Mooney M20 / M21 / M201 ![]() M-201
![]() M.20A
First flown on August 10,1953 with a Lycoming O-320 engine, the 150-hp engine was upgraded to O-360-A 180 hp as the M-20A, improving the Mark 20's takeoff, climb and cruise performance with an acceptably small sacrifice in economy. Mooney owners could count on a cruise speed of 150 knots at 75-percent power, making the Mark 21 the fastest airplane for the horsepower in its class. It wasn't long before Mooneys were outselling all other single-engine retractables, an honor they would hold until the ascendancy of the Piper Arrow in the late 1960s. This all-wooden wing aircraft was in production until 1961 when the all-metal M20B was introduced. This was superseded by the M20C Mk2l in 1962.
![]() 1969 Mooney M20E
Square windows were introduced in 1967 for O-360-AID-powered Ranger and Executive, and M20J or Model 201, both of which had Lycoming IO-360-A1B6D engines.
![]() 1978 Mooney Ranger
The Ranger is recognizable by looking first at the chin beneath the propeller spinner. Executives and Chaparrals, both with Lycoming IO-360-A1A engines, have a filter housing that is flush with the cowling, but the air filter on the Ranger, powered by the Lyc O-360-A1D, is set up with its lower edge jutting out just a bit. Otherwise, a Ranger is exactly like a Chaparral, which is, with the exception of 10 inches of fuselage length, exactly like an Executive. All three air-planes have the same wingspan: 35 feet. ![]() Mooney M20TN Acclaim Type S
M20
Engine: Lycoming O-320
M20A
Engine: Lycoming O-360A1A, 180 hp
Cruise: 165 mph
Seats: 4 M20C Mk.21 / Aerostar Ranger
Engine: Lycoming O-360-A1D, 180 hp
Wingspan: 35 ft 0 in / 10.67 m
Length: 24 ft 1 in / 7.34 m
Cabin length: 8 ft 8 in / 2.64 m
Cabin max width: 3 ft 4.5 in / 1.04 m
Cabin max height: 3 ft 8.5 in / 1.13 m
Baggage compartment: 13.5 cu.ft / 0.38 cu.m
Empty weight: 1525 lb / 691 kg
MTOW: 2575 lb / 1168 kg
Max speed SL: 153 kt / 176 mph / 283 kph
ROC SL: 1000 fpm / 305 m/min
Service ceiling: 19,500 ft / 5743 m
Range 45min res: 1001 mi / 1610 km
Seats: 4
Ranger M20C
Engine: 1 x Lycoming O-360-A1D, 180 hp
Seats: 4
Wing loading: 15.4 lb/sq.ft
Pwr loading: 14.3 lb/hp
Gross wt: 2575 lb
Empty wt: 1525 lb
Equipped useful load: 961 lb
Payload max fuel: 649 lb
Range max fuel/75% pwr: 694nm/4.8hr
Range max fuel / 55% pwr: 799 nm/ 6.6 hr
Service ceiling: 16,500 ft
75% cruise: 143 kt
55% cruise: 122 kt
Stall: 49-58 kt
1.3 Vso: 64 kt
ROC: 800 fpm
Min field length: 1550 ft
Fuel cap: 312 lb
Undercarriage: retractable.
M20 Ranger
Engine: Lycoming 0‑360‑AlD, 180 hp
TBO: 2,000 hrs
Prop: constant‑speed, two‑blade, 74‑inch dia
Length: 23 ft. 2 in
Height: 8 ft. 4 in
Wingspan: 35 ft
Wing area: 174 sq. ft
Wing loading: 15.11 lb./sq.ft
Seats: 4
Empty weight, IFR equipped: 1,606 lbs
Useful load, IFR equipped: 969 lbs
Equipped payload (750 miles fuel, 75 % power): 715 lb
Gross weight: 2,575 lbs
Power loading: 14.2 lb/hp
Fuel capacity: 52 gals./312 lbs
Minimum runway requirement: 1,550 ft
Rate of climb: 800 fpm
Service ceiling: 16,300 ft
Maximum speed: 147 knots
Cruise (75 % @ 10,000 ft): 143 knots
Economy cruise (57 % @ 10,000 ft.): 123 knots
Maximum range (75% power): 948mi
Stall speed, clean: 58 knots
Stall speed, landing config: 49 kts
Cabin width (elbow to elbow): 43.5in.
