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EVEKTOR-AEROTECHNIK Harmony LSA Operating Instructions Manual

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EVEKTOR - AEROTECHNIK a.s.
Letecka 1384
686 04 Kunovice
CZECH REPUBLIC
AIRCRAFT OPERATING INSTRUCTIONS
LIGHT SPORT AIRCRAFT
Serial number:
Registration mark:
Document number:
Date of issue:
This manual must be on the airplane board during operation. This manual
contains
information
and also contains supplementary information provided by the airplane
manufacturer - Evektor - Aerotechnik a.s.
This aircraft must be operated in compliance with the information
FOR
HARMAOIUS
June 01, 2011
which
must
and limitations stated in this manual.
Copyright © 2011
EVEKTOR - AEROTECHNIK, a.s.
Tel.: +420572 537 111
Fax: +420 572 537 900
email: marketing@evektor.cz
www.evektoraircraft.com
be
provided
to
the
pilot

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  • Page 1 EVEKTOR - AEROTECHNIK a.s. Letecka 1384 Tel.: +420572 537 111 686 04 Kunovice Fax: +420 572 537 900 CZECH REPUBLIC email: marketing@evektor.cz www.evektoraircraft.com AIRCRAFT OPERATING INSTRUCTIONS LIGHT SPORT AIRCRAFT Serial number: Registration mark: HARMAOIUS Document number: June 01, 2011 Date of issue: This manual must be on the airplane board during operation.
  • Page 3 Section 0 Technical Information AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS CONTENTS 0. TECHNICAL INFORMATION Log of Revisions ............0-3 List of Effective Pages...........0-5 AOI Sections..............0-8 June 01, 2011...

  • Page 4: June

    Section 0 Technical Information AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Intentionally left blank June 01, 2011...

  • Page 5: Log Of Revisions

    Section 0 Technical Information AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Log of Revisions All revisions or supplements to this manual, except actual weighing data, are issued in form of revisions, which will have new or changed pages as appendix and the list of which is shown in the Log of Revisions table. The new or changed text in the revised pages will be marked by means of black vertical line on the margin of page and the revision number and date will be shown on the bottom margin of page.
  • Page 6 Section 0 Technical Information AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Rev. Affected Affected Date Appro- Date Date of Sign. Section Pages Insertion June 01, 2011...
  • Page 7 Section 0 Technical Information AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 0.2 List of Effective Pages Section Page Date Section Page Date 06/01/2011 Title page 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 2-10 06/01/2011...
  • Page 8 Section 0 Technical Information AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Section Page Date Section Page Date 06/01/2011 06/01/2011 5-12 06/01/2011 06/01/2011 5-13 06/01/2011 06/01/2011 5-14 06/01/2011 06/01/2011 5-15 06/01/2011 06/01/2011 5-16 06/01/2011 06/01/2011 5-17 06/01/2011 06/01/2011 5-18 06/01/2011 06/01/2011 06/01/2011 4-10 06/01/2011 4-11...
  • Page 9 Section 0 Technical Information AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Section Page Date Section Page Date 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 8-10 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 06/01/2011 7-10 06/01/2011 06/01/2011 7-11...
  • Page 10 Section 0 Technical Information AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS AOI Sections Section GENERAL ................1 LIMITATIONS ................2 EMERGENCY PROCEDURES ..........3 NORMAL PROCEDURES ............4 PERFORMANCE ..............5 WEIGHT AND BALANCE ............6 AIRPLANE AND SYSTEM DESCRIPTION ......7 AIRPLANE HANDLING, SERVICING AND MAINTENANCE .............8 SUPPLEMENTS..............9 June 01, 2011...

  • Page 11: Table Of Contents

    Section 1 General AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS SECTION 1 1. GENERAL Introduction ..............1-3 Certification basis ............1-3 1.2.1 Data location..............1-4 Warnings, cautions, notes..........1-4 Descriptive data .............1-5 1.4.1 Airplane description............1-5 1.4.2 Powerplant................ 1-5 1.4.3 Main technical data ............1-6 1.4.4 Three-view drawing............

  • Page 12: General

    Section 1 General AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Intentionally left blank June 01, 2011...

  • Page 13: Introduction

    This Aircraft Operating Instructions has been prepared to provide pilots and instructors with information for safe and efficient operation of the HARMONY LSA airplane. It also contains supplementary information considered to be important by the airplane manufacturer. Certification basis...

