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The LAMBADA is designed with safety, excellent performance and economy in mind.
The LAMBADA is manufactured in two versions, a full length flaperon and an aileron only version. The aileron only version meets the standards for S-LSA. The flaperon version has a slightly better roll rate and thermal ability than the aileron only version, which has a higher MTOW and Vne
LAMBADA - brief technical description:
The LAMBADA ultralight motorglider is a two-seat, single-engine, mid-wing aeroplane with side-by-side seating.The aircraft is of all-composite construction.
The flaperon version of the LAMBADA wing has flap settings of 5°, 9° and 16° with the airbakes operating beyond the 16° detent. The aileron version is equiped with airbrakes only. The tailplane is a T-tail design.
The undercarriage may be tricycle or tail-dragger with a steerable tailwheel. The main wheels are equipped with hydraulic brakes and the main undercarriage is sprung, made of a continuous laminated composite construction. Integral fuel tanks are located in the wing leading edge.
The UFM 13 Lambada motorglider may be equipped with removable wing extensions. Wings are produced in four sections, allowing for a change in wingspan from 42" 8" (13 m) to 49' 2" (15m). The extensions increase the wingspan and performance of the aircraft.
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LAMBADA Specifications: |
| Wingspan |
42' 8" (49' 2" |
13 (15) m |
| Length |
21' 8" |
6.6 m |
| Height |
6' 5" |
1.95 m |
| Wing area |
136 sq ft |
12.6 sq m |
| Aerofoil section |
SM 701 |
SM 701 |
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| MTOW: |
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| - Flaperon version |
1144 lbs |
520 kg |
| - Aileron only |
1320 lbs |
600 kg |
| Empty weight |
584 / 617 lbs |
265 /280 kg |
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| Engine options: |
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| Rotax 912 UL |
80 HP
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80 HP |
| Rotax 912 ULS |
100 HP |
100 HP |
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| Minimum speed |
34 kts
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63 km/h |
| Cruise speed |
86 kts |
160 km/h |
| Maximum speed: |
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| - Flaperon version |
108 kts |
200 km/h |
| - Aileron only |
120 kts |
222 km/h |
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| Glide ratio |
~26:1 (30:1) |
~26:1 (30:1) |
| Climb solo |
700 (1400)fpm |
3.5 (7.0)m/s |
| Climb MTOW |
500 (900)fpm |
2.5 (5.0)m/s |
| Min. sink rate |
200 fpm |
1.1 m/s |
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| Fuel tank/s |
1 / 2x13 USgal |
1 / 2x50 l |
| Cockpit width |
39 / 41" |
990 / 1041 mm |
| Seats |
2 |
2 |
LAMBADA Motorglider Standard inclusions:
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| Engine Rotax 912 UL |
Canopy with flipers |
| Propeller WOODCOMP SR200 |
Camloc screws on the cowling |
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| Silicon fuel line protection |
Position light (Strobe) preparation |
| Stainless exhaust |
Tow hook preparation |
| 2 x 50 liters fuel tank |
Compensated Vario preparation |
| Pilot seat on the left |
Rescue system preparation |
| Tail dragger undercarriage (wheels 14x4) |
Carbon fuselage
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| Standard VFR instrumentation: |
Wingtips for 15m span |
| Air speed indicator |
Winglets - "Shark fins" |
| Altimeter |
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| Vertical speed indicator |
First aid kit |
| Magnetic compass |
Fire extinguisher |
| Engine instruments |
Special fuel filter ("gas colator") |
| Bank indicator (ball) |
Parking brake
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| Basic radio pre-equipment preparation |
Nylon tapes on ailerons |
| Extraboom microphone and speaker preparation |
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