Aircraft › Cessna › 150 / 152 › A152
The Cessna A152 Aerobat is the Aerobat variant represented by the source-linked acrobatic-category loading data. The calculator uses a maximum takeoff and landing weight of 1,670 lb.
Model-level data must be matched to the individual aircraft, installed equipment, approved modifications and current weight and balance records.
Cessna A152 Aerobat Weight and Balance Calculator →
Cessna A152 Aerobat specifications
| Manufacturer | Cessna |
|---|---|
| Model | A152 |
| Production years | 1978–1985 |
| Certification | FAA 3A19 |
Cessna A152 Aerobat weights and capacities
| Maximum takeoff weight | 1,670 lb |
|---|---|
| Maximum landing weight | 1,670 lb |
Cessna A152 Aerobat engine and configuration
| earlier serial-number range per TCDS | Lycoming O-235-L2C · earlier serial-number range per TCDS |
|---|---|
| later serial-number range / aircraft reworked per SK152-15 or SK152-16 per TCDS | Lycoming O-235-N2C · later serial-number range / aircraft reworked per SK152-15 or SK152-16 per TCDS |
Fuel capacity and configuration
| Fuel | Fuel configuration represented by the source-linked WBcalc calculator. Verify the installed fuel system and applicable approved aircraft documentation. |
|---|
Baggage and loading applicability
| Baggage | 120 lb maximum |
|---|
Cessna A152 Aerobat history and development
The Cessna A152 Aerobat is associated with the 1978–1985 production period. The source-linked configuration on this page is supported by FAA Type Certificate Data Sheet 3A19.
Cessna A152 Aerobat certification and applicability
| Source | FAA Type Certificate Data Sheet 3A19 |
|---|---|
| Production period | 1978–1985 |
| Category represented | Acrobatic |
Cessna A152 Aerobat fuel capacity
The represented configuration uses 24.5 U.S. gallons of usable fuel at a loading arm of 42 inches.
Cessna A152 Aerobat model applicability and configuration
This page represents the configuration supported by FAA Type Certificate Data Sheet 3A19. Verify serial-number applicability, installed equipment, fuel system, supplements and approved modifications for the individual aircraft.
Cessna A152 Aerobat vs Cessna 152
| Specification | Cessna A152 Aerobat | Cessna 152 |
|---|---|---|
| Maximum weight | 1,670 lb | 1,670 lb |
| Primary usable fuel represented | 24.5 US gal | 24.5 US gal |
| Category represented | Acrobatic | Utility |
| Production period | 1978–1985 | 1978–1985 |
Cessna A152 Aerobat weight and balance
The source-linked calculator represents a maximum takeoff weight of 1,670 lb and maximum landing weight of 1,670 lb.
The represented loading data includes Baggage Area 1: 120 lb maximum, arm range 50 to 76 in; Baggage Area 2: 40 lb maximum, arm range 76 to 94 in. These are station limits; do not infer a combined baggage allowance unless the applicable approved data explicitly provides one.
Enter the current empty weight and arm from the individual aircraft weight and balance record rather than using a generic empty-weight value.
Open Cessna A152 Aerobat Weight and Balance Calculator →
Cessna A152 Aerobat frequently asked questions
What maximum weight does the Cessna A152 Aerobat configuration use?
The source-linked configuration represented by WBcalc uses a maximum takeoff and landing weight of 1,670 lb.
How much usable fuel is represented for the Cessna A152 Aerobat?
The primary represented fuel configuration uses 24.5 U.S. gallons of usable fuel. Where multiple tank options are listed, the installed configuration must be verified.
What category is the Cessna A152 Aerobat represented in?
The source-linked calculator represents the acrobatic-category configuration.
Reference sources
FAA: FAA Type Certificate Data Sheet 3A19
Related 150 / 152 models
- Cessna 152 - 1978–1985