  • Page 14: Data Location

    Section 1 General AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 1.2.1 Data location The certification documentation is available from the US importers or airplane manufacturer on a request of competent aviation authority and/or Designated Airworthiness Representative. Contact address: Visit www.evektoraircraft.com for US importers. Airplane Manufacturer: Evektor - Aerotechnik, a.s.

  • Page 15: Descriptive Data

    Doc. No. HARMAOIUS Descriptive data 1.4.1 Airplane description HARMONY LSA airplane is a metal-composite low-wing monoplane of semimonocoque structure with two side by side seats and steerable nose wheel landing gear. For further description see Section 7 - Airplane and system description.

  • Page 16: Main Technical Data

    Section 1 General AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 1.4.3 Main technical data Wing Span 30.45 ft Area 111.47 sq.ft MAC depth 3.873 ft Wing loading with vortex generators 11.84 lbs/sq.ft Wing loading no vortex generators 11.38 lbs/sq.ft Aileron - area 3.35 sq.ft Flap - area 5.60 sq.ft...

  • Page 17: Three-View Drawing

    Section 1 General AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 1.4.4 Three-view drawing Figure 1-1 June 01, 2011...

  • Page 18: Definitions And Abbreviations

    Section 1 General AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Definitions and abbreviations NOTE The abbreviations on placards in the airplane cockpit are printed in BOLD CAPITAL LETTERS in the text of this Aircraft Operating Instructions. ACCU accumulator ALT ENC encoding altimeter air traffic control bar 1 bar = 100 kPa BEACON...

  • Page 19: June

    Section 1 General AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS system is switched off or control element is in off- position system is switched on or control element is in on- position pascal 1Pa = 1N/m pound per sq.in (1PSI = 6.89 kPa) revolutions per minute runway sq.ft...
  • Page 20 Section 1 General AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Intentionally left blank 1-10 June 01, 2011...
  • Page 21 Section 2 Limitations AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS SECTION 2 2. LIMITATIONS Introduction ..............2-3 Airspeed .................2-3 Airspeed indicator marking ...........2-4 Powerplant..............2-5 Powerplant instrument marking........2-6 Miscellaneous instrument marking.......2-6 Weight................2-6 Centre of gravity.............2-7 Approved manoeuvres ..........2-7 2.10 Manoeuvring load factors..........2-7 2.11 Flight crew..............2-7 2.12 Kinds of operation ............2-8 2.13 Fuel .................2-9 2.14 Oil..................2-10...

  • Page 22: Limitations

    Section 2 Limitations AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Intentionally left blank June 01, 2011...

  • Page 23: Limitations

    Section 2 Limitations AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Introduction Section 2 contains operation limitation, instrument marking and basic placards necessary for safe operation of airplane and its engine, standard systems and equipment. Limitation for optional systems and equipment are stated in section 9 - Supplements.

  • Page 24: Airspeed Indicator Marking

    Section 2 Limitations AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Airspeed indicator marking Airspeed indicator markings and their color-code significance are shown in the table below: Marking Range Meaning KIAS mph IAS Red line at maximum weight (flaps in landing position 50°) 44 –...

  • Page 25: Powerplant

    Section 2 Limitations AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Powerplant Engine manufacturer: Bombardier-Rotax GMBH Engine type: ROTAX 912 ULS (S2 for IFR version) Power: 73.5 kW / 100 HP maximum take-off maximum continuous 69 kW / 95 HP Engine speed: 5800 RPM maximum take-off max.

  • Page 26: Powerplant Instrument Marking

    Section 2 Limitations AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Powerplant instrument marking The color-code of instruments is shown in the following table: Red line Green arc Yellow arc Red line Lower Normal Caution Upper Instrument Units limit operation range limit range RPM indicator 1400 - 5500...

  • Page 27: Centre Of Gravity

    Reference datum origin is the 2.74 in (69.5 mm) behind wing leading edge. MAC = 46.48 in (1180.5 mm) Approved maneuvers HARMONY LSA airplane is approved to perform the following maneuvers: steep turns up to bank angle of 60 climbing turns...

