Sorry to respond to myself, but wanted to add some detail:

  Mass Properties Report (English units: lbf, in, slug-ft^2)
                                      Weight    CG-X    CG-Y    CG-Z
    Base Vehicle                      1500.0    41.0     0.0    36.5
0   Pilot                              180.0    36.0   -14.0    24.0
1   Co-Pilot                             0.0    36.0    14.0    24.0
2   Left Passenger                       0.0    70.0   -14.0    24.0
3   Right Passenger                      0.0    70.0    14.0    24.0
4   Baggage                              0.0    95.0     0.0    24.0
0   Fuel                                 100      56    -112    59.4
1   Fuel                                 100      56     112    59.4
                                                                                
                        
    Total:                            1880.0    42.1    -1.3    37.7

The CG-X arms should match what's in the TCDS and POH.

The propeller file also does not match between JSBSim and FlightGear. JSBSim 
has the same tables, but they were commented out and replaced with new 
tables.

Using a script I wrote to simulate a softfield takeoff technique[1], I see the 
following:

datafiles as they are in FGDATA:
Flaps 0%
Time   Speed   RPM    Height    Event
(s)    (knot)         (ft agl)
 0       0     1900         0   Brake Release
11      40     2332         0   Rotation
17      59     2430         0   Lift off
22      71     2525         8             
32      83     2621        84   456 fpm

Flaps 30%
Time   Speed   RPM    Height    Event
(s)    (knot)         (ft agl)
 0       0     1900        0   Brake Release
11      40     2330        0   Rotation
17      58     2423        0   Lift off
23      67     2500       14 
33      75     2565       90   492 fpm

Using JSBSim's IO-320 and Propeller
Flaps 0%
Time   Speed   RPM    Height    Event
(s)    (knot)         (ft agl)
 0       0     1900         0   Brake Release
 9      39     2500         0   Rotation
13      58     2600         0   Lift off
23      84     2800        50   Engine over red-line
33      98     2875       200   900 fpm

Flaps 30%
Time   Speed   RPM    Height    Event
(s)    (knot)         (ft agl)
 0       0     1900         0   Brake Release
 9      39     2500         0   Rotation
12      53     2600         0   Lift off
18      70     2680        15
23      77     2800       130   Engine over red-line
33      87     2830       216   516 fpm

[1] The aim of the script was to get off the ground asap then lower the nose 
to gain airspeed. It does not try to establish a best climb speed.


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