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1973 Commander 690A for sale

1973 Commander 690A

Multi Engine Turboprop

Contact for Price
Location OH
Total Time 10,103 hrs
Seats 7
Reg # PR-GES Brazil
Cruise 280 kts (519 km/h)
✓ Clean NTSB

Listing Details

Seller reported
Year
1973
Make
Commander
Model
690A
Total Time
10,103 hr
Location
OH
Seller
FX Solutions
Source
aircraftdealer.com
> Peter Schiff CCU > Recent Prop Overhauls > ADS-B Out > Garmin Flight Deck > Supreme Commander Mod > Certified Known Ice Airframe: Total Time: 10,103 Total Landings: 12,033 Engines: Engine 1: Honeywell TPE331-10T-515K Serial Number: P-79177C (Left Engine) Hours: 9,852 Cycles: 12,006 Hot Section Due: 11,652 Hrs GBI Due: 11,589 Hrs Engine 2: Honeywell TPE331-10T-515K Serial Number: P-79211C (Right Engine) Hours: 9,696 Cycles: 11,915 Hot Section Due: 11,496 Hrs GBI Due: 11,433 Hrs Props: MT MTV-27-1-E-C-F-R(G) Serial Number: 230397 (Left Prop) Hours: 204.5 MT MTV-27-1-E-C-F-R(G) Serial Number: 230398 (Right Prop) Hours: 204.5

Commander 690A — Model Specs

Model specification

Standard specs for this model. Actual aircraft may differ.

Seats
7
Cruise Speed
280 kts (519 km/h)
Range
1,300 nm (2,408 km)
Ceiling
31,000 ft (9,449 m)
Useful Load
2,500 lbs (1,134 kg)
Horsepower
717 HP
Fuel Burn
70 GPH (265 L/h)
Engines
2

Estimated Cost of Ownership

AeroGurus estimate

Fuel Burn
70.0 GPH
~$455/hr
Variable Cost
$359/hr
fuel + mx + reserves

AeroGurus estimates based on industry averages for the . Actual costs vary by location, usage, maintenance history, and configuration. Not a financial quote.

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Commander 690A loan calculator

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About the Commander 690A

The Commander 690A is a twin-turboprop Aero Commander for buyers who want rugged utility, high-wing visibility, and legacy turbine capability in a distinctive platform. It is not a mainstream King Air substitute; support familiarity, engine type, inspections, and structural history matter heavily. Compared with piston Commanders, the 690A moves into turbine economics; compared with a King Air, it is more niche and support-path dependent.

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