  • Page 28: Kinds Of Operation

    Section 2 Limitations AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS WARNING DO NOT EXCEED MAXIMUM WEIGHTS! THEIR EXCEEDING LEADS AIRPLANE OVERLOADING AND TO DEGRADATION OF FLIGHT CHARACTERISTICS DETERIORATION OF MANOEUVRABILITY. 2.12 Kinds of operation The airplane is standard approved for VFR daylight flights. WARNING NIGHT FLIGHTS ACCORDING TO VFR, FLIGHTS ACCORDING TO IFR (BY INSTRUMENTS) ARE APPROVED ONLY WHEN...

  • Page 29: Fuel

    Section 2 Limitations AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 2.13 Fuel Fuel tank volume (each) 15.85 U.S. gallons Total 31.7 U.S. gallons Usable fuel 31.2 U.S. gallons Unusable fuel 0.5 U.S. gallons (0.25 US gal per tank) June 01, 2011...

  • Page 30: Oil

    Section 2 Limitations AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS NOTE It is not recommended to fully tank the fuel tanks. Due to fuel thermal expansion keeps about 2.11U.S. Gallons of free space in the tank to prevent fuel bleed through the vents in the wing tips thus preventing environmental contamination.

  • Page 31: Limitation Placards

    Section 2 Limitations AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 2.17 Limitation placards The following placards are located on the instrument panel: The following placard is located on the instrument panel: WAR NING ASI AND ALT ON EFIS A RE INFORM ATIVE ONLY! SEE ANALOGUE INSTRUMENTS.
  • Page 32 Section 2 Limitations AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS The following placard is located in the baggage compartment: The following placard is located behind the baggage compartment: It prohibits use of that place for additional stowage due to airplane aft C.G. limit. 2-12 June 01, 2011...
  • Page 33 Section 2 Limitations AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS The following placards are located on sides of the tip-up canopy: Day VFR airplane Or (Night VFR airplane) or (IFR airplane) This Light Sport Aircraft has been approved by the Manufacturer for IFR flights with the following limitations: Not authorized for IFR flights into known or forecast possible icing conditions.
  • Page 34 Section 2 Limitations AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Intentionally left blank 2-14 June 01, 2011...
  • Page 35 Section 3 Emergency Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS SECTION 3 3. EMERGENCY PROCEDURES Introduction ..............3-3 Speeds for performing emergency procedures...3-3 Engine failure ..............3-3 3.3.1 Engine failure at take-off run ..........3-3 3.3.2 Engine failure at take-off ........... 3-3 3.3.3 Engine failure in flight............

  • Page 36: Doc. No. Harmaoius Section

    Section 3 Emergency Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Intentionally left blank June 01, 2011...

  • Page 37: Emergency Procedures

    Section 3 Emergency Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Introduction Section 3 describes operations and procedures for emergency situation solutions that could possibly occur during airplane operation. Speeds for performing emergency procedures Airspeed for the best gliding ratio 59 KIAS (68 mph IAS) (flaps retracted) Precautionary landing 55 KIAS (63 mph IAS)

  • Page 38: Engine Failure In Flight

    Section 3 Emergency Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 4. Flaps as needed 5. FUEL SELECTOR 6. Ignition 7. ATC report 8. Master switch 9. After touch down brake as needed 3.3.3 Engine failure in flight 1. Gliding speed 59 KIAS (68 mph IAS) 2.

  • Page 39: Engine Fire

    Section 3 Emergency Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 8. THROTTLE lever idle (choke opened) or increased idle (choke closed) The propeller is rotating: 9. Ignition BOTH The propeller is not rotating: 10. Ignition START 11. If engine starting does not occur, increase gliding speed up to 108 KIAS (124 mph IAS) (see NOTE), so that air-flow turns the propeller and engine will start.

  • Page 40: Fire In Flight

    Section 3 Emergency Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 5. COLD AIR knob (if installed) push After the engine stops: 6. Gliding speed 55 KIAS (63 mph IAS) 7. Ignition 8. Master switch 9. Land 10. Airplane leave 11. Manual extinguisher (if available) 3.5.3 Fire in flight 1.

  • Page 41: Fire In The Cockpit (If Manual Extinguisher Available Aboard)

    Section 3 Emergency Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 10. Emergency landing carry out according to paragraph 3.8.1 11. Airplane leave 12. Manual extinguisher (if available) use as needed Fire in the cockpit (if manual extinguisher available aboard) 1. Fire source identify 2.

