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FORMS 83 15. WEIGHTS (a) Weight of aircraft bare (including water in radiators).lbs. (b) Weight of fuel (tanks full).........................lbs. (c) Weight of oil (tanks full)............................lbs. (d) Weight of crew......................................lbs. (e) Weight allowed for operational equipment............lbs. (f) Maximum pay load authorized (when the fuel and oil tanks are full)......................................lbs. (g) Maximum total weight authorized (a) Landplane......lbs. (b) Seaplane........lbs. 16. DETAIL WEIGHT OF (a) Wing group........lbs. (b) Tail surfaces...........lbs. (c) Fuselage or hull....lbs. (d) Power plant............lbs. (e) Landing gear or floats................................lbs. (The total of this group should equal the weight of aircraft bare.) 17. Position of Centre of Gravity with full authorized load measured from the leading edge of the lower wing and from the centre line of thrust (a) Landplane .............................................. (b) Seaplane ............................................... 18. List of equipment including instruments. .................................................................................................................................................................................... 19. DIMENSIONS (a) Over-all span.. (b) Over-all length.. (c) Over-all height.. (d) Wing curve..... (e) Sweepback..... (f) Dihedral..... (g) Stagger.......... (h) Gap ............................. (i) Total wing area, including ailerons............. ........ 20. UPPER PLANE LOWER PLANE (a) Span ................. (a) Span ................... (b) Chord ................ (b) Chord .................. (c) Incidence ................ (c) Incidence ............... (d) Area, with ailerons.... (d) Area, with ailerons ...... (e) Auxiliary aerofoils..... 21. AILERONS (a) Number .............. (b) Arrangement ........... (c) Upper, length ......... Lower, length ............... Upper, chord .......... Lower, chord ................. Upper, area ........... Lower, area............. (d) Span of aileron balance. (e) Balance area............. (f) Total aileron area ..... 22. CENTRE SECTION (a) Dimensions ............. (b) Area .................