010 - Page 281

Tecnam P2010
587 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
AFMS N°D02 FOR VARIABLE PITCH PROPELLER EQUIPPED AIRPLANES
Page V4-20
5.6. TAKEOFF
For 5000ft density altitude and above, or high ambient temperatures, a FULL RICH mixt
may cause rough running of the engine or a loss of performance. The mixture may be
justed to obtain smooth engine operations.
Lean to maximum RPM at Full Throttle prior to take-off where airports are at 5000ft d
ens
altitude or higher.
During climb, a rough method of correctly leaning is to slowly reduce mixture lever until
increase of appr.ly 50-100 RPM is noticed at constant IAS or EGT reaches 1375°F mark.
1. Pitot HEAT: ON if required
2. Fuel pump: ON
3. Brakes: apply
4. Throttle: FULL and check approximately 2680
±
20 RPM
WARNING
Engine proper performance at full throttle shall be checked early in the ground roll
in order to abandon take-off if necessary.
A rough engine, sluggish RPM increase or failure to reach take-off RPM are reasons
for abandoning the take-off. If the engine oil is cold, an oil pressure in the yellow sec-
tor is permissible.
5. Engine instruments: check parameters within the limits
6. Brakes: Release
7. Rotation speed V
R
: 60 KIAS
8. Airspeed: 67 KIAS
Above a safe height:
9. Propeller lever: 2600 RPM
10. Landing lights: OFF
NOTE
Section 4 Normal procedures
CHECKLISTS
2
nd
Edition, Rev. 0

Table of Contents

Other manuals for Tecnam P2010

Related product manuals