Ranger
Engine: Lycoming O‑360‑A1D, 180 hp
TBO: 2,000 hrs
Propeller: Hartzell two‑blade, constant‑speed, 74‑in
Length: 23 ft. 2 in
Height: 8 ft. 4 in
Wingspan: 35 ft
Airfoil: NACA 632‑215 at root, NACA 641‑412 at tip
Aspect ratio: 7.338
Wing area: 167 sq. ft
Wing loading: 15.4 lb/sq.ft
Seats: 4
Empty weight: 1,525 lbs
Useful load: 1,050 lbs
Payload with full fuel: 738 lbs
Gross weight: 2,575 lbs
Power loading: 14.3 lb/hp
Fuel capacity: 52 USG/312 lbs
Baggage capacity: 120 lbs
Baggage area: 15 cu.ft
Minimum runway requirement: 1,550 ft
Rate of climb: 860 fpm
Service ceiling: 19,500 ft
Maximum speed: 153 knots
Cruise (75% @ 10,000 ft.): 143 knots
Economy cruise (65% @ 10,000 ft.): 135 knots
Range @ max cruise (45‑min res): 684 nm
Range @ economy cruise (45‑min res): 745 nm
Duration @ max cruise (no res): 5.5 hrs
Stall speed (clean): 58 knots
Stall speed (gear and flaps down): 49 knots
M‑20D Master
Simplified M20C
Undercarriage: fixed
M20 Chaparral / M20E Super 21
Engine: Lycoming IO‑360‑A1A, 200 hp
TBO: 1,600 hrs
Propeller: Hartzell two‑blade, constant‑speed, 74‑in
Length: 23 ft. 2 in
Height: 8 ft. 4 in
Wingspan: 35 ft
Airfoil: NACA 632‑215 at root, NACA 641‑412 at tip
Aspect ratio: 7.338
Wing area: 167 sq. ft
Wing loading: 15.4 lb/sq.ft
Seats: 4
Empty weight: 1,600 lbs
Useful load: 975 lbs
Payload with full fuel: 663 lbs
Gross weight: 2,575 lbs
Power loading: 12.8 lb/hp
Fuel capacity: 52 USG/312 lbs
Baggage capacity: 120 lbs
Baggage area: 15 cu.ft
Minimum runway requirement: 1,550 ft
Rate of climb: 1,125 fpm
Service ceiling: 21,200 ft
Maximum speed: 165 knots
Cruise (75% @ 10,000 ft.): 158 knots
Economy cruise (65% @ 10,000 ft.): 150 knots
Range @ max cruise (45‑min res): 534 nm
Range @ economy cruise (45‑min res): 700 nm
Duration @ max cruise (no res): 4.1 hrs
Stall speed (clean): 58 knots
Stall speed (gear and flaps down): 49 knots
Cabin width (elbow to elbow): 43.5in
Seats: 4
M20F / Aerostar Executive
Engine: Lycoming IO-360-AlA, 200 hp at 2700 rpm
TBO: 1600 hours
Prop: Hartzell 74” Constant speed
Power Loading: 13.7 lbs/hp
Wingspan: 35 ft
Wing Area: 167 sq.ft
Airfoil: NACA 632‑215 at root, NACA 641‑412 at tip
Wing Loading: 16.4 lbs./sq.ft
Length: 24 ft
Height: 8’4”
Seats: 4
Baggage Capacity: 120 lbs
Gross Weight, Normal Category: 2,740 lbs
Empty Weight: 1,640 lbs
Equipped payload (750 miles fuel, 75 % power): 752 lb
Fuel Capacity, Standard Tanks: 64 USG / 384lb
Payload max fuel: 627 lb
Max speed; 185 mph
Cruise Speed (75% pwr): 177 mph
Cruise 67% pwr: 171 mph
55% cruise: 130 kt
1.3 Vso: 70 kt
Maneuvering Speed: 135 mph
Stall Speed, Clean: 68 mph
Stall Speed, (gear and) full flaps: 62 mph
Takeoff Distance: 834 ft
Landing Distance: 785 ft
Takeoff, over 50ft. obstacle: 1,384 ft
Landing, over 50 ft. obstacle: 1,786 ft
Best Rate of Climb, S.L.: 960 fpm
Service Ceiling: 18,800 ft
Max. Endurance Range, Standard Tanks, No Reserve: 8:41 hours; 1,060 st.mi.
