Aircraft › Mooney › M20 Series › M20E
The Mooney M20E is a four-seat, low-wing, retractable-gear piston single in the M20 family. The source-linked WBcalc configuration uses a 2,575 lb maximum takeoff and landing weight and 52 U.S. gallons usable fuel.
Mooney M20E Weight and Balance Calculator →
Mooney M20E specifications
| Manufacturer | Mooney |
|---|---|
| Model | M20E |
| Production years | 1964–1975 |
| Aircraft type | Four-seat retractable-gear piston single |
| Seats | 4 |
| Engine | Lycoming IO-360 family |
| Landing gear | Retractable tricycle |
| Certification | FAA 2A3 |
Mooney M20E weights and capacities
| Maximum takeoff weight | 2,575 lb |
|---|---|
| Maximum landing weight | 2,575 lb |
| Maximum baggage | 120 lb combined |
Mooney M20E history and development
The M20E is associated with the 1964–1975 production period in the aircraft family and is certificated under FAA Type Certificate Data Sheet 2A3.
Mooney M20E certification and applicability
| FAA type certificate | 2A3 |
|---|---|
| Production period | 1964–1975 |
| Category | Normal |
Mooney M20E fuel capacity
The source-linked WBcalc configuration represents 52 U.S. gallons of usable fuel at an arm of 48.4 inches.
The represented fuel load is part of the aircraft loading calculation and must be evaluated together with occupants, baggage and the individual aircraft's current empty weight and arm.
Mooney M20E model applicability and configuration
Individual M20E aircraft can differ because of approved engine, fuel-system, equipment and other modifications. Use the current aircraft records and applicable approved documents.
Mooney M20E vs M20C
| Specification | M20E | M20C |
|---|---|---|
| Engine family | Lycoming IO-360 | Lycoming O-360 |
| Maximum weight represented | 2,575 lb | 2,575 lb |
| Usable fuel represented | 52 US gal | 52 US gal |
Mooney M20E weight and balance
The source-linked M20E calculator represents a maximum takeoff and landing weight of 2,575 lb, 52 U.S. gallons of usable fuel and a 120 lb baggage limit.
Maximum combined baggage represented by the model-level data is 120 lb. Loading that amount is not automatically acceptable in every condition; the resulting center of gravity must also remain within the applicable envelope.
Open Mooney M20E Weight and Balance Calculator →
Mooney M20E frequently asked questions
What maximum takeoff weight does the represented Mooney M20E configuration use?
The source-linked configuration uses a maximum takeoff weight of 2,575 lb.
How much usable fuel does the represented M20E hold?
The source-linked configuration represents 52 U.S. gallons of usable fuel.
What engine family is associated with the Mooney M20E?
The M20E is associated with the Lycoming IO-360 engine family; exact installed-engine applicability should be checked from the individual aircraft records.
Reference sources
FAA: Type Certificate Data Sheet 2A3
WBcalc source-linked calculator dataset: mooney/m20e
Related M20 Series models
- Mooney M20C - 1962–1978
- Mooney M20F - 1966–1977
- Mooney M20G - 1968–1970