1985 King Air C90A

N316MD | LJ-1104

HX Assessment

A King Air C90A configured for owners seeking turbine performance, cabin-class comfort, and a meaningful performance upgrade over the standard platform. With Blackhawk PT6A-135A engines, Raisbeck enhancements, Garmin avionics, and complete records since new, this aircraft reflects a practical modernization of a proven turboprop design.

Time and Utilization

Airframe

9,130.6 hours AFTT

Left Hand Engine/Prop

146.8 hours SMOH

Right Hand Engine/Prop

146.8 hours SMOH

Damage History Disclosure

No known damage history reported in logbooks

HX Perspective

The King Air C90A represents one of the most refined iterations of the original C90 concept, retaining the size and operating profile that made the early King Airs successful while incorporating improvements that enhanced utility, comfort, and day-to-day operation. Positioned below the larger 200-series aircraft, the C90A provides owners with a pressurized cabin, turbine reliability, and executive transportation capability without the acquisition costs, fuel consumption, and operational demands associated with larger turboprops. Its enduring appeal stems from this balance. The aircraft offers a meaningful step beyond piston twins while remaining approachable for owner-operators and small flight departments. Decades after production, the C90A continues to occupy a distinct place in the market because the platform remains highly adaptable to modern avionics, performance upgrades, and evolving mission requirements. For many operators, the C90A represents not the smallest King Air, but the point at which capability, complexity, and operating economics come into alignment.

Ownership suitability ultimately depends on mission profile, operating philosophy, and maintenance expectations, which are best evaluated in direct conversation.

Configuration and Systems

The following reflects the aircraft’s installed configuration and systems; suitability depends on mission and operating expectations.

Avionics & Flight Deck

Modern Garmin-based IFR panel centered around a GDU-620 PFD, GTN 650, GNS 530W, ADS-B compliance, weather, traffic, and a KFC-250 autopilot.

Engines & Powerplant

Blackhawk PT6A-135A engine conversion increases output to 750 SHP per side, enhancing climb performance and supporting the aircraft’s upgraded mission profile.

Approved Modifications

Raisbeck performance package includes Quiet Turbofan four-blade propellers, aft body strakes, and a gross weight increase to 10,350 pounds.

Cabin Configuration

Executive cabin with center club seating, dual work tables, forward refreshment cabinet, and aft lavatory supporting regional business and family travel.

Maintenance Status

Complete logbooks since new, no reported damage history, and recent completion of major inspection and recurring maintenance requirements.

Mission Capability

Well-suited for owners seeking turbine reliability, pressurization, and executive transportation capability without the size and operating costs of larger King Air models.