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Mooney M20J 201

Mooney M20J 201 specifications, V-speeds, useful load, performance context, and variant notes for the 200 hp model basis.

M20J 201 model basisSingle-engine land airplanePersonal transport and cross-country travel
Engine
Lycoming IO-360-A3B6, 200 hp
Seats
4
Cruise
155 kt
Range
750 nm
Service ceiling
18,000 ft
Fuel capacity
64 gal
Useful load
1,000 lb
Gross weight
2,740 lb

Reference disclaimer

For training and reference purposes only. Figures describe the stated variant under standard conditions. Verify against the applicable POH/AFM and current aircraft records.

Overview

The Mooney M20J 201 is a four-seat, retractable-gear, single-engine land airplane designed for efficient cross-country travel. Its 200 hp Lycoming IO-360-A3B6 engine, high cruise speed, and compact cabin create a different operating profile from the fixed-gear trainers in this database.

This record covers the M20J model basis. The aircraft's serial range, avionics, optional equipment, modifications, and current weight record determine the applicable loading and performance. M20 family names are not interchangeable shorthand for the same figures.

Performance

The stated cruise value of 155 kt and range value of 750 nm are book values under source conditions. Actual results change with altitude, power setting, mixture, wind, temperature, loading, engine condition, and reserve planning.

The climb references are VX 78 KIAS for angle and VY 88 KIAS for rate. Retractable gear and a higher cruise speed make configuration and energy management important parts of the performance discussion. The POH charts remain the reference for the aircraft's current weight and conditions.

V-speeds

The model basis lists VNE 196 KIAS, VNO 165 KIAS, and VA 113 KIAS at maximum weight. Maneuvering speed changes with weight. The flap limit for this record is VFE 110 KIAS.

The VX, VY, and VA glossary entries explain the terms. The current POH, cockpit markings, and aircraft records control.

Weight and balance

The published useful load of 1,000 lb leaves a practical loading tradeoff with the 64 gal fuel capacity. Four occupants and baggage may require a fuel decision, and rear baggage loading can affect center of gravity. The actual empty weight can differ significantly from a handbook example after avionics and interior changes.

Use current empty weight, arms, fuel quantity, occupant weights, and baggage stations in a loading calculation. The weight and balance calculator is for training and reference only.

Training notes

The M20J is useful for pilots transitioning into faster cross-country aircraft with retractable gear. Its compact cabin, higher cruise speed, and energy management make checklist discipline and speed control central to the training discussion. The aircraft's fixed-pitch assumptions should not be borrowed from simpler trainers.

Variants

The M20C and turbocharged M20K 231 are related Mooney models with different engine and performance data. Keep separate records when the applicable POH and aircraft characteristics change the answer to a model-specific reference query.

Sources

The structured values use the Mooney M20J Pilot's Operating Handbook and FAA Approved Airplane Flight Manual, with model context from FAA Type Certificate Data Sheet 2A3. Confirm the applicable revision, serial range, and aircraft records before using any figure.

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