pp39a4f0dc.jpg
ppfa330471.jpg
pp4159cf08.jpg
pp180d7cc8.jpg
pp9d400a83.jpg
ppf84f1a7f.jpg
pp0782d8aa.jpg
ppa549b394.jpg
pp7b1c7f44.jpg
pp382498f5.jpg
ppabae4c92.jpg
pp3f68ed8d.jpg
ppe498b431.jpg
pp83827cdb.jpg
pp8526a732.jpg
ppbe697970.jpg
ppaaa25640.jpg
pp504b832f.jpg
pp0c20ae9c.jpg
pp0984a35e.jpg
pp14d2d7d3.jpg
pp11b66f52.jpg
pp87759109.jpg
TECHNICAL   
GALLERIES   
ppbc7fec4e.jpg
ppe0a392e1.jpg
ppd25684d7.jpg
ppd6f8ec66.jpg
ALLEGRO 2007.....FANTASY AIR  
© Copyright .AERO .SIAM. CO. LTD ..         ..e-mail....paul@aero-siam.com..                 ......REGIONAL DEALER .. SOUTH EAST ASIA        

Aero Siam
pp8bcc02ac.jpg
Allegro 2000 - Performance
80 HP
100 HP
Vne
Speed range is 42 - 137 mph which is wide for this type of aircraft
137mph  
220kph
Top Speed
The 100hp reaches Vne at only 5400RPM (cruise pitch) demonstrating the efficiency of the low-drag airframe
127mph  205kph
137mph
220 kph

Cruise Speed
Cruise speed varies from a fast cruise at 115 mph to economical cruise at 80 mph. Low noise with comfortable seating and visibility make long trips easy.

110 mph
175 kph

110 mph 175 kph



Stall Speed Gross wt
Flap  - 4.5          
Like high performance gliders, the Allegro has negative flap for cruise efficiency
50 mph
80 kph
Flap   +15          
46 mph
73 kph
Flap   +48        
The large and powerful flaps allow excellent short field landings making this a STOL aircraft

43 mph
69 kph

Rate of Climb
(At gross wt) Low weight and minimum drag give a good climb rate. Solo climb rate for the 100hp is 1,500 fpm

900fpm
3.7m/s

1200 fpm
5 m/s


Glide ratio
Glide ratio indicates the drag efficiency of the airframe and affects all  performance parameters. Careful streamlining is everywhere including the smooth composite fuselage and low-drag cooling design. The long tapered wings also contribute to the excellent glide ratio.  From 3,000, the Allegro will glide nearly 7 miles.


12 : 1

Sink Rate
Engine idle, at 70 mph the Allegro has a gentle sink rate of 500 fpm taking 6 minutes to descend from 3,000 feet. With full flaps, the rate is over 800 fpm and it can sideslip at 1,000 fpm .
500 -1400 fpm
2.5 - 7.0 m/s


Take Off
The 100hp engine combined with the 48 degree flaps make this a true STOL aircraft
500ft /
150m
400ft / 120m
(To clear 50ft / 15m)
1150ft /
350m
800ft / 250m


Landing
Good visibility all round, powerful flaps, hydraulic brakes and tough composite landing gear make the Allegro easy to land

400ft / 120m
(To clear 50ft / 15m)

700ft / 220m





Fuel Burn

Cruise Speed
 80hp - 16.5 ltrs/hr / 4.5 gal/hr                      5200 rpm
100hp - 21.5 ltrs/hr / 5.8 gal/hr  
118mph
/189kph
129 mph / 197 kph
 80hp - 14 ltrs/hr / 3.78gal/hr                         4800 rpm
100hp - 18 ltrs/hr / 5.0 gal/hr
107mph
/171kph
116 mph / 185 kph
  80hp - 12 ltrs/hr / 3.2 gal/hr                          4400 rpm
 100hp - 15.5 ltrs/hr / 4.2 gal/hr  
100mph
/162kph
109 mph / 175 kph
  80hp - 10 ltrs/hr / 2.7 gal/hr                         4000 rpm
100hp - 13 ltrs/hr / 3.5 gal/hr
92mph
/147kph
100 mph / 160 kph
  80hp - 9 ltrs/hr / 2.5 gal/hr                       3600 rpm
100hp - 10.5 ltrs/hr / 2.8 gal/hr  
77mph
/123kph
84 mph / 135 kph



Range
Standard tank capacity is 63 litres / 17 gallons - all figures nil wind, no reserve at fast cruise  110 mph (175 kph)  
450 miles / 650 km
400 miles / 560 km
Optional wing tanks increase this to 103 litres / 28 gallons which offer remarkable range at economical cruise speed especially for the 80 hp engine. Figures at  85 mph (135 kph)

900 mi / 1,450 km

800 mi / 1300 km


Endurance

Standard tank at minimum power cruise of 70 mph (115 kph) - all figures nil wind no reserve

7 hrs

5.5 hrs
Optional wing tanks

11 hrs

9.5 hrs
* Figures for 80hp are TAS at sea level with prop pitched to full cruise for economy. Max RPM is 5500 giving a top speed of 126mph/ 203kph. Changing the pitch to nearer a climb setting will increase speeds at all RPM and allow a higher climb rate and  top speed (Vne) of 137mph/220kph.
See Thom’s very detailed performance figures for the 80hp HERE

Note that for South East Asia with a typical density altitude of 3,000 feet, RPM required will be about 300 higher to reflect an effective  power loss of about 6%. Figures do not apply to the ultralight version in Thailand