The
Waco E series
is a small family of
American
-built cabin
biplanes
built between 1939 and 1942, which differed primarily by engine installation.
Development and design
edit
The
E series
was the final development of the prewar Waco line of biplane designs. A full four-seater, it had the best performance of any of the Wacos. First flown in 1939, it had a much slimmer and more streamlined
fuselage
than earlier Waco C and S models and heavily
staggered
unequal-span parallel-chord
wings
with rounded tips. Wings were plywood-skinned, and also had wire cross-bracing between the wings in place of the solid
struts
used on previous models.
[3]
Engines varied in power from 285 to 450?hp (213 to 336?kW), giving the E series a high cruising speed for the period of up to 195?mph (314?km/h).
[4]
Production ceased in 1942.
Note
: the
Waco GXE
of 1929/30 was an unrelated biplane design with non-staggered wings
The E series was sold to wealthier private pilot owners who required the comfort of a fully enclosed cabin and a high cruising speed, combined with a longer range. Because of the type's good performance, 15 examples were impressed by the
United States Army Air Forces
during
World War II
for communications work as the
UC-72
. Several of the USAAF examples were returned to civilian use after the end of the war and five E series aircraft remained airworthy in 2001.
[5]
WACO ARE
Waco SRE impressed as USAAF UC-72
(Source?: Aerofiles)
- ARE Aristocrat
- 300?hp (224?kW)
Jacobs L-6
(4 built, one impressed as UC-72A)
- HRE Aristocrat
- 285?hp (213?kW)
Lycoming R-680
(5 built, 2 impressed as UC-72C)
- SRE Aristocrat
- 400?hp (298?kW)
Pratt & Whitney R-985 Wasp Junior
SB-2 (21 built, 12 impressed as UC-72)
- WRE Aristocrat
- 420?hp (313?kW)
Wright R-975
- model offered to potential customers, but none built
- UC-72
- 12 impressed Waco SRE for USAAF
- UC-72A
- One impressed Waco ARE
- UC-72C
- Two impressed Waco HRE
Specifications (SRE)
edit
Data from
Simpson p. 576
General characteristics
- Crew:
1 pilot
- Capacity:
3 passengers
- Length:
27?ft 10?in (8.48?m)
- Wingspan:
34?ft 9?in (10.59?m)
- Height:
8?ft 8?in (2.64?m)
- Empty weight:
2,734?lb (1,240?kg)
- Max takeoff weight:
4,200?lb (1,905?kg)
- Powerplant:
1 × Pratt & Whitney R-985 SB-2 nine-cylinder radial air-cooled piston, 400?hp (300?kW)
Performance
- Maximum speed:
202?mph (325?km/h, 176?kn)
- Cruise speed:
195?mph (314?km/h, 169?kn)
- Stall speed:
57?mph (92?km/h, 50?kn)
- Range:
1,070?mi (1,720?km, 930?nmi)
- Service ceiling:
23,500?ft (7,200?m)
- Rate of climb:
1,550?ft/min (7.9?m/s)
Aircraft of comparable role, configuration, and era
Related lists
- ^
Aerofiles
- ^
Green p.306
- ^
Simpson p. 576
- ^
Simpson p. 576
- ^
Simpson p. 576
- Green, William, The Aircraft of the World, 1965, MacDonald & Co (Publishers) Ltd, ISBN none
- Simpson, Rod, Airlife's World Aircraft, 2001, Airlife Publishing Ltd,
ISBN
1-84037-115-3