Standard Aircraft Company / Dayton-Wright / Fisher Body / Wright-Martin - USA
Manufacturer(s)
United States (retired)
Operators
1917
Service Year
United States
National Origin
Retired
Project Status
2
Crew
1,605
Units
COMMERCIAL AVIATION
Used in roles serving the commercial aviation market, ferrying both passengers and goods over range.
INTELLIGENCE-SURVEILLANCE-RECONNAISSANCE
Surveil ground targets / target areas to assess environmental threat levels, enemy strength, or enemy movement.
TRAINING
Developed ability to be used as a dedicated trainer for student pilots (typically under the supervision of an instructor).
26.6 ft
(8.10 meters)
Length
44.0 ft
(13.40 meters)
Width/Span
10.8 ft
(3.30 meters)
Height
1,356 lb
(615 kilograms)
Empty Weight
1,951 lb
(885 kilograms)
Maximum Take-Off Weight
+595 lb
(+270 kg)
Weight Difference
1 x Hall-Scott A-7 air-cooled engine developing 100 horsepower and driving two-bladed wooden propeller at the nose.
Propulsion
68 mph
(109 kph | 59 knots)
Max Speed
5,807 ft
(1,770 m | 1 miles)
Ceiling
351 miles
(565 km | 305 nm)
Range
260 ft/min
(79 m/min)
Rate-of-Climb
MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030