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Mooney M20S Eagle Systems Description

Mooney M20S Eagle · Systems Description

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Overview

This document provides a comprehensive systems description for the Mooney M20S Eagle, a model introduced as an entry-level aircraft in the Mooney lineup. It details the aircraft's specifications, performance capabilities, and operational features, aimed at pilots and aviation enthusiasts. The M20S Eagle is equipped with a Continental IO-550-G engine, offering a balance of performance and efficiency. The document outlines the aircraft's design, including its structural integrity, avionics, and engine management systems, making it a valuable resource for understanding the M20S Eagle's operational characteristics and maintenance requirements.

  • Maximum gross weight: 3,200 lbs
  • Cruise speed: 175 knots at 75% power
  • Engine: Continental IO-550-G, 244 hp @ 2,400 RPM
  • Useful load: 1,006 lbs
  • Fuel capacity: 75 gallons (usable)

Document

Source

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

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Document details

Type
Systems Description
Year
1999
Pages
6
File size
5.6 MB
Publisher
aeroresourcesinc.com
Documentation completeness
4/7

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In this document

Aircraft Specifications

The Mooney M20S Eagle has a maximum gross weight of 3,200 pounds and a basic empty weight of 2,194 pounds, resulting in a useful load of 1,006 pounds. It features a fuel capacity of 75 gallons (usable) and a payload capacity of 556 pounds with full fuel. The aircraft is powered by a Continental IO-550-G engine, producing 244 horsepower at 2,400 RPM.

Performance Data

The M20S Eagle has a maximum cruise speed of 175 knots at 75% power and a service ceiling of 18,500 feet. The aircraft can achieve a rate of climb of 1,050 feet per minute at sea level. Takeoff distances include a ground roll of 1,650 feet and a distance over a 50-foot obstacle of 2,000 feet.

Engine Management

The Eagle's engine management is simplified for pilots, requiring minimal adjustments during climb and cruise. The engine operates efficiently at 2,400 RPM, and pilots need to lean the mixture approximately every 1,000 feet during ascent. The aircraft does not require cowl flaps due to its engine design.

Avionics and Features

The M20S Eagle is equipped with a standard Bendix/King avionics stack, including a VHF navcom, IFR GPS, and autopilot. The aircraft also features dual batteries and a modern gauge package from Moritz Corporation, providing both analog and digital readouts for engine management.

Design and Construction

The Mooney M20S Eagle is built with a welded steel-tube cage for safety and a robust wing structure. The aircraft's design emphasizes performance and efficiency, with a focus on maintaining a comfortable cabin environment for pilots and passengers.

Safety notes

  • Ensure proper leaning of the mixture during climb to maintain engine efficiency.
  • Monitor engine gauges for optimal performance and safety.

