Diamond DA 40 Flight Manual page 46

Operating
Limitations
k) Propeller designation
l) Propeller diameter
m) Propeller pitch angle (0.75 R) : 10.5° to 30°
n) Oil specification:
Airplane engine oil should be used which meets SAEJ1899 (MIL-L-22851) Standard
(ashless dispersant type). During the first 50 hours of operation of a new or newly
overhauled engine, or after replacement of a cylinder, airplane engine oil should be used
which meets SAEJ1966 (MIL-L-6082) Standard (straight mineral type). The viscosity
should be selected according to the recommendation given in the following table:
OAT at
Ground Level
All temperatures
above 80 °F
(above 27 °C)
above 60 °F
(above 16 °C)
30 °F to 90 °F
(-1 °C to 32 °C)
0 °F to 90 °F
(-18 °C to 32 °C)
0 °F to 70 °F
(-18 °C to 21 °C)
below 10 °F
(below -12 °C)
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: MTV-12-B/180-17 or
MTV-12-B/180-17f
: 1.80 m (+ 0 mm, - 50 mm)
5 ft 10.9 in (+ 0.0 in, - 2.0 in)
During the first 50 hours:
SAEJ1966 / MIL-L-6082
Mineral Oil
---
SAE 60
SAE 50
SAE 40
SAE 20-W50
SAE 30
SAE 20
Rev. 8 01-Dec-2010
After 50 hours:
SAEJ1899 / MIL-L-22851
Ashless Dispersant Oil
SAE 15-W50, SAE 20-W50
SAE 60
SAE 40 or SAE 50
SAE 40
SAE 20-W50 or SAE 15-W50
SAE 30, SAE 40,
or SAE 20-W40
SAE 30 or SAE 20-W30
EASA
Doc. # 6.01.01-E
approved
DA 40 AFM