Mooney Chaparral Pilot's Operating Handbook
Mooney M20E Chaparral · Pilot's Operating Handbook
Overview
This document serves as the Pilot's Operating Handbook for the Mooney M20E Chaparral, a modernized version of the Super 21. It provides essential information for pilots regarding the aircraft's performance, operational procedures, and specifications. The Chaparral is noted for its speed, gentle handling characteristics, and reliability. The handbook covers various aspects of flying the aircraft, including engine performance, weight and balance, and emergency procedures, making it a crucial resource for both new and experienced pilots. It also compares the Chaparral with other models in the Mooney line, highlighting its unique features and specifications.
- Gross weight: 2,575 lbs
- Empty weight: 1,600 lbs
- Fuel capacity: 52 gallons
- Top speed: 190 mph
- Climb rate: 1,400 fpm
- Stall speed (flaps down): 57 mph
- Base price: $20,755
Document
Source
Originally published by www.aeroresourcesinc.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Pilot's Operating Handbook
- Year
- 1969
- Pages
- 4
- File size
- 3.5 MB
- Publisher
- www.aeroresourcesinc.com
Specifications & performance
Extracted from this document.
Specifications
- Engine (hp)
- 200
- Length (ft)
- 24
- Wingspan (ft)
- 30
- Engine model
- Lycoming IO-360-A1A
- Empty weight (lb)
- 1,380
- Fuel capacity (gal)
- 52
- Rate of climb (fpm)
- 1,000
- Service ceiling (ft)
- 15,000
- Max takeoff weight (lb)
- 2,500
Performance
- Fuel burn (gph)
- 9.5
Weight & balance
- Useful load (lb)
- 1,120
- Basic empty weight (lb)
- 1,380
- Max takeoff weight (lb)
- 2,500
Common. Rarer than 14% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Mooney M20E Chaparral.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the M.20E Chaparral to your watchlist and track it in one place.
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In this document
Aircraft Specifications
The Mooney M20E Chaparral has a gross weight of 2,575 lbs, an empty weight of 1,600 lbs, and a useful load of 975 lbs. It features a fuel capacity of 52 gallons, a wingspan of 35 feet, a length of 23 feet 2 inches, and a height of 8 feet 4 inches. The aircraft is powered by a Lycoming IO-360-A1A engine, producing 200 horsepower at 2,700 RPM.
Performance Data
The Chaparral has a top speed of 190 mph and a range of approximately 1,015 statute miles. It can climb at a rate of 1,400 feet per minute at sea level. The stall speed with flaps and gear down is 57 mph, while the stall speed with flaps and gear up is 64 mph.
Operational Procedures
For takeoff, use half flaps and pull back on the control wheel when reaching 60 mph. Retract flaps at 80 mph and climb at 120 mph. The aircraft's gear speed is 120 mph, and flap speed is 125 mph.
Emergency Procedures
In case of an emergency, the gear can be manually lowered using a handle located on the left wall of the cabin. The aircraft is equipped with a heated pitot tube as standard equipment to prevent icing.
Instrument Panel Layout
The instrument panel features a modern layout with individual throttle, propeller, and mixture controls. The electric flap switch is located on the throttle quadrant, and an annunciator panel provides warnings for various aircraft functions.
Safety notes
- Always monitor for icing conditions during winter flights.
- Ensure the Positive Control (PC) system is operational before flight.
Full document text
Quite a bit of modernization has gone into the Chaparral (the Super 21 's new name), After ferry flight from Texas to Washington, D.C., PILOT editor describes new model as 'fast, surprisingly gentle and forgiving' and above average in reliability and economy Instrument panel and controls of N9053V. Throttle quadrant is In center (red knob is mix- ture control). Pilot's wheel has clock in hub, PC cutoff button on upper left corner. PC can only be cut off by holding the button down. The annunciator panel and gear switch are just to right of altimeter. Photos by the author •• If I were going to buy an economi- cal, high-performance single-engine air- plane for my own use these days, I'd look long and hard at Mooney's Chaparral, I recently flew Chaparral No. 4 from the factory at Kerrville, Tex" back to Washington, D.C., on a delivery flight, and found myself more than pas singly enamored of this excellent little ship. It's fast, surprisingly gentle and forgiving, and if its immediate pred- ecessors can be used as a guide, above average in reliability and economy. The Chaparral has the smaller of the two cabins currently being offered in the four-place models. If I were going to fly alone most of the time, I'd take the Chaparral. But if I wanted to carry any passengers with reasonable comfort, particularly in the back seat, I'd prefer the Executive 21, the top of Mooney's single-engine line. Basically, it's the identical airplane with a somewhat big- ger cabin. Quite a bit of modernization has gone into the Chaparral. The gear and flaps are electric, standard equipment. The instrument panel and other interior fittings have been noticeably improved. So has the exterior; for the first time in a long time (my personal opinion) the overall external color schemes now are attractive and in good taste. Gone for good, I hope, are some of the rain- 36 THE AOPA