Maximum speed: 161 knots
Cruise (75% @ 10,000 ft.): 150 knots
Economy cruise (65% @ 10,000 ft.): 141 knots
Range @ max cruise (45‑min res): 649 nm
Range @ economy cruise (45‑min res): 834 nm
Duration @ max cruise (no res): 5.1 hrs
Range 75% pwr, 45 min res: 977 sm
Average Fuel Consumption, Normal Cruise: 10.2 gph
Cabin width (elbow to elbow): 43.5in
M20G Statesman
Similar to Ranger, longer fuselage, extra window
M20J 201
Engine: 1 x Lycoming IO-360-AB6D, 200 hp
TBO: 1800 hrs
Prop: McCauley 2 blade, constant speed 74 in
Seats: 4
Length: 24.7 ft
Height: 8.3 ft
Wingspan: 35 ft
Wing area: 170 sq.ft
Wing aspect ratio: 7.4
Max ramp wt: 2740 lbs
Max take off wt: 2740 lbs
Standard empty wt: 1640 lbs
Max useful load: 1069 lbs
Max landing wt: 2740 lbs
Baggage cap: 130 lbs
Wing loading: 16.1 lbs/sq.ft
Power loading: 13.7 lbs/hp
Max useable fuel (std): 64 USG, 384 lbs
Climb rate: 1030 fpm @ 89 kts
Climb gradient: 694 ft/nm
Rate of climb @ 8000 ft: 630 fpm
Service ceiling; 18,800 ft
Max speed: 185kts
Cruise @ 65% power @ 8,000ft: 157kts
Fuel flow @ 65% power @ 8,000ft: 56 pph
Endurance @ 65% power @ 8,000ft: 6.6 hr
Stalling speed clean: 63 kts
Stall speed flaps/gear down: 55 kts
T/O 50 ft: 1302 ft
Ldg 50 ft: 1700 ft
Turbulent air penetration speed: 120 kts
Retractable undercarriage.
M20J Allegro
1978 201
Engine: Lycoming IO-360-A3B6D, 200 hp
TBO: 2000 hr
Propeller: Const. spd.
