Aircraft › Extra Aircraft › EXTRA NG › EXTRA NG
The EXTRA NG is a model in the EXTRA NG family. It is described here as a Two-seat unlimited-aerobatic composite piston aircraft. EASA type-certificate reference: EASA.A.620.
Extra Aircraft EXTRA NG specifications
| Manufacturer | Extra Aircraft |
|---|---|
| Model | EXTRA NG |
| Aircraft type | Two-seat unlimited-aerobatic composite piston aircraft |
| Seats | 2 |
| Landing gear | Fixed conventional (tailwheel) |
| Certification | EASA EASA.A.620 |
Extra Aircraft EXTRA NG weights and capacities
| Maximum takeoff weight | 2,094 lb |
|---|---|
| Standard fuel capacity | 51.8 gal total / 51 gal usable |
Aerobatic fuel-use and category limits are configuration/mission dependent.
Extra Aircraft EXTRA NG engine and configuration
| Engine | Lycoming · AEIO-580-B1A · 315 hp · @ 2,700 rpm |
|---|
Baggage and loading applicability
| Baggage | Aerobatic fuel-use and category limits are configuration/mission dependent. |
|---|
Extra Aircraft EXTRA NG history and development
The EXTRA NG is a tandem-seat carbon-composite aerobatic aircraft certified under EASA.A.620. Its Lycoming AEIO-580-B1A is rated at 315 hp at 2,700 rpm. Manufacturer and TCDS data distinguish Normal-category and several Aerobatic-category mass/load-factor cases: 950 kg is the Normal-category MTOW, while the most demanding single-seat aerobatic case uses a lower mass. Total fuel capacity is 196 L with 193 L usable, and the acro-tank subset is smaller.
Extra Aircraft EXTRA NG fuel capacity
Standard total fuel: 51.8 U.S. gallons. Standard usable fuel: 51 U.S. gallons.
Extra Aircraft EXTRA NG configurations and applicability
Normal category
| Maximum takeoff weight | 2,094 lb |
|---|
Aerobatic ACRO I single-seat
| Maximum takeoff weight | 1,808 lb |
|---|
Aerobatic ACRO II two-seat
| Maximum takeoff weight | 1,984 lb |
|---|
Extra Aircraft EXTRA NG model applicability and configuration
Do not use the 950 kg Normal-category mass for every aerobatic manoeuvre. EASA.A.620 defines separate aerobatic mass/load-factor combinations and the POH controls fuel-system use for aerobatics.
Extra Aircraft EXTRA NG weight and balance
Maximum takeoff weight: 2,094 lb. Aerobatic fuel-use and category limits are configuration/mission dependent. The top-level page uses 950 kg (2,094 lb) as the Normal-category MTOW. Aerobatic operation requires the lower category-specific masses and approved loading conditions. Use the approved aircraft-specific documentation and current weight-and-balance record for operational calculations. WBcalc does not currently provide a model-specific EXTRA NG calculator.
Extra Aircraft EXTRA NG frequently asked questions
What engine does the EXTRA NG use?
The engine listed for this model is Lycoming AEIO-580-B1A.
What is the maximum takeoff weight of the EXTRA NG?
The represented maximum takeoff weight is 2,094 lb.
How much usable fuel does the EXTRA NG carry?
The represented standard usable fuel capacity is 51 U.S. gallons.
Reference sources
EASA: Type Certificate Data Sheet EASA.A.620 - EXTRA NG
Extra Aircraft: EXTRA NG technical data