Aircraft › Airbus Poland › PZL Koliber Series › PZL-110 KOLIBER
The PZL-110 KOLIBER is a model in the PZL Koliber Series family. It is described here as a Single-engine light training / touring aircraft.
Airbus Poland PZL-110 KOLIBER specifications
| Manufacturer | Airbus Poland |
|---|---|
| Model | PZL-110 KOLIBER |
| Aircraft type | Single-engine light training / touring aircraft |
| Landing gear | Fixed tricycle |
| Certification | EASA EASA.A.091 |
Airbus Poland PZL-110 KOLIBER weights and capacities
Airbus Poland PZL-110 KOLIBER engine and configuration
| Engine | PZL-Franklin · 4A-235-B31 · 116 hp · @ 2,800 rpm |
|---|
Certified weight limits and applicability
| Normal Category | Takeoff 1,808 lb · Normal Category |
|---|---|
| Utility Category | Takeoff 1,698 lb · Utility Category |
| BCAR Semi-Aerobatic configuration | Takeoff 1,653 lb · BCAR Semi-Aerobatic configuration |
Fuel capacity and configuration
| Fuel | 27.74 gal total · 25.36 gal usable |
|---|
Baggage and loading applicability
| Normal Category | Normal Category |
|---|---|
| Utility Category - no person or luggage on rear seats | Utility Category - no person or luggage on rear seats |
Airbus Poland PZL-110 KOLIBER history and development
PZL-110 KOLIBER 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-110 KOLIBER 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-110 KOLIBER 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-110 KOLIBER 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-110 KOLIBER calculator.
Reference sources
EASA: EASA Type Certificate Data Sheet EASA.A.091 - PZL Koliber
EASA: EASA.E.087 - Franklin 4A-235-B31 engine rating, 116 hp at 2800 rpm