Landing gear type: Tri/Retr Gross weight: 2740 lb
Empty weight: 1640 lb
Useful load: 1100 lb
Fuel: 64 USG
Wingspan: 35 ft Overall length: 24 ft. 8 in
Height: 8 ft. 4 in
Wing area: 167 sq. ft
Seating capacity: 4
Cabin width: 43.5 in Cabin height (in.): 44.5
Baggage capacity (lbs.):120
Cruise speed 75% power: 169 kt Cruise speed 65% power: 156 kt
Max range (w/ reserve) 75% power: 835 nm
Max range (w/ reserve) 65% power: 881 nm
Fuel consumption 75% power: 10.8 USgph Fuel consumption 65% power: 9.7 USgph
Stall speed (gear, flaps down): 55 knots
Best rate of climb: 1030 fpm Service ceiling: 18,800 ft Takeoff ground roll: 913 ft
Landing ground roll: 770 ft
Mooney 205
Engine: Lycoming IO-360-A3B6D, 200 hp@2700 rpm @SL
TBO: 2000 hr Fuel type: 100LL
Propeller: McCauley CS Landing gear type: Tri/Retr. Max ramp weight: 2740 lb Gross weight: 2740 lb Max landing weight: 2740 lb
Empty weight, std: 1695 lb Useful load, std: 1045 lb Payload, full std. fuel: 661 lb Usable fuel, std: 64 USG Oil capacity: 8 qts
Wingspan: 36 ft. 1in Overall length: 24 ft. 9 in
Height: 8 ft. 4 in
Wing area: 174.8 sq. ft
Wing loading: 15.7 lbs./sq. ft
Power loading: 13.7 lbs./hp Wheel size: 6.00 x 6 in Seating capacity: 4 Cabin doors: 1 Cabin width: 43.5 in Cabin height: 45 in
Baggage capacity:120 lbs /13.5 cu. ft
Cruise speed 75% power: 171 kt Cruise speed 65% power: 162 kt
Max range (w/ reserve) 75% power: 740 nm
Vs: 61 kt Vso: 54 kt Best rate of climb: 1050 SL fpm Best rate of climb, 8,000 ft: 700 fpm Service ceiling: 18,600 ft Takeoff ground roll: 900 ft
Takeoff over 50-ft. obstacle: 1700 ft
Landing ground roll: 677 ft Landing over 50-ft. obstacle: 1600 ft
M20K Turbo 231 First built: 1978
Engine: 1 x Continental TSIO-360-GB-1, 210 hp
TBO: 1800 hrs
Fuel; 100/100LL
Prop: McCauley 2 blade, constant speed 74 in
Seats: 4
Length: 25.4 ft
Height: 8.3 ft
Wingspan: 36.1 ft
Wing area: 174.8 sq.ft
Wing aspect ratio: 7.4
Max ramp wt: 2900 lbs
Max take off wt: 2900 lbs
Standard empty wt: 1800 lbs
Max useful load: 1100 lbs
Payload full std fuel; 462 lbs
Max landing wt: 2900 lbs
Wing loading: 16.6 lbs/sq.ft
Power loading: 13.8 lbs/hp
Max useable fuel: 453 lbs
Fuel Capacity (std); 78.6 US Gal
Usable Fuel (std);75.6 US Gal
Climb rate: 1080 fpm @ 96 kts
Climb gradient: 675 ft/nm
Rate of climb @ 8000 ft: 1020 fpm
Certificated (& service) ceiling; 24,000 ft
Turbulent air penetration speed: 119 kts
Retractable undercarriage
Wheel base; 5 ft 11 9/16 in
Wheel Track; 9 ft 3/4 in
Wheel Size; Nose; 5.00x5 Mains; 6.00x6
Cabin Length; 114 in
Cabin Width; 43.5 in
Cabin Height; 44.5 in
Baggage Capacity; 130 lbs
Trim; Stabilizer.
Max Level Speed; 201 kts
Never Exceed Speed; 196 kts.
Cruise 75%, 24,000 ft: 192 kt
Cruise 65%, 24,000 ft: 178 kt
Cruise 55%, 24,000 ft: 163 kt
Range 75%, 21,000 ft: 1000 nm
Range 65%, 9,000 ft: 1080 nm
Range 55%, 12,000 ft: 1170 nm
Stall Speed Flaps up/gear up; 61 kts
Stall Speed Flaps down/ gear down; 57 kts
Best Angle of Climb; 71 kts
Take-off Ground Run; 1250 ft
Take-off 50 ft; 2250 ft
Landing Ground Roll; 1150 ft
Landing over 50 ft; 2300 ft
M20K Encore 1998
Engine: Lycoming IO-360-A1B6, 200 hp
TBO: 2000 hr
Propeller: Const. spd.
