F-35A Lightning II
Overview
The F-35A Lightning II is a military aircraft manufactured by Lockheed Martin, with the profile centered on its ctol stealth fighter role. Its recorded first flight is 2006-12-15. The current production-status field is listed as In Production. The listed crew requirement is 1. Power is provided by 1 Pratt & Whitney F135 engine. Recorded dimensions include length 51 ft 4 in, wingspan 35 ft, height 14 ft. Maximum takeoff weight is listed as 70,000 lb. Listed performance includes maximum speed Mach 1.6 kt, range ~590 nm combat radius nautical miles, service ceiling 50,000 ft. Its ICAO type designator is F35A. Figures shown here describe the listed type or configuration and may vary by sub-variant, certification basis, or operator fit.
Quick Facts
Specifications
| ICAO Type Code | F35A |
|---|---|
| Military Designation | F-35A |
| First Flight | Dec 15, 2006 |
| Crew | 1 |
| Length | 51 ft 4 in |
| Wingspan / Rotor Diameter | 35 ft |
| Height | 14 ft |
| Max Takeoff Weight | 70,000 lb |
| Max Speed | Mach 1.6 |
| Range | ~590 nm combat radius |
| Service Ceiling | 50,000 ft |
| Engine Manufacturer | Pratt & Whitney |
| Engine Model | F135 |
| Engine Count | 1 |
Family
Part of the Lockheed Martin F-35 Lightning II family.
Data verification status: Verified
Source: U.S. Air Force