Canadair 41 Tutor (CL41)
Published characteristics for the Canadair 41 Tutor from the FAA Aircraft Characteristics Database, with its airport-design classifications per FAA AC 150/5300-13B Change 1. Values the FAA does not publish are shown as “—”. Plan conforming taxiway intersections and fillets for this aircraft in Taxi Stubber, or compare aircraft in the interactive lookup.
Design classifications
| Airplane Design Group (ADG) | I (computed per AC 150/5300-13B) |
| Taxiway Design Group (TDG) | 1A (FAA-assigned) |
| Aircraft Approach Category (AAC) | — |
Aircraft characteristics
| FAA designator | CL41 |
| ICAO code | CL41 |
| Manufacturer | CANADAIR |
| Model | Canadair 41 Tutor |
| Approach speed | — |
| Wingspan (without winglets) | 32 ft |
| Wingspan (with winglets) | 32 ft |
| Length | — |
| Tail height | 9.4 ft |
| Wheelbase | 12.5 ft |
| Cockpit to main gear (CMG) | 12.5 ft |
| Main gear width (MGW) | 14.3 ft |
| Max takeoff weight (MTOW) | 7,787 lb |
| Max landing weight (MALW) | — |
Taxiway geometry for TDG 1A
Per FAA AC 150/5300-13B Change 1, Appendix J, a taxiway designed for this aircraft's Taxiway Design Group uses:
| Taxiway width | R-Fillet (90°) | R-CL (90°) | R-Outer (90°) |
|---|---|---|---|
| 25 ft | 0 ft | 19 ft | 32 ft |
Example airports with runways for the Canadair 41 Tutor
Airports whose longest open paved runway is at least 3,200 ft long and 60 ft wide — an illustrative planning heuristic based on this aircraft's design group and maximum takeoff weight, not a performance calculation. Actual requirements vary with weight, weather, elevation, and operator rules. Browse all airports →
Design a taxiway for the Canadair 41 Tutor →
Related aircraft
Source: FAA Aircraft Characteristics Database. For conceptual planning only — verify all values against current FAA publications and manufacturer documents. Browse all aircraft →