Landing gear type: Tri/Fixed Gross weight: 2535 lb Empty weight: 1576 lb
Useful load: 959 lb
Fuel capcity: 54 USG
Wingspan: 32 ft Overall length: 25 ft. 2 in
Height: 9 ft. 10 in
Wing area: 128 sq. ft Seating capacity: 4-5
Cabin width: 50 in Cabin height: 46 in Baggage capacity: 143 lb
Cruise speed 75% power: 130 kt
Cruise speed 65% power: 123 kt
Max range (w/ reserve) 65% power: 800 nm
Fuel consumption 75% power: 12.4 USgph Fuel consumption 65% power: 11.0 USgph
Stall speed (gear, flaps down): 53 kt
Best rate of climb: 937 fpm Service ceiling: 16,000 ft
Takeoff ground roll: 1067 ft
Landing ground roll: 623 ft
M20L M20M Bravo
Engine: Lycoming TIO-540-A1FB, 270 hp
TBO: 2000 hr
Propeller: Const. spd.
Landing gear type: Tri/Retr. Gross weight: 3368 lb Empty weight: 2268 lb
Useful load: 1100 lb Fuel: 89 USG Wingspan: 36 ft. 1 in Overall length: 26 ft. 9 in
Height: 8 ft. 4 in
Wing area: 174.8 sq. ft
Seating capacity: 4
Cabin width: 43.5 in Cabin height: 44.5 in
Baggage capacity: 120 lb
Cruise speed 75% power: 220 kt Cruise speed 65% power: 215 kt
Max range (w/ reserve) 75% power: 750 nm
Max range (w/ reserve) 65% power: 840 nm
Fuel consumption 75% power: 17.6 USgph Fuel consumption 65% power: 16.6 USgph
Stall speed (gear, flaps down): 59 kt
Best rate of climb: 1230 fpm Service ceiling: 25,000 ft Takeoff ground roll: 1080 ft
Landing ground roll: 1200 ft M20M MSE
Engine: Lycoming IO-360-A3B6D, 200 hp@2700 rpm@SL
TBO: 2000 hr Fuel type: 100/100LL
Propeller type/diameter: McCauley CS Landing gear type: Tri/Retr. Max ramp weight: 2900 lb Gross weight: 2900 lb Landing weight: 2900 lb
Empty weight, std: 1726 lb Useful load, std: 1174 lb Payload, full std. fuel: 790 lb Usable fuel: 64 USG Oil capacity: 8 qts
Wingspan: 36 ft. 1 in Overall length: 24 ft. 8 in
Height: 8 ft. 4 in
Wing area: 175 sq. ft
Wing loading: 16.6 lbs./sq. ft
Power loading: 14.6 lbs./hp Wheel base: 6 ft Wheel track: 9 ft. 2 in Wheel size: 6.00 x 6 in Seating capacity: 4 Cabin doors: 1 Cabin width: 43.5 in Cabin height: 44.5 in
Baggage capacity: 120 lb
Cruise speed 75% power @ 8,000 ft.: 168 kt Cruise speed 65% power @ 8,000 ft.: 160 kt
Max range (w/ reserve) 75% power: 850 nm
Fuel consumption 75% power: 10.8 USgph Fuel consumption 65% power: 9.1 USgph
Fuel consumption 55% power: 7.7 USgph Vs: 62 kt Vso: 58 kt Best rate of climb: 1030 fpm Best rate of climb, 8000 ft: 750 fpm
Service ceiling: 18,600 ft
Takeoff over 50-ft. obstacle: 1520 ft
Landing ground roll: 770 ft
Landing over 50-ft. obstacle: 1610 ft
M20M TLS
Engine: Lycoming TIO-540-AF1A, 270 hp
Vne: 195 kt
MAUW: 3368 lb
Max ldg wt: 3200 lb
Cruise: 220 kt @ 25,000 ft
Cruise: 200kt @ 12,000ft
Range IFR res: 1070nm.
M20R Ovation
Engine: 280-hp.
Length: 26.739 ft / 8.15 m
Height: 8.333 ft / 2.54 m
Wingspan: 36.089 ft / 11.0 m
Aspect ratio: 7.4
Wing area: 175.023 sq.ft / 16.26 sq.m
Max take off weight: 3367.0 lb / 1527.0 kg
Weight empty: 2268.9 lb / 1029.0 kg
Max. payload weight: 1144.4 lb / 519.0 kg
Landing speed: 59 kts / 110 km/h
Cruising speed: 190 kts / 352 km/h @ 9000 ft.