PILOT I FEBRUARY 1969 bow nightmares that have been so characteristic of this line of planes. The redesign of the instrument panel is attributed largely to the participation of John Allen (AOPA 126865), former head of Alon, which was the last com- pany to produce the Ercoupe (or Air- coupe) in its orginal form. When Alon merged with Mooney in October 1967, Allen and Lee Higdon (the other half of "Alon") joined the Mooney staff. Allen now is Mooney's production head; production is hiB speciality. For years he ran Beech's Plant No.2, which pro- duced Bonanzas and Debonairs. Allen's expertise can be seen in the Chaparral's interior layout, particularly the instrument panel. He's also had a marked effect on production methods, and already has cut the number of total man hours needed to produce one of these planes. The Chaparral is the former Super 21, and wasn't produced last year. The rea- son it wasn't, I was told, was that they wanted to concentrate on the Executive 21 with the larger cabin. Now they've revived the Super 21 and renamed it Chaparral; Mooney's leaning more and more toward western names (Mustang, Ranger, etc.). The Chaparral is No. 2 in a four- model line based on the Model 20 de- sign. Top is the Executive 21 (M-20F) with the bigger cabin and a 200 h.p. fuel-injected Lycoming IO-360-A1A; base price is $23,200. The Chaparral (M-20E) is next, with the same engine but smaller cabin; base price is $20,755. No.3 is the Statesman (M-20G) which is the Executive 21 with the 180 h.p. Lycoming 0-360-A1D carburetor engine; base price $20,400. No. 4 in the line is the Ranger (M-20C) with the small cabin, the 180 h.p. engine, and a base 53V at Washington National. There's still a little ice on the leading edge of the wing and on the thermometer after letting down through that cloud deck from on top at 11,000 feet. Color scheme is a lot more attractive than that on previous Mooneys, one of which is standing next to 53V. price of $17,480. Mooney expects the Ranger to be the biggest volume seller in 1969. The Chaparral I picked up at the plant was for Metropolitan Mooney, Teterboro, N.J., Mooney's distributor for a large northeast area. N9053V proved to have the full basic comple- ment of instruments for IFR, but just one lone radio: a single Mark 12A. I say that not because a Mark 12A is not ample for VFR flying; it certainly is. But the weather was terrible at Kerrville from the moment I arrived, and was forecast to stay that way. On top of that, it was winter, and wherever there are clouds you're almost sure to find ice. So I was facing a return flight in some undetermined amount and breadth of instrument conditions. With Charlie Prince (Mooney's single- engine sales manager) along, I even had to fly around the local area getting acquainted with 53V under low clouds. We finally found a hole and went up on top to feel out 53V's flight charac- teristics. I'm glad we did, because they're a joy and delight. With PC (that's Mooney's "Positive Control," their single-axis Brittain autopilot which is on all the time, and can only be turned off by holding down a cutout button on the control wheel) the Chap- arral in slow flight was so quiet, gentle and maneuverable that it reminded me of a sailplane. Even with the PC button held down, the Chaparral stalls with great gentility, and retains excellent maneuverability. But with PC operating normally, the careless or unfortunate pilot getting caught on top of a 10,000- foot overcast would only need to keep his wits about him, advise someone on the ground of his problem, then lower the gear, ease off the power, trim the nose up a little, put his hands in his lap and wait until he saw the ground. In slow flight, for example, with flaps and gear down and holding about 70 m.p.h. indicated, PC does an excellent job of holding the airplane straight and
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level; it's so quiet, it gives you the im- pression of just hanging there, like a free balloon. Stalling speed with flaps and gear The Chaparral trademark is on the wing tips. For you who are not Texans, a chaparral ;s a roadrunner, which is a bird noted for its speed. '~.:, I . .,---- ~ IHI ~ •..... • . , (1.....• - "" '"':!I 100D61 '-: .\1I&~a~d: ChaDarralby MAX KARANT AOPA 18 I ! I 37 COMPARATIVE DATA Mooney Chaparral 2,575 1,600 975 52 35 23/2 8/4 15.4 Lye. 10-360-A1A 200/2,700 190 1,015 1,400'~ 57 18,800 $20,755 down is 57 (flaps are 33° down fully extended). With flaps and gear up, stall is 64, according to the manual. The stall itself is mild and gentle. You use half flaps for takeoff, and pull back on the wheel when the airspeed gets to 60. When it hits 80, retract the flaps, then go to 120 for cruising climb. One peculiar point: the flaps apparently are sturdier than the gear; gear speed is 120, flap speed 125. At 65% power, true airspeed was about 175 m.p.h. This is only approxi- mate, however, because 53V's primary instruments, including the airspeed in- dicator, altimeter, directional gyro and horizon, vibrated and oscillated con- stantly. The power instruments were a little steadier, and I assumed that the settings for 65% power were accurate. However, the Alcor Ekonomix EGT sys- tem also seemed to have something wrong with it; when leaning the mixture at cruising altitude the EGT needle