Weight and balance data
- Type certificate data sheet (TCDS)
- TCDS# EASA.A.006 Issue 13 (EASA)
- Manufacturer
- Costruzioni Aeronautiche Tecnam S.p.A.
- Engines
- 1x Rotax 912 S2 (98.6 HP despegue)
- Maximum takeoff weight
- 1,278 lbs (580 kg)
- Reference empty weight
- 772 lbs (350 kg)
- Empty weight arm
- 65.35"
- CG limits
- 66.66" to 70.15" aft of datum
Loading stations and arms
| Station | Arm (in) | Maximum (lbs) |
|---|---|---|
| Pilot | 70.87 | — |
| Copilot | 70.87 | — |
| Baggage | 88.98 | 44 |
| Fuel | 60.24 | 157 |
CG envelope points
Envelope polygon vertices (arm in inches aft of datum, weight in pounds).
| Point | Arm (in) | Weight (lbs) |
|---|---|---|
| 1 | 66.66 | 700 |
| 2 | 66.66 | 1,278 |
| 3 | 70.15 | 1,278 |
| 4 | 70.15 | 700 |
Data reliability and sources
Reliability:estimated reference values · Last verified: 2026-10-14
Sources:
- EASA TCDS EASA.A.006 Issue 13 (P2002-JF), Sección A: https://www.easa.europa.eu/en/downloads/7514/en
- Tecnam P2002 JF Aircraft Flight Manual, Doc. 2002/028 3rd Ed. Rev. 15 (copia de escuela, I-SKYN), Secciones 2 y 6: https://www.skyservices-flightacademy.com/wp-content/uploads/2020/06/P2002_JF_AFM_-_Ed3r15_I-SKYN.pdf
Pending verification:
- Peso vacío y brazo de la aeronave individual (obligatorio: W&B Report propio)
- Brazos de asientos y combustible tomados solo del AFM (copia no controlada): verificar con el AFM de su número de serie
- MTOW 600 kg (MOD2002/29, SB010-CS) y 620 kg (MOD2002/87, SB0105-CS) no modelados: este perfil usa 580 kg
- El rango de CG es angosto (3.5"): cargas livianas con piloto solo pueden quedar cerca del límite delantero
- Combustible: la conversión por volumen de la app usa densidad AVGAS (6.0 lb/gal); con MOGAS el peso real es algo mayor
- Ediciones anteriores del AFM (Rev. 0) indican equipaje a 2.2 m; TCDS y Rev. 15 indican 2.26 m (usado aquí)
Empty weight and arm differ for every airframe: use the values from your aircraft's weight and balance report (you can add them as a custom aircraft in the calculator).
Frequently asked questions
How is the Tecnam P2002 JF weight and balance calculated?
Multiply each station's weight by its arm to get its moment, add up weights and moments (including the empty weight) and divide the total moment by the total weight to get the CG. The Tecnam P2002 JF is within limits when the weight does not exceed the maximum and the weight/CG point lies inside the envelope.
What is the maximum weight of the Tecnam P2002 JF?
The reference maximum takeoff weight of the Tecnam P2002 JF is 1,278 lbs (580 kg), per TCDS# EASA.A.006 Issue 13 (EASA). Always confirm it in your aircraft's POH/AFM.
What are the CG limits of the Tecnam P2002 JF?
The Tecnam P2002 JF CG must be between 66.66" (forward limit) and 70.15" (aft limit) aft of datum. The effective limit depends on weight: the envelope on this page shows its full shape.
Can I use this calculator for my Tecnam P2002 JF?
Yes, as a reference. Every Tecnam P2002 JF has its own empty weight and arm depending on its equipment: enter them from its weight and balance report as a custom aircraft. The POH/AFM is always the official reference.