1977 CESSNA 337G SOLD
No longer listed as of May 2026. The price below is the last asking price — the final sale price is not disclosed.
No photo available
Contact for Price
- Year
- 1977
- Make
- Cessna
- Model
- 337G
- Total Time
- 2,829 hr
- Location
- TX
- Seller
- Lisa Hutton
- Source
- avpay.aero
Listing closed
View similar 337G for sale →
Performance & Capacity
- Seats
- 6
- Cruise
- 175 kts
- Max Speed
- 142 kts
- Range
- 900 nm
- Useful Load
- 1,400 lbs
- Burn
- 18.0 gph
- Engines
- 2 · Reciprocating
- Power
- 210 hp
- MTOW
- 12,500 lbs
- ICAO Type
- C337
Manufacturer-published specs for the Cessna 337G model. Actual aircraft may vary by configuration / modifications.
Operating Cost (est.)
- Hourly Variable
- $260
- Annual Fixed
- $25,000
- Engine Overhaul
- $25,000
- TBO
- 1,500 hrs
AeroGurus estimates based on industry averages for the Cessna 337G. Actual costs vary by location, usage, maintenance history, and configuration.
Market price band
Cessna 337G typical:
$110,000 – $174,900
median $111,999
across 7 active listings
Description
Airframe
1977 Cessna 337G
Registration: N53704
S/N: 33701795
Cessna Cargo Pack
Date of annual: September 2023
Fuel Capacity: 148 gallon usable
Stall Speed: 68 mph
Useful Load: 1539.29
Range: 1,200 miles
Cruise speed: 195 mph
Engine
Front Engine: Continental IO-360-G
S/N: 352671
Time SMOH: 1753.1
Front Engine Overhaul: April 28, 2000
Oil Consumption: 13.0 Hours/Quart
Compressions 9/23: (1) 74 (2) 75 (3) 72 (4) 75 (5) 67 (6) 73
Rear Engine: Continental IO-360-G
S/N: 1031594
Time SNEW: 973.5
Rear Engine Installed: May 1, 1997
Oil Consumption: 11.0 Hours/Quart
Compressions 9/23: (1) 72 (2) 74 (3) 72 (4) 71 (5) 70 (6) 70
Blackstone Labs providing engine oil analysis, complete report history available
Air Wolf Air/Oil Separator & STC on front engine to protect cargo pack from oil blow back.
Challenger permanent oil filters & STC on both engines. Additional O-Rings & cores included. Gaskets for 8 additional oil changes are included. Two filter cores are also included, to be changed at 500 hrs TIS. Current cores only have 69 hrs TIS. O-Rings & cores are readily available through Aircraft Spruce.
GAMI Fuel Injectors
Insight G4T, complete engine monitor integrated with TAS-1000 air data & fuel computer. Fuel computer integrated with 430Ws flight planning data for destination & alternate fuel. Data stored with SAVVY.
Propeller
Front Propeller: McCauley D2AF34C310
S/N: 150438
Installed: November 22, 2016
Time SNEW: 689
Rear Propeller: McCauley D2AF34C307-A
S/N: 170011
Installed: February 17, 2017
Time SNEW: 642.3
Avionics
Aspen Evolution 2500 Pro Max -Dual PFD & MFD (new installation) with AOA on PFD & MFD
Dual Garmin 430Ws (both refurbished by Garmin within the last three years
Free-Flight Interface for Aspen/Garmin communication
Garmin Flight Stream 210 (send flight plans to panel from FF or GP)
Garmin 30ES Transponder
Garmin GDL-52R ADS-B, FIS-B, and XM (in)
FreeFlight FDL-978 ADS-B RX/TX
Garmin GMA-340/ICS integrated with XM Radio
Insight Strike Finder, heading stabilized, lightning strike system. At last annual unit returned for LED display upgrade
Insight TAS-1000 Air Date Computer fully integrated with Garmin 430Ws
Insight Windicator. Wind direction & velocity indicator (easier to visualize than Garmin displays)
Cessna 400A autopilot maintained by Autopilots Central. Integrated with Aspen’s and Garmin’s for LPV approaches.
During the Aspen installation, every wire between the firewall & panel was identified via P/N & the Cessna 337 Avionics Manual, each wire was inspected & tested. Wires that showed any aging or were replaced after testing were marked with P/N+”R”. Wires from old installations were removed. All the Cessna wires are in appropriate bundles as well as the Aspen. Garmin & Insight Harness, Complete harnesses can be removed for bench checking. This was a very painstaking process, but ensures the avionics are as if in a new airframe.
Additional Features
SK 337-40C Fuel Cap/Doors-Prevents misfueling with Jet fuel.
SK 337-46A Alternator Restart Pack
RT Aerospace Main Landing Gear Removal STC – Significantly improves SE climb performance during landing gear retraction.
Arctic Air Real A/C “Puron” air conditioner. Mounted in the rear baggage area, easily removed. Digital controller on panel.
Aerox 22cf portable oxygen bottle, secured under rear seat. Four port regulator with four flow adjustable cannulas.
5th & 6th child seats removed for air conditioner
Cessna 400 Series voltage regulators installed via 337
During Aspen installation, circuit breaker panel was replaced & all breakers were replaced with pullable breakers. Panel was replacarded to reflect the equipment changes.
Precision vertical mount compass.
Fire/Gear monitor mirror on each wing.
Rosen Sun Visors STC.
Lightspeed headsets (4)
24 volt batterminder battery trickle charger with temperature sensor.
Aircraft on SavvyQA (Maintenance advice, breakdown assistance & engine data analysis)
Exterior
The aircraft’s exterior boasts a pristine white base adorned with rich emerald green & gold accents. The deep green hue takes center stage, forming a striking stripe along the fuselage that widens towards the rear from a focal point. The distinctive boom tail mirrors this bold shade of green, serving as its primary color scheme. Delicate gold embellishments trace the edges of the green, accentuating smaller details & highlighting the clean contrast of the N number. At the nose, a gray finish complements a black propeller accented by a subtle white stripe & a pristine white tip.
Interior
Boarding this aircraft is a breeze thanks to its accessible entry, & once inside, you’ll find ample space to accommodate either four seats with the air conditioner or six seats if it’s removed. The tan leather seats are impeccably maintained, ensuring a comfortable flight regardless of duration. The interior panels are adorned in a light tan hue, com
About the Cessna 337G
The Cessna 337G Skymaster is a six-seat, twin-engine piston aircraft with the unique push-pull centerline thrust configuration. Burning approximately 18 gallons per hour total, the 337G eliminates asymmetric thrust hazards in an engine failure, making it the safest conventional twin for single-engine operations. It appeals to practical pilots who value twin-engine safety without the complexity of managing critical engines.
Produced 1973–1976.