Piaggio P.180 Avanti

The Piaggio P.180 Avanti is one of the most distinctive aircraft in general aviation: a pressurized twin-turboprop business aircraft built around a patented three-lifting-surface configuration with rear-mounted pusher propellers. Designed by Piaggio engineers starting in 1979 (with a brief Learjet collaboration 1983-1986), the configuration was patented in 1982, first flew in 1986, received Italian certification on 7 March 1990 and FAA certification on 2 October 1990. The Avanti II (upgraded PT6A-66B engines, glass panel, 402 KTAS max cruise) was certified by EASA in 2005. The Avanti EVO followed in 2014 with new five-blade scimitar props, aerodynamic winglets, reduced cabin noise, redesigned nacelles, and improved hot-and-high performance.

The Avanti is marketed as a jet alternative: it delivers near-jet cruise speeds (402 KTAS) at roughly 30% lower fuel burn than a comparable light jet, while offering a stand-up, cabin-class pressurized cabin (6.1 ft wide, 5.8 ft tall, 14.9 ft long, 393 cu ft). The pusher configuration places the propellers behind the cabin, yielding a quiet forward cabin and unobstructed forward visibility. Production has been consistently low-volume (roughly 250 airframes built across all variants), and the aircraft flies almost exclusively with corporate, charter, and air-ambulance operators — private owner-flown Avantis exist but are rare due to type-rating and insurance hurdles.

Piaggio Aerospace declared insolvency on 22 November 2018 following the withdrawal of Abu Dhabi's Mubadala, and the company spent more than six years in Italian extraordinary administration. On 27 December 2024 Turkey's Baykar acquired Piaggio Aerospace, with the preliminary business transfer signed 27 January 2025. As of 2026 the FAA has published ADs under the "Baykar Piaggio Aerospace S.p.A." type-certificate holder name, indicating the type certificate has formally transferred. Production of new EVOs under Baykar ownership has not yet resumed at meaningful volume, but parts and engineering support have stabilized.

See also Beechcraft Starship 2000A for the other famous three-surface canard pusher turboprop — the two aircraft are frequently compared, though the Avanti succeeded commercially where the Starship failed.

Which airplane the specifications above describe. This page's frontmatter is the Avanti II / EVO, Increased-MTOW option (12,100 lb takeoff) — the configuration standard on virtually all current production and most of the used fleet. Weights, fuel, empty weight, stall and maneuvering speeds, climb rate, and takeoff/landing distances above are traced to a Piaggio factory specification for the Avanti II at that specific weight option (see Performance Notes); the original 1990-2005 P.180 Avanti (lower MTOW, PT6A-66 rather than -66B) and the EVO's own further speed gains over the II are both handled as Variants-table rows rather than folded into the frontmatter.

The EVO row's ~400-402 KTAS figure is real and widely corroborated (independently by an Aviation Week data table reflected in Wikipedia's aircraft infobox, retrieved 2026-09-11) but is not backed by a primary Piaggio EVO performance document this session could locate — see Performance Notes for how that compares with the Avanti II's own factory-published cruise grid.

Primary source: Piaggio Aero Industries' own "P.180 Avanti II Specification and Description," Rev. 5.0 (Preliminary), January 2005, "Valid for SN 1105 onward" — the same serial threshold the type certificate uses for the Avanti II avionics standard. This is the only performance document for this type located this session with stated conditions (altitude, weight option, power setting) attached to every figure; no free POH/AFM exists for a type-certificated business turboprop like the Avanti (training is factory/FlightSafety-only and the AFM is not publicly distributed), so this factory specification is treated as the primary performance source, per runbook rule 25.

