Lambert Mission 106
http://dbpedia.org/resource/Lambert_Mission_106 an entity of type: Thing
The Lambert Mission 106 is a conventionally laid out, high-wing ultralight, seating two side-by-side. Designed in Belgium, there are ULM and LSA versions.
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Lambert Mission 106
xsd:integer
34244564
xsd:integer
999467575
xsd:double
9.32
xsd:integer
65
rdf:langString
flaps down
xsd:double
11.8
rdf:langString
met
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c.2003
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two
<litre>
78.0
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Lambert Aircraft Engineering BVBA
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Jane's All the World's Aircraft 2011/12
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In production
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Two seat ultralight
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including taxes in 2010
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€42,500 tailwheel
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€43,500 nosewheel
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The Lambert Mission 106 is a conventionally laid out, high-wing ultralight, seating two side-by-side. Designed in Belgium, there are ULM and LSA versions.
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NACA 230102
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*Dyson Avionics D100 EFIS and EMS D10 standard
xsd:double
5.08
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maximum at sea level
xsd:integer
157
xsd:integer
260
xsd:integer
82
xsd:integer
1
xsd:double
2.15
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tailwheel undercarriage
xsd:double
6.1
xsd:integer
185
xsd:integer
450
xsd:integer
495
<second>
6600.0
xsd:integer
210
rdf:langString
c.10
xsd:integer
3
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DUC Swirl ground adjustable pitch
xsd:integer
700
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at 75% power
xsd:nonNegativeInteger
7225
xsd:nonNegativeInteger
0
<euro>
42500.0
43500.0