Initial climb rate: 1150 ft/min
Service ceiling: 20013 ft / 6100 m
Cruising altitude: 9006 ft / 2745 m
Wing load: 19.27 lb/sq.ft / 94.0 kg/sq.m
Range: 1129 nm / 2090 km
Endurance: 7 h
Crew: 1+3
1997 Ovation
Engine: Cont. IO-550G, 280 hp
TBO: 2000 hr
Propeller: Const. spd.
Landing gear type: Tri/Retr. Gross weight: 3368 lb Empty weight: 2225 lb Useful load: 1134 lb Fuel: 89 USG Wingspan: 36 ft. 1 in Overall length: 26 ft. 9 in
Height: 8 ft. 4 in
Wing area: 175 sq.ft
Seating capacity: 4
Cabin width: 42.5 in Cabin height: 44.5 in
Baggage capacity: 120 lb
Cruise speed 75% power: 190 kt Cruise speed 65% power: 182 kt
Max range (w/ reserve) 75% power: 935 nm
Max range (w/ reserve) 65% power: 1015 nm
Fuel consumption 75% power: 17 USgph Fuel consumption 65% power:14 Usgph
Stall speed (gear, flaps down): 59 kt
Best rate of climb: 1200 fpm Service ceiling: 20,000 ft
Takeoff ground roll: 900 ft
Landing ground roll: 1000 ft
2005 Mooney Ovation2 GX
Base Price: USD$418,150
Engine: Continental IO-550G, 280 hp@2500@SL
TBO hr: 2000
Fuel type: 100LL
Propeller diameter: 73 in
Landing gear type: Tri./Retr.
Max ramp weight: 3368 lb
Gross weight: 3368 lb
Landing weight: 3368 lb
Empty weight, std: 2205 lb
Useful load: 1163 lb
Payload, full std. fuel: 567 lb
Usable fuel, std: 89 USG
Oil capacity: 12 qts
Wingspan: 36 ft. 1 in.
Overall length: 26 ft. 9 in.
Height: 8 ft. 4 in.
Wing area: 174.5 sq. ft
Wing loading: 19.3 lbs./sq. ft
Power loading: 12.0 lbs./hp
Seating capacity: 4
Cabin doors: 1
Cabin interior length: 12.1 in
Cabin interior height: 3.7 in
Cabin interior width: 3.6 ft
Baggage capacity: 120 lb
Range (w/ res) 75% power @ 9,000 ft.: 970 nm
Range (w/ res) 55% power @ 9,000 ft.: 1240 nm
Cruise Speed (8000 ft.): 192 kts
Endurance (75%) (970nm@9000 ft.): 5.0 hr
Endurance (55%) (1240nm@9000 ft.): 7.9 hr
Best rate of climb (SL): 1250 fpm
Service ceiling: 20,000 ft
Vso: 60 kt
Takeoff ground roll: 900 ft
Takeoff over 50-ft. obstacle: 1700 ft
Landing ground roll: 1000 ft
Landing over 50-ft. obstacle: 1600 ft
2007 Mooney Ovation3
Base price: $469,000
Engine: Continental IO-550G, 310hp @SL
TBO: 2000 hr
Fuel type: 100/100LL
Propeller type: Hartzell CS/3-blade
Landing gear type: Tri./Retr
Max ramp weight: 3374 lb
Gross weight: 3374 lb Landing weight: 3374 lb Empty weight, std: 2267 lb Useful load, std: 1107 lb
Useful fuel, std: 102 USG Optional fuel: 130 USG
Payload, full std. fuel: 495 lb
Wingspan: 36 ft. 1 in Overall length: 25 ft. 9 in
Height: 8 ft. 4 in
Wing area: 174.8 sq. ft
Wing loading: 19.3 lbs./sq.ft Power loading: 10.9 lbs./hp
Seating capacity: 4
Cabin doors: 1 Cabin width: 43.5 in
Cabin height: 44.5 in
Cruise speed 75% power: 197 kt @8000 ft
Fuel consumption 75% power: 17.1 Usgph
Fuel consumption 45% power: 10.1 Usgph
Vso (kts.): 59
Best rate of climb, SL: 1300 fpm Service ceiling: 20,000 ft
Takeoff distance: 900 ft
Takeoff over 50 ft. obstacle: 1620 ft Landing distance: 1000 ft Landing over 50 ft. obstacle: 1600 ft
2009 M20R Ovation 3
New price: $517,522
Engine: Continental IO-550G-A/P, 300 hp@SL
TBO: 2000 hr
Fuel type: 100LL
Propeller type: 3-blade, CS Hartzell
Landing gear type: Tri./Retr.
