Aircraft › Cessna › 172 › 172A
The Cessna 172A is represented here by the source-linked normal-category landplane configuration from FAA Type Certificate Data Sheet 3A12.
The represented configuration uses a maximum takeoff and landing weight of 2,200 lb and 37 U.S. gallons of usable fuel.
Cessna 172A Weight and Balance Calculator →
Cessna 172A specifications
| Manufacturer | Cessna |
|---|---|
| Model | 172A |
| Production years | 1960 |
| Certification | FAA 3A12 |
Cessna 172A weights and capacities
| Maximum takeoff weight | 2,200 lb |
|---|---|
| Maximum landing weight | 2,200 lb |
| Maximum baggage | 120 lb combined |
Cessna 172A engine and configuration
| Configuration 1 | Continental · O-300-C · 145 hp · @ 2,700 rpm |
|---|---|
| Configuration 2 | Continental · O-300-D · 145 hp · @ 2,700 rpm |
Fuel capacity and configuration
| Fuel | Fuel quantity and loading arm correspond to the normal-category landplane configuration represented by the source-linked FAA TCDS 3A12 data. |
|---|
Cessna 172A history and development
The Cessna 172A is associated with the 1960 production period. This page is limited to verified model-specific loading and certification information rather than attempting to generalize data across other Cessna 172 variants.
Cessna 172A certification and applicability
| FAA type certificate | 3A12 |
|---|---|
| Production period | 1960 |
| Category represented | Normal |
| Configuration | Landplane |
Cessna 172A fuel capacity
The source-linked configuration represents 37 U.S. gallons of usable fuel at a loading arm of 48 inches.
Fuel capacity and loading data must be matched to the exact model and approved aircraft configuration rather than copied from another Cessna 172 variant.
Cessna 172A configurations and applicability
Cessna 172A normal-category landplane configuration
Applicability: Cessna 172A configuration represented by FAA TCDS 3A12.
| Maximum takeoff weight | 2,200 lb |
|---|---|
| Maximum landing weight | 2,200 lb |
| Usable fuel | 37 US gal |
Configuration sources: FAA: FAA TCDS 3A12, Model 172A normal-category landplane
Cessna 172A model applicability and configuration
This page represents the Cessna 172A normal-category landplane configuration supported by FAA TCDS 3A12, Model 172A normal-category landplane.
Verify serial-number applicability, installed equipment, supplements, modifications and the current aircraft weight and balance record before flight.
Cessna 172A vs Cessna 172B
| Specification | Cessna 172A | Cessna 172B |
|---|---|---|
| Maximum weight | 2,200 lb | 2,200 lb |
| Usable fuel represented | 37 US gal | 39 US gal |
| Production period | 1960 | 1961 |
Cessna 172A weight and balance
The source-linked calculator represents a maximum takeoff weight of 2,200 lb and maximum landing weight of 2,200 lb.
The represented baggage station is limited to 120 lb.
Enter the current empty weight and arm from the individual aircraft weight and balance record. Do not substitute generic empty-weight or loading data from another 172 model.
Open Cessna 172A Weight and Balance Calculator →
Cessna 172A frequently asked questions
What maximum weight does the Cessna 172A configuration use?
The source-linked normal-category landplane configuration uses a maximum takeoff and landing weight of 2,200 lb.
How much usable fuel is represented for the Cessna 172A?
The source-linked configuration represents 37 U.S. gallons of usable fuel at a loading arm of 48 inches.
What category is the Cessna 172A represented in?
The calculator and reference page represent the normal-category landplane configuration supported by FAA TCDS 3A12.
Can data from another Cessna 172 model be used for the Cessna 172A?
Not automatically. Maximum weight, fuel quantity, loading stations and other approved data can differ between 172 variants, so use the documentation applicable to the individual aircraft.
Reference sources
FAA: FAA TCDS 3A12, Model 172A normal-category landplane
Related 172 models
- Cessna 172B - 1961