  • Page 42: Emergency Landing

    Section 3 Emergency Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Emergency landing 3.8.1 Emergency landing - with non-operating engine 1. Airspeed 59 KIAS (68 mph IAS) 2. Landing area choose, determine wind direction 3. Safety harness tighten up 4. Flaps landing position (50°) 5.

  • Page 43: Landing With Burst Tire

    Section 3 Emergency Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 3.8.3 Landing with burst tire CAUTION WHEN LANDING AT HOLDING, KEEP THE WHEEL WITH BURST TIRE ABOVE THE GROUND AS LONG AS POSSIBLE BY MEANS OF AILERONS. IN CASE OF NOSE WHEEL BY MEANS OF ELEVATOR.

  • Page 44: Other Emergency Procedures

    Section 3 Emergency Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS CAUTION ALTITUDE LOSS TURN RECOVERING FROM THE SPIN IS 500 UP TO 1000 FT. 3.10 Other emergency procedures 3.10.1 Vibration If abnormal vibrations occur on the airplane then: 1. Set engine RPM to the mode in which the vibrations are the lowest 2.

  • Page 45: Canopy Opening In Flight

    Section 3 Emergency Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 3.11 Canopy opening in flight WARNING ALWAYS MAKE SURE BEFORE A TAKEOFF, THAT COCKPIT CANOPY IS FULLY CLOSED - THE RED WARNING LIGHT ON THE DASHBOARD MUST GO OFF OR, IF THE AIRPLANE IS EQUIPPED WITH DIGITAL INTEGRATED INSTRUMENTS LIKE DYNON EFIS, TL INTEGRA, FLYMAP ETC., THE APPROPRIATE LIGHT ON THE DISPLAY MUST INDICATE CLOSED CANOPY!!
  • Page 46 Section 3 Emergency Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Intentionally left blank 3-12 June 01, 2011...
  • Page 47 Section 4 Normal Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS SECTION 4 4. NORMAL PROCEDURES Introduction ..............4-3 Recommended speeds for normal procedures....4-3 4.2.1 Take-off ................4-3 4.2.2 Landing................4-3 Assembly and disassembly ..........4-3 Pre-flight check ..............4-4 Normal procedures and checklist .........4-8 4.5.1 Before engine starting ............

  • Page 48: Doc. No. Harmaoius Section

    Section 4 Normal Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Intentionally left blank June 01, 2011...

  • Page 49: Normal Procedures

    4.2.2 Landing Approaching speed for normal landing (flaps in landing position - 50°) 60 KIAS (69 mph IAS) Assembly and disassembly Description of assembly and disassembly is given in the HARMONY LSA Aircraft Maintenance and Inspection Procedures. June 01, 2011...

  • Page 50: Pre-Flight Check

    Section 4 Normal Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Pre-flight check Carry out pre-flight check according to the following procedure: Figure 4-1 Scheme of airplane preflight check WARNING CHECK BEFORE PRE-FLIGHT CHECK THAT IGNITION IS SWITCHED OFF! NOTE The word “condition”, used in procedures of pre- flight check, means visual check of surface, damage, deformation,...
  • Page 51 Section 4 Normal Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 1. Left landing gear leg - check  landing gear leg attachment and condition  landing gear wheel condition  tire condition and inflation  condition and attachment of wheel covers ...
  • Page 52 Section 4 Normal Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 7. Tail units - check  tail skid condition  surface condition  condition of rudder and elevator attachment  freedom of rudder and elevator movement  condition of trim tab, condition of elevator trim tab control 8.
  • Page 53 Section 4 Normal Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS  check on cooling liquid volume in the expansion tank on the engine body (replenish as required up to max. 2/3 of the expansion tank volume) Checks before every flight: ...

  • Page 54: Normal Procedures And Checklist

    Section 4 Normal Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Normal procedures and checklist 4.5.1 Before engine starting 1. Pre-flight check and check on weight and centre of gravity position done 2. External power source connect as (if socket is installed) necessary 3.
  • Page 55 Section 4 Normal Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 8. BEACON (if installed) (if necessary) 9. Brakes apply 10. Ignition START (see CAUTION) after starting up BOTH CAUTION ACTIVATE STARTER FOR 10 SEC. AS A MAXIMUM, AND THEN LET IT COOL DOWN FOR 2 MINUTES. AFTER STARTING UP ENGINE, DO NOT CARRY OUT SUDDEN RPM CHANGES, AFTER POWER DECREASE WAIT FOR ABOUT 3 S IN ORDER TO REACH CONSTANT...

