Re: W&B problem
DJ, see red text, this is a paste from the TCDS but I lost the formating so you may want to look for that text in the actual TCDS, I suspect your IA knows this. The oil not being counted isn't commonly known, nonetheless it is true
IV - Model BC12-D, 2 PCLM, Approved November 23, 1945; Model BCS-12D, 2 PCSM, Approved February 19, 1946
(Same as Model BC12-65 except for alternate tail surface, revised aileron travel, alternate one piece windshield and other
miscellaneous structural and non-structural changes). (Model BC12-D1 eligible as Model BC12-D when items 601 and 204
and 6 gal. right-hand wing tank are installed).
Engine Continental A-65-8 (see item 114(d) for optional engines)
Fuel 73 min. grade aviation gasoline
Engine Limits For all operations, 2300 r.p.m. (65 hp.)
Propeller Limits Static r.p.m. at full throttle: not over 2250, not under 2070.
No additional tolerance permitted.
Diameter: not over 72 in., not under 70 in.
Airspeed Limits Landplane: Level flight or climb 105 m.p.h.
(True Indicated) Glide or dive 140 m.p.h.
Seaplane: Level flight or climb 95 m.p.h.
Glide or dive 129 m.p.h.
Center of Gravity (C.G. Range) Landplane: (+14.2) to (+20.0)
Seaplane: (+14.2) to (+20.0) with Edo floats (item 205)
(+14.6) to (+20.0) with Heath floats (item 211)
Empty Weight C.G. Range Landplane: (+14.8) to (+17.9)
Seaplane: (+14.8) to (+18.3) with Edo floats (item 205)
(+15.2) to (+18.3) with Heath floats (item 211)
When empty weight C.G. falls within pertinent range, computation of critical fore and aftC.G. positions is unnecessary. Ranges are not valid for non-standard arrangements.
Maximum Weight Landplane: 1200 lb.
Seaplane: 1278 lb.
Number of Seats 2 (+23)
Maximum Baggage Landplane: 50 lb. (+40)
Seaplane: 30 lb. (+40)
Fuel Capacity 18 gal. (12 gal. fuselage tank at (-9) and 6 gal. wing tank at (+24). See NOTE 3.
Oil Capacity 4 qt. (-21)
Control Surface Movements Elevators Up 27o Down 25o
Elevator tab Up 25° Down 30°
Ailerons Up 23° Down 23°
Rudders Right 26o Left 26o
Serial No. Eligible 6402 and up
Required Equipment Landplane: 1, 2, 3, 4, or *8; 104, 108, 202, 203, 210(a), 401
Seaplane: 1, 3, 4 or *8; 104, 108, 205, 401
DJ, see red text, this is a paste from the TCDS but I lost the formating so you may want to look for that text in the actual TCDS, I suspect your IA knows this. The oil not being counted isn't commonly known, nonetheless it is true
IV - Model BC12-D, 2 PCLM, Approved November 23, 1945; Model BCS-12D, 2 PCSM, Approved February 19, 1946
(Same as Model BC12-65 except for alternate tail surface, revised aileron travel, alternate one piece windshield and other
miscellaneous structural and non-structural changes). (Model BC12-D1 eligible as Model BC12-D when items 601 and 204
and 6 gal. right-hand wing tank are installed).
Engine Continental A-65-8 (see item 114(d) for optional engines)
Fuel 73 min. grade aviation gasoline
Engine Limits For all operations, 2300 r.p.m. (65 hp.)
Propeller Limits Static r.p.m. at full throttle: not over 2250, not under 2070.
No additional tolerance permitted.
Diameter: not over 72 in., not under 70 in.
Airspeed Limits Landplane: Level flight or climb 105 m.p.h.
(True Indicated) Glide or dive 140 m.p.h.
Seaplane: Level flight or climb 95 m.p.h.
Glide or dive 129 m.p.h.
Center of Gravity (C.G. Range) Landplane: (+14.2) to (+20.0)
Seaplane: (+14.2) to (+20.0) with Edo floats (item 205)
(+14.6) to (+20.0) with Heath floats (item 211)
Empty Weight C.G. Range Landplane: (+14.8) to (+17.9)
Seaplane: (+14.8) to (+18.3) with Edo floats (item 205)
(+15.2) to (+18.3) with Heath floats (item 211)
When empty weight C.G. falls within pertinent range, computation of critical fore and aftC.G. positions is unnecessary. Ranges are not valid for non-standard arrangements.
Maximum Weight Landplane: 1200 lb.
Seaplane: 1278 lb.
Number of Seats 2 (+23)
Maximum Baggage Landplane: 50 lb. (+40)
Seaplane: 30 lb. (+40)
Fuel Capacity 18 gal. (12 gal. fuselage tank at (-9) and 6 gal. wing tank at (+24). See NOTE 3.
Oil Capacity 4 qt. (-21)
Control Surface Movements Elevators Up 27o Down 25o
Elevator tab Up 25° Down 30°
Ailerons Up 23° Down 23°
Rudders Right 26o Left 26o
Serial No. Eligible 6402 and up
Required Equipment Landplane: 1, 2, 3, 4, or *8; 104, 108, 202, 203, 210(a), 401
Seaplane: 1, 3, 4 or *8; 104, 108, 205, 401
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