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Mooney M20 / M21(2)

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Aviation Mooney M20 / M21(2)


Certification to Federal Aviation Administration USA 2A3:

M20C
1852, 1940 to 3466 (1962-66)
20-1186 and up (1977-1978)

M20E
1964-65

M20F
22-013 and up (1974)

M20G
680001 to 680164 (1968)

M20J
24-0084, 24-0764 to 24-1037 (1979-1980)
24-3079 and up (1989-1990)

M20M
1991-2003

M20R
All


Specifications:

M20

Engine: Lycoming O-320

M20A

Engine: Lycoming O-360A, 180 hp

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

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