Full document text

lends itself to an efficient production-line manufacturing process. From a safety standpoint, pilots appreciate the Mooney's welded steel-tube cage that surrounds the cabin and the remarkably strong wing with its tip-to-tip continuous carry-through spar. Manufacturing experts, though, wring their hands at the number of hours that it takes to build a Mooney. Inefficient as the process may be, the end product seems to justify the means. Pilots keep buying Mooneys, and while other manufacturers have come and gone and sometimes come back, for decades Mooney has hung in there, churning out airplanes year after year. Sure, there were tedious months and brief manufacturing hiatuses years ago. And as recently as a year ago, the compa- ny seemed on the brink of bankruptcy, buried under unprofitable subcon- tracting deals with other aerospace manufacturers. The Eagle's 10-550 makes life easy on the pilot: push all three levers forward and leave them there for the initial climb. In mid-1997, Paul Dopp and his investment firm of AVAQ Partners bought a controlling interest in Mooney; previously, a French consor- tium owned the majority of the compa- ny. Dopp is no stranger to Mooney Air- craft. He owned it and Aerostar Aircraft in the early 1970s. Dopp's new manage- ment team shed the unprofitable sub- contracts and set about recapitalizing Mooney. In mid-1998, Dopp's son, Chris, was named president, and he has been running the operation ever since. Recognizing that there is little new efficiency to be gained in manufactur- ing the Mooney's complex wing and fuselage, the management team looked at the product line to see if it could be trimmed down to reduce costs. At the time, Mooney was building four mod- els: the Allegro (nee MSE, nee 201), the Encore (nee 252), the Ovation, and the Bravo (nee TLS).The Allegro and Encore used the shorter fuselage; the other two shared the longer fuselage that debuted with the Mooney PFM in 1987. The Dopps decided that building only one fuselage style would be more efficient. Knowing that pilots favor the longer ver- AOPA PILOT· 48 . FEBRUARY 1999 sion, they discontinued the shorter one, leaving the Ovation and the Bravo as the only products. Recognizing that the Ova- tion's nearly $400,000 price would be an obstacle to many buyers, Mooney decid- ed to offer a lower-cost version that still utilized the longer fuselage. The result is the Mooney Eagle, which debuted late last year at AOPA Expo '98 in Palm Springs, California. Mooney considers the M20S Eagle its entry-level airplane, replacing the Alle- gro. Because of the Eagle's $319,000 price tag, entry level is obviously a rela- tive term. But when you look at what you get for the Eagle's price versus what the Allegro offered, it should be fairly Overhead light switches (above) and a well- designed panel give the Eagle a professional look. Among the options are a second nav- com, a Stormscope, and the eagle-head- and-talon paint scheme. easy for prospective buyers to justify the 10-percent premium that the Eagle commands over recent Allegros. In addition to the 20-inch-longer fuse- lage, the Eagle offers greater perfor- mance through the 244-horsepower Continental IO-550-G, which turns a two-blade McCauley propeller. The Allegro flew behind a 200-hp Lycoming 10-360 and a two-blade McCauley. Unlike the Allegro, the Eagle comes standard with dual batteries. It also carries a maximum gross weight of 3,200 pounds, 300 pounds more than the smaller airplane. Eagle fuel capaci- ty is up nine gallons to 75 usable. Like the Allegro and the rest of the Mooney fleet, the Eagle comes with an AlliedSighal Bendix/King avionics stack. Mooney at first announced that the Eagle would carry Trimble's TrimLine avionics. The change was an attempt to differentiate the lower-priced Eagle from AOPA PILOT· 49 . FEBRUARY 1999 the Ovation and Bravo, which Mooney considers its top-of-the-line products. (The 1999 average-equipped prices for the Ovation and Bravo are $405,900 and $467,900, respectively.) Last fall. however, Trimble announced that its general avia- tion avionics product line was for sale. No buyer quickly emerged, so-fearing an orphaned product line and needing to move quickly-Mooney decided to equip the Eagle with a limited Bendix/King stack. The standard airplane carries a sin- gle Bendix/King VHF navcom with glideslope, a KLN89B IFR GPS with mov- ing map, and a transponder; a PS Engi- neering PMA 7000 audio panel with intercom and marker beacons; and an S- Tec System Thirty hVo-axis autopilot. New to the Eagle and the entire 1999 Mooney fleet are the Moritz Corporation engine and power management gauges. The gauges provide both analog and digital readouts. Power,for example, can be quick- ly set by using the analog displays. Fine- tuning is easier with the digital readouts. While other manufacturers have come and gone-and come back again- Mooney has hung in there, churning out airplanes year after year. The Eagle and the Ovation have a lot more in common than their gauge pack- ages and the long fuselage. They also share the same engine model. In the Ova- tion, the 10-550-G turns at a comfortable 2,500 rpm, producing 280 hp. Other vari- ants of the 10-550 produce 300 or 310 hp at 2,700 to 2,800 rpm. Mooney engineers set a benchmark of a 175-knot cruise speed for the Eagle. It turns out that max power of 244 hp is necessary to deliver 175 kts at 75-percent power. According to the engineers, the engine delivers 244 hp at 2,400 rpm. At that rpm, the engine is not working very hard, and, as a result, it should routinely reach its 2,OOO-hourTBO. Mooney specs say that the Eagle at max gross weight and standard conditions will indeed do ]75 knots true airspeed, versus the Ovation's 188knots. On our test flight, when we were some 300 pounds below maximum weight and at 75-percent power,