The stored cruise/range pair (356 KTAS / 1,456 nm) is deliberately the document's HIGH-ALTITUDE, not headline, row. The factory document publishes a cruise-speed-by-altitude grid (395 KTAS at FL300, 380 at FL350, 356 at FL390, all "Maximum Cruise Power," typical mid-cruise weight) but publishes range only at FL390 — so FL390 is the only altitude where a stated speed and a stated range share one row, and runbook rule 3 forbids pairing a speed from one altitude with a range from another. The faster, more commonly quoted figures — 395 KTAS at FL300 (this same document), 398 KTAS max speed at FL280, and the ~400-402 KTAS widely reported for the later EVO — are real but have no range figure attached to them in any primary source found this session, so they are recorded here rather than in frontmatter.

No fuel-flow (GPH) figure is published anywhere in the factory document — only speed and range at fixed altitude/power settings, with no duration alongside the range figures from which a burn rate could be backed out without an invented assumption. fuel_burn_gph is therefore exempted rather than estimated; a buyer should get an operator-reported burn figure directly before budgeting a mission.

Climb, ceiling and runway performance above are all the Increased-MTOW figures from the same document: 2,770 fpm both-engines-operating rate of climb at sea level/ISA, 40,000 ft two-engine service ceiling (distinct from the certificate's separately-stated 41,000 ft Maximum Operating Altitude, which is a pressurization/structural limit, not a climb-based ceiling), and takeoff/landing distances that are BOTH obstacle (over-50-ft) distances by the document's own footnotes — Piaggio does not publish a separate ground-roll figure for either. A prior version of this page had a takeoff obstacle distance sitting in the ground-roll field, and at the lower (Standard, not Increased) MTOW option besides; both have been corrected.

The three-surface configuration gives the Avanti exceptional low-drag cruise, but it also means the wing is small (172 sq ft) and highly loaded — approach speeds are jet-like (Vso 97 KIAS at the Increased-MTOW landing weight, per the same factory document), and the aircraft does not like short or contaminated runways. The pusher props are also susceptible to FOD from rough surfaces, and the forward canard (which carries flaps) stalls first by design to provide natural pitch-down stall protection, which pilots describe as remarkably benign despite the aircraft's performance envelope.

At standard max fuel (418 gal usable / 2,802 lb), full-fuel payload is useful_load_lbs (4,400) - max_fuel_weight_lbs (2,802) = 1,598 lb — Piaggio's own figure, netting out one pilot at 200 lb, is 1,398 lb, close enough to confirm the arithmetic (the 200 lb gap is exactly that one crew member). That is roughly six to seven 200-lb occupants with light bags, comfortably filling the typical 9-seat (2 crew + 7 pax) configuration this page's frontmatter describes, at the stored 1,456 nm IFR range (FL390, Maximum Cruise Power).

An airframe fitted with the optional extended-range tank (Mod 80-1091/SB 80-0424, S/N 1105+, 476.0 gal usable) trades roughly 58 gallons (389 lb) of payload for meaningfully more range — Piaggio's own factory document does not publish a range figure for that configuration, so the improvement is not quantified here, but the fuel-weight difference alone (476.0 - 418.1 = 57.9 gal, ~388 lb) is a direct trade against the payload figures above. A buyer evaluating range on a specific airframe should confirm which tank it carries.

The Avanti's payload-range envelope is one of its most attractive features: unlike light jets in the same price class, it rarely forces an uncomfortable tradeoff between seats and range on realistic business missions. The main tradeoff is runway — the 3,400 ft balanced field length rules out many smaller general aviation airports that a King Air or Pilatus PC-12 could comfortably use.

Business travel (10) — this is the Avanti's core design mission. Pressurized stand-up cabin, 6-8 executive seats, lavatory, 400+ KTAS cruise, FL410 ceiling, and jet-competitive trip times with substantially lower fuel burn. Ramp presence is unmatched. See Business Travel.

Cross-country (9) — 1,500 nm NBAA range with reserves covers most domestic US city pairs nonstop, and the FL410 ceiling keeps the aircraft above most weather. Scored below 10 only because range falls short of transcontinental US nonstop at max cruise. See Cross-Country Flying.

Cargo hauling (3) — 3,700 lb useful load is respectable but the cabin door and interior are optimized for passengers, not freight, and a few aircraft have been converted to air-ambulance/medevac configurations with reasonable success.

