Model Specs & Performance

Model:
Corben Baby Ace Model D

Corben Junior Ace Model E
Cost (US$) Plans only: $125.00
Kit: $18,950.00
Plans only: $145.00
Kit: $20,950.00
CONSTRUCTION AND ENGINE
Group Code CONV CONV
Landing Gear FG (tailwheel or trike) FG (tailwheel or trike)
Seats 1 2 Side-by-Side
Construction Material Metal tube and fabric Metal tube and fabric
Engine Continental, Lycoming Continental, Lycoming
Horsepower 65-100 85-120
Propeller 2 blade metal or wood 2 blade metal or wood
Cabin Width 24 inches (61 cm) 30 or 36 inches
(76 or 91 cm)
WEIGHTS AND SIZES
Gross Weight 950 lbs (430 kg) 1320 lbs (600 kg)
Empty Weight 575 lbs (260 kg) 700 lbs (345 kg)
Useful Load 375 lbs (170 kg) 620 lbs (270 kg)
Fuel Capacity 17 gal (64 l) 22 gal (83 l)
Wingspan 26.5 ft (8 m) 26.5 ft (8 m)
Wing Area 110 ft2 (10.2 m2) 110 ft2 (10.2 m2)
Wing Loading 8.6 lbs/ft2 (42 kg/m2) 12 lbs/ft2 (58.6 kg/m2)
Ultimate "G" Loading n/a n/a
Overall Length 17.9 ft (5.46 m) 18 ft (5.49 m)
Height n/a n/a
PERFORMANCE
Maximum Speed 96 kts @ sea level 113 kts @ sea level
Cruise Speed 87 kts 95 kts
Stall Speed
(@ gross weight)
30 kts 38 kts
Service Ceiling 10,500 ft (3,200 m) 10,500 ft (3,200 m)
Takeoff Distance 300 ft (91.5 m) 600 ft (183 m)
Landing Distance 250 ft (76 m) 300 ft (91.5 m)
Rate of Climb
(gross)
1200 fpm 500 fpm
Maximum Range n/a n/a
COST
Cost (US$) Plans only: $125.00
Kit: $18,950.00
Plans only: $145.00
Kit: $20,950.00

Note: Specifications are from factory production aircraft. All prices and specifications are subject to change without notice. Performance data given are approximate.


Engine Options
Ace Aircraft are very versatile airframes and can be built with a wide range of engine options from certified aircraft engines to engines from Hog-Air, Jabiru, Rotax, Rotec Radial, TCM and others.
Hog-Air Jabiru Rotax
Rotec Radial TCM
 

~~~BABY ACE / JUNIOR ACE RIGGING DATA~~~

     *DATUM: LEADING EDGE OF WING.    

      *LEVEL REFERENCE: UPPER LONGERON.

       *CENTER OF GRAVITY:   AFT LIMIT=18.36"

                                                   FORWARD LIMIT=11.88"

                                                   EMPTY CG= 12.5" TO 13.5"

      *INCIDENCE ANGLES:      REFERENCE= UPPER LONGERON

                                                   HORIZ. STAB.= 0.0 DEGREES

                                                   WING= +1.18 DEGREES

                                                   ENGINE= 0.0 DEGREES VERT./HOR.

                                                   VERTICAL FIN= 0.0 DEG. (FUSE C/L)

       *CONTROL SURFACE TRAVEL:

                                                    AELERONS: 20 DEG. UP/DN

                                                    ELEVATOR: 32 DEG. UP/DN

                                                    RUDDER: 27 DEG. L/R

       *WING RIGGING (AIRCRAFT LEVEL):             

                  DIHEDRAL: APPROX. 0.75 DEG.

                 AFTER SETTING DIHEDRAL, ADJUST STRUTS SUCH

         THAT THE TIP RIB IS AT SAME ANGLE AS ROOT RIB FOR

          EACH WING PANEL, THEN LENGTHEN REAR STRUT 1.5 TO

          2 TURNS OF ADJUSTING FORK TO SET TIP WASHOUT.

    

                                                  

                               

                                            

 

 

 

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