- Holder
- The Waco Aircraft Company
- Revision
- 0
- Revised
- June 8, 1937
- Status
- Current
- Product
- Aircraft · Small Airplane
- Models
- 3
- Registered
- 14 aircraft
The release keeps the latest revision of each data sheet. Model names are as the data sheet lists them.
On this page
Models · 3
| Model | Also known as | Note |
|---|---|---|
| UKS-7 | ||
| VKS-7 (Army UC-72D) | ||
| VKS-7F |
Airworthiness directives · 1
ADs whose products are models on this data sheet, matched by model and maker.
Registered aircraft
Registry models that point at this data sheet, with their registered aircraft.
STCs approved under this data sheet · 6
STC SA04652CHTo allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specificationSTC SA01757WITo allow the use of UL91 or UL94 (minimum) grade aviation fuelSTC SA4503NMRemove original cloth covering and install Ceconite coveringSTC SA01831WITo allow the use of UL91 (minimum) grade aviation fuelSTC SA02033ATModification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.STC SA00680SEInstallation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.
What the data sheet saysOCR
This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.
MODEIS: Waco UKS-7, VKS-7 (Army UC-72D), VKS-7F
I.C._NUMBER: 648
I - Model UKS-7, 5 PCL-SB (Approved 6/8/37)
(Same as UKS-6, ATC 528, except wing fittings, landing gear moved forward 4 inches,
fixed trim tab added to rudder, miscellaneous changes in fuselage and controls)
Engine Continental W670K or W670K1
Fuel 65 minimum octane aviation gasoline
Engine limits Maximum, except take-off
(K) : or 2200 rpm (230 hp) (K1)
(one minute)
2175 pm (225 hp) (K) ; or 2200 Ipm (230 hp) (K1)
Airspeed limits
Glide or dive - 168 mph True Ind.
Propeller limits Maximum permissible diameter 102 inches
C. G. range Landplane (-14.4)
Maximum weight Landplane 3250 1ts.
No. seats
Maximum baggage 100 1bs. (+45)
Fuel capacity 70 gallons (two 35 gallon tanks in upper wing) (-11.5)
0il capacity 5 gallons (-44)
Control surface
movement Not available
Serial numbers eligible 4551 and up
Required equipment Landplane:
Iten 11819) 1192 1103(a), 104(a), 105(a), 106, 107, 108(a) ,
Seaplane:
101 (a), 102, 103 (a), 104 (a), 107, 108 (a).
110, 151.
II - MODEI VKS-7 (Army UC-72D), 5 PCI-SB (Approved 6/8/37)
(Same as UKS-7 except engine installation)
Engine Continental W670M or W670M1
Fuel 80 minimum octane aviation gasoline
Engine limits Maximum, except take-off
2200 rpm (240 hp) (M) ; or 2200 Ipm (250 hp) (M1)
Take-off (one minute)
2200 rpm (240 Fp) (M) or 2200 rpm (250 hp) (M1)
Airspeed limits Level flight or climb -
Glide or dive - 168 mph Irue
Propeller limits Maximum permissible diameter 102 inches
C.G. range Landplane (-14.4) to (-2.5
Maximum weight Iandplane 3250 1bs.
Maximum baggage 100 1bs. (+45)
Fuel capacity (two 35 gallon tanks in upper wing) (-11.5)
Control surface
Not avialable
Serial numbers eligible 4551 and up and all AAF numbers of Model UC-72D.
Use manufacturer's number when available.
Required equipment
Items 101 (a), 102, 103(a), 104(a), 105(a), 106, 107,
108 (a). 109,
Items 101 (a) . 102, 103 (a). 104 (a), 107, 108 (a).
III - MODEL VKS-7F, 5 PCIE (Approved 7/28/42)
(Same as VKS-7 except addition of split flaps on lower surface of upper wing,
Flettner rudder tab, miscellaneous changes to structure and control system)
Engine Continental W670M
Fuel 80 minimum octane aviation gasoline
Engine limits Maximum, except take-off
in. Hg.. 2200 IIm (240 hp)
Take-off (one minute)
-- in. Hg.. 2200 Ipm (240 hp)
Airspeed limits Level flight or climt - 140 mch True Ind.
Glide or dive - 168 mph True
Flaps extended - 102 mph True
Propeller limits Maximum permissible diameter 102 inches
C.G. range
Maximum weight 3250 1bs.
NO - seats 5 (2 at -3), (3 at +27)
Maximum baggage 1ks. (+45)
Fuel capacity 70 gallons (two 35 gallon tanks in upper wing) (-11.5)
Cil capacity 3-1/2 gallons (-44)
control surface
Not available
Serial numbers eligible Required equipment 5279 and 6101 and up 108 (a), 109, 110 a03 11; 10+ (b), 105 (b), 106, 107, 101(b).
