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Mooney M20M TLS and Bravo
The M20M, approved by the FAA in 1989 and sold as the TLS and the Bravo, is the M20 with a turbocharged 270 hp Lycoming TIO-540-AF1A. The FAA data sheet gives a maximum takeoff weight of 3,368 pounds for most aircraft, 89 US gallons of usable fuel and a maximum operating altitude of 25,000 feet, which the EASA data sheet confirms. Span, length and height are from the EASA data sheet. It seats four, has retractable gear and is filed under ICAO code M20T.
- Seats
- About 4
- Engines
- One piston engine in the nose: Lycoming TIO-540-AF1A or -AF1B
- Max takeoff weight
- 3,400 lb (1,528 kg)
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Specifications
| Length | 26 ft 9 in (8.15 m) |
|---|---|
| Wingspan | 36 ft 1 in (11.00 m) |
| Height | 8 ft 4 in (2.54 m) |
| Fuselage width | 3 ft 9 in (1.15 m) |
| Ceiling | 25,000 ft (7,600 m) |
| Fuel capacity | 90 US gal (337 L) |
| Status | In service |
| Type codes | ICAO M20T |
Private aircraft show specs only. No flight data is shown for them.