Aircraft › Cessna › 150 / 152 › A150L
The Cessna A150L Aerobat is the Aerobat variant represented by the source-linked acrobatic-category loading data. The calculator uses a maximum takeoff and landing weight of 1,600 lb.
Model-level data must be matched to the individual aircraft, installed equipment, approved modifications and current weight and balance records.
Cessna A150L Aerobat Weight and Balance Calculator →
Cessna A150L Aerobat specifications
| Manufacturer | Cessna |
|---|---|
| Model | A150L |
| Production years | 1971–1974 |
| Certification | FAA 3A19 |
Cessna A150L Aerobat weights and capacities
| Maximum takeoff weight | 1,600 lb |
|---|---|
| Maximum landing weight | 1,600 lb |
Cessna A150L Aerobat engine and configuration
| Engine | Continental O-200-A |
|---|
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 A150L Aerobat history and development
The Cessna A150L Aerobat is associated with the 1971–1974 production period. The source-linked configuration on this page is supported by FAA Type Certificate Data Sheet 3A19.
Cessna A150L Aerobat certification and applicability
| Source | FAA Type Certificate Data Sheet 3A19 |
|---|---|
| Production period | 1971–1974 |
| Category represented | Acrobatic |
Cessna A150L Aerobat fuel capacity
The represented configuration uses 22.5 U.S. gallons of usable fuel at a loading arm of 42 inches.
Cessna A150L 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 A150L Aerobat vs Cessna A150M Aerobat
| Specification | Cessna A150L Aerobat | Cessna A150M Aerobat |
|---|---|---|
| Maximum weight | 1,600 lb | 1,600 lb |
| Primary usable fuel represented | 22.5 US gal | 22.5 US gal |
| Category represented | Acrobatic | Acrobatic |
| Production period | 1971–1974 | 1975–1977 |
Cessna A150L Aerobat weight and balance
The source-linked calculator represents a maximum takeoff weight of 1,600 lb and maximum landing weight of 1,600 lb.
The represented loading data includes Baggage Area 1: 120 lb maximum; Baggage Area 2: 40 lb maximum. 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 A150L Aerobat Weight and Balance Calculator →
Cessna A150L Aerobat frequently asked questions
What maximum weight does the Cessna A150L Aerobat configuration use?
The source-linked configuration represented by WBcalc uses a maximum takeoff and landing weight of 1,600 lb.
How much usable fuel is represented for the Cessna A150L Aerobat?
The primary represented fuel configuration uses 22.5 U.S. gallons of usable fuel. Where multiple tank options are listed, the installed configuration must be verified.
What category is the Cessna A150L 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 A150M Aerobat - 1975–1977