| Consolidated | Reference Source | Notes | ||
| PB-2A | ||||
| No of Crew | 2 | 8 | ||
| Engine: | ||||
| Qty | 1 | 2 | ||
| Model | V-1570-61 | 2 | ||
| Displacement | (cu in) | 1570 | 8 | |
| Power | ||||
| Military | (HP) | |||
| War Emergency | (HP) | |||
| Normal | (HP) | |||
| Take Off | (HP) | 700 | 5 | |
| Eng Dims | ||||
| Length | (ft) | |||
| Width/Dia | (ft) | |||
| Height | (ft) | |||
| Base Engine Wt | (lb) | 1040.76 | 5 | |
| Propeller | ||||
| # Blades | 3 | 8 | ||
| Dia | (ft) | |||
| Manufacturer | Curtiss (Elec) | |||
| Type | Variable Pitch | |||
| Wing | ||||
| Span | (ft) | 43.9 | 2 | |
| Root Thickness | (%) | 18.0% | 2 | |
| (in) | 19.7 | 2 | ||
| Total Area | (sq ft) | 297 | 2 | |
| Wing (less Ailerons & Flaps) | (sq ft) | |||
| Ailerons | (sq ft) | |||
| Flaps | (sq ft) | |||
| Tail Area | (sq ft) | 58.8 | 3 | NACA Research Memorandom L7E15 |
| V Tail Area | (sq ft) | 18.7 | 3 | NACA Research Memorandom L7E15 |
| Fin | (sq ft) | |||
| Rudder | (sq ft) | |||
| H Tail Area | (sq ft) | 40.1 | 3 | NACA Research Memorandom L7E15 |
| Stabilizer | (sq ft) | |||
| Elevator | (sq ft) | |||
| Total Control Surf Area | (sq ft) | |||
| Length | ||||
| Overall | (ft) | |||
| Fuselage | (ft) | 29.5 | 2 | |
| Body | (ft) | 28.16 | ||
| Body Depth | (ft) | |||
| Body Width | (ft) | |||
| Fuel Tank Volume | (gal) | |||
| Wing Tanks | (gal) | |||
| FuselageTanks | (gal) | |||
| Oil Tank Volume | (gal) | |||
| Water Injection Tank Volume | (gal) | |||
| Wetted Area (sqf) | (sq ft) | |||
| Pwr Ldng | (lb/HP) | 7.97 | 2 | |
| Wing Ldng | (lb/sq ft) | 17.5 | 2 | |
| Struct. Des. GW | (lb) | |||
| Ultimate Load Factor | (G's) | |||
| Design Speed | (mph) | |||
| Not to Exceed Speed | (mph) | |||
| Total Struct Weight | 1902 | 2 | ||
| Total Wing | 900 | 2 | ||
| Wing (less Ailerons & Flaps) | ||||
| Ailerons | ||||
| Flaps | ||||
| Fuselage Carry-Through | ||||
| Tail | 125 | 2 | ||
| H Tail | 86 | 2 | ||
| Stabilizer | ||||
| Elevator | ||||
| V Tail | 39 | 2 | ||
| Fin | ||||
| Rudder | ||||
| Body + Eng Section + LG | ||||
| Body + LG | 817 | |||
| Body | 534 | 2 | ||
| Fuselage | ||||
| Engine Section | ||||
| Landing Gear | 343 | 2 | ||
| Mn Landing Gr | 316 | 2 | ||
| Tail/Nose Aux LG | 27 | 2 | ||
| Tail Hook | ||||
| Booms | ||||
| Nacelles | ||||
| Total Propulsion Weight | 1917 | 2 | ||
| Engine w/ Accessories | 1247 | 2 | ||
| Engine(s) as Installed | 1032 | 2 | ||
| Accessories | 215 | 2 | ||
| Turbocharger(s) | ||||
| Controls | 12 | 2 | ||
| Propeller(s) | 291 | 2 | ||
| 2-Blade | ||||
| 3-Blade | 291 | 2 | ||
| 4-Blade | ||||
| Starting System | 35 | 2 | ||
| Water Injection System | ||||
| Tanks | ||||
| Piping Etc | ||||
| Cooling System | 201 | 2 | ||
| Lube System | 24 | 2 | ||
| Tanks | ||||
| Piping Etc | ||||
| Fuel System | 107 | 2 | ||
| Tanks | ||||
| Piping Etc | ||||
| Total Sys. & Eqpmt. | 413 | 2 | ||
| Instruments | 30 | 2 | ||
| Surface Controls | 83 | 2 | ||
| Hydraulics | ||||
| Electrical Equip | 75 | 2 | ||
| Electronics | ||||
| Arm Prov/Equipment & Armor | ||||
| Furnishings | 225 | 2 | ||
| Anti-Ice (If not in Furn) | ||||
| Other /Misc | ||||
| Hoisting Gear | ||||
| Floatation Gear | ||||
| Empty Wt | 4232 | 2 | ||
| Basic Mission Useful Load | 1347 | 2 | ||
| Crew | 400 | 2 | ||
| Equipment | ||||
| Oil | 45 | 2 | ||
| Fuel | 540 | 2 | ||
| Fuel & Oil Trapped in Systems | ||||
| Water for Engine Injection | ||||
| Bombs/Torp Etc | ||||
| Radio (if Not in Empty Wt) | ||||
| Nav Equipment | ||||
| Oxygen System | ||||
| Armament | 206 | 2 | ||
| Guns & Ammo | 206 | 2 | ||
| Guns | 63 | 2 | ||
| Ammo | 143 | 2 | ||
| Pyrotechnics | ||||
| Camera | ||||
| Other | ||||
| Other Useful Load | 156 | 2 | ||
| Basic Mission GW | 5579 | 2 | ||
| Additional Loads | ||||
| Fuel | +540 | 2 | ||
| Bombs Etc | +170 | 2 | ||
| Guns | ||||
| HVA Rockets | ||||
| Max Useful Load | 1907 | Calculated from data in Ref [2] | ||
| Max GW | 6200 | Calculated from data in Ref [2] | ||
| Additional Load Notes | 90 gal in Wing Tanks | 2 | ||
| 10 x 17lb Bomb | 2 |
