WACO AIRCRAFT COMPANY

MODELS:  Waco EGC-8 (Army UC-72B), 5 PCLB

T.C. NUMBER: 665

    Engine                    Wright R760E-2
    Placard limits            Maximum, except take-off
                              2200 rpm (320 hp)
                              Take-off (one minute)
                                2400 rpm (350 hp)
    Placard speeds            Level flight or climb - 158 mph True Ind.
                              Glide or dive - 213 mph True Ind.
                              Flaps extended - 100 mph True Ind.
    Fuel capacity             95 gallons (2 tanks, one in each wing at 47.5 gallons)
                                (-14)
    Oil capacity              6 gallons (-50)
    No. passengers            4 (front -13, rear +22)
    Baggage                   (Passenger type) 100 lbs. (+52)
                              (Cargo type) (See Item 210)
    Standard weight           3800 lbs.
    C.G. limits               (-18.0) and (-8.2)
    Datum                     Lower wing leading edge
    Leveling means            Lower surface upper wing at strut points
    Certification basis       Type Certificate No. 665
    Production basis          None (See NOTE A)
    Serial numbers            5051 and up per NOTE A and all AAF numbers eligible

    EQUIPMENT:
        (* Means net increase)

    Class I:
        101.  Engine ring cowl                          29 lbs.       (-73)
        102.  Landing lights (Grimes retractable)       11 lbs.       (-23)
        103.  Starter (direct electric)                 20 lbs.       (-55)
        104.  Generator (15 amp.)                       21 lbs.       (-55)
        105.  Battery (Exide 6TS-13-1)                  42 lbs.       (+23)
        106.  Wheel cuffs                                4 lbs.
        107.  7.50-10 wheels (Hayes 750M hydraulic)
              with 7.50-10 tubes and 8.50-10 tires)
              (wheels must be placarded for these
              tires)
        108.  10.5 inches streamline tail wheel or
              10x3 with H.D. tire
        109.  Throw-over type control column
        110.  Breeze engine shielding
        111.  Standard paint (gunmetal gray)
        112.  Oil cooler (Drawing 20965)
        113.  Heater and ventilator
        114.  Propeller - Hamilton Standard hub,
              2B20, blades 6109A-12. 6104A- 13,
              6135A-12 or 6135A 13. Diameter
              8'1/8" maximum, 7'9-7/8" minimum.         104 lbs.      (-88)

    Class II:
        200.  Miscellaneous items as noted on
              approved weight and balance report
        201.  Additional 25 gallon fuel tank installed
              under rear seat (including gage and
              wobble pump) (eligible as 4-place type
              only)                                     23 lbs.       (+48)
        202.  7-1/2 gallon oil capacity                               (-50)
        203.  Leather upholstery                        12 lbs.       (0)
        204.  Litter
              (a)  Air Corps type 24 lbs.                             (+72)
              (b)  Precision (carried in baggage
                   compartment as baggage)              25 lbs.
        205.  Parachute seats - rear                    41 lbs.*      (+27)
        206.  Extra door and wing walk                  16 lbs.*      (+19)
        207.  Larger generator                                        (-55)
        208.  Larger battery (Reading AR-9)              8 lbs.*      (+23)
        209.  Extra radio equipment between (-22)
              and (+25)
        210.  Cargo type with cargo compartment and
              large baggage door (See NOTE 2)
        211.  Propeller-
              Fixed metal - Curtiss 55503               72 lbs.       (-88)
        212.  Constant speed propeller governor and
              governor control installation (Waco
              Drawing 45907, pitch range 10 degrees
              to 23 degrees).  For installation with
              item 114.                                 10 lbs.       (-78)

    Class III:
        301.  Radio
              (a)  32 lbs. provided C.G. of instal-
                   lation is between (-22) and (+25)
              (b)  56 lbs. at (+ 25)
        302.  Special paint                         Maximum 45 lbs.*  (+17)
        303.  Miscellaneous extra instruments           40 lbs.*      (-43)
        304.  Pressure fire extinguisher
              (a)                                       15 lbs.       (-53)
              (b)                                       19 lbs.       (+7)
                                                      (tank under rear seat)
        305.  Tail wheel lock (neglect increase)

        306.  Flares (three 1-1/2 minimum electric)     17 lbs.*      (+78)
        307.  Parachute seats - front (Waco-Switlik     30 lbs.*      (-13)
        308.  "Y" type control column                    4 lbs.*      (-33)
        309.  Cactus proof tubes                        12 lbs.*      (-27)
        310.  Larger starter                                          (-55)
        311.  Vacuum pump                                4 lbs.       (-53)
        312   Wheel streamlines                         22 lbs.       (-27)

    NOTE A.  Each aircraft manufactured after 4/13/43, must, prior to original
        certification, satisfactorily pass:
        (a)  An inspection for workmanship, materials and conformity before any
             covering, metal priming or final finish is applied. All woodwork may
             be varnished.
        (b)  A final inspection of the completed aircraft.
        (c)  Check of flight characteristics.


    NOTE 1.  Eligible for export as follows subject to inspection for equipment
        specified in Chapter XII of Inspection Handbook:
         (a)  Canada
              - Landplane
              - Skiplane - not eligible.
         (b)  All other countries except New Zealand.

    NOTE 2.  Weight and balance report including list of equipment included in
        certificated weight empty, and loading instructions when necessary, must be
        submitted for each cargo type aircraft with original inspector's report and
        and each subsequent report covering changes in Class I or Class II equipment.