Powrachute Pegasus 582 Owner's manual

Original Issue Date 28.05.2007 Revision Date: 28.05.2007

POWRACHUTE Pilot Operating Handbook Model: PEGASUS 582

Table of Content

Powrachute Pegasus Pilot Operating Handbook………………..…...……...

1

1. Table of Content………………………………................................................................................2

2. General Information………………………………........................................................................3

2.1 Description of the PPC………………………………............................................................4

3. Operating Limitations……………………………….....................................................................

3.1 Fuel and Fuel Capacity……………………………….............................................................6

3.2 Oil………………………………........................................................................................................6

3.3 Operating Weights………………………………....................................................................6

3.4 Maximum Wind………………………………...........................................................................6

3.5 Service Ceiling………………………………..............................................................................6

3.6 Load Factors……………………………….................................................................................6

3.7 Prohibited Maneuvers………………………………..............................................................6

3.8 Engine Limits……………………………….................................................................................6

4. Emergen y Pro edures……………………………….................................................................7

4.1 Emergencies During Wing Inflation………………………………..................................7

4.2 Emergencies in flight………………………………................................................................7

5. Normal Pro edures……………………………….........................................................................8

5.1 Launching of the wing………………………………..............................................................8

5.2 Collapsing of the wing on landing……………………………….......................................9

5.3 Packing and unpacking the wing………………………………........................................9

5.4 Potential for rollover……………………………….................................................................9

5.5 Landing Flare……………………………….............................................................................10

5.6 Preflight Checklist (Detailed)…………………………….................................................11

5.7 Preflight Checklist (Abbreviated)…………………………….........................................1

6. Performan e……………………………….....................................................................................16

6.1 Takeoff Distances………………………………....................................................................17

6.2 Rate of Climb……………………………….............................................................................17

6.3 Fuel Consumption………………………………....................................................................17

7. Air raft Speed………………………………..................................................................................17

8. Weight and Balan e………………………………......................................................................18

9. Systems and Des riptions………………………………........................................................19

9.1 Chassis Overview……………………………….....................................................................20

9.2 Electrical System Overview……………………………….................................................22

9.3 Rotax 82 Engine………………………………....................................................................24

9.4 Engine Break-In………………………………..........................................................................24

9.5 Component Propeller……………………………….............................................................26

9.6 Component Parachute………………………………...........................................................27

10. Handling, Servi e and Maintenan e………………………………...................................28

10.1 Transporting………………………………...............................................................................29

11. Environmental Restri tions………………………………......................................................30

12. Warm up pro eedure………………………………...................................................................31

13. Pre Start Up and Takeoff…………………………...............................……............................32

14. Wing Layout………………………........................………...............................................................33

15. Post Flight………………………………...........................................................................................34

16. Supplements............................................................................................................................3

17. Data Lo ation and Conta t Information..................................................................36

18. Warnings and Pla ards.....................................................................................................37

19. Revisions....................................................................................................................................38

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Original Issue Date 28.05.2007 Revision Date: 28.05.2007

POWRACHUTE Pilot Operating Handbook Model: PEGASUS 582

In accordance with the ASTM specification F 2243-03 each Pegasus PPC

includes a Pilot Operating Handbook (POH). The content and format

herewith is defined by F 2243-03

2.

General Information

Read this before your first flight!

Every pilot has to understand the limitations and specifications of this light

sport aircraft. The Pilot Operating Handbook must be read thoroughly.

Please pay attention to the pre-flight and daily checks. Maintenance

instructions for the Pegasus are given in a separate maintenance manual.

Also note that no amount of information we can give you in writing will

serve as a substitute for proper training. Before you attempt to fly your

Pegasus PPC, seek out a qualified instructor to teach you how to fly safely.

No other single fa tor is as important to your safety as proper

training! If you need help in locating an instructor in your area, contact

Powrachute and we will help you find one. The pilot in command alone is

responsible for ensuring the continued airworthiness of this aircraft and

for its operation within the limits details herein. All persons entering this

aircraft do so at their own risk.

Manufa turer:

Powrachute, LLC.

942 Spring Creek Ct

Middleville, MI 49333

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Original Issue Date 28.05.2007 Revision Date: 28.05.2007

POWRACHUTE Pilot Operating Handbook Model: PEGASUS 582

2.1. Des ription of the PPC.

Your Pegasus Power Parachute is comprised of several components which are carefully

matched by Powrachute, LLC to meet our stringent quality standards. The components

and their features are discussed in this manual.

The main systems that make up the Pegasus Power Parachute are

Chassis - Engineered and constructed by Powrachute, LLC.

Electrical System - A self-charging system that powers all accessories

Rotax 582 Engine and Gearbox - Manufactured by Bombardier

Cooling System - Engineered to keep your engine running at optimal temperature

Exhaust System - Durably mounted to the engine

PowerFin Propeller - A smooth, balanced combination

Per ormance Designs - A perfect balance of lift and handling

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Original Issue Date 28.05.2007 Revision Date: 28.05.2007

POWRACHUTE Pilot Operating Handbook Model: PEGASUS 582

3. Operating Limitations

In order to safely enjoy flying your Pegasus Power Parachute, the following precautions

must ALWAYS be followed. Failure to do so ould result in serious bodily injury or

death!



Never fly in winds stronger than your piloting skills will allow you to be safe. Winds

above 15 mph can be considered dangerous for a PPC.



Do not fly in rain or snow, or when conditions could turn rainy or snowy.



Never fly if you are impaired by alcohol or medications.



Do not fly if you have any medical conditions which could cause you to black out or lose

control of the aircraft in any way.



Always fly from a field that is of sufficient length and free of obstructions.



Always take off and land directly into the wind. NEVER take off or land with the wind.



You should never attempt to operate your powered parachute without proper training.



Use of helmets is always recommended.



Your PPC should always be operated within the legal boundaries set up by the FAA for

these types of crafts. This means you must be a licensed pilot and have your craft legally

registered with the FAA and carry an airworthiness card and limitations.



You may, under no circumstances, carry a passenger with a student pilot certificate.



Never overload your craft or exceed the manufacturers recommended gross weight limit.



Your craft must be carefully inspected before each and every flight.



Always warm your engine up to operating temperature before flying.



Always wear lap and shoulder belts.



NEVER fly your aircraft if you know of a problem or suspect there to be one.



Always fly in a safe manner, and never fly over anything that you wouldn’t want to land

on!



Never modify your Pegasus PPC without the express consent of Powrachute, LLC.

Original Issue Date 28.05.2007 Revision Date: 28.05.2007

POWRACHUTE Pilot Operating Handbook Model: PEGASUS 582

3.1 Fuel and Fuel Capa ity

Fuel Specification: Premium Automotive Unleaded MIN 89oct rated.

Fuel Capacity: 10 US Gallons (Optional 1 gallon tank available)

3.2 Oil

For complete oil specifications see Rotax Manual located in the Pegasus

maintenance manual.

3.3 Operating Weights

Minimum load front seat: (PIC): 120lbs

Maximum Load per seat: 320lbs ea.

3.4 Maximum Wind

Maximum wing speed 1 mph no gust factor

Maximum cross wind mph no gust factor

Cross wind take offs and landings demand a lot of training and skill, the higher the cross wind, the

greater your skill must be.

3.5 Servi e Ceiling

Maximum service ceiling is 10,000ft due to sport pilot restrictions.

3.6 Load Fa tors

+6 g / - 0 g

3.7 Prohibited Maneuvers

The Pegasus is not certified for aerobatics. Steep turns beyond 60deg

should not be performed. Flights only in VFR conditions. Night flight

requires special optional lighting and a Private Pilots license with an

endorsement.

3.8 Engine Limits

Max EGT 1200F

Max CHT 300F

Max Coolant 17 F

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Original Issue Date 28.05.2007 Revision Date: 28.05.2007

POWRACHUTE Pilot Operating Handbook Model: PEGASUS 582

4. Emergen y Pro edures

4.1. Emergen ies During Wing Inflation

Any anomaly that occurs during the inflation of the wing prior to take off

that does not immediately correct itself or cannot be corrected prior to

actual takeoff is cause to abort the takeoff. Close the throttle, switch off

the ignition (MAG Switches), push the flight steering foot bars full forward

and pull in steering lines by hand to collapse the wing behind the aircraft.

Inspect the aircraft for any source of trouble or review your takeoff

procedures for any problems. If corrections cannot be made, suspend

flying activities till corrections are made. If possible, make necessary

corrections, pack up the wing, go back to the end of the runway, setup and

try again.

If cart rolls over do not try and stop it with feet or hands. Keep hands and

feet tucked in. STUT down the mags and when roll over has stopped

release your seat belt and help passenger if needed.

4.2 Emergen ies in flight

The most likely emergency in flight is loss of engine power. The first priority

in such an occurrence is to pick out an emergency landing site and begin

procedures to approach and land maintaining control of the aircraft

throughout. If you are at low altitude you may have very little time to make

a safe landing. Concentrate on the safe landing task first and foremost.

If you have a lot of altitude allowing time to determine the cause of the

engine stoppage, you may attempt a restart or other action after

selecting a landing site and beginning the emergency approach. In the

majority of cases a safe restart is unlikely so do not spend a great deal of

time on this effort. Concentrate on making a safe landing first.

The power off landing will be at a much higher sink rate that the “normal”

landing with power on being used to control the sink rate. Begin your

landing “flare “ at about 1 ft up and use full flare to keep the touchdown

as light as possible. Use full flare and pull in the steering lines by hand as in

a normal landing.

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Original Issue Date 28.05.2007 Revision Date: 28.05.2007

POWRACHUTE Pilot Operating Handbook Model: PEGASUS 582

5. Normal Pro edures

Training Supplement.

There are some peculiar characteristics of powered parachutes that

need to be emphasized when training flying students. All students should

be trained using the FAA prescribed standards for examination and

practical tests as a guide as to what knowledge and skills the student will

need. The manufacturer's Pilot Operating Handbook should also be used

as a guide for training. For beginning students unfamiliar with any form of

flight, this should be a straight forward process. Particular care on the

part of the instructor however needs to be paid to powered parachute

students who may have experience with other forms of flight. The powered

parachute has some characteristics that are quite different from other

aircraft. Pilots of other aircraft develop habits that could be a hindrance to

safe flight in a powered parachute without proper training.

5.1 Laun hing of the wing:

The powered parachute wing is not ready for flight until it has been "kited

up" and has assumed the proper shape and overhead position for flight.

Sufficient time must be spent on this phase of training to see that the

student is proficient in handling this part of powered parachute

operations. Wing layout, inspection while laid out, kite up sequence, final

visual inspection prior to takeoff and actual takeoff need to be covered as

a part of every students training. Special throttle control required in this

operation needs to be emphasized. In particular, pilots of other forms of

aircraft may need to have this part of the operation made clear as it

differs markedly from what they may be used to.

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Original Issue Date 28.05.2007 Revision Date: 28.05.2007

POWRACHUTE Pilot Operating Handbook Model: PEGASUS 582

5.2 Collapsing of the wing on landing:

Because of the non rigid form of the powered parachute wing, it needs

special handling upon landing to prevent damage. Landing techniques to

control collapse of the wing and make it fall behind the aircraft on landing

are essential to prevent the wing falling on hot engine parts, getting fouled

in the propeller or run over by the landing gear. This procedure is

essential to training for all students. Again special care must be exercised

with students who have experience in other forms of aircraft in order to

point out the need for special procedures unfamiliar to them.

5.3 Pa king and unpa king the wing:

Because of the non rigid nature of the powered parachute wing and it's

susceptibility to ultraviolet ray damage from prolonged sunlight exposure,

it needs to be stowed in a bag or other container when not in use. This

requires that it be packed and unpacked with each use. Instruction in the

proper methods for performing packing and unpacking that will minimize

wear and damage to the wing and it's related accessories is essential.

5.4 Potential for rollover:

Because a powered parachute wing is situated many feet above the

center of gravity of the aircraft, the aircraft has a potential to be dragged

over or pulled over by combined forces of wind and propeller thrust under

certain conditions. Commonly referred to as a "rollover". Instruction in

proper techniques to minimize this risk is essential. Instruction as to what

operational signals indicate an impending rollover or pullover and

appropriate pilot actions is also essential. Again, pilots with experience in

other forms of aircraft need special emphasis on these issues to point out

how they differ from what they understand and the habits they have

developed.

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Original Issue Date 28.05.2007 Revision Date: 28.05.2007

POWRACHUTE Pilot Operating Handbook Model: PEGASUS 582

5.5 Landing Flare:

Another unique feature of powered parachutes is the use of the in flight

turning or "steering" controls when landing. Using both the left and right

controls simultaneously allows for "braking" or "flaring" on final approach

just before touchdown to reduce speed and "round out" or level off the

descent for a smooth touchdown. It is essential to learn this technique and

achieve sufficient proficiency for use in the event of an engine failure in

flight. Again, powered parachute students with experience in other forms

of aircraft need special emphasis on this difference from what they are

used to.

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Original Issue Date 28.05.2007 Revision Date: 28.05.2007

POWRACHUTE Pilot Operating Handbook Model: PEGASUS 582

5.6 Preflight Che klist (Detailed)

Before each flight the pilot in command of the flight should conduct a

preflight inspection to assure that the aircraft is in a safe condition for

flight. The following is a detailed description of a suggested procedure for

such a preflight inspection. The pilot in command is encouraged to develop

his or her own inspection routine to suit their own individual aircraft

configuration and needs. The following is only a suggested guide.

For convenience this suggested procedure starts at the left side of the

front or nose wheel and proceeds rearward, around and back to the right

front side of the nose wheel examining each point along the way. This is a

detailed description of suggested procedure. An abbreviated checklist will

be repeated afterwards which can be used as a checklist in the field to

remind the pilot of what items are suggested to be covered in the preflight

inspection.

Nose wheel, Brake and ground steering.

Check for security of the nose wheel on it’s axle with nut secure, security

of wheel fork and pivot bolt, brake mechanism secure and operating,

centering springs OK, steering arm secure. Wheel and steering turn

freely.

Left Hand flight steering foot bar, steering line, pulley and trim system.

Check that foot bar is secure, pivots freely, steering line in good order,

pullies in good order and trim system secure, moves freely and in proper

takeoff position.

Instrument Pod, instruments, switches, displays.

Check that instrument pod is secure, all instruments and switches secure,

switches in safe position before engine startup.

Front ground steering .

Check for proper range of steering and check all nuts and bolts.

Front seat & belts left hand side.

Check that front seat and seat belts are securely fastened to airframe.

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Original Issue Date 28.05.2007 Revision Date: 28.05.2007

POWRACHUTE Pilot Operating Handbook Model: PEGASUS 582

Rear seat and belts left hand side.

Check that rear seat and seat belts are securely fastened to airframe.

Left side riser connections, steering line, pulley, links and riser.

Check left side riser connections to airframe, brackets secure, links finger

tight plus no more than ¼ turn, never over tighten these links. Mallion

Rapide links are only ones approved. Steering line properly routed, in good

condition, pulley, riser in good condition and properly connected (no

twists).

Rear suspension and pivots left side.

Check that all left side suspension pivots are smooth and free from

excessive wear, springs shocks and tubes in good order.

Wheel, tire and axle left side.

Check that left side tire is in good condition, properly inflated, axle secure,

axle nut secure.

Left side battery, radiator and radiator mounts.

Check left side battery mount secure, battery secure and free of leaks, left

side radiator mounts secure, radiator free of leaks, drain cock closed.

Left side of engine.

Check left side exhaust, exhaust springs, sparkplugs, plug caps and plug

wires.

Left side prop cage.

Check left side prop cage tubes, all tubes secure, bolts secure, etc.

Propeller and gearbox.

Check gearbox for leaks, move prop to check for normal gearbox

backlash, examine prop for damage, cleanliness, distortion, etc.

Right hand side of engine.

Check right side carburetor and mounting, check carb boots for cracks,

throttle and choke linkages and fuel lines.

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Original Issue Date 28.05.2007 Revision Date: 28.05.2007

POWRACHUTE Pilot Operating Handbook Model: PEGASUS 582

Right hand suspension.

Check that all right side suspension pivots are smooth and free from

excessive wear, springs shocks and tubes in good order.

Wheel, tire and axle right side.

Check that right side tire is in good condition, properly inflated, axle

secure, axle nut secure.

Coolant overflow bottle and header tank.

Check that coolant bottle is secure, filled to proper level, lines are secure,

no leaks, cap is secure. Check header tank and hoses. Tank secure, cap

secure, lines and clamps secure, no leaks.

Oil Tank

Check that oil bottle is secure, filled to proper level, lines are secure, no

leaks and cap is secure.

Strobe light.

Check strobe light for secure mounting, wiring in good order, lens secure,

etc.

Fuel tank and fuel gage right side.

Check fuel tank for leaks, secure mountings, check fuel gage for fuel level

and any leaks. Check fuel tank vent for security and lack of blockage or

leaks. Check the fuel filter for any contamination.

Gascolator and fuel sample.

Visually check gascolator, securely connected to airframe and fuel lines,

draw sample, check for water, correct fuel color, dirt or other

contamination.

Rear throttle.

Check rear throttle control and linkage for proper action and security.

Rear seat and belts right hand side.

Check that rear seat and seat belts are securely fastened to airframe.

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Original Issue Date 28.05.2007 Revision Date: 28.05.2007

POWRACHUTE Pilot Operating Handbook Model: PEGASUS 582

Right side riser connections, steering line, pulley, links and riser.

Check right side riser connections to airframe, brackets secure, links

finger tight+?, steering line properly routed, in good condition, pulley, riser

in good condition and properly connected (no twists).

Front seat & belts right hand side.

Check that front seat and seat belts are securely fastened to airframe.

Throttle controls.

Check throttle controls, assembly secure to airframe, linkages secure,

cables and housings in good condition, friction set correctly, throttle levers

move smoothly thru full range.

Right Hand flight steering foot bar, steering line, pulley and trim system.

Check that foot bar is secure, pivots freely, steering line in good order,

pullies in good order and trim system secure, moves freely and in proper

takeoff position.

Nose wheel, right side.

Check for security of the nose wheel on it’s axle with nut secure, security

of wheel fork and pivot bolt.

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Original Issue Date 28.05.2007 Revision Date: 28.05.2007

POWRACHUTE Pilot Operating Handbook Model: PEGASUS 582

5.7 Preflight Che klist (Abbreviated)

The following is an abbreviated checklist which can be used during a

preflight inspection to remind the pilot of those items to be checked. See

the detailed preflight checklist for exact procedures to follow.

Nose wheel, Brake and ground steering.

Left Hand flight steering foot bar, steering line, pulley and trim system.

Instrument Pod, instruments, switches, displays.

Ground Steering controls

Front seat & belts left hand side.

Rear seat and belts left hand side.

Left side riser connections, steering line, pulley, links and riser.

Rear suspension and pivots left side.

Wheel, tire and axle left side.

Battery, radiator and radiator mounts.

Left side of engine.

Left side prop cage.

Propeller and gearbox.

Right hand side of engine.

Right hand suspension.

Wheel, tire and axle right side.

Coolant overflow bottle and header tank.

Strobe light.

Oil tank.

Rear throttle.

Rear seat and belts right hand side.

Right side riser connections, steering line, pulley, links and riser.

Front seat & belts right hand side.

Throttle and choke controls.

Right Hand flight steering foot bar, steering line, pulley and trim system.

Nose wheel, right side.

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Original Issue Date 28.05.2007 Revision Date: 28.05.2007

POWRACHUTE Pilot Operating Handbook Model: PEGASUS 582

6. Performan e

The performance figures stated below are given at sea level of the

international standard atmosphere conditions. Operations at higher

altitudes and temperatures WILL reduce takeoff and climb performance.

Pegasus Power Para hute Performan e

16

Seating

Dual Seats

Empty Weight

418 lbs.

Max Gross Weight / PD500 Wing

1100lbs @ Sea Level -5% per 1000ft msl

Canopy Span

32.9 feet

Canopy Area

500 square feet (with standard chute)

Fuel Capacity

10 U.S. gallons

Propeller

3-blade PowerFin composite

Length

128 inches

Height

84 inches



Standard Engine

Rotax 582



Power

65 horsepower @ 6500 RPM



Power Loading

16.9 lbs per horsepower



Cruise Speed

30-32 mph



Glide Ratio

4 1 Max



Rate of Climb

900 feet per minute max



Takeoff Distance

350 feet at gross weight



Landing Distance

250 feet at gross weight

Original Issue Date 28.05.2007 Revision Date: 28.05.2007

POWRACHUTE Pilot Operating Handbook Model: PEGASUS 582

6.1 Takeoff Distan es

Take-off range over a 0ft obstacle with 6 0lb gross after lift off point @

Sea Level: 210ft ….4000 Ft MSL: 320ft

Take-off range over a 0ft obstacle with 1100lb gross after lift off point @

Sea Level: 330ft…. 4000 Ft MSL: 490ft

6.2 Rate of Climb

Best Rate of climb at max gross payload 6 0lb: 700ft per min

Best Rate of climb at max gross payload 1100lb: 380ft per min

6.3 Fuel Consumption

Fuel consumption is variable based on the payload and engine rpms at

cruise. At Max power 6 00rpms the Rotax 82 will burn 7.2 US Gallons

per hour. Average cruise settings should yield 4. - US gallons per hour.

7. Speed

Speed will be determined by gross weight of the PPC.

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Original Issue Date 28.05.2007 Revision Date: 28.05.2007

POWRACHUTE Pilot Operating Handbook Model: PEGASUS 582

8. Weight and Balan e

Aircraft Information:

" "o._______________________________________________________

Serial "o.____________________________________________________

Empty Weight________________________________________________

Max Weight__________________________________________________

Use ul Load__________________________________________________

Wing Make and Model_________________________________________

Front Seat PIC (Pilot In Command) Loading range:

5&8 Setting 80-130lbs Pilot Weight

4&7 Setting 130-180lbs Pilot Weight

3&6 Setting 180-230lbs Pilot Weight

2&5 Setting 230-280lbs Pilot Weight

1&4 Setting 280-330lbs Pilot Weight

"ote:

*Empty Weight

The total weight of complete plane, all permanently installed accessories and equipment.

*Gro Weight

The maximum authorized weight as specified by the wing manufacture for particular

wing being used.

*U eful Load

The difference between empty weight and gross weight.

If weight falls outside specified range please contact Powrachute @ 574-286-9670

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Original Issue Date 28.05.2007 Revision Date: 28.05.2007

POWRACHUTE Pilot Operating Handbook Model: PEGASUS 582

9. Systems and Des ription

The airframe of the Pegasus Power Parachute is constructed of 6061-T6

aircraft-grade aluminum and 4130 chromoly steel to be durable yet

lightweight. It includes many features which differentiate it from most of

the competition. Full-length main rails, aluminum fuel cell, It also includes

two separate bucket seats for comfort and safety, and the most ground

clearance in the industry.

The components of the airframe are discussed in more detail on the

following pages.

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Original Issue Date 28.05.2007 Revision Date: 28.05.2007

POWRACHUTE Pilot Operating Handbook Model: PEGASUS 582

9.1 Chassis Overview

Serial Number - The serial number of your Pegasus PPC is located on a plate located

on the left side main frame rail behind the pylon tube. You should refer to this serial

number in any communications with Powrachute regarding your Pegasus PPC.

Main Frame Rails - The main rails of the Pegasus are constructed of sturdy chromoly

steel alloy for strength.

Prop Ring - Protection… First, they protect people and animals from the spinning

propeller. Second, the prop rings protect delicate chute lines from the prop and

engine during takeoff and landing. Finally, the ring provides protection for you and your

machine should you ever roll the machine over or have an accident.

Fuel Tank - The fuel tank on your Pegasus PPC is made out of aluminum. An optional

fuel level sensor can be added so the fuel level can be read from the EIS system.

Suspension System - The rear suspension of the Pegasus PPC has been engineered

to smooth out bumps on even the roughest flying surfaces. The suspension consists of

spring over oil shock coupled with soft turf glide tires. This combination provides a

suspension that is effective, durable, and lightweight. Powrachute recommends that

you keep the air pressure in them to no more than 10-12 lbs. This will keep them

sufficiently soft to help smooth out rough terrain.

Ground Steering Lever - As you sit in the front seat of the Pegasus, the ground

steering lever is strait in front of the PIC. This handle allows you to steer the craft

while it is taxiing on the ground. Push the steering lever to the right to turn left and to

the left to turn right. The springs will help self center the steer bar when let go.

Throttle Lever - The throttle lever, controlled by the right hand, regulates the output of

the engine. The throttle is configured like most operating equipment, meaning that you

push the throttle forward to make the craft climb and pull it back to descend. The front

throttle is connected to a rear throttle lever, which allows the throttle to be controlled

from the rear seat.

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Original Issue Date 28.05.2007 Revision Date: 28.05.2007

POWRACHUTE Pilot Operating Handbook Model: PEGASUS 582

Steering Bars - As you sit in the pilot seat, your feet should rest comfortably on the

steering bars. Adjust the steer bars so that you can fully depress the bars. The

steering bars control the direction of the craft while in the air. Depressing the left

steering bar causes the craft to turn left, while depressing the right steering bar

causes the craft to turn right. The chute steering lines should be firmly attached to the

trim lock.

Primer - The engine primer is located by the throttle on the right side. The primer is

used to aid in easy engine starting. By priming the engine with fuel prior to starting,

the engine starts much easier than with a choke. The primer can also be used in an

emergency to shut down the engine (should your mag switches fail, for example). To

shut the engine down with the primer, simply pump the primer until the engine floods

with fuel and shuts down.

Optional Brake - Powrachute offers a disk brake option. The brake allows the pilot to

control taxiing speeds while on the ground. Note that the effectiveness of the brake is

diminished by the lightness of the machine’s front end, so the brakes should not be

relied upon to quickly bring the machine to a full stop. The brake lever is mounted on

the ground steering lever.

Nylon Riser Straps - The parachute is mounted to the Pegasus airframe via extremely

strong riser straps, total lift capacity 24,000lbs. The straps combine high strength

with some elasticity to provide safe yet smooth flight. The riser straps should be

carefully inspected before each flight, and the parachute should be secured to the

straps only by a qualified instructor. NEVER disconnect your chute from the straps

unless you are qualified to do so.

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Powrachute PEGASUS 582 Owner's manual

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