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the Eagle turned in 181 knots true at 7,500 feet on about 13.5gallons per hour. AOPA PIl.OT· 50. Fl.BBlJARY 1999 , '•• : I Y.;\ ••••••- ••••••• ~ .,p .• :--;" AU' ••••• - - .1":-' .! . a IMI The Ovation's 10-550 swings a three- blade McCauley prop. The lighter two- blade on the Eagle meant that Mooney could remove about 16 pounds of bal- last from the tail. As a result, pilots will notice a slightly different pitch sensitivi- ty between the two airplanes. The Eagle is a bit more responsive in pitch; in that sense it flies more like an Allegro than an Ovation. As in the Ovation, the 10-550 makes life easy on the pilot. For takeoff in the Eagle, push all three knobs forward and leave them there for the initial climb. Throughout the climb, the pilot's only engine management duty is to give the The new Moritz engine gauges show both dig- ital and analog values (left), but the fuel, OA7; vacuum, and volt/amp gauges are only digital. mixture control about one turn every thousand feet or so to keep the engine leaned. The highly derated engine flies very cool and requires no cowl flaps. At cruise altitudes above 5,000 feet or so, the only engine management necessary after leveling off is leaning to best power or best economy. At lower altitudes, a slight reduction in manifold pressure may be necessary, depending on the performance desired. The slow-turning prop produces minimal vibration and makes for a quiet cabin. With the 3,200-pound max gross weight and a basic empty weight of 2,194 pounds, the Eagle has a useful load of 1,006 pounds. Fill the tanks with 75 gallons of fuel and you have a pay- load of 556 pounds, enough for three adults and bags. At about 14 gph, the AOPA PILOT' 51 • FEBRUARY 1999 140 KIAS 104 KlAS 174 KIAS 195 KIAS 68 KIAS 66 KlAS 59 KIAS Rate of climb, sea level 1,050 fpm Cruise speed/endurance w/45-min rsv, std fuel (fuel consumption) @ 75% power, best power 175 kt/4.25 hr @ 8,000 ft (89 pph/l4.8 gph) @ 55% power, best economy 155 kt/7.5 hr 10,000 ft (55.2 pph/9.2 gph) Service ceiling 18,500 ft Landing distance over 50-ft obstacle 2,400 ft Landing distance, ground roll 1,150 ft Limiting and Recommended Airspeeds Vx (best angle of climb) 85 KIAS Vy (best rate of climb) 105 KIAS VA (design maneuvering) 108 KIAS VFE (max flap extended) 123 KIAS VLE (max gear extended) 165 KIAS VLQ (max gear operating) Extend Retract VNO (max structural cruising) VNE (never exceed) VR (rotation) VS1 (stall, clean) Vso (stall, in landing configuration) For more information, contact Mooney Aircraft Cor- poration, Louis Schreiner Field, Kerrville, Texas 78028; telephone 800/456-3033, fax 830/896-8180; or visit the Web site (www.mooney.com). All specifications are based on manufacturer's cal- culations. All performance figures are based on stan- dard day, standard atmosphere, sea level, gross weight conditions unless otherwise noted. 1,650 ft 2,000 ft 13 kt >- Powerplant Specifications Continental IO-550-G 244 hp @ 2,400 rpm Recommended TBO 2,000 hr Propeller McCauley two-blade, 75-diameter, constant-speed 26 ft 9 in 8 ft 4 in 36ft I in 175sqft 18.3Ib/sq ft 13.llb/hp 4 10 ft 6 in 3 ft 8 in 3 ft 9 in 2,1941b 3,2001b I,0061b 556lb 3,200lb 78 gal (75 gal usable) 468lb (450 lb usable) 8qt 120 Ib, 20.9 cu ft Mooney M20S Eagle Base price: $319,000 Price as tested: $334,500 Length Height Wingspan Wing area Wing loading Power loading Seats Cabin length Cabin width Cabin height Empty weight Max gross weight Useful load Payload w/full fuel Max takeoff weight Fuel capacity, std Oil capacity Baggage capacity Performance Takeoff distance, ground roll Takeoff distance over 50-ft obstacle Max demonstrated crosswind component endurance stretches to about 4.5 hours with a 45-minute reserve. To carry four adults, you need to take off with 54 gal- lons of fuel, which still allows more than three hours of flight with reserves. The Ovation and the Bravo have max gross weights of 3,368 pounds, and they carry more fuel-89 gallons each. Their basic empty weights are higher than the Eagle's, however, giving all three air- planes approximately the same full-fuel payloads. Pilots will appreciate the Eagle's comfortable cloth seats, the new engine gauges, and the reliable sys- tems for which Mooney is known. They'" take comfort in the many redundant features and the proven avionics. But in the end, pilots will appreciate the Eagle for what it is: a fast new entrant to the Mooney family; an honest 175 knots on 14 to 15 gph. Manufacturing efficiencies or not-the Eagle fits the Mooney mold. 0 To view additional photos of the Eagle, visit the AOPA OnlineGallery (www. aopa.org/pilot/gallery). E-mail the author at thomas.haines@aopa.org AOPA PILOT' S2. FEHHUAHY 1999