Hi yall ;D
I add'it a center fuel tank to a Boeing 377 Stratocruiser.
I need to increas the max fuel weight, or do I need to increas the max_gross_weight in the aircraft cgf. I'm not sher wich of the numbers I need to work with. Well heres how the weight figers look in the aircraft cgf.
[fuel]
max fuel 9000 USG=46,740lbs @ 6.0lbs/USG
LeftMain=0,-15,0,3895,0
RightMain=0,15 ,0,3895,0
Center1=0.05, 0.0, 0,2500, 60
fuel_type=1.000000
number_of_tank_selectors=3
electric_pump=1
[WEIGHT_AND_BALANCE]
;load assumed symetrical versus CoG
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
max_number_of_stations = 50
empty_weight=83860 ;inc galley, toilets, catering etc
station_load.0= "2000,0,0,0, 10 Crew & Bags"
station_load.1= "4760,30.0,0,0, 28 Pax (33 max)" ;@ 170 lbs
station_load.2= "4760,-30.0,0,0, 28 Pax (33 max)" ;@ 170 lbs
station_load.3= "840,15,0,0, Fwd Bags&Cargo" ; @ 30 lbs
station_load.4= "840,-15,0,0, Aft Bags&Cargo" ; @ 30 lbs
//station_load.1=13200,0,0,0 ;66 pax with bags = max payload with full tanks. Applies to B377-10-32 operated by BOAC and all B377s after resale to second hand users so this is the default payload
\\station_load.1=12200,0,0,0 ;61 pax with bags. Applies to B377-10-30 as flown by NWA and most B377-10-26 as flown by PAA, but see separate aircraft.PAA for the B377-10-26 Super Stratocruiser
\\station_load.1=12000,0,0,0 ;60 pax with bags. Applies to B377-10-29 as flown by AOA and PAA
\\station_load.1=11000,0,0,0 ;55 pax with bags. Applies to B377-10-34 as flown by UAL and B377-10-32 as ordered by SAS but delivered to BOAC
\\station_load.1=14400,0,0,0 ;Max payload as flown by RANSA after full cargo conversion
station_load.5 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.6 = "0.0, 0.0, 0.0, 0.0, FsStation"
Max take off weight=147,000 ;later increased to 147,000 after full cargo conversion
147,000 - 46740 fuel = 99060 and 99060 - 83860 = 15200 / 200 = 76 SOB
Default ramp weight is 147,000lbs with max fuel and weight limited payload
Max landing 129,000 ;later increased to 129,000 after full cargo conversion - some RANSA aircraft only
Moments of Inertia
empty_weight_roll_MOI=625000
empty_weight_pitch_MOI=900000
empty_weight_yaw_MOI=1700000
empty_weight_coupled_MOI=0.0
max_gross_weight=147,000
Thanks for any input on this mater.








