Engine Instrument Markings; Weight Limits - Pipistrel Sinus 503 Flight And Maintenance Manual

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Propeller
SINUS
fixed pitch
variable pitch

Engine instrument markings

WARNING:
fill in engine specific values.
Instrument
Tachometer (RPM)
Oil temperature
Cylinder head temp.
Oil pressure
Fuel quantity

Weight limits

Sinus ultralight motorglider basic model weights
WEIGHT
empty aircraft weight
max. takeoff weight (MTOM)
fuel capacity
max. fuel weight allowable
minimum cockpit crew weight
maximum cockpit crew weight
joint parachute rescue sys. and luggage weight
WARNING!
Should one of the above-listed values be exceeded, others MUST be reduced in
order to keep MTOM below 450 / 472,5 kg. However, the joint parachute rescue system and lug-
gage weight must NEVER be exceeded as it can influence aircraft's balance to the point when the
aircraft becomes uncontrollable!
Owners of Sinus ultralight motorglider equipped with the GRS parachute rescue system (weigh-
ing 14 kg on itself), must keep luggage weight below 1 kg (model 503), 2kg (model 582),
4 kg (model 912) to keep aircraft's centre of gravity within safe range.
Model 503
Pipistrel BAM 2
Pipistrel VARIO
Red line Green arc
(minimum) (normal)
Model 503
450 / 472,5 kg
no limit
Model 582
Pipistrel BAM 2
Pipistrel VARIO
Yellow arc
(caution)
Model 582
265kg 274 kg
450 / 472,5 kg
2 x 30 l 2 x 30 l
45,6 kg 45,6 kg
no limit
180 kg 180 kg
15 kg 16 kg
17
SINUS motorglider
Limitations
REV. 0
Model 912
Pipistrel BAM 2
Pipistrel VARIO
Red line
(maximum)
Model 912
284kg
450 / 472,5 kg
2 x 30 l
45,6 kg
no limit
180 kg
18 kg