SPECIFICATIONS PERTINENT TO ALL MODELS:
Datum Leading edge of lower wing
Leveling means Lower surface of upper wing at strut points must be
Certification basis Type Certificate No. 648 (Aero. Bulletin 7A)
Production basis
Export eligibliity ligitle for export as follows,
for equipment specified in MOp
- Seaplane (UKS-7 and VKS-7 only) - Maximum
weight 3430 1bs.
- Skiplane - Not eligible. However,
complies with Canadian requirements for
ski installation when equipped with special
(D) New debianouneries except hustralia and
EQUIPMENT:
Propellers and Propeller Accessories
108- Propeller - Curtiss Model 55501 -
Diameter 8'0" maximum, 7'10"
(Must be installed with blades
at right angles to engine crankthrow
(either 90 or 270 degree position).
Restrict engine operation to 2000 rpm
maximum and placard tachometer
Adjustable metal propeller +27 105- Ibs. (-79) (-79)
Hamilton Standard propeller,
blades 6135A-6 or 6135A-7.
Diameter 8'6-1/8" maximum, 8'3-7/8"
Pitch rarge 10 degrees
to 14.5 degrees.) (VKS-7F only) +51 1bs. (-79)
Engine and Engine Accessories - Fuel and Oil System
101. (a) Engine ring cowl 27 Ibs. (-63)
101 Or
(b) Engine ring cowl (Drawing 21992) 34 1bs. (-63)
(Eclipse F-80) 20 lbs. (-51)
5 lbs. (-65)
201. Large starter +10 1bs. maximum (-53)
cil heater 3 lbs.
15 gallon fuel tank (1 or 2 in lower
17 1bs. each
6-1/2 gallon oil tank (UKS-7 or
VKs-7 only) No weight change
5 gallon oil tank (VKS-7F only) No weight change
309. Engine shielding 11 Ibs. (-75)
Landing Gear and Floats
105. 7.50-10 wheels (Hayes 750M)
8.50-10 4-ply tires (Models
UKS-7 and VKS-7 only) 63 1bs. (-28)
320 or
105. (b) 7.50-10 4-ply tires 60 1bs. (-28)
106. 10x3 tail wheel 5 1bs. (+183)
109. Wheel cuffs 4 1bs. (-28)
111 Or
316. Wide type landing gear - tread
103-1/2 inches
151. Edo 38-3430 floats with water rudders
UKS-7 or VKS-7 only) *318 1bs. (-6)
213 or
301- Wheel streamlines 21 1bs. (-24)
skis (eligible on any airplane o]
chese models provided the propeller
installation meets the minimum 9 inch
ground ciearance. The maximum weight
for the skiplane will be the same as
for the corresponding landplane or
that showr. in parenthesis after each
ski model, whichever is less) Use actual weight change
(maximum 2500 1bs.)
302. Cactus proof tubes Tail wheel lock Neglect weight increase +5 1bs.
319. Steerable tail wheel (Drawing 22727
or Drawing 23143) +6 1bs. (+178)
Electrical Equipment
103. Generator
(a) Eclipse G-1 21 1bs. (-52)
(D) Eclipse G-2 21 Ibs. (-52)
104. (a) Battery - Reading ARL-11 35 lts. (-44)
Battery and box - Reading R-33-I 33 1bs. (-44)
202. Large generator + 6 1bs. maximum (-54)
214. Battery - Exide 6-TS-13 41 1bs. (-44)
308. Landing lights (Grimes retractable)
(UKS-7 or VKS-7) (+7)
(VKS-7F only) • 1bs. (-18)
Interior Equipment
110. control column - throw-over type 11 1bs. (-24)
205. Leather upholstering *12 lbs. (+7)
206. Litter installation +25. 1bs. (+97)
207. Rear parachute type seats
211. Sound proofing
303- "Y" type control column +3 1bs. (-24)
307. Flares
(a) Three 1-1/2 minute
(b) Five one minute
312. Cabin ventilators
314. Cabin heater (UKS-7 or VKS-7 only)
315. Front parachute type seats
318. Revised windshield (URA-7 or VKS-7 only)
Cabin heater (Models VKS-7 and VKS-7F
(Surface Combustion Co. Model
AGU-15N-L2) (See Waco Drawing 23719) *15 1bs. (+27)
vertical tail surface
(replacing landplane type)
+10 1ks. (+185)
Extra door and wing walk +16 Its. (+19)
Airbrakes (UKS-7 or VKS-7 only) +10 Its.
Bonding (VKS-7F only) 6 1bs. (-3)
NOTE A. Each aircraft manufactured subsequent to 1/11/49, must prior to origina!
certification, satisfactorily pass:
(a) An inspection for workmanship, materials and conformity during
construction.
(D) A final inspection of the completed aircraft.
(c) check of flight characteristics.