Aircraft Category
Aircraft category in aviation refers to performance-based groupings, especially for approach speeds, which determine instrument approach minima and protected ai...
Approach category is an aviation classification based on aircraft approach speed at maximum certificated landing weight, governing instrument approach minima and safety margins.
Approach category is a regulatory classification that groups aircraft by their approach speed—specifically, the reference landing speed (VREF) or 1.3 times the stalling speed in landing configuration (VSO)—measured at the aircraft’s maximum certificated landing weight. This classification is codified in international and national regulations, including ICAO Doc 8168, 14 CFR 97.3, and FAA Advisory Circulars. The approach category is a permanent certification feature of each aircraft and is not variable based on actual landing weight, actual approach speed, or operational conditions.
All instrument approach procedures (IAPs) and approach charts use approach categories to define the applicable minima for decision altitude (DA), minimum descent altitude (MDA), and visibility. These minima ensure obstacle clearance and safe maneuvering by accounting for the different speeds, turn radii, and performance characteristics of each category.
The approach category is calculated using these parameters and does not change unless the aircraft’s maximum certificated landing weight is officially amended.
| Category | VREF / 1.3 VSO (knots) | Typical Aircraft | Circling Protected Area Radius (NM) |
|---|---|---|---|
| A | < 91 | Cessna 172, Piper Archer | 1.3 |
| B | 91 – 120 | King Air C90, Beech Baron | 1.5 |
| C | 121 – 140 | Embraer 145, Challenger 350 | 1.7 |
| D | 141 – 165 | Boeing 737-900, Gulfstream G550 | 2.3 |
| E | ≥ 166 | F-16, B-1B Lancer (military only) | 4.5 |
The approach category is fixed at certification and recorded in the aircraft’s documentation. It is not affected by actual in-flight weight, modifications, or the speed flown on a given approach—except when the aircraft’s maximum certificated landing weight is formally revised by the manufacturer and regulatory authority.
Key points:
All IAPs provide minima for each approach category. These minima are based on the maneuvering speeds and turn radii of aircraft within each category. Pilots must use the minima for their certified approach category, or the next higher if operational speed exceeds their category’s upper limit.
A Challenger 350 (Category C, VREF 137 knots) must use Category C minima. If operationally forced to fly at 145 knots (above C limit), the pilot must use Category D minima.
Circling approaches require lateral maneuvering to a runway not aligned with the approach course. The circling protected area is determined by the approach category, providing obstacle clearance based on the maximum allowed speed for each category.
| Category | Circling Speed Limit (KIAS) | Protected Area Radius (NM) |
|---|---|---|
| A | 100 | 1.3 |
| B | 135 | 1.5 |
| C | 180 | 1.7 |
| D | 205 | 2.3 |
| E | 240 | 4.5 |
Exceeding speed or using lower minima risks exiting the protected area and losing obstacle clearance.
If operational needs require flying at a higher speed than your category’s limit, you must use the next higher category minima. If those minima are not published, exercise extra caution and ensure maneuvering remains within the appropriate protected area.
Considerations:
To legally lower an aircraft’s approach category, the manufacturer must issue a service bulletin reducing the maximum certificated landing weight, and the regulatory authority must approve this change. Once documented, the approach category is recalculated, and the aircraft may use the lower minima.
Example:
A Gulfstream G450 with a reduced max landing weight, after regulatory approval and documentation update, changes from Category D to C.
Aircraft: Embraer Legacy 600 (Category C)
Scenario: Icing requires 145 knots circling speed.
Action: Use Category D minima and ensure maneuvering remains within the 2.3 NM radius.
Operator: Mixed-fleet business jet company
Practice: All approaches briefed for certified category; SMS tracks approaches exceeding certified speed.
Aircraft: Gulfstream G450
Modification: Reduced max landing weight.
Result: Official change to Category C, authorized to use lower minima.
| Category | VREF / 1.3 VSO (knots) | Circling Speed Limit (KIAS) | Typical Aircraft | Protected Area Radius (NM) |
|---|---|---|---|---|
| A | < 91 | 100 | Cessna 172, Piper Archer | 1.3 |
| B | 91–120 | 135 | Beech Baron, King Air C90 | 1.5 |
| C | 121–140 | 180 | Embraer 145, Challenger 350 | 1.7 |
| D | 141–165 | 205 | Boeing 737-900, Gulfstream | 2.3 |
| E | ≥ 166 | 240 | Military (F-16, B-1B) | 4.5 |
For full regulatory details, refer to:
Understanding and applying approach category correctly is vital for safe, compliant, and efficient instrument flight operations.
No. Approach category is determined by the aircraft’s reference landing speed at maximum certificated landing weight. It cannot be reduced based on actual weight for a particular flight.
You must use the approach minima for the next higher category if published. If higher minima are not available, exercise extreme caution and ensure all maneuvering remains within the protected area for the speed flown.
Only through a formal, logbook-documented revision to the aircraft’s maximum certificated landing weight, approved by the regulatory authority (FAA, EASA, etc.).
Category A: 1.3 NM, B: 1.5 NM, C: 1.7 NM, D: 2.3 NM, E: 4.5 NM (mainly military). These radii ensure obstacle clearance during circling maneuvers.
No. Only a higher category minima may be used if your actual approach speed exceeds your certified category’s upper limit. Regulatory minima are always based on certified maximum landing weight.
Ensure your operations meet regulatory standards for instrument procedures. Learn more about approach category, protected areas, and compliance for safer, more efficient flights.
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