Mooney 1998 Bravo

Friday, February 01, 2008 at 12:00 AM ET

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Key Takeaways:

The article presents detailed specifications for the 1998 Mooney Bravo aircraft, identifying its engine as a 270 HP Lycoming TIO-540-A1FB.
This 4-seater aircraft has a gross weight of 3368 lbs and a useful load of 1100 lbs, with a fuel capacity of 89 gallons.
Key performance figures include a cruise speed of up to 220 knots (75% power) and a maximum range of 840 nautical miles (65% power with reserve).
The Mooney Bravo boasts a service ceiling of 25,000 ft, a best rate of climb of 1230 fpm, and a low stall speed of 59 knots.

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Mooney 1998 Bravo

Engine make/model:

Lyc. TIO-540-A1FB

Horsepower:

270

TBO hrs.:

2000

Propeller:

Const. spd.

Landing gear type:

Tri/Retr.

Gross weight (lbs.):

3368

Empty weight (lbs.):

2268

Useful load (lbs.):

1100

Fuel (gals.):

89

Wingspan:

36 ft. 1 in.

Overall length:

26 ft. 9 in.

Height:

8 ft. 4 in.

Wing area (sq. ft.):

174.8

Seating capacity:

4

Cabin width (in.):

43.5

Cabin height (in.):

44.5

Baggage capacity (lbs.):

120

PERFORMANCE

Cruise speed (kts.):

75% power:

220

65% power:

215

Max range (w/ reserve) (nm):

75% power:

750

65% power:

840

Fuel consumption (gph):

75% power:

17.6

65% power:

16.6

Estimated endurance (65% power with 1-hr. reserve):

4 hrs. 18 mins.

Stall speed (gear, flaps down) (knots):

59

Best rate of climb (fpm):

1230

Service ceiling (ft.):

25,000

Takeoff ground roll (ft.):

1080

Landing ground roll (ft.):

1200