Aircraft › Diamond Aircraft › DA20 › DA20-C1
The Diamond DA20-C1 is a two-seat, low-wing, fixed-tricycle-gear piston aircraft. The source-linked WBcalc calculator represents the Type 2 fuel-system configuration documented by Diamond DA20-C1 Flight Manual Revision 29.
Diamond Aircraft DA20-C1 Weight and Balance Calculator →
Diamond Aircraft DA20-C1 specifications
| Manufacturer | Diamond Aircraft |
|---|---|
| Model | DA20-C1 |
| Production years | 1998–present |
| Aircraft type | Two-seat piston single |
| Seats | 2 |
| Landing gear | Fixed tricycle |
| Certification | EASA EASA.IM.A.223 |
Diamond Aircraft DA20-C1 weights and capacities
| Maximum takeoff weight | 1,764 lb |
|---|---|
| Maximum landing weight | 1,764 lb |
| Standard fuel capacity | 24.5 gal total / 24 gal usable |
| Maximum baggage | 44 lb combined |
Diamond Aircraft DA20-C1 engine and configuration
| Engine | Continental · IO-240-B32B · 125 hp |
|---|
Diamond Aircraft DA20-C1 history and development
The DA20-C1 is associated with production beginning in 1998 in the aircraft family and remains represented in Diamond's current DA20 product line.
Diamond Aircraft DA20-C1 certification and applicability
| Catalog production period | 1998–present |
|---|---|
| Represented W&B configuration | Type 2 fuel system |
| Category | Utility for the represented calculator configuration |
Diamond Aircraft DA20-C1 fuel capacity
The Type 2 fuel system represented by WBcalc has 24.5 U.S. gallons total capacity and 24.0 U.S. gallons usable.
Diamond Aircraft DA20-C1 configurations and applicability
Type 2 fuel-system configuration
Applicability: DA20-C1 Type 2 fuel-system configuration represented by Diamond DA20-C1 Flight Manual Revision 29.
| Maximum takeoff weight | 1,764 lb |
|---|---|
| Maximum landing weight | 1,764 lb |
| Total fuel | 24.5 US gal |
| Usable fuel | 24 US gal |
The WBcalc calculator is scoped to this fuel-system configuration.
Configuration sources: Diamond Aircraft: DA20-C1 Flight Manual, Revision 29
Current-production DA20-C1 powerplant
Applicability: Current Diamond factory specification; exact applicability must be confirmed for the individual aircraft.
| Engine | Continental IO-240-B32B |
|---|---|
| Engine type | Normally aspirated, fuel-injected piston engine |
| Power | 125 hp |
Current Diamond factory specifications identify the Continental IO-240-B32B rated at 125 hp.
Configuration sources: Diamond Aircraft: Current DA20 Series technical specifications
Diamond Aircraft DA20-C1 model applicability and configuration
The calculator is specifically scoped to the Type 2 fuel system. Other DA20-C1 fuel-system configurations must be evaluated using their applicable approved data.
Diamond DA20-C1 vs DA20-A1 / DA20-100
| Specification | DA20-C1 | DA20-A1 / DA20-100 |
|---|---|---|
| Maximum weight represented | 1,764 lb | 1,653 lb |
| Usable fuel represented | 24.0 US gal | 19.5 US gal |
| Current factory engine | Continental IO-240-B32B, 125 hp | Rotax 912 S3 represented configuration |
Diamond Aircraft DA20-C1 weight and balance
The represented Type 2 configuration uses a maximum takeoff and landing weight of 1,764 lb, 24.0 U.S. gallons usable fuel and a 44 lb combined baggage limit.
Open Diamond Aircraft DA20-C1 Weight and Balance Calculator →
Diamond Aircraft DA20-C1 frequently asked questions
What engine does the current Diamond DA20-C1 use?
Current Diamond factory specifications identify the Continental IO-240-B32B rated at 125 hp.
What maximum weight does the represented DA20-C1 configuration use?
The Type 2 fuel-system configuration represented by WBcalc uses a maximum takeoff and landing weight of 1,764 lb.
How much usable fuel does the represented DA20-C1 hold?
The Type 2 fuel system represented here provides 24.0 U.S. gallons usable from 24.5 gallons total.
Reference sources
Diamond Aircraft: DA20-C1 Flight Manual, Revision 29
Diamond Aircraft: Current DA20 Series technical specifications
Related DA20 models
- Diamond Aircraft DA20-A1 - 1994–1998