- Holder
- The Waco Aircraft Company
- Revision
- 0
- Status
- Current
- Product
- Aircraft · Small Airplane
- Models
- 3
- Registered
- 4 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 |
|---|---|---|
| CUC-1 | ||
| CUC-2 | ||
| CUC |
Airworthiness directives · 0
ADs whose products are models on this data sheet, matched by model and maker.
No ADs matched this data sheet’s models
Registered aircraft
Registry models that point at this data sheet, with their registered aircraft.
STCs approved under this data sheet · 9
STC SA04652CHTo allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specificationSTC SA4503NMRemove original cloth covering and install Ceconite coveringSTC SA2693NMInstallation of Electronics International digital volt/amp gauges and accessories.STC SA02033ATModification to install an air-oil separator to prevent oil from being aspirated from the engine breather line.STC SA8075SWInstallation of fiberglass covering. (M-62 SERIES PT-19) (G-73 SCHWEIZER)STC SA2687NMInstallation of Truboplus/ Electronics Int'l gauges and switches.STC SA2350NM PAGE 2Installation of Electronics International Inc digital carburetor/outside air temperature gaugesSTC SA2190NM PAGE 2Installation of electronics International Digital Volt/Amp Gauges and Accessories.STC SA2350NMInstallation of Electronics International Inc digital carburetor/outside air temperature gauges listed on the attached continuation sheet and the associated accessories.
What the data sheet saysOCR
This is OCR from the scanned FAA data sheet. OCR can misread letters and numbers.
MODEIS: Waco CUC, CUC-1, CUC-2, 5 PCIB
I.C. NUMBER: ATC 575
I - SPECIFICATIONS PERTINENT TO ALL MODELS
Placard speeds Level flight or climb - 158 mph True Ind. Glide or dive - 214 mph True Ind.
Flaps extended - 112 mph True Ind.
Fuel capacity 70 gallons (two tanks in upper wirgs at 35 gallors)
oil capacity 5 gallons
No. passengers 4 maximum (See NOTE 2)
Laggage (See NOTE 2)
Maximum weight 3200 1bs. (See NOTE 3 for 3350 Ibs.)
C.G. limits
Catum Iower wing leading edge
Leveling means Lower surface upper wing at strut points
Specification basis Approved Type Certificate No.
Serial numbers 3951 and up manufactured prior to 9/30/39 eligirle.
Approval expired as of that date.
EQUIPMENT:
(* Means net increase)
Class I:
101. Engine ring cowl
Battery (under rear seat) 40 1bs.
103. Starter (direct electric) 26 lts.
104. Generator 12 1hs.
105. 6.50-10 wheels and 8.50-10 4-ply
tires (wheels must be placarded
for tires as noted)
106. 10.5 inch streamline tail wheel
107. Throw-over type control column
108. Upper wing flaps - electrically or
109. Propeller
wood - fixed or adjustabie pitch
(Models CUC and CUC-1) 46 Irs.
Controllable metal (Hamilton
Standard, 2B20 hut, 6109A-12 OI
6135A-1 blades (Model CUC-2) 105 Its.
Miscellaneous items as noted in
approved weight and balance report.
Class III:
301. 95 gallon fuel capacity (two tanks at
gallons each) and 6-1/4 gallon
oil capacity 8 lts. *
302. Landing lights (retractable) 11 lbs.*
303. 1-1/2 minute) 17 1bs. *
304. Leather upholstery 1bs. *
305. Litter installation 14 ibs.
306- Radio and shielding 45 1bs.
307. Special paint
308. Miscellaneous extra instruments
309. Propellers
(a) Fixed metal (Curtiss 55501) 51 1bs.
(b) Adjustable metal 86 1bs.
(c) Controllable metal (Hamilton
Standard 2B20 hut, blades 6109A-9
or 6135A-9) (Models CUC and CUC-1) 105 1ts.
(d) Eclipse automatic metal 125 1bs.
310- "y" type cortrol column 4 1bs. *
311. Aileron tab installation No change in weight
312. Large elevators (Drawing number 32305) No change in weight
313. Heater and ventilator
314. wheel streamlines 21 1bs.*
315. Extra door and wing walk 16 1bs.
NOTE 1. figible ror export as follows subject to inspection for equipment
specified in Chapter XII of Inspection Handbook (1/10/39)
Canada
- Landplane
- Skiplane - not eligible
(b) All other countries except Great Britain and Australia.
NOTE 2. Five-place airplanes must have:
(a) Additional safety belt installed on rear seat.
(b) Baggage compartment placarded as follows unless actual weight and
balance shows a lesser restriction necessary:
"Maximum allowable 100 1bs.
Maximum with 3 passengers on rear seat 0 lbs."
NOTE 3. Standard weight in excess of 3200 1bs. (maximum 3350 1hs.).
(a) Controllable metal or automatic metal propeller must be installed.
(₺) Serial numbers 4326 and up are eligible. (These airplanes have revised
interplane strut fitting, landing gear and certain members of the
fuselage structure.)
serial numbers 3951 thru 4325 are eligible upon receipt of manu-
facturer's affidavit that pertinent airplane has been reinforced in
accordance with approved technical data. (Serial numbers 4304, 4309,
4312, 4313, 4314. 4316 and "319 have been so reinforced.)
NOTE 4. Models CUC-1 and CUC-2 same as model CUC except engines. Model COC-1
approximately 20 ibs. heavier than model CUC, and modei CUC-Z approxımatel
lbs. heavier than model CUC. Al1 CUC-2 airplanes must have:
one-half inch fuel line and fittings installed between strainer and
(b) Placard displayed in fuel valves stating: "Always use both tanks for
take-off and for flight at low altitudes."
Inspector's report should include notation that above requirements are
complied with.
II - MODEI CUC, DESIGNATION 5 PCLB (See NOTES 2 and 4)
Engine Wright R760E
Placard limits Maximum, except take-ofi
-- in.Hg.. 2000 rpm (250 hp)
Take-oti (one minute)
-- in. Hg.. 2000 rpm (250 hp)
III - MODEL CUC-1, DESIGNATION 5 PCLE (See NOTES 2 and 4)
Engine Wright R760E-1
Placard limits Maximum, except take-off
27 in. Hg.. 2100 rpm (250 hp)
Take-off (one minute)
-- in.Hg.. 2100 rpm (285 hp)
IV - MODEL CUC-2, DESIGNATION 5 PCLB (See NOTES 2 and 4)
Engine Wright R760F-2
Placard limits Maximum, except take-off
29.5 in.Hg.. 2200 rpm (250 hp)
(one minute)
-- in.Hg.. 2400 rpm (350 hp)