Cessna P-337 Skymaster

Year 1974
Type Multi-Engine
Make Cessna
Model P-337 Skymaster
Price $159,000
Registration N4BF
Serial P3370190
Total Time 2320
SMOH 650/650 SFOH
Location NY


ULTIMATE Pressurized / DeIced low-time Skymaster!!  LOADED!!

1974 Cessna P-337 Skymaster (T337G):

Awesome low-time pressurized Skymaster!  Amazing avionics plus de-ice equipped too!

You will NOT find another P-337 like this one.  GREAT value and attractively priced!

Hurry!  Call Manny at AirplanesUSA today! (954) 359-6000.

Ser. # P3370190


2320 TT Since New
No damage history

Engine Specs:

Continental TSIO-360-C Engines (225 HP each, TBO=1400)
Both 650 SFOH (Jan. 2003)
Teflon engine hoses
JPI 1200 Graphic Engine Monitor
Shadin Digital Fuel Flow Monitor


Both overhauled Dec. 2011
New blades (front) Dec. 2011
Prop sync meter


Next annual inspection due May 1, 2016
Next pitot-static inspection due Nov.1, 2015
All logbooks


Garmin GMA 340 Audio Panel with music input and auto mute for radio transmissions
Garmin GNS 530 WAAS Nav/Com GPS with moving map
Garmin GNS 430 WAAS Nav/Com GPS with moving map
Garmin GTX 327 Digital Transponders with encoders (2)
Garmin LOC-VOR-G/S Indicators (2)
Aspen EFD 1000 Pro PFD
Aspen EFD 1000 MFD with external battery
Aspen EWR Satellite System (XM weather)
King KRA 10A Radar Altimeter
S-Tec 65A Autopilot with Altitude pre-select
Avidyne TAS 605 Traffic
Insight Strikefinder
Electric Attitude Indicator
Pneumatic Attitude Indicator
Standby Altimeter
Davtron digital clock
Note: Aspen equipment warrantee extended for 2 years in August, 2015.

Year Interior:

Good general condition
Leather seating and side panels
5 Seats: 2 crew, middle row bench seat + 1 rear seat
Aux panel lights with auto emergency power (if less than 28v)
Aux oxygen bottle
Rosen sun visors

Year Exterior:

Good general condition
White with Red/Gold stripe paint scheme
Whelen LED landing and taxi lights
Whelen strobe lights

RT Aerospace gear door STC modification
De-icing: wing and horizontal stabilizer boots, electric windshield, heated pitot-static system, hot front prop.
Concorde lead acid battery
Electric trim
Useful load = 1,428 lbs.

Aircraft location:
Aircraft is hangared in Long Island, NY

Call Manny Camacho at AirplanesUSA (954) 359-6000.
Aircraft may be seen by appointment.
AirplanesUSA always encourages proper pre-purchase inspections.
Information provided is believed accurate although not guaranteed.
Flight times may vary with normal aircraft utilization.
Aircraft may be subject to prior sale or withdrawal from the market.
** See www.AirplanesUSA.com for the latest photos and details. **


Cessna P337



Two Continental TSIO-360-CB, 225 hp at 2,800 rpm

Recommended TBO

1,400 hr


McCauley constant-speed, full-feathering, 76-in diameter


29 ft 10 in


9 ft 2 in


38 ft 2 in

Wing area

202.5 sq ft

Wing loading

23.2 lb/sq ft

Power loading

10.4 lb/hp



Cabin length

10 ft 7 in

Cabin width

3 ft 6 in

Cabin height

4 ft 2 in

Empty weight

3,218 lb

Maximum gross weight

4,700 lb

Useful load

1,482 lb

Payload w/full fuel

594 lb

Fuel capacity, std

151 gal (148 gal usable)
906 lb (888 lb usable)

Oil capacity, ea engine

8 qt


Takeoff distance, ground roll

945 ft

Takeoff distance over 50-ft obstacle

1,500 ft

Max demonstrated crosswind component

12 kt

Rate of climb, sea level, two engine

1,170 fpm

Rate of climb, 10,000 feet, two engine

1,010 fpm

Rate of climb, sea level, one engine

375 fpm

Rate of climb, 10,000 feet, one engine

245 fpm

Max level speed, 20,000 feet

212 kt

Cruise speed/endurance w/45-min rsv, std fuel (fuel consumption, total)

@ 75% power, best economy, 10,000 ft

186 kt/4.9 hr (26.3 gph/158 pph)

@ 75% power, best economy, 20,000 ft

205 kt/4.8 hr (26.5 gph/159 pph)

@ 65% power, best economy, 10,000 ft

177 kt/5.6 hr (23.3 gph/140 pph)

@ 65% power, best economy, 20,000 ft

192 kt/5.6 hr (23.3 gph/140 pph)

Service ceiling

20,000 ft

Landing distance over 50-ft obstacle

1,675 ft

Landing distance, ground roll

795 ft

Limiting and Recommended Airspeeds

VX (best angle of climb)


VY (best rate of climb)


VYSE (best single-engine rate of climb)


VA (design maneuvering)

139 KIAS

VFE (max flap extended, one-third flaps)

165 KIAS

VFE (max flap extended, full)

110 KIAS

VNO (max structural cruising)

169 KIAS

VNE (never exceed)

205 KIAS

VS1 (stall, clean)


VSO (stall, in landing configuration)


All specifications are based on manufacturer´s calculations. All performance figures are based on standard day, standard atmosphere, sea level, gross weight conditions unless otherwise noted.

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