went down instead of up, and I was never able to get a clear temperature peak. As a result, I could only rely on a nonstop range somewhat shorter than the airplane is able to fly. This was particularly annoying because I was IFR much of the time from Kerr- ville to Washington. This IFR operation, incidentally, was interesting to me for two reasons. First, I was on edge most of the time, be- cause 53V's total radio capability con- sisted of that lone Mark 12A. Secondly, I was interested in why I felt that way. Of course, one radio is minimal for IFR. But I reflected at some length on the amount of IFR that used to be done routinely with one radio, and the tre- mendous amount of flying that was done with no radio at all. I couldn't help thinking about how far general avia- tion has advanced, to the point where today I find myself feeling sort of naked flying IFR without two VOR and ILS receivers, dual 360-channel com- munications, DME, transponder, ADF, marker beacon, autopilot with couplers, excellent aircraft instruments, and so on. Surely we have reached an advanced state of snobbery ... ? On the other hand, there I was, either in the solid cloud deck, or with a VFR-on-top clearance, with one radio, shaky instruments, in a new, untried airplane. What would I do if I lost the radio? Or if the permanently cocked horizon quit entirely? In the former case, and depending on where I was at the time, I'd probably turn off the air- way and let down slowly until I was VFR underneath. The loss of the horizon wouldn't have bothered me, because 53V also was equipped with a Turn Coordina- tor and PC-either or both of which would suffice. And because of the neces- Gross weight (Ibs.) Empty weight (Ibs.) Useful load (Ibs.) Fuel capacity (gals.) Span (ft.) Length (ft./in.) Height (ft./in.) Wing loading (Ibs./sq. ft.) Engine Power (h.p./r.p.m.) Top speed (m.p.h.) Range (statute miles) Climb (f.p.m. @ S.L.) Stall (flaps and gear down) Service ceiling Base price This is the emergency gear-extension system, on the left side of the cabin wall on the pilot's side. In front of the pilot, on the floor, are the com· bination sump drainage system (spring-loaded ring at left) and fuel selector valve for the plane's two tanks. Directly below the throttle quadrant are the trim and flap indicators. Above them is the ram-air knob for use only during climbs and cruiSing. sity of keeping PC always operational, Mooney has added the heated pitot tube as standard equipment. Also, it was winter. And although no one was reporting icing, I always figure that winter and clouds automatically constitute a threat. As a matter of fact, I got varying amounts of ice (none serious) on approaches to Monroe, La.; Nashville; Tri-Cities, Tenn.; and Wash- ington. 53V performed normally, even though I was occasionally apprehensive. I kept asking the ATC centers for icing reports, and when I could reach them (sometimes I had to relay through other aircraft because of the Mooney's poor microphone) none had any reports. I ended up giving them a couple myself. My cruising altitudes ranged all the way from 5,500 to 11,000 feet, depend- ing on the cloud tops and winds aloft. At 5,500 feet, I used 24 inches and 2,400 r.p.m., for an indicated airspeed of 160 m.p.h. The engine delivers its full 200 h.p. at 2,700 r.p.m. You use 25 inches and about 2,500 r.p.m. for climb. At 65 % power this engine is supposed to burn about 9.5 g.p.h., which would be a maximum endurance of 51/2 hours for the Chaparral's 52 gallons. The instrument layout and appear- ance are particularly attractive. Throttle, prop and mixture controls, for example, now are like those on a multi-engine plane, with a quadrant and individual handles that move back and forth. The electric switch for the flaps also is on this quadrant. Just below the throttle quadrant is the ram air control. This novel little feature, familiar to Mooney owners, is simply a little door in the nose which, when opened, bypasses the air filter Piper Arrow 2,500 1,380 1,120 50 30 24/3 8 15.6 10-360 180/2,700 170 857 875 61 15,000 $16,900 38 THE AOPA PILOT I FEBRUARY 1969 OAt 2,200 Ibs. -~- .-- -. L L L ," ".1.11 C ···.e "" --- 9893), now with Piper at Vero Beach, designed that remarkable little plane nearly 30 years ago. It was originally certificated March 25, 1940. In its way, and all out of proportion to its size, it revolutionized private flying. It was cer- tificated as spinproof, and its stall was little more than a gentle mush. Many of these Ercoupes still are flying, and the basic design itself has gone through almost as many changes as it has manu- facturers. The Cadet version currently being produced by Mooney is, in a way, a sad commentary on general aviation's progress. They've put a single rudder and fin on it, added rudder pedals, and have redesigned it back to the point where what was once the Ercoupe now produces both a sharp stall-and a spin! Mooney said they had to add a trainer to their line and, when they merged with Alon, decided to use the Ercoupe, then being produced by Alon, for that trainer. So, presumably to meet the requirements of flight schools and instructors, they have now deliberately put the full stall and spin back in! Closest competitive plane to the Chap- paral is Piper's Arrow. And it's because of the popularity of the Arrow that Mooney stopped claiming to sell the most retractables some time ago. 0 ally, showing both pilot and engineers how the proposed helicopter would per- form, said IBM officials. The electronic system also will simulate external forces, such as wind and turbulence .•• James F. Atkins, executive vice presi- dent at Bell, said, "The new system makes our design work more economi- cally, gives engineers a better insight into their work, and greatly reduces the time involved in setting up and solving de- sign problems." 0 ~ \ Test pilots at Bell Helicopter Com- pany, Fort Worth, Tex., soon will be test flying a newly designed helicopter before it has even been built. The pilots will be using a mock-up cockpit that is linked to a specially de- signed IBM computing system. Called the Hybird, the system combines two analog computers with a digital com- puter-an IBM system 360 Model 44. Linked to a mock-up cockpit, the IBM system will simulate flights electronic- Gene Colvin, experimental test pilot for Bell Helicopter Company, left, is briefed by an engineer on Bell's new IBM data processing system designed to simulate test flights electronically. Computer Designs Bell Helicopters gossips. So I talked with Ralph Harmon, company president; Dick Martin, vice- president for single-engine sales;' John Allen; and others. The gist of what I got from them is that they are short of working capital, due almost entirely to the unexpectedly high costs of de- veloping and marketing the Japanese turboprop MU-2, the pressurized Mus- tang, and the Cadet (which is what I'd call a loused-up Ercoupe). Harmon says flatly that they're over all these cost humps now. But he also made it quite clear that he· is now operating head of the company, and that Hal Rachal, an attorney and former opera- ting head, now is board chairman and is concerning himself primarily with legal matters. He attributed most of the gossip I asked about to a couple of dissident sales representatives. As for overall sales, Martin-the salesman-says they now are "tremen- dous," and that they already exceed the company's ability to produce planes under the best conditions. In model year 1969 they expect to produce 784 units of all models; the best year they've ever had hit 779. One quick word about the Cadet, largely because of my own personal experience with the Ercoupe dating back to the early 1940's. Fred Weick (AOPA and takes its air directly into the engine. You only use it in climb or cruising flight, and then only when you're flying clear of dust or visible moisture. But when you do use it, it boosts the plane's performance by as much as 15 m.p.h., according to Mooney. I turned it on and off several times at cruising altitudes, and the manifold pressure actually in- creases about IV2 inches when it's open. Most of the engine instruments are strung in a neat rectangular line across the top of the panel, including two fuel gauges, cylinder head temperature, oil pressure, oil temperature and the ammeter. One peculiarity: Mooney has for some time been calibrating the fuel gauges in pounds of fuel, instead of gal- lons. No particular reason I could find, but the pilot does have to divide what the instrument says by six to find out how many gallons remain. Mooney it- self quotes its engines' performance in gallons per hour, notwithstanding this added little bit of confusion. Just to add to the confusion, the fuel pressure gauge is calibrated in pounds per square inch. There's a novel little annunciator panel of six lights beside the flight instruments; any of those lights when on warn the pilot that that particular function is not normal. In the floor, between the pilot's feet, is a small metal ring attached to the lowest point in the plane's fuel system. You just pull up on the spring-loaded ring to drain the system during runup. In an emergency the gear can be lowered manually, by a folded handle on the left wall of the cabin, next to the pilot's knees. The noise level in cruising flight is quite good, especially considering that there's a 200 h.p. engine running just ahead of the windshield. Using my tape recorder mike to test the noise level, I preset the volume control, then moved the mike slowly around the inside of the cabin. The needle reached its peak right at the center post of the wind- shield. Mooney's using the latest version of PC: the Brittain Turn Coordinator, tied to PC. There's an added roll trim knob on the Turn Coordinator so that now, in effect, you can adjust the plane's heading with that knob while flying hands-off. The cabin heater in 53V was excel- lent. At 9,500 feet the outside tempera- ture was just 14°F, yet with just the slightest movement of the heater knob I had abundant heat in the cabin. On the ground at Washington, I got into the back seat to see how it felt. My conclusion was that I would not relish carrying four people on a long trip. May- be a couple of small children in back, with the front seats pulled forward, but certainly not four adults with any com- fort. I can see why Mooney added the Executive 21 and Statesman to their line, with their stretched cabins. While I was at the Mooney plant, I asked about the rumors currently mak- ing the rounds. Everything from being short of cash to collapse and bank- ruptcy has been passed around by 39