Gross weight: 3368 lb
Empty weight, std: 2261 lb
Useful load, std: 1107 lb Usable fuel, std./opt: 100/300 USG
Payload, full std. fuel: 495 lb
Wingspan: 36 ft. 1 in Overall length: 26 ft. 9 in
Overall height: 8 ft.3 in
Wing area: 175 sq. ft
Wing loading: 19.3 lbs./sq. ft
Power loading 10.86 lbs./hp
Seating capacity: 4
Cabin doors: 1
Cabin width: 43.5 in
Cabin height: 44.5 in
Vso: 59 kt
Best rate of climb, SL: 1300 fpm
Service ceiling: 20,000 ft
Cruise speed, 75% power: 197 kt
Fuel consumption, 75% power: 19 Usgph
Max range, 102 USgals: 1860 nm
Takeoff ground roll: 1620 ft
M20S Eagle
Engine: 244 hp / 182 kW Continental IO-550
Prop: two blade
Max cruise: 175 kt
Initial ROC: 1150 fpm / 350m/min
Max range: 1210 nm / 2240 km
2001 Mooney Eagle2
Base price: US$360,000
Engine: Continental IO-550G, 244 hp @ 2400 rpm@SL
TBO: 2000 hr
Fuel type: 100/100LL
Propeller: McCauley CS/73 in Landing gear type: Tri/Retr. Max ramp weight: 3300 lb Gross weight: 3300 lb Landing weight: 3300 lb
Empty weight, std: 2200 lb Useful load, std: 1100 lb Payload, full std. fuel: 650 lb Usable fuel: 75 USG Oil capacity: 12 qts
Wingspan: 36 ft. 1 in Overall length: 26 ft. 9 in
Height: 8 ft. 4 in
Wing area: 175 sq. ft
Wing loading: 18.3 lbs./sq. ft
Power loading: 13.1 lbs./hp Wheel base: 6 ft. 7 in Wheel track: 9 ft. 2 in Wheel size: 6.00 x 6 in Seating capacity: 4 Cabin doors: 1 Cabin width: 43.5 in Cabin height: 44.5 in
Baggage capacity: 120 lb
Cruise speed 75% power @ 8,300 ft.: 180 kt Fuel consumption 75% power: 12.7 Usgph
Fuel consumption 65% power: 11.0 USGph
Fuel consumption 55% power: 9.2 USGph
Stall speed (flaps up): 66 kt
Stall speed (flaps down): 59 kt
Best rate of climb: 1150 fpm
Best rate of climb, 8000 ft: 760 fpm
Service ceiling: 18,500 ft Landing ground roll: 1100 ft
M20 TN Acclaim
Price: US$495,000
Engine: Continental IO-550-G, 262 bhp@25,000 ft
Fuel type: 100LL Propeller diameter: 76 in. Landing gear type: Tricycle/Retractable/Trailing Link Max ramp weight: 3374 lb Gross weight: 3368 lb Landing weight: 3200 lb
Empty weight, std: 2353 lb Useful load, std: 1015 lb
Useful fuel, std: 102USG Payload, full std. fuel: 418 lb Oil capacity: 8 qts Wingspan: 36 ft. 5 in Overall length: 26 ft. 6 in
Height: 8 ft. 6 in
Wing area: 175 sq. ft
Wing loading: 19.25 lbs./sq. ft
Power loading: 12.03 lbs./hp Wheel base: 79 in Wheel track: 110 in Wheel size: 6.00 x 6 in Seating capacity: 4 Cabin doors: 2 Cruise speed, 25,000 ft 100% power: 237 kt Cruise speed 94% power: 231 kt Cruise speed 75% power: 206 kt Cruise speed 65% power: 198 kt
