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DAHER TBM-700C2

High-performance single-engine turboprop focused on efficient IFR travel with short-field flexibility.

The DAHER (SOCATA) TBM-700C2 is a pressurized, single-engine turboprop designed to cover regional-to-cross-country missions at jet-like cruise speeds while retaining access to shorter runways than most light jets. It is typically configured for one pilot plus up to five passengers, emphasizing dispatch reliability, fast climb, and practical operating economics for owner-operators and small flight departments.

Currently for sale

Mission Alignment

The TBM-700C2 fits missions where a single pilot wants turbine performance for point-to-point travel, including high-altitude weather avoidance and terrain clearance. It works well when passenger count is limited and when the ability to use smaller airports reduces ground time. For consistently full seats, bulky luggage, or strict corporate twin/jet policies, the airframe may be a compromise.

Best For

Owner-flown IFR trips in the 300–900 nm range where speed matters
Access to shorter runways and smaller airports versus light jets
High-utilization business travel with modest passenger counts

Not Ideal For

Frequent missions requiring 6–8 passengers with full baggage
Operations that demand twin-engine redundancy or jet cabin volume

Cabin Experience

The pressurized cabin is arranged around a club-style seating concept with a forward cockpit separated from the cabin, providing a quieter, more stable ride than pistons at similar trip lengths. Cabin comfort is oriented toward functional business travel: upright seating, adequate personal space for a turboprop, and baggage accommodations suited to typical carry-on and soft luggage loads rather than large hard cases.

Configuration Notes

Typical configuration is 1+5 seating; some aircraft have a belted lavatory or alternate aft seating layouts depending on vintage and STCs.
Baggage capacity and access vary by configuration; confirm usable baggage volume with full fuel and passengers.
Cabin noise levels depend on insulation packages and propeller condition; evaluate during a representative cruise segment.

Technology & Systems

The TBM-700C2’s avionics and systems philosophy centers on workload reduction for single-pilot IFR with conventional turboprop systems architecture. Fleet avionics vary significantly by year and retrofit history, from legacy EFIS suites to modern glass upgrades, so capability should be evaluated aircraft-by-aircraft rather than assumed from model designation.

Buyer Checks

Identify the installed avionics suite (original vs retrofit) and confirm WAAS/LPV capability, ADS-B compliance, and autopilot functionality for your typical IFR use.
Review de-ice/anti-ice equipment (boots, prop heat, windshield heat, inertial separator) and verify system condition if operating in known-icing environments.
Confirm engine trend monitoring and available data (engine monitor, downloads) to support condition-based operation and early anomaly detection.

Operating Profile

Operationally, the TBM-700C2 is used for fast climbs to the mid-to-high flight levels, efficient cruise, and straightforward single-pilot handling. Runway requirements are generally compatible with many regional and community airports, but real-world performance depends on weight, temperature, elevation, and surface condition. Trip planning typically balances speed with fuel stops and payload, especially when carrying multiple passengers and baggage.

Key Triggers

If typical missions are short and frequent with low passenger counts, the turboprop profile can be a strong fit versus light jets on total trip time and operating complexity.
If missions regularly push maximum range with full seats and baggage, expect more frequent payload/range tradeoffs or additional fuel stops versus larger cabin aircraft.

Maintenance & Ownership

Supportability is generally good through established TBM service networks, but maintenance outcomes depend heavily on engine program status, compliance with airframe and avionics service bulletins, and the quality of prior maintenance records. Prebuy evaluation should focus on engine health, propeller condition, pressurization integrity, and corrosion/structural inspection items typical for the type and age range.

Watch-outs

Engine status: verify time since overhaul/hot section, trend data, and any outstanding engine-related inspections or bulletins for the installed PT6 variant.
Landing gear, pressurization, and environmental systems: confirm proper cycling, leak rates, and maintenance history; these can drive downtime if neglected.
Avionics age and integration: older suites can be reliable but may limit capability; verify parts support and recent repairs/upgrades.
De-ice system condition (boots, valves, controls) and documentation of periodic checks if the aircraft was used in icing environments.

Strengths & Trade-offs

Strengths

Fast cruise and strong climb for a single-engine turboprop, enabling efficient IFR travel
Access to shorter and smaller airports than most jets, improving point-to-point flexibility
Owner-operator friendly cockpit and operating concept with comparatively moderate operating complexity

Trade-offs

Cabin size and baggage capacity are limited compared with light jets and larger turboprops
Single-engine operations may not align with some corporate policies or overwater/mountain risk preferences
Avionics and equipment vary widely by airframe; capability is not uniform across the fleet

Ideal Buyer Profile

Best Suited For

Experienced owner-pilots seeking turbine speed for regional and cross-country trips
Small teams that value smaller-airport access and quick turn capability
Operators prioritizing efficient, repeatable 1–5 passenger missions

Less Aligned For

Organizations requiring a larger cabin, enclosed lavatory comfort, or consistent 6+ passenger lift
Flight departments with mandated twin-engine or jet-only operating policies

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1207 Delaware Ave #3093, Wilmington, DE, US 19806