  • Page 56: Before Taxiing

    Section 4 Normal Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS NOTE Start engine with the fuel selector set to LEFT. If you would start the engine with the fuel selector set to RIGHT and the left tank is full, than fuel bleed from the left tank vent may occur (and pollute environment) because a fuel return hose is led only into the left tank and returning fuel will...

  • Page 57: Before Take-Off

    Section 4 Normal Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 4.5.5 Before take-off 1. Brakes brake 2. Ignition check carry out, see NOTE NOTE Carry out ignition check in the following way: Set engine speed to 4000 RPM. Switch ignition gradually to L, BOTH, R position and return to BOTH.

  • Page 58: Take-Off

    Section 4 Normal Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 16. Master switch check ON 17. Safety harnesses tighten up 18. Canopy closed 19. Transponder (if installed) ON or ALT 4.5.6 Take-off 1. THROTTLE lever max. take-off power 2. During take-off run smoothly lighten up the nose landing gear until airplane take-off occurs.

  • Page 59: Cruise

    Section 4 Normal Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 4.5.8 Cruise 1. THROTTLE lever as necessary 2. Airspeed max. 5500 RPM 3. Engine instruments check 4. Fuel quantity check CAUTION FUEL GAUGES DISPLAY TRUE FUEL QUANTITY ONLY ON GROUND AND IN A LEVEL FLIGHT.

  • Page 60: Descent

    Section 4 Normal Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 4.5.9 Descent 1. THROTTLE lever as necessary 2. Airspeed as necessary 3. Trim as necessary 4. Engine instruments check 5. CARB.PREHEATER (if installed) as necessary CAUTION AT LONG APPROACHING AND DESCENDING FROM HIGH ALTITUDE IT IS NOT SUITABLE TO REDUCE THROTTLE TO MINIMUM FOR REASON...

  • Page 61: Final

    Section 4 Normal Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 8. Approaching speed 60 KIAS (69 mph IAS) 9. Flaps Take-off pos. (15°) 10. Trim as necessary 11. Parking brake (if installed) check for lever down CAUTION PARKING BRAKE MUST RELEASED (LEVER DOWN) TO PREVENT LANDING WITH BRAKED WHEELS.

  • Page 62: After Landing

    Section 4 Normal Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 4.5.14 After landing 1. Flaps retracted pos. (0°) 2. Trim NEUTRAL 3. Outside lights (if installed) 4. Transponder (if installed) 5. Electric fuel pump (if installed) 4.5.15 Engine shut-off 1. THROTTLE lever idle 2.

  • Page 63: Airplane Parking

    Section 4 Normal Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 4.5.16 Airplane parking 1. Ignition check OFF 2. Master switch check OFF 3. FUEL SELECTOR Pull the safety button on the fuel selector, turn the handle to the OFF position and then release safety button. Now the handle is blocked in the OFF position.
  • Page 64 Section 4 Normal Procedures AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Intentionally left blank 4-18 June 01, 2011...

  • Page 65: Performance

    Section 5 Performance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS SECTION 5 5. PERFORMANCE Introduction ..............5-3 Performance data............5-4 5.2.1 Airspeed indicator system calibration......... 5-4 5.2.2 Stall speeds ..............5-5 5.2.3 Take-off distance .............. 5-6 5.2.4 Landing distance............... 5-7 5.2.5 Climb performance............5-8 Additional information ..........5-10 5.3.1 Cruise ................
  • Page 66 Section 5 Performance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Intentionally left blank June 01, 2011...

  • Page 67: Introduction

    Section 5 Performance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Introduction Section 5 provides data for airspeed calibration, stall speeds, take- off performance and additional information, provided by the airplane manufacturer. The stated performance data has been computed from actual flight tests with the airplane and engine in good condition and using average piloting techniques.

  • Page 68: Performance Data

    Section 5 Performance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Performance data 5.2.1 Airspeed indicator system calibration NOTE Assumed zero instrumentation error. Valid for airplane take-off weight 1320 lbs (600 kg) and with vortex generators along the whole span of the wing. MTOW 1320 lb Flaps Flaps...

  • Page 69: Stall Speeds

    Section 5 Performance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 5.2.2 Stall speeds Conditions: wing level stall - engine at idle power turning flight stall - engine at 75% max. continuous power airplane weight: 1320 lbs (600 kg) Vortex generators along the whole span of the wing NOTE The stated stall speeds are valid for all flight altitudes.

