Range Map

Origin: · two fingers to move map

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1

Tank-dry, where fuel runs out at catalogue's stored cruise burn.

Excludes reserves: range beyond the dashed circle requires a leaner cruise than what we store. Great-circle, still air, book cruise. Estimates only: always verify against the POH.

Payload vs. Range

Occupants:

Fuel on board

Cargo

nm

Range

Cargo is additional payload after occupants and baggage.
full tanks
Available Range / nm
Mission capable. This load flies with full fuel.
Fuel reduced by . left aboard for nm range.
Over max payload by . At this load it cannot lift a single occupant.

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Mission Profile

Used market Only available used
190
KTAS
Cruise Speed
1,155
nm
Max Range
20,000
ft
Service Ceiling
5
Occupants
751
lbs
Wet Payload
Endorsements & ratings:
  • High-Performance
  • Complex
  • Pressurization
  • Multi-Engine
Cessna P337G Pressurized Skymaster. Photo: Pedro Aragão, CC BY-SA 3.0.
Cessna P337G Pressurized Skymaster. Photo: Pedro Aragão, CC BY-SA 3.0.

Estimated Ownership Costs

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About the Cessna P337 Pressurized Skymaster

Type certificated 1977

Overview

The Cessna P337 Pressurized Skymaster is the top of the push-pull line: a turbocharged, pressurised twin that keeps the Skymaster’s centerline-thrust safety while adding flight-levels comfort and near-200-knot cruise. Pressurisation seals the cabin and lets the airplane climb above much of the weather, directly addressing the standard Cessna 337 Skymaster’s two weakest points: noise and cruise speed. Production ran from 1973 (T337G-P) through the P337H of 1977 to 1980; specifications here reflect the P337H on FAA TCDS A6CE.

Like every Skymaster, the P337 carries one engine forward as a tractor and one aft as a pusher on the fuselage centerline, so an engine failure brings no yaw, no critical engine, and no V_mc hazard. It is, in effect, a pressurised cabin twin with the single-engine handling of a high-performance single.

Key Features for GA Buyers

  • Pressurised comfort. Pressurisation holds a roughly 10,000-foot cabin at the 20,000-foot certified ceiling, cutting fatigue on long cross-country legs and largely solving the standard 337’s notorious cabin noise.

  • Turbocharged altitude performance. Two turbocharged Continental TSIO-360-C engines (225 hp each) hold power into the flight levels, delivering true airspeeds around 190 knots, a genuine step up from the naturally-aspirated 337’s 144 KTAS.

  • Centerline-thrust safety. The P337 keeps the docile single-engine behavior of the line. Losing an engine degrades climb but produces no dangerous yaw, and the airplane requires the same centerline-thrust multi-engine rating rather than a conventional twin rating.

  • Range. With 148 gallons usable, the P337 reaches roughly 1,150 nm with reserves at altitude, meaningfully more than the standard 337.

Trade-offs

  • Highest complexity in the line. Two turbocharged engines, a pressurisation system, two propellers, and the complex gear make the P337 the most demanding Skymaster to own and maintain. Annual inspection costs run around $4,000 or more.
  • Shorter TBO and pricier overhauls. The turbocharged TSIO-360-C carries a 1,400-hour TBO, shorter than the naturally-aspirated IO-360, and turbo overhauls cost more, budget on the order of $52,000 per engine, roughly $103,000 for the pair.
  • Turbo and pressurisation upkeep. Turbochargers, intercoolers, door seals, and pressurisation controllers are recurring expenses the standard 337 never sees. Confirm system condition carefully on any prebuy.
  • Wing spar inspections. The recurring FAA wing spar airworthiness directive applies (initial at 10,000 hours on pressurised airframes, then every 500 hours). Verify compliance before purchase.
  • Rear-engine thermal load. As with every Skymaster, the rear pusher runs hot in its enclosed cowl and typically reaches TBO first.
  • Niche rating and resale. The centerline-thrust rating and small fleet limit the pool of qualified pilots, instructors, and insurers. Plan training and resale around a thin market.

See Also

  • Cessna 337 Skymaster – the naturally-aspirated, unpressurised sibling; lower cost and complexity, slower cruise, no flight-levels capability. Compare
  • Piper PA-34 Seneca – a conventional turbocharged twin in the same class; faster and more common, with the V_mc considerations the Skymaster avoids. Compare
  • Beechcraft Baron 58 – the larger, faster conventional cabin twin; stronger cruise and payload at a higher price and full V_mc exposure. Compare
  • Cessna 310 – Cessna’s conventional cabin-class twin; more speed and payload, without the centerline-thrust handling. Compare

Technical Specifications

Dimensions & Weights

Wingspan 38 ft
Height
9 ft
Length
30 ft
Parking area (ft²2)
1,674 ft²
Max Takeoff Weight
4,700 lbs
Max Landing Weight
4,400 lbs
Useful Load
1,639 lbs
Fuel Capacity
148 gal

Performance

Cruise Speed
190 KTAS
Never-Exceed (VNE)
Source: FAA Type Certificate Data Sheet 205 KIAS
Max Structural Cruise (VNO)
Source: FAA Type Certificate Data Sheet 169 KIAS
Approach Speed
80 KIAS
Stall, Clean (VS1)
71 KIAS
Range
1155 NM
Service Ceiling
20,000 ft
Rate of Climb
375 - 1250 fpm
Takeoff over 50 ft obstacle
1,500 ft
Landing over 50 ft obstacle
1,675 ft

Engines

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Sources

Where the figures on this page come from. Cessna P337 Pressurized Skymaster specifications are traced to published references; estimated values are flagged inline next to the figure.

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Cruise
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Range
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