MitchellWing A-10 Motorglider
Specifications and Data

Feature MitchellWing Owner's Manual A-10 (Orig. Release '98?) Ameriplanes Website A-10D Zenoah G25B-1 equipped 18 JLS - A-10 Factory built in 1984, S/N 123, w/ Zenoah G25B-1
Wing Span - ft
Wing Area - sq.ft
Aspect Ratio
Engine - Mfr
_HP
_Displacement - cc
Empty Weight - lb
Useful Load - lb
Gross Weight - lb
Wing Loading - lb/sq ft
Design Stress - g's
Pwr Loading - lb/hp
Speeds - mph
_Vne
_Vmax
_Vcr
_Vstall - Pwr Off
_Rotation Speed - mph
_Maneuv. Speed - mph
_Appr'ch Speed - mph
Rate of Climb - ft/min
_Best ROC Speed
Rate of Sink - ft/min
_Best ROS Speed
Glide Ratio
_Best L/D Speed
Fuel Capacity - gal
Range - 75% Pwr - gph
_Hours - No Res.
_Miles - No wind
Takeoff - Wind calm
_Ground Run - ft
_Dist. 50' obs. - ft
Landing - Wind calm
_Ground Roll - ft
_Dist. 50' obs. - ft
Service Ceiling - ft
34.33'
156
8.7
Zenoah (G25B-1?)
23
242
250
288
538
3.1?
+6/-5.5
18.8?

63
63
58
27
32
50
40
650
40
240
35
16:1
40
3.0
1.25*
2.4*
140*

225
535

200
700
12,000

*Range and endurance values based on 1.25gph@75% are highly suspect. Fuel consumption is likely to be closer to 2.5 gal/hr, IMHO. JEC
34.33'
136?
8.7
Zenoah G25B-1
22
242
270
280
550
3.5?
+6/-5.5
18.8?

80
70
62
28
n/s
n/s
n/s
650
n/s
240
n/s
16:1
n/s
3.0
1.25*
2.4*
140*

250
600

250
750
12,000

*Ditto remarks offered in Owner's Manual column. JEC
34.33'
156
8.7
Zenoah G25B-1
22 (manf.stated, prop?)
242
288 (as of 11/17)
240 (avg. flying)
518 (avg. w/5 gal fuel)
3.32
+4.6/-2.3
23.55

63?
63?
62?
28?tbd
32?tbd
50
40
650?tbd
40?tbd
240?tbd
35?tbd
16:1?
40?tbd
5.0
2.5?tbd
2.0?tbd
140?tbd

250?tbd
600?tbd

250?tbd
750?tbd
12,000?tbd

?tbd - Values for 18 JLS to be determined by actual measurement and/or analysis at a later date. JEC


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    JoeCook1@csi.com
    Last Updated 12/28/01