Flight training, backcountry, aerobatics, local fun (1-2) — all disqualified. Type rating required, 3,000+ hour insurance minimums, six-figure annual operating costs, and a pressurized cabin-class turboprop is absurd for any of these missions.

Surveying (2) — too fast, too expensive, and sensor mounting on a pusher configuration is awkward.

Original Avanti (1990-2005): Most came with Collins Pro Line II analog/EFIS hybrid panels. A significant fraction have been upgraded to Pro Line 21 or Garmin G600 TXi retrofits to maintain ADS-B Out compliance and FANS/CPDLC capability for international operations.

Avanti II (2005-2014): Rockwell Collins Pro Line 21 integrated avionics standard, three-tube PFD/MFD, dual FMS, integrated TCAS II, TAWS-B, weather radar. WAAS/LPV capability added mid-production; pre-WAAS aircraft command a discount.

Avanti EVO: Pro Line 21 with enhanced graphics, synthetic vision (SVS), enhanced vision (EVS) optional, ADS-B Out standard. Some EVOs have been delivered with Pro Line Fusion cockpits.

Avionics upgrades on earlier airframes are expensive ($200k-$500k typical) because the Avanti's certification basis and tight panel real-estate make STC work non-trivial. See Aircraft Valuation Methodology and the avionics reference pages for detail.

The STC ecosystem for the Avanti is thin compared with Kingairs or Citations because of the low fleet size. Notable items:

• Five-blade MT composite props — retrofit available for original Avantis; reduces cabin noise and ground noise footprint substantially. Install cost roughly $200k.
• Winglets — factory on EVO, retrofit STC available for earlier airframes (~$150k).
• ADS-B Out / WAAS GPS upgrades — required for US operation; typical install $75k-$150k depending on baseline equipment.
• Interior refurbishment — full cabin refurb runs $250k-$600k through specialty shops (Duncan, Elliott, Western Aircraft).
• Medevac conversion — several Avantis have been converted for air-ambulance service; the wide flat-floor cabin accommodates two stretchers plus medical crew.
• Extended-range fuel tank (Piaggio Mod. 80-1091 / SB 80-0424) — an OPTIONAL factory modification available on S/N 1105 and up (per FAA TCDS A59EU Note 14) that raises usable fuel from the standard 418 gallons to 476.0 gallons usable. This is a factory-approved type-design option, not an aftermarket STC, and it is not standard equipment — the certificate says so explicitly. A buyer evaluating a specific airframe's range should confirm whether this modification is installed rather than assume either figure; the frontmatter above stores the standard (non-extended) tank.

Parts availability: fair. During 2018-2024 administration the factory parts pipeline was intermittent and several operators resorted to parts pooling and PMA sourcing. As of 2026, under Baykar, parts support has stabilized but remains less predictable than King Air or Citation. Single-source Piaggio-specific components (canard skins, fuselage structures, nacelle parts) can have multi-week lead times.

Mechanic familiarity: specialist. Only a handful of shops in the US have meaningful Avanti expertise — notably Epps Aviation (Atlanta), Western Aircraft (Boise), and select FlightSafety-partnered MROs. Routine line maintenance can be done by any Part 145 turboprop shop familiar with PT6A, but any structural, pressurization, or three-surface aerodynamic work should go to a specialist.

Cost baseline (Liberty Jet, Aircraft Cost Calculator): Total annual operating budget around $668,000 at 200 flight hours/year and around $1,020,000 at 400 hours/year. This includes fuel, maintenance reserves, crew, insurance, hangar, training, and engine reserves. Direct operating cost (fuel + maintenance reserves) is roughly $1,800-$2,200/hour. Annual inspection alone runs $30,000-$60,000 assuming no significant findings. See Maintenance Ecosystem.

Pricing tiers (Aircraft Bluebook Spring 2025, AvBuyer):

• Early P.180 Avanti (1990-2001): $1.05M - $1.6M. Analog panels, lower MTOW, often mid-life or approaching hot-section/overhaul on engines.
• Late P.180 Avanti (2001-2005): $1.5M - $2.0M
• Avanti II (2005-2010): $1.7M - $2.5M
• Avanti II (2010-2014): $2.5M - $3.65M
• Avanti EVO (2014-2020): $4.5M - $6.5M
• Avanti EVO (2020-2024): $6.5M - $7.7M (new list was $7.4M-$7.8M)

Engine status drives a disproportionate share of value on early airframes. PT6A-66/66B TBO is 3,600 hours and hot-section inspection at 1,800 hours; the house reference (reference/engine-overhaul-pricing.md) prices a PT6A-66B overhaul at $430,000 per engine (class-band figure), so two engines approaching overhaul can swing a $1.5M airframe's value by roughly $400k-$860k. Avionics currency (ADS-B Out, WAAS, FANS 1/A for international) and interior condition also heavily influence valuation. See Aircraft Valuation Methodology.

The Piaggio Aerospace insolvency (2018-2024) depressed used values because of parts-supply uncertainty; the Baykar acquisition in December 2024 and subsequent return of factory support has begun to stabilize and modestly lift prices through 2025-2026.

Price fields were NOT re-verified this session and are carried over unchanged from the prior pass (Aircraft Bluebook Spring 2025 / AvBuyer, per the tiers above); they are not newly sourced or newly confirmed.

Empty weight, recorded for transparency. The stored empty_weight_lbs: 7,700 is Piaggio's own "Standard Equipped Empty" figure (Basic VIP interior, explicitly excluding crew) — chosen over a previously-stored 8,375 lb because 7,700 reconciles exactly against two of the same factory document's own published figures (useful load and payload-with-max-fuel; see the mfr passage), while 8,375 lb reconciled against neither and traced to a single secondary source (Wikipedia, citing Aviation Week). A specific airframe's actual empty weight depends on its as-delivered interior and avionics options and should always be confirmed from its own weight-and-balance record before a purchase decision.

The Avanti has a substantial AD history that prospective buyers must understand. Recent FAA ADs (2020-2026) include:

• Nose landing gear steering select/bypass valve sealing (2020)
• Fuselage lower skin corrosion — inner/outer skin panels in the cabin belly area (2022)
• Air data computer / standby altimetry errors (2022)
• Horizontal tail trim actuator fitting corrosion-induced cracking (2023)
• HPP flexible hydraulic hose leakage (2025)
• Vertical stabilizer corrosion and cracking (2026, issued under the Baykar Piaggio Aerospace TC)

The 2026 vertical stab corrosion AD is the most significant recent item and should be a pre-buy focus. Corrosion in general is the Avanti's chief airframe concern — the complex three-surface structure, composite/metal interfaces, and sealed pressure vessel make moisture intrusion hard to detect until it is serious. Other recurring issues include pusher-prop FOD damage, exhaust stack cracking on PT6A installations, and landing gear actuator wear. Pre-buy inspections should be performed by a Piaggio-authorized service center (not a general turboprop shop) and should include thorough inspection of the fuselage belly, horizontal stab, vertical stab, and engine nacelle structures.

The Avanti is a cabin-class pressurized turboprop, and underwriting reflects that. See GA Insurance Underwriting. Typical requirements:

• Commercial or ATP with multi-engine land and instrument ratings (a type rating is required)
• FlightSafety initial + recurrent (FlightSafety is the only approved training provider)
• 3,000 total time, 1,500 ME/turbine, 100 in type for standard "qualified pilot" rates

Annual premiums at standard rates:

• Liability only ($1M): $12,000-$17,000/year for qualified pilots
• Hull + $1M liability: 1.0-1.5% of hull value for experienced single-pilot-owner, 1.5-2.5% for low-time/shared/fractional operations

On a $2.5M Avanti II, that translates to roughly $27,000-$50,000/year hull-plus-liability total. On a $6M EVO, $65,000-$120,000/year. Low-time owner-pilots will struggle to get bound at all without several hundred hours of mentor pilot time post-type-rating.