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General Weight Summary Format

In general the weights reported in the references listed above fall into a  "Weight Breakdown Structure" similar to the one shown below shown below, with a few small exceptions, as discussed below.

In general

Basic Mission Gross Weight = Basic Empty Load + Useful Loads
Maximimum Gross Weight = Basic Mission Gross Weight + Additional Loads

Where

Basic Empty Weight
- is the sum of Groups 1 through 3 below
  1. Structural Weight
  1. Power Plant Weight
  1. Fixed Systems & Equipment

Useful Loads - is the sum of items 1 through 7 below
  1. Crew
  2. Equipment
  3. Oil
  4. Fuel
  5. Radio/Communications Equipment (if not included in the Fixed Equipment Group)
  6. Armament, including both
  1. Other Useful Load Items
Additional Loads - is equal to the some of Items 1 through 4 below
  1. Additional Fuel (including Drop Tanks)
  2. Additional Optional Armament, including both
  1. Additional Optional Bombs, Torpedoes and/or Rocket Loadouts
  2. Additional Other Miscellaneous or Special Load Items

Caveats/Comments

  1. For a few aircraft (primarily early war or pre-war types) Electronics/Communications systems (such as radios) were identified as part of the useful load instead of as part of the Fixed Systems & Equipment weight group.  I will try and highlight such instances in the analyses of the data and parametric plots developed.
  2. It is currently unclear what all is included in the "Engine Section" weight group.  For most of the aircraft it appears that this includes the the engine mounts as well as cowling and cooling flaps for aircraft with radial engines. However for a few aircraft such as the XP-63A a very low value of 4lb is given, while for the P-63A-10 and P-63C no value is given, leading to the suspicion that the weights of the enine mount for those aircraft may be included elsewhere in the weight estimate (such as in the "Fuselage" weight or "Engine Accessories" weight groups.
  3. It appears that "Fuselage" weight is equal to the sum of the "Body" and "Engine Section" weight groups.  However for the weight listed in Ref [1] for several of the Brewster F2A and B339 variant aircraftit appears that the "Landing Gear'weight group has been included with the "Body" weight group. As such I have included a row for "Body + LG" in the tables below, that I intend to populate for the other aircraft types soon, to allow for a comparison between the reported weights for those Brewster Aircraft and the other aircraft in the tables.  Similarly, for the XF2A-1 listing from Ref [1] it appears that the wiht listed for the "Body" group also includes the "Enine Section" weight in addition to the "Landing Gear" weight, so a line has also been added to the table for "Body + Engine Section + LG" as well.
  4. For a few aircraft Turbocharger and Watr Injection weights are listed separately, whereas it it appears that for some other aircraft listings (which are known to have these systems) these values may be included in the Engine (As Installed) or Engine Accessories weight groups.
  5. For a few aircraft Anti-Icing systems weights are listed separately, whereas it is indicated in some of the references that this weight is included in the Furnishings weight group.
Notes: This website has been developed with a number of low cost or free programs including Hot Metal Pro, KompoZer, Microsoft Designer and Da Button Factory.com

Rev 2-18-25

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