I just recently purchased a kr2 that was started in 1984. It is complete
up to weight and balance and seems to have very good workmanship. The
engine is a modified  revmaster. With the following information I am
trying to calculate if I infact have an increased Gross Weight
considering the increased wing span and increased HP?

Engine                  2100D- 75hp. vs factory 2100 -65hp
wing span                            23-8 vs factory 20-8
Length                                15-4 vs  factory 14-6 (includes
spinner)
Total wing area            ?___         vs factory 78s/f
Empty weight                   659lbs  vs factory 480
Gross weight                     ?___    vs factory 900 lbs
Usefull load                     ?___     vs factory 420lbs

_MFG NOTES;_
Wingloading        11.5 lbs/sq.ft
Power Loading    13.9 lbs/hp
Gross Weight      _/* 900 lbs*/_


_Weight and balance_
factory;  +4/-4 inches from aft of main spar at wing root
              8 to 16 in aft of L/E
Actual;
Datum @ firewall
Spar @    24in  to 26.25 in
Fwd c/g   21.4in   Aft c/g 29.4
Empty Weight   659 lbs
Empty weight cg  18.9in
Full fuel header tank weight   731 lbs
Full Fuel c/g w/out pilot     18.99"
Pilot #1 w/out fuel  23.54in ,     W/12gal. fuel 23.75
Pilot #2 w/out fuel  24.21in,      W/12gal. fuel 23.38
Main Wheels C/L    82-1/2"

Fixed gear tail drager with 7" pneumatic tire.

_Wing;_
124"length x 50" i/b x30" o/b
       124 x 30= 3720 +{(124x20~2)=1240}=3720+1240=4960x2 wings
=9920~144"= 68.9 S/F.
       Why does this not calculate above  mfg 78s/f ??? What don't I
see?  Try another way,
Alternate figure; figure added lenght to each wing tip;;
       18"x30"= 540"x 2 wing tips= 1080~144= 7.5 S/F, add to factory 78=
85.5 s/f
       85.5 x 11.5 factory wing loading=/_ *983 LBS*_ = 83 lbs i/ncrease
in gross weight !!???
Maybee I need to add Horz stab surface to first calculations or maybee
lower fuselage area between wings?
       stab and elevator;
       35 1/2"x 26 I/B x 22 1/2 O/B calculates to 7.5 S/F
       7.5s/f  + calculated wing area of 68.9 s/f = 76.4s/f  ( still
less than factory 78)

_Engine._
       75h/p x 13.9 lbs/hp =_*/1042 lbs/* _gross weight capabilities???

WHAT IS MY CORRECT GROSS WEIGHT SO I CAN FLY WITH PILOT #1 @ 170 lbs
AND PILOT #2 @ 212 Lbs =382 LBS +730 lbs =/ /*_/1112 lbs/ _*w/out baggage ?

Thank You in advance
Keith and Brent Wiese









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