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Tecnam P2010 - Page 515

Tecnam P2010
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AFMS N° D08 FOR ALTERNATIVE AVIONICS CONFIGURATION AND
VARIABLE PITCH PROPELLER EQUIPPED AIRPLANES
Page GV 2-9
7. PAINT
To ensure that the temperature of the composite structure does not exceed limits,
the outer surface of the aeroplane must be painted with white paint, except for ar-
eas of registration marks, placards, and ornament.
Refer to Aircraft Maintenance Manual (AMM), ATA Chapter 4 and 51, for spe-
cific paint requirements.
8. PROPELLER
MANUFACTURER: .…….. MT Propeller
MODEL: …………….……. MTV 15B/193-52
TYPE: .……………….…… wood/composite 2-blade, variable pitch
DIAMETER: ……………... 1930 mm (76in) (no reduction is permitted)
9. MAXIMUM OPERATING ALTITUDE
Maximum operating altitude is 12000 ft (3658 m) MSL.
CAUTION
At altitudes above 10000 ft (3048 m) up to and including 12000 ft (3658
m), flight crew is recommended to use supplemental oxygen.
10. AMBIENT TEMPERATURE
Ambient temperature: from -25°C to +50°C.
WARNING
Flight in expected and/or known icing conditions is forbidden.
Ed. 1, Rev. 0
Section 2 Limitations
PAINT, PROPELLER, MAX ALTITUDE AND OAT

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