Aircraft › Cessna › 172 › 172F
The Cessna 172F 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 2,300 lb and 36 U.S. gallons of usable fuel.
Cessna 172F Weight and Balance Calculator →
Cessna 172F specifications
| Manufacturer | Cessna |
|---|---|
| Model | 172F |
| Production years | 1965 |
| Certification | FAA 3A12 |
Cessna 172F weights and capacities
| Maximum takeoff weight | 2,300 lb |
|---|---|
| Maximum landing weight | 2,300 lb |
| Maximum baggage | 120 lb combined |
Cessna 172F 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 172F history and development
The Cessna 172F is associated with the 1965 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 172F certification and applicability
| FAA type certificate | 3A12 |
|---|---|
| Production period | 1965 |
| Category represented | Normal |
| Configuration | Landplane |
Cessna 172F fuel capacity
The source-linked configuration represents 36 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 172F configurations and applicability
Cessna 172F normal-category landplane configuration
Applicability: Cessna 172F configuration represented by FAA TCDS 3A12.
| Maximum takeoff weight | 2,300 lb |
|---|---|
| Maximum landing weight | 2,300 lb |
| Usable fuel | 36 US gal |
Configuration sources: FAA: FAA TCDS 3A12, Model 172F normal-category landplane
Cessna 172F model applicability and configuration
This page represents the Cessna 172F normal-category landplane configuration supported by FAA TCDS 3A12, Model 172F normal-category landplane.
Verify serial-number applicability, installed equipment, supplements, modifications and the current aircraft weight and balance record before flight.
Cessna 172F vs Cessna 172G
| Specification | Cessna 172F | Cessna 172G |
|---|---|---|
| Maximum weight | 2,300 lb | 2,300 lb |
| Usable fuel represented | 36 US gal | 36 US gal |
| Production period | 1965 | 1966 |
Cessna 172F weight and balance
The source-linked calculator represents a maximum takeoff weight of 2,300 lb and maximum landing weight of 2,300 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 172F Weight and Balance Calculator →
Cessna 172F frequently asked questions
What maximum weight does the Cessna 172F configuration use?
The source-linked normal-category landplane configuration uses a maximum takeoff and landing weight of 2,300 lb.
How much usable fuel is represented for the Cessna 172F?
The source-linked configuration represents 36 U.S. gallons of usable fuel at a loading arm of 48 inches.
What category is the Cessna 172F 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 172F?
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 172F normal-category landplane
Related 172 models
- Cessna 172G - 1966