Weight and balance data
- Type certificate data sheet (TCDS)
- TCDS# 3A19 Revision 50 (FAA)
- Manufacturer
- Cessna Aircraft Company (Textron Aviation)
- Engines
- 1x Lycoming O-235-L2C / O-235-N2C (110/108 HP)
- Maximum takeoff weight
- 1,670 lbs (757 kg)
- Reference empty weight
- 1,136 lbs (515 kg)
- Empty weight arm
- 29.93"
- CG limits
- 31.0" to 36.5" aft of datum
Loading stations and arms
| Station | Arm (in) | Maximum (lbs) |
|---|---|---|
| Pilot | 39.0 | — |
| Front passenger | 39.0 | — |
| Baggage area 1 | 64.0 | 120 |
| Baggage area 2 | 84.0 | 40 |
| Fuel | 42.0 | 147 |
CG envelope points
Envelope polygon vertices (arm in inches aft of datum, weight in pounds).
| Point | Arm (in) | Weight (lbs) |
|---|---|---|
| 1 | 31.0 | 1,000 |
| 2 | 31.0 | 1,350 |
| 3 | 32.65 | 1,670 |
| 4 | 36.5 | 1,670 |
| 5 | 36.5 | 1,000 |
Data reliability and sources
Reliability:estimated reference values · Last verified: 2026-10-14
Sources:
- FAA TCDS 3A19 Rev. 50, Sección IX Model 152: https://dyzz9obi78pm5.cloudfront.net/app/image/id/615b69bfb50d81224e7b245f/n/3a19-rev-50.pdf
- Cessna Model 152 Pilot's Operating Handbook (1979), Secciones 2 y 6 (copia de referencia para instrucción): https://www.touringmachine.com/PDFs-Txt/Cessna-152_POH.pdf
Pending verification:
- Peso vacío y brazo de la aeronave individual (obligatorio: W&B Report propio)
- Tanques long range (37.5 gal usables a 39.5") no modelados: solo tanques estándar
- Peso de rampa 1675 lbs (5 lbs para puesta en marcha y rodaje) no modelado
- Límite combinado de equipaje (áreas 1 + 2 ≤ 120 lbs) no validado automáticamente
- Asiento infantil opcional en área 1 no modelado
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 Cessna 152 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 Cessna 152 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 Cessna 152?
The reference maximum takeoff weight of the Cessna 152 is 1,670 lbs (757 kg), per TCDS# 3A19 Revision 50 (FAA). Always confirm it in your aircraft's POH/AFM.
What are the CG limits of the Cessna 152?
The Cessna 152 CG must be between 31.0" (forward limit) and 36.5" (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 Cessna 152?
Yes, as a reference. Every Cessna 152 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.