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Piper PA-30 Turbo Twin Comanche/Turbo Twin Comanche (PA30)

Published characteristics for the Piper PA-30 Turbo Twin Comanche/Turbo Twin Comanche 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)A

Aircraft characteristics

FAA designatorPA30
ICAO codePA30
ManufacturerPIPER
ModelPiper PA-30 Turbo Twin Comanche/Turbo Twin Comanche
Approach speed76 kt
Wingspan (without winglets)25.2 ft
Wingspan (with winglets)25.2 ft
Length
Tail height8.3 ft
Wheelbase7.3 ft
Cockpit to main gear (CMG)7.3 ft
Main gear width (MGW)10 ft
Max takeoff weight (MTOW)3,600 lb
Max landing weight (MALW)3,600 lb

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 widthR-Fillet (90°)R-CL (90°)R-Outer (90°)
25 ft0 ft19 ft32 ft

Example airports with runways for the Piper PA-30 Turbo Twin Comanche/Turbo Twin Comanche

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 Piper PA-30 Turbo Twin Comanche/Turbo Twin Comanche →

Related aircraft

Source: FAA Aircraft Characteristics Database. For conceptual planning only — verify all values against current FAA publications and manufacturer documents. Browse all aircraft →