Cruise speed 55% power: 180 kt
Max range 100% power: 932 nm
Max range 94% power: 1097 nm Max range 75% power: 1373 nm Max range 65% power: 1455 nm
Max range 55% power: 1594 nm Fuel flow 100% power: 22.1 USgph Fuel flow 94% power: 20.7 USgph
Fuel flow 75% power: 14.5 USgph Fuel flow 65% power: 12.0 USgph
Fuel flow 55% power: 10.2 USgph
Service ceiling: 25,000 ft
M20TN Acclaim Type S
Base price: $599,900
Engine: Continental TSIO-550-G, 280 hp @SL
TBO: 2000 hr
Fuel type: 100/100LL
Propeller: 3-blade, CS Hartzell
Landing gear type: Tri./Retr. Gross weight: 3374 lb Empty weight, std: 2370 lb
Useful load, std: 1004 lb Usable fuel: 100 USG Payload, full std. fuel: 404 lb
Wingspan: 36 ft. 5 in. Overall length: 26 ft. 9 in. Height: 8 ft. 4 in. Wing area: 175.7 sq. ft Wing loading: 19.2 lbs./sq. ft
Power loading: 12.1 lbs./hp Wheel size: 6.00 x 6 in
Seating capacity: 4 Cabin doors: 1 Cabin width: 43.5 in
Cabin height: 45 in
Cruise speed, 75% power: 237 kt @ FL250
Vso: 59 kt Climb rate, SL: 1240 fpm Max operating altitude: 25,000 ft
1988 Mooney 252 TSE
Base price: $330,000
Engine: Continental TSIO-360-MB1, 210
TBO: 1800 hr
Fuel type: 100LL
Propeller: 3-blade McCauley/74 in Landing gear type: Tri./Retr. Max ramp weight: 2900 lb Gross weight: 2900 lb Landing weight: 2900 lb
Empty weight, std: 1800 lb Useful load, std: 1100 lb Payload, full std. fuel: 647 lb Useful fuel, std: 75 USG Oil capacity: 8 qts
Wingspan: 36 ft. 1 in. Overall length: 25 ft. 5 in. Height: 8 ft. 4 in Wing area: 175 sq. ft
Wing loading: 16.6 lbs./sq. ft
Power loading: 13.8 lbs./hp Wheel base: 71.6 in Wheel track: 108.75 in Wheel size, nose: 5.00 x 5 in Wheel size, main) :6.00 x 6 in Seating capacity: 4
Cabin doors: 1 Cabin width: 43.5 in Cabin height: 44.5 in
Baggage capacity: 120 lb
Cruise speed 75% power @ 20,000 ft.: 201 kt Cruise speed 65% power @ 10,000 ft.: 180 kt
Range (w/ reserve) 75% power @ 10,000ft.: 541nm
Range (w/ reserve) 75% power @ 20,000 ft.: 541nm
Max range (w/ reserve) 75% power: 980 nm
Fuel consumption 75% power: 12.7 Usgph Vs: 61 kt
Vso: 59 kt Best rate of climb: 1080 fpm Best rate of climb, 8,000 ft: 1100 fpm Service ceiling: 28,000 ft Takeoff ground roll: 1250 ft
Takeoff over 50-ft. obstacle: 2200 ft
Landing ground roll: 1140 ft Landing over 50-ft. obstacle: 2300 ft ![]() Mooney Ranger
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