WACO AIRCRAFT COMPANY

MODELS:  Waco UKC, UKC-S, UKS-6, VKC, VKC-S, VKS-6

T.C. NUMBER:   ATC 528

I - SPECIFICATIONS PERTINENT TO ALL MODELS

     Fuel                     50 gallons (two 25 gallon tanks in upper wings)
     Oil                      4 gallons
     No. passengers           3 or 4 (See NOTE 3)
     Baggage                  Landplane 100 lbs. (including tools 14 lbs.)
       (See NOTE 3)           Seaplane 109 lbs. (including anchor, rope and tools
                                carried under passenger seats:
                                35 lbs. with P-3300 floats and
                                25 lbs. with 38-3430 floats)
     Standard weight          Landplane 2850 lbs. (serials 3838 to 3855);
                                3000 lbs. (Serials 3856 and up) (See NOTE 4);
                                3250 lbs. (See NOTE 4)
                              Seaplane 3250 lbs.
     C.G. limits              Landplane (-14.4) and (-2.4)
                              Seaplane (-12.7) and (-3.7)
     Datum                    Lower wing leading edge
     Leveling means           Lower surface upper wing at strut points
     Serial numbers           3638 and up manufactured to 9/30/39 eligible.
                                Approval expired as of that date.

     EQUIPMENT:
         (* Means net increase)

     Class I:
     Landplane:
         101.  Engine ring cowl                         23 lbs.
         102.  Starter (Heywood)
         103.  Heater
         104.  Battery                                  10 lbs.
         105.  8 inch streamline tail wheel
         106.  6.50-10 wheels (Autofan) with
               7.50-10 tires (wheels must be
               placarded for these tires)
         107.  Wing root fairing
         108.  Propeller - wood                         42 lbs.

     Seaplane:  (Items 101 to 104 and 107 PLUS)
         151.  Edo P-3300 or 38-3430 floats with
               water rudders
         152.  Seaplane type fins (upper per Drawing
               19261 and fin underneath fuselage per
               Drawing 19262) and rudder per Drawing
               19484
         153.  Air brakes                               10 lbs.
         154.  Propeller - adjustable metal

     Class II:
         200.  Miscellaneous items as noted in
               approved weight and balance report
         201.  Miscellaneous radio equipment (in
               excess of Item 316)
         202.  Ambulance equipment (litter)             12 lbs.

     Class III:
         301.  Landing lights (Grimes retractable)      11 lbs.
         302.  Wheel streamlines                        24 lbs.
         303.  Propeller
               (a)  Adjustable metal                    29 to 37 lbs.* (-79)
               (b)  Fixed metal                         10 lbs.*      (-79)
         304.  Flares
               (a)  Three 1-1/2 minute                  17 lbs.       (+70)
               (b)  Five 1 minute                       13 lbs.       (+70)
         305.  Fuel tank installations
               (a)  70 gallon capacity (one 35 gallon
                    tank in each upper wing)            18 lbs.*
               (b)  100 gallon capacity (landplane
                    only) (one 35 gallon tank in each
                    upper wing and one 15 gallon tank
                    in each lower wing)                 53 lbs.*
         306.  5 or 6-1/2 gallon oil tank              No change in weight
         307.  Shielding                                11 lbs.
         308.  Air Brakes (flaps)                       10 lbs.
         309.  Miscellaneous extra instruments
         310.  Engine crankcase cooling disc
               (mounted on forward part of
               engine crankcase)                         3 lbs.
         311.  Paint
               (a)  Black and vermillion (over
                    gunmetal grey, aluminum or blue)    30 lbs.*
               (b)  White and French grey (over gun-
                    metal grey, aluminum or blue)       45 lbs.*
         312.  7.50-10 cactus proof tubes               10 lbs.
         313.  Tail wheel lock
         314.  Extra door and wing walk                 16 lbs.
         315.  "Y" type control column                   5 lbs.*
         316.  Radio (30 lbs. provided C.G. of instal-
               lation is between rear seat and
               instrument board)

     NOTE 1.  Eligible for export as follows, subject to inspection for equipment
         specified in Chapter XII of Inspection Handbook (4/7/37):
         (a)  Canada
              - Landplane
              - Skiplane - not eligible.  However, structure complies with Canadian
              requirements for ski installation when special landing gear per Waco
              Drawings 20496 and 20497 is installed.
              - Seaplane - serial numbers 4265 and up.  Maximum standard weight
                3250 lbs.
              - Amphibian - not eligible.
         (b)  Great Britain provided wing spar root fittings are reinforced, upper
              and lower wing rear spar reinforcement extended and the rear interplane
              struts increased in size in accordance with approved technical data
              (manufacturer's affidavit required).
         (c)  All other countries except Australia.

     NOTE 2.  All airplanes eligible as amphibian type provided weight and balance
         report including list of equipment included in certificated weight empty,
         and loading instructions when necessary, is submitted for each aircraft
         with original inspector's report and each subsequent report covering changes
         in such equipment.

         Standard weight      3300 lbs.
         C.G. limits          (-9.0) and (- 4.5)

         Class I equipment:
             Seaplane type fins (upper per Drawing 19261 and fin underneath fuselage
         per Drawing 19262) and rudder per Drawing 19484; Edo 49-3800 floats; other
         equipment included in weight and balance report.

     NOTE 3.  Five-place airplanes must have:
         (a)  Additional safety belt installed on rear passenger seat.
         (b)  Baggage capacity reduced to 75 lbs. unless actual weight and balance
              shows a lesser restriction necessary.

     NOTE 4.  Serial numbers 3856 and up eligible at standard weight of 3250 lbs.
         with the following:
         (a)  Landing gear per Waco Drawing 20497 and structural changes outlined in
              pages 8 and 9 of Waco Report 383.  (These changes incorporated at
              factory on serial numbers 4268 and up.)
         (b)  (1)  wing spoilers or
              (2)  Large size UMF vertical tail surfaces (rudder height
                   58-9/16 inches.)

     NOTE 5.  Yearly models:
             1934 UKC or VKC
             1935 UKC-S or VKC-S
             1936 UKS-6 or VKS-6
         In the case of the 1936 designation:
             First letter shows engine
             Second letter shows wing
             Third letter shows type
             Number indicates year.

II - MODELS UKC, UKC-S, UKS-6, 4 or 5 PCL-S-AmB

   Engine                     Continental R-670A (R-670, C, E or G)
   Placard limits             Maximum, except take-off
                                -- in. Hg., 2000 rpm (210 hp)
                              Take-off (one minute)
                                -- in. Hg., 2000 rpm (210 hp)

III - MODELS VKC, VKC-S, VKS-6, 4 or 5 PCL-S-AmB

    Engine                    Continental R-670B (R-670D, F or H)
    Placard limits            Maximum, except take-off
                                -- in. Hg., 2000 rpm (225 hp)
                              Take-off (one minute)
                                -- in. Hg., 2000 rpm (225 hp)