  • Page 70: Take-Off Distance

    Section 5 Performance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 5.2.3 Take-off distance Conditions: - engine: max. take-off power - flaps: Take-off (15°) - carburetor preheating: - airplane weight: 1320 lbs - altitude: 0 ft ISA - ambient air temperature: ISA Conditions CONCRETE GRASS Airport...

  • Page 71: Landing Distance

    Section 5 Performance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 5.2.4 Landing distance Conditions: - engine: idle - flaps: Landing II (fully extended) - carburetor preheating: - airplane weight: 1320 lbs - altitude: 0 ft ISA - ambient air temperature: ISA ISA Conditions CONCRETE GRASS...
  • Page 72 (0°) carburetor preheating: airplane weight: 1320 lbs vortex generators along the whole span of the wing ambient air temperature: Harmony LSA RATE OF CLIMB Rotax 912 ULS, Warpdrive prop 950 fpm 900 fpm 850 fpm 800 fpm 0 ft ISA...
  • Page 73 Section 5 Performance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Harmony LSA RATE OF CLIMB Rotax 912 ULS, Warpdrive prop 950 fpm 900 fpm 850 fpm 800 fpm 0 ft ISA 750 fpm 700 fpm 2000 ft ISA 650 fpm 600 fpm...

  • Page 74: Additional Information

    1320 lbs (600 kg) vortex generators along the whole span of the wing ambient air temperature: Harmony LSA Horizontal speeds Rotax 912 ULS, Warpdriv e 3bl.,w/HPL hub, tapered tips, 68in, nickel LE 120 KCAS 115 KCAS...

  • Page 75: Horizontal Speeds

    Section 5 Performance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Harmony LSA Horizontal speeds Rotax 912 ULS, Warpdriv e 3bl.,w/HPL hub, tapered tips, 68in, nickel LE 140 mph 135 mph 130 mph 125 mph 120 mph 115 mph 110 mph 105 mph...
  • Page 76 Section 5 Performance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 55%MCP 65%MCP 78%MCP MT/OP Max.Continuous Max.Takeoff Pow er Power 4300 rpm 4800 rpm 5000 rpm 5500 rpm 5800 rpm (5 min) IAS km/h] 0 ft ISA CAS km/h] TAS km/h] IAS km/h] 2000 ft ISA CAS km/h] TAS km/h]...

  • Page 77: Endurance

    Section 5 Performance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 5.3.3 Endurance Conditions: Altitude 2000 ft ISA flaps: retracted (0°) carburetor preheating: airplane takeoff weight: 1320 lbs (600 kg) airplane empty weight: 802 lbs (364 kg) vortex generators along the whole span of the wing LOAD LIMITS Ma x.ta ke-off w eight 600 kg...

  • Page 78: Balked Landing Climb

    Take-off, Landing II airplane weight: 1320 lbs (600 kg) vortex generators along the whole span of the wing ambient air temperature: Harmony LSA BALKED LANDING ROC with the flaps extended to the T akeoff position 900 ft/m in 800 ft/m in...
  • Page 79 Section 5 Performance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Harmony LSA BALKED LANDING ROC with the flaps extended to the Takeoff position 900 ft/m in 800 ft/m in 0 ft ISA 700 ft/m in 600 ft/m in 2000 ft ISA...
  • Page 80 Section 5 Performance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Harmony LSA BALKED LANDING ROC with the flaps extended to the T akeoff position 900 ft/m in 0 ft ISA 800 ft/m in 700 ft/m in 2000 ft ISA 600 ft/m in...

  • Page 81: Effect On Flight Performance And Characteristics

    Section 5 Performance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 5.3.5 Effect on flight performance and characteristics Flight performances and characteristics are not considerably affected by rain or insect stuck on the airplane surface. 5.3.6 Demonstrated crosswind performance Maximum demonstrated speed of wind at airplane operation 24 kts (28 mph) Maximum demonstrated speed of cross wind for take-off and...

  • Page 82: Ceiling

    Section 5 Performance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 5.3.7 Ceiling ROC fpm Ceiling ft Ceiling m Service ceiling 16980 5180 Absolute ceiling 19150 5840 5.3.8 Noise data Not measured. 5-18 June 01, 2011...
  • Page 83 Section 6 Weight and Balance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS SECTION 6 6. WEIGHT AND BALANCE Introduction ..............6-3 Weight and Balance Record..........6-4 Permitted Payload Range ..........6-5 Operational Weight and Balance Computation....6-6 6.4.1 Computational Procedure..........6-6 Airplane Loading Schedule Chart.........6-8 Table of Static Moments ..........6-10 Airplane Loading Graph ..........6-11 CG Moment Envelope ..........6-12...
  • Page 84 Section 6 Weight and Balance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Intentionally left blank June 01, 2011...

  • Page 85: Weight And Balance

    Section 6 Weight and Balance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Introduction This Section includes Weight and Balance Record of empty airplane, Permitted Payload Range within which the airplane may be safely operated, and a method to determine whether the operational weight and CG location will be within the permitted limits range.

  • Page 86: Weight And Balance Record

    Section 6 Weight and Balance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Weight and Balance Record June 01, 2011...

  • Page 87: Permitted Payload Range

    Section 6 Weight and Balance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Permitted Payload Range BAGGAGE [lb] June 01, 2011...

  • Page 88: Operational Weight And Balance Computation

    Section 6 Weight and Balance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Operational Weight and Balance Computation An important part of preflight planning is to determine that the aircraft is loaded so its weight and CG location are within the allowable limits. This is possible by using hereafter explained Loading graph method, using weights, arms, and moment indexes.
  • Page 89 Section 6 Weight and Balance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS useful load items (crew, fuel, baggage) so that after a repeated computation the intersection of Take-off Weight and Total Static Moment will be inside the CG Moment envelope. WARNING SAFETY OF FLIGHT PERFORMED WITH THE AIRPLANE LOADED OUTSIDE PERMITTED LIMITS OF WEIGHT AND STATIC MOMENTS...

  • Page 90: Airplane Loading Schedule Chart

    Section 6 Weight and Balance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Airplane Loading Schedule Chart Type/Model: Harmony LSA Seria l No.: Registration: Input data LOADING SCHEDULE CHART Your Aircraft Sa mple Aircraft Weight Moment W eight Moment (kg) (kg.m) (kg) (kg.m)
  • Page 91 Section 6 Weight and Balance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Type/Mode l: Ha rmony LSA Seria l No.: Input data Registration: LOADING SCHEDULE CHART Your Aircraft Sample Aircra ft W eight Moment Weight Moment (kg) (kg.m) (kg) (kg.m) (3) = (1) x (2) (3) = (1) x (2) Item Empty Airpla ne...

  • Page 92: Table Of Static Moments

    Section 6 Weight and Balance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Table of Static Moments CREW BAGGAGE FUEL W eight Moment Weight Moment Quantity W eight Moment (kg) (kg.m) (kg) (kg.m) (liters) (kg) (kg.m) 24,4 10,0 29,3 10,3 20,0 14,4 34,2 15,4 30,0...

  • Page 93: Airplane Loading Graph

    Section 6 Weight and Balance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Airplane Loading Graph Harmony LSA Loading Graph Crew Fue l Baggage Load Moment (kg.m) Harmony LSA Loading Graph Crew Fuel Baggage Load Moment / 100 (lb-in) 6-11 June 01, 2011...

  • Page 94: Cg Moment Envelope

    Section 6 Weight and Balance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS CG Moment Envelope Harmony LSA CG Moment Envelope 20111413 Loaded Airplane M oment (kg.m) Harmony LSA CG Moment Envelope 1400 1380 1360 1340 Sample 1320 1300 1280 1260 1240...

  • Page 95: Operational Weight And Cg Envelope

    Section 6 Weight and Balance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Operational Weight and CG Envelope Harmony LSA Operational Weight and CG Envelope 20111413 Loaded Airplane CG position (% M AC) Harmony LSA Operational Weight and CG Envelope 1400 1380...

  • Page 96: Equipment List

    Section 6 Weight and Balance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 6.10 Equipment List The equipment installed in the airplane of particular serial number is shown in the following Equipment list. Airplane Serial Registration Date: No.: Description Type Part No. Manufacturer Installed 6-14...
  • Page 97 Section 6 Weight and Balance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Airplane Serial Registration Date: No.: Description Type Part No. Manufacturer Installed 6-15 June 01, 2011...
  • Page 98 Section 6 Weight and Balance AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Intentionally left blank 6-16 June 01, 2011...

  • Page 99: Airplane And System Description

    Section 7 Airplane and System Description AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS SECTION 7 7. AIRPLANE AND SYSTEM DESCRIPTION Introduction ..............7-3 Airframe ................7-3 7.2.1 Fuselage................7-3 7.2.2 Wing ................. 7-3 7.2.3 Horizontal tail unit (HTU) ........... 7-3 7.2.4 Vertical tail unit (VTU) ............7-4 Control ................7-4 7.3.1 Longitudinal control ............
  • Page 100 Section 7 Airplane and System Description AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 7.12 Fuel system ..............7-13 7.12.1 Fuel tanks............... 7-13 7.12.2 Fuel selector ..............7-13 7.12.3 Fuel filter................. 7-14 7.12.4 Indication of fuel quantity ..........7-14 7.12.5 Fuel tank draining ............7-14 7.13 Electrical system............7-16 7.13.1 Lighting................

  • Page 101: Introduction

    More detailed information on optional systems and equipment are available in section 9, Supplements. Airframe The airframe of HARMONY LSA airplane is a combination of semimonocoque structure consisting of metal reinforcement, frames and duralumin sheet skin, with a composite back side of fuselage and composite canopy.

  • Page 102: Control

    Section 7 Airplane and System Description AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 7.2.4 Vertical tail unit (VTU) VTU is of trapezoidal shape. Its fin is an integral part of the fuselage. The rudder is suspended on the fin by means of two hinges.

  • Page 103: Aileron Trim Tab Control

    Section 7 Airplane and System Description AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 7.3.4 Elevator trim tab control The elevator trim tab is controlled by the lever located in between the pilot seats. The control lever is interconnected with the trim tab by means of bowdwen-cables.

  • Page 104: Controls In Cockpit

    Section 7 Airplane and System Description AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Controls in cockpit Figure 7–1 Cockpit control elements Control stick Rudder pedals Flap control lever 4a Electric trim (option) 4b Elevator trim control lever Fuel tank selector Static pressure selector (option) Switches Master switch (depending on equipment)

  • Page 105: Instrument Panel

    Wheels can be fitted with fiber-glass aerodynamic pants. 7.7.2 Brakes The HARMONY LSA airplane is equipped with disk hydraulic brakes on main landing gear wheels. Brake system is composed of toe-brake pedals (these are a part of rudder control pedals), brake...

  • Page 106: Baggage Compartment

    Section 7 Airplane and System Description AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Each of seats is fitted with four-point safety harness which is composed of safety belts, shoulder straps and lock. The safety harness is anchored in the fuselage sides behind the seats and on the seat sides.

  • Page 107: Power Unit

    7.11 Power unit 7.11.1 General The engine ROTAX 912 ULS (100 hp) is standard used to power HARMONY LSA airplane. IFR version is fitted with certified ROTAX 912S. ROTAX 912 is a four-cylinder, four-stroke engine with opposite cylinders, central cam shaft and OHV valve mechanism.

  • Page 108: Engine Intruments

    Section 7 Airplane and System Description AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 7.11.3 Engine instruments The following analog instruments located on the instrument panel serve for engine performance monitoring. The digital engine monitoring system can be installed in the airplane instead of analog engine instruments.

  • Page 109: Engine Cooling System

    Section 7 Airplane and System Description AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 7.11.4 Engine cooling system Engine cooling is combined, cylinder heads are cooled by water, and cylinders are cooled by air. Cooling circuit of cylinder heads is designed as a closed system containing pump, expansion reservoir (1) with pressure closure (3), cooler of cooling liquid (2) and drainage reservoir (4).

  • Page 110: Engine Lubrication System

    Section 7 Airplane and System Description AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 7.11.5 Engine lubrication system Engine lubrication system is performed with the dry crank case. Engine lubrication system is equipped with oil pump (1) ensuring oil feeding from reservoir (4) located on the fire wall through the oil cooler (5) and the oil cleaner (6) to the lubricated points of engine.

  • Page 111: Ignition System

    Fuel system serves for keeping fuel in the airplane and its feeding to the engine. Fuel system of HARMONY LSA airplane is composed of integral fuel tanks, fuel line, fuel selector, fuel filter, mechanical fuel pