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Serial Number 1646

Date of Issue: 23 June 2017

Revision - Original

Airspeed Limits

(Best Rate of Climb)

65KT

(Stall Speed, No Flaps)

33KT

(Stall Speed, Full Flaps)

28KT

(Max Flap Extension Speed)

72KT

(Maneuvering Speed)

97KT

(Max Struc. Cruising Speed)

108KT

(Max Speed @ 5800rpm for 5 minutes)

103KT

(Never Exceed Speed)

130KT

Wind speed limits

Maximum allowed headwind speed

20kn

Maximum allowed crosswind speed:

8kn (inexperienced pilot)
15kn (Experienced pilot/Instructor)

Power plant limits

Maximum allowed speed:

5800rpm for 5 minutes

Maximum continuous speed:

5500rpm

Idling speed, approximately:

1400rpm

Maximum cylinder head temperature:

266 deg F

Maximum oil temperature:

275deg F

Minimum air temperature at starting:

13deg F

Maximum air temperature at starting:

122deg F

Oil pressure:

16.7psi

Weights

Minimum crew weight:

132 lbs

Maximum take-off weight:

1320 lbs

Empty weight (typical)

766 lbs

Maximum COG locations from front edge of wing:
Forward limit

26% MAC

Aft limit:

34% MAC

Max. Baggage weight

33 lbs

Tailwind take-off and landing should be avoided.

- Do not apply full deflections above this speed

The V

speed must not be exceeded under any circumstances!

All speeds stated in this Manual are Indicated Air Speeds IAS!

Содержание Legend 600

Страница 1: ...ion Original 1 Callsign N54SK Serial no 1646 Dated 23 June 2017 Jen kovsk 1815 286 01 slav Phone 420 605 296 563 Fax 420 327 312 630 www aeropilotcz com CIN 27108431 TIN CZ27108431 Pilot Operating Han...

Страница 2: ...1646 Date of Construction 06 16 2016 Registration N54SK Airworthiness Category Special Light Sport Aircraft S LSA Issue Date of POH 06 23 2017 This airplane must be operated in compliance with inform...

Страница 3: ...iginal 3 Record of Revisions Any revisions to the handbook must be recorded in the following table The responsible airworthiness authority must endorse it where applicable Revision Section Pages Date...

Страница 4: ...ION 5 GENERAL INFORMATION 7 LIMITATIONS 15 EMERGENCYPROCEDURES 19 NORMAL PROCEDURES 23 PERFORMANCE 30 WEIGHT AND BALANCE AND EQUIPMENT LIST 33 DESCRIPTION OF AIRPLANE AND SYSTEMS 36 HANDLING AND SERVI...

Страница 5: ...performed The aircraft s owner is responsible for correctness of operation records Important information Changes and Amendments to this Manual Any changes to applicable regulations or to this aircraf...

Страница 6: ...LEGEND 600 S LSA AS MANUFACTURED ON PREMISES BY THE AEROPILOT SRO AIRCRAFT THAT DIFFER FROM THE PRODUCTION STANDARD IN WHATEVER WAY ARE NOT ADDRESSED IN THIS MANUAL EXCEPT TO THE EXTENT SAID AIRCRAFT...

Страница 7: ...boarding of crew and loading of baggage Adjustable seats allow the pilots of all heights to find comfortable position A stiff Kevlar cabin four point seat harnesses and rocket assisted rescue system p...

Страница 8: ...Serial Number 1646 Date of Issue 23 June 2017 Revision Original 8 Aircraft Drawing Measurement in Inches and Millimeters...

Страница 9: ...64 Depth of MAC mean aerodynamic chord 3 93 feet Wing profile MS 313 B At root 4 27 feet At tip 3 15 feet Wing flaps surface 11 83ft2 Flaps deflections 15 30 40 Tail Horizontal tail plane span 9 19 fe...

Страница 10: ...Composite Performance Summary SUMMARY OF PERFORMANCE SPECIFICATIONS Call Sign N54SK Type Name LEGEND 600 Serial No Year of manufacture 1646 2016 Empty weight 766 lbs Max Take off weight 1320 lbs Usefu...

Страница 11: ...Battery Charger Unit BIT Built In Test CAS Calibrated Air Speed CFI Certified Flight Instructor CFII Certified Flight Instructor Instrument CFR Code of Federal Regulations FAA CG Center of Gravity DIS...

Страница 12: ...b TOD Top of Descent VFR Visual Flight Rules VMO Maximum Allowable Airspeed VOR Very High Frequency Omni directional Range Radio VORTAC Collocated VOR and TACAN Stations VS Vertical Speed VSI Vertical...

Страница 13: ...een the runway and the wind direction It is known that runway 17 means a direction of 170 from that subtract the wind direction of 140 This gives a 30 angular difference or wind angle Next locate the...

Страница 14: ...o OM 912 Latest revision edition of Rotax SD 912 064UL as applicable to type of engine fitted Operator manual for GPS Flight and Engine Instruments COM radio transponder and GPS SkyView SVHDX Version...

Страница 15: ...ATA AND LIMITATIONS Call Sign N54SK Type Name LEGEND 600 Manufacturer AEROPILOT SRO Serial No Year of manuf 1646 2017 Empty weight 766LBS Max Take off weight 1320LBS Payload 554LBS Stall Speed 38 KT N...

Страница 16: ...on Original 16 USA REGISTRATION DECAL Call Sign N54SK Type Name LEGEND 600 Manufacturer AEROPILOT SRO Serial No Year of manuf 1646 2015 Empty weight 766 LBS Max Take off weight 1320 LBS Payload 554 LB...

Страница 17: ...ed speed 5800rpm for 5 minutes Maximum continuous speed 5500rpm Idling speed approximately 1400rpm Maximum cylinder head temperature 266 deg F Maximum oil temperature 275deg F Minimum air temperature...

Страница 18: ...neuvers Turns up to 60 banking angle climbing and diving up to 30 from horizontal plane INTENTIONAL SPINS AEROBATCIS AND FLIGHT IN IMC PROHIBITED Load factors per UL 2 regulation Maximum positive load...

Страница 19: ...f the ignition Tighten safety harnesses Main switch off In flight Dive and glide maintain speed 65kts minimum More than 300ft above terrain select suitable landing location If cause of engine failure...

Страница 20: ...ning horizon at approx 150ft altitude Apply take off flaps maintain speed 65knots Carefully check the location Climb a little maintaining ground visibility if conditions permit fly small left circuit...

Страница 21: ...e of vibrations Proceed as follows should any unnatural vibrations occur Adjust engine speed to a value which minimizes the vibrations Land at nearest airport or perform safety landing If vibrations k...

Страница 22: ...as possible without the use of brakes if possible Always try to land with headwind and with engine off Recovering from unintentional spin Intentional spins are prohibited The aircraft has never been...

Страница 23: ...Serial Number 1646 Date of Issue 23 June 2017 Revision Original 23 Normal Procedures Pre flight inspection...

Страница 24: ...level according to engine manufacturer s manual check coolant Check engine cowling fastening Check tightness of fuels hoses tank caps fuel filters Check fuel filter for impurities and water Refueling...

Страница 25: ...ters or less marked on the fuel gauges select the other tank with the fuel valve and continue flying until fuel levels in both tanks equalize If both fuel tanks become empty 10 liters or less marked o...

Страница 26: ...l cylinder head and oil temperature reaches 122deg F minimum Test maximum rpm check transition from minimum to maximum rpm and back Check function of both ignition circuits by switching off the first...

Страница 27: ...re or oil temperature reaches maximum operating limit you must reduce engine power and climbing rate Climb to altitude necessary for subsequent flight Mandatory actions after take off Height above ter...

Страница 28: ...il the main wheels touch down Always touch down on main landing gear wheels Pull up yoke gradually to maintain nose gear above ground for as long as possible When nose gear finally touches down apply...

Страница 29: ...h off Main switch Switch off Fuel cocks close Stopping the aircraft parking Taxi very carefully before stopping the aircraft paying attention to obstacles and terrain Brake the aircraft and shut off t...

Страница 30: ...rspeed Conversion Table Stall speeds Conditions Max TOW engine at idle Flaps deflection Knots IAS Height loss during recovery ft Horizontal flight 0 47 26 15 41 38 30 36 50 Turn with 30 bank angle 0 5...

Страница 31: ...x Continuous power 5500rpm aircraft weight 600kgs Ideal climbing speed rate Knots IAS Ft Min 1500ft ISA 65 1100 4000ft ISA 65 850 8000ft ISA 65 650 Cruise Flight Performance data corresponding to inle...

Страница 32: ...Endurance hh mm 10 00 8 34 8 00 6 40 6 00 Range Nm 817 782 765 700 678 Verified performance with crosswind Max allowed headwind for take off and landing 20 Knots Max allowed crosswind for take off an...

Страница 33: ...mpartment with maximum allowed load Empty fuel tanks Weighing for forward centre of gravity Empty baggage compartment Move seats to foremost position Full fuel tanks Weight and balance record of the a...

Страница 34: ...ding Problem shown below Loading Provisions and Calculations Figure 1 shows the distance or ARM from the datum point set at the leading edge of the aircraft for the Pilot Passenger seats the Fuel Tank...

Страница 35: ...non GPS SkyView 7 SVD700 TBD Galaxy Rescue System Model manufacturer serial No GALAXY 6 600SD Activation By pulling the handle on central panel Descent speed max m s 6 6m s At take off weight 600 kg M...

Страница 36: ...and screws Aerodynamically balanced elevator has electrically servo actuated trim tab The elevator deflection is 21 up and 13 down Fixed part of trapezoidal swept vertical tail is offset from a longi...

Страница 37: ...ce versa Engine throttle moving combined controller located on the middle panel forward from its central position in the flight direction increases engine output and vice versa Brake control pulling c...

Страница 38: ...N Oil type SHELL HELIX H x 7 AV 10 W 40 Oil capacity 3L Reduction gear gear ratio 2 43 1 Fuel tank volume main tank 130L Propeller Diameter pitch at 75 Woodcomp Klassic ground adjustable Weight 5kg Ma...

Страница 39: ...de Choke Central controller left instrument panel Throttle Central controller bottom part of middle panel Brakes Central controller bottom part of middle panel Longitudinal trim Control yokes Wing fla...

Страница 40: ...Serial Number 1646 Date of Issue 23 June 2017 Revision Original 40 Central controller functions Drawing 30 Flaps extend 31 Flaps retract 32 Engine throttle 33 Wheel brake parking brake...

Страница 41: ...he auxiliary pointed pin first then replace it with M8 screw Check that no cables or hoses are pinched during assembly Connect strut to the wing Install two aerodynamic covers on the strut and then in...

Страница 42: ...ed When transporting over longer distance or in closed cargo bay of a truck elevator must be removed If elevator is not removed it must be fitted with red pennants or accompanying vehicle must be proc...

Страница 43: ...ions halve this interval to 50 hours Demanding operating conditions include Glider towing Ambient temperatures continuously exceeding 35 C or very dusty conditions This inspection consists of the foll...

Страница 44: ...eck of cables and attachment Check attachment of rescue system and its components ropes containers Verify function of tow hook control cable if installed Reinstall engine cowling propeller cone ceilin...

Страница 45: ...ight solo duration 15 flights 1 hour a 40 minutes Turns bank angle 15 45 solo duration 3 flights 1 hour Maintaining attitude heading prevention of loss of height duration 2 flights 30 minutes Landing...

Страница 46: ...of landing is concerned the instructor explains the effect of wind length of runway possible turbulence near ground and other factors which may influence the decision during planning of landing He poi...

Страница 47: ...ble to use glissade to correct landing approach In the free area the student is able to select area suitable for landing and plan the landing correctly 4 10 Lesson 10 Landing with crosswind Training m...

Страница 48: ...f runway length without further use of engine power The instructor is responsible for safe performance of this Lesson taking into account the altitude position of aircraft in traffic pattern wind spee...

Страница 49: ...Training methodology The instructor defines flight route with landing at different airfield Definition is the same as in Lesson 20 The only difference is that the student flies solo The instructor ve...

Страница 50: ...t time with actual fuel consumption V Always choose your bearing and altitude so that you will be able to make emergencylanding VI Always fly with a sufficient speed margin especially during the take...

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