Aircraft / Mooney / M-20M Bravo
Mooney Certified · Fixed-wing · United States
M-20M Bravo
Seats 4 4
Power 280 hp 209 kW
Cruise 175 kt 324 km/h
US register 249 aircraft 249 aircraft
Photo: Jwh · CC BY-SA 3.0 lu Photo: Alec Wilson from Khon Kaen, Thailand · CC BY-SA 2.0 Photo: The original uploader was Rsduhamel at English Wikipedia. · CC BY-SA 3.0
About the M-20M Bravo
The Mooney M20M is an American type-certificated fixed-wing aircraft configured with a low wing, retractable tricycle gear, and a single piston engine. It provides a four-seat enclosed cabin, making it suitable for general aviation touring and personal transport.
Originating as part of a long-running family of designs conceived by its namesake designer, the aircraft first took to the air in the early 1950s after the company relocated. Early iterations featured wooden wing and tail structures later replaced by metal, while the airframe itself combines steel-tube cabin framing with aluminum semi-monocoque construction. Over decades of intermittent production runs involving multiple company ownership changes, thousands of units have been built.
Engines fitted 243 aircraft
Engine Power Share of fleet Aircraft
Lycoming TIO-540
310 hp
237
Lycoming IO-540
300 hp
2
Lycoming O-540
250 hp
2
Lycoming IGSO-540
380 hp
2
M-20M Bravo variants
Designation Seats Engine power Max take-off weight Cruise speed Range
M-20M Bravo This page
4 4 280 hp 209 kW 3,368 lb 1,528 kg 175 kt 324 km/h 1,100 nm 2,037 km
M-20M Tls
4 4 280 hp 209 kW 3,368 lb 1,528 kg 175 kt 324 km/h 1,100 nm 2,037 km
Specifications N/A · Continental TSIO-550-G
US Metric
Dimensions
Length 26 ft 0 in 7.92 m 7.92 m 26 ft 0 in
Wingspan 36 ft 0 in 10.97 m 10.97 m 36 ft 0 in
Wing area 175 sq ft 16.2 m² 16.2 m² 175 sq ft
Weights
Empty weight 2,380 lb 1,080 kg 1,080 kg 2,380 lb
Max take-off weight 3,368 lb 1,528 kg 1,528 kg 3,368 lb
Performance
Cruise speed 175 kt 324 km/h 324 km/h 175 kt
Max speed 242 kt 448 km/h 448 km/h 242 kt
Stall speed 53 kt 98 km/h 98 km/h 53 kt
Range 1,100 nm 2,037 km 2,037 km 1,100 nm
Service ceiling 25,000 ft 7,620 m 7,620 m 25,000 ft
Powerplant
Engine Continental TSIO-550-G
Engine power 280 hp 209 kW 209 kW 280 hp
ICAO type designator M20T
Type certificate EASA.IM.A.266
On the US register 249
Registered in Brazil, Australia, United States, Canada
1996 · 1,800 h USD
Low $220,000
Typical $253,000
High $286,000
By year built · United States · USD
Built Hours Low Typical High
1990 2,220 $187,000 $215,000 $243,000 1991 2,220 $192,000 $220,000 $249,000 1992 2,220 $197,000 $225,000 $255,000 1993 3,530 $195,000 $223,000 $252,000 1994 3,290 $201,000 $230,000 $260,000 1995 3,290 $205,000 $236,000 $267,000 1996 1,800 $220,000 $253,000 $286,000 1997 1,680 $227,000 $260,000 $295,000 1998 1,680 $233,000 $267,000 $302,000 1999 1,680 $238,000 $274,000 $309,000 2000 1,680 $244,000 $280,000 $317,000 2001 1,500 $253,000 $290,000 $328,000
By year built · United Kingdom · GBP
Built Hours Low Typical High
1990 2,220 £126,000 £161,000 £201,000 1991 2,220 £129,000 £165,000 £206,000 1992 2,220 £133,000 £169,000 £212,000 1993 3,530 £131,000 £167,000 £209,000 1994 3,290 £135,000 £172,000 £216,000 1995 3,290 £139,000 £176,000 £221,000 1996 1,800 £149,000 £189,000 £237,000 1997 1,680 £153,000 £195,000 £244,000 1998 1,680 £157,000 £200,000 £250,000 1999 1,800 £160,000 £204,000 £255,000 2000 1,800 £164,000 £209,000 £262,000 2001 2,060 £166,000 £212,000 £265,000
By year built · Euro countries · EUR
Built Hours Low Typical High
1990 2,220 €151,000 €192,000 €241,000 1991 2,220 €154,000 €197,000 €247,000 1992 2,220 €158,000 €201,000 €253,000 1993 3,530 €157,000 €199,000 €250,000 1994 3,290 €161,000 €205,000 €258,000 1995 3,290 €165,000 €211,000 €264,000 1996 1,800 €177,000 €226,000 €283,000 1997 1,680 €183,000 €233,000 €292,000 1998 1,680 €187,000 €238,000 €299,000 1999 1,800 €191,000 €243,000 €305,000 2000 1,800 €196,000 €249,000 €312,000 2001 2,060 €199,000 €253,000 €317,000
M-20M Bravo running costs $474 an hour
A year
Low Typical High
Fuel $10,645 $13,694 $15,949 Oil $248 $310 $403 Engine overhaul reserve $4,583 $5,417 $8,842 Propeller overhaul reserve $917 $1,083 $1,250 Annual inspection and maintenance $3,000 $4,000 $5,000 Hangar $3,000 $6,300 $9,600 Insurance $2,541 $3,189 $3,837 Depreciation $6,685 $13,370 $20,055
Total $31,619 $47,363 $64,936
Per hour $316 $474 $649
Engine
Model Lycoming TIO-540-AF1B
Power 310 hp
Overhaul 1,800 h / 12 yr
Fuel burn 14.1 – 17.8 gal/h
Fuel price $8.20 /US gal
Value lost a year 5.4%