2016 Acclaim Ultra Specifications

Mooney M20V Acclaim Ultra · Specifications

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Overview

The document provides detailed specifications and performance data for the Mooney M20V Acclaim Ultra, highlighting its design upgrades and features. It outlines the aircraft's general characteristics, performance metrics, propulsion details, fuel specifications, dimensions, and weight limits. This information is crucial for pilots and aviation enthusiasts to understand the capabilities and operational parameters of the aircraft. The document emphasizes the aircraft's modern cockpit design, advanced avionics, and enhanced ergonomics, making it a significant upgrade in the Mooney lineup.

Take-off distance: 2,100 ft (MTOW, 50 ft obstacle)
Landing distance: 2,650 ft (MLW, 50 ft obstacle)
Maximum rate of climb: 1,375 fpm
Maximum operating altitude: 25,000 ft
Maximum cruising speed: 242 KTAS
Range with standard fuel (89 gal): 700 NM
Range with long-range fuel (100 gal): 830 NM
Engine: Continental TSIO-550-G, 280 hp, TBO: 2,200 hrs

Document

Source

Originally published by www.aerocontact.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type: Specifications
Year: 2016
Pages: 2
File size: 5.5 MB
Publisher: www.aerocontact.com

Specifications & performance

Extracted from this document.

Specifications

Range (nm): 700
Engine (hp): 280
Height (ft): 8
Length (ft): 26
Propeller: Hartzell Scimitar Three-Blade
Wingspan (ft): 36
Engine model: Continental TSIO-550-G
Max speed (kt): 242
Cruise speed (kt): 175
Fuel capacity (gal): 89
Rate of climb (fpm): 1,375
Service ceiling (ft): 25,000
Max takeoff weight (lb): 3,368

Performance

Landing over 50ft: 2,650
Takeoff over 50ft: 2,100
Landing distance (ft): 2,650
Takeoff distance (ft): 2,100

Weight & balance

Useful load (lb): 1,000
Max ramp weight (lb): 3,380
Max takeoff weight (lb): 3,368

Documentation completeness

5/7

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In this document

General

The Mooney M20V Acclaim Ultra seats four passengers and features retractable landing gear. It is equipped with the Garmin G1000 avionics system, enhancing navigation and flight management capabilities.

Performance

The aircraft has a take-off distance of 2,100 feet and a landing distance of 2,650 feet, both measured under standard conditions with specific weight limits. It boasts a maximum rate of climb of 1,375 feet per minute and can operate at altitudes up to 25,000 feet. The maximum cruising speed is 242 knots true airspeed (KTAS), with a range of 700 nautical miles (NM) on standard fuel and 830 NM on long-range fuel.

Propulsion

Powered by a Continental TSIO-550-G engine, the M20V Acclaim Ultra delivers 280 horsepower. The engine has a time between overhaul (TBO) of 2,200 hours, and it utilizes a Hartzell Scimitar three-blade propeller.

Fuel

The aircraft uses 100LL fuel (ASTM D 910) with a standard fuel capacity of 89 US gallons and a long-range fuel capacity of 100 US gallons.

Dimensions

The M20V Acclaim Ultra has a wingspan of 36 feet 6 inches, a length of 26 feet 8 inches, and a tail height of 8 feet 4 inches. The cabin width measures 43.5 inches.

Weight

The typical useful load for the aircraft is 1,000 pounds. The maximum ramp weight is 3,380 pounds, while the maximum take-off weight is 3,368 pounds.

Full document text

SPECIFICATIONS Specifications and performance data are preliminary at this time and subject to change. 2016 ACCLAIM ULTRA SPECIFICATIONS For the first major upgrade in more than ten years, Mooney has completely reimagined its flagship aircraft. It now features an elegant cockpit, seamless ergonomics and a radically redesigned interior. Not a switch, jack or control has escaped scrutiny, as evidenced by touches such as USB outlets throughout and a center console for keypad, side controls and lighting. Beneath its striking livery, a single-piece composite shell around the cockpit replaces overlapping sheet metal, and streamlines its sleek aesthetics. And the doors (now included pilot- side as well) were widened an additional four inches to provide unparalleled ingress and egress. GENERAL Seats 4 Landing Gear Retractable Avionics Garmin G1000 PERFORMANCE Take-off distance 2,100 ft (isa, sl, mtow, 50 ft obstacle) Landing distance 2,650 ft (isa, sl, mlw, 50 ft obstacle) Maximum Rate of Climb 1,375 fpm Maximum Operating Altitude 25,000 ft Maximum Cruising Speed 242 ktas Range - Standard Fuel (89 gal) 700 nm* Range - Long Range Fuel (100 gal) 830 nm* Long Range Cruising Speed 175 ktas Range - Standard Fuel (89 gal) 1,100 nm** Range - Long Range Fuel (100 gal) 1,275 nm** * 45 min reserve, isa, no wind, 25,000 ft ** 45 min reserve, isa, no wind, 16,000 ft PROPULSION Engine Continental TSIO-550-G Horsepower 280 hp Engine TBO 2,200 hrs Propeller Hartzell Scimitar Three-Blade FUEL Fuel Type 100LL (ASTM D 910) Standard Fuel 89 usg Long Range Fuel 100 usg DIMENSIONS Wingspan 36 ft 6 in Length 26 ft 8 in Tail Height 8 ft 4 in Cabin Width 43.5 in WEIGHT Typical Useful Load 1,000 lbs Maximum Ramp Weight 3,380 lbs Maximum Take-off Weight 3,368 lbs WARRANTY Airframe 3/5 years Engine 3/5 years Avionics 2/5 years FOR MORE INFORMATION ON THE NEW ACCLAIM ULTRA AND THE NAME OF THE AUTHORIZED MOONEY DEALER NEAREST YOU, PLEASE CONTACT: Jared Absher, Director – Sales & Marketing | (830) 792-2941 | jabsher@mooney.com Mooney International Corporation | 165 Al Mooney Road North | Kerrville, Texas 78028 P I LOT P E R F E C T

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