Aircraft › Airbus Poland › PZL Koliber Series › PZL-KOLIBER 150A
The PZL-KOLIBER 150A is a model in the PZL Koliber Series family. It is described here as a Single-engine light training / touring aircraft.
Airbus Poland PZL-KOLIBER 150A specifications
| Manufacturer | Airbus Poland |
|---|---|
| Model | PZL-KOLIBER 150A |
| Aircraft type | Single-engine light training / touring aircraft |
| Landing gear | Fixed tricycle |
| Certification | EASA EASA.A.091 |
Airbus Poland PZL-KOLIBER 150A weights and capacities
Limit applies to persons and/or luggage on rear seats; aircraft weight and CG limits must also be satisfied.
Airbus Poland PZL-KOLIBER 150A engine and configuration
| Engine | Lycoming · O-320-E2A · 150 hp · @ 2,700 rpm |
|---|
Certified weight limits and applicability
| Normal Category | Takeoff 1,874 lb · Normal Category |
|---|---|
| Utility Category | Takeoff 1,698 lb · Utility Category |
Fuel capacity and configuration
| Fuel | 46.7 gal total · 42.5 gal usable |
|---|
Baggage and loading applicability
| Baggage | Limit applies to persons and/or luggage on rear seats; aircraft weight and CG limits must also be satisfied. |
|---|
Airbus Poland PZL-KOLIBER 150A history and development
PZL-KOLIBER 150A is a member of the PZL Koliber Series family represented in the aircraft reference data. The certification record lists this model under EASA.A.091 - PZL Koliber Series. Model-specific differences can include propulsion, maximum weight, fuel system, landing gear, mission equipment and approved configuration. preserves model and certification context while model-specific values that have not been verified remain unverified values.
Airbus Poland PZL-KOLIBER 150A fuel capacity
exact model-specific fuel capacity / usable fuel has not yet been verified from the applicable certification record, approved flight manual, or manufacturer data. Do not infer it from a neighboring Airbus Poland model or suffix.
Airbus Poland PZL-KOLIBER 150A model applicability and configuration
Verify exact model designation, serial number, installed propulsion, fuel system, landing-gear or special configuration and approved equipment against the applicable certification/manufacturer record and individual aircraft documentation.
Airbus Poland PZL-KOLIBER 150A weight and balance
Use exact model/serial-number loading data and the individual aircraft's approved weight-and-balance record. No baggage or payload limit is inferred from a related Airbus Poland model. The exact model-specific maximum takeoff weight / gross weight remains unverified until the applicable approval or manufacturer section is verified. Operational loading must use the aircraft-specific empty weight, CG, station arms and limitations. Use the approved aircraft-specific documentation and current weight-and-balance record for operational calculations. WBcalc does not currently provide a model-specific PZL-KOLIBER 150A calculator.
Reference sources
EASA: EASA Type Certificate Data Sheet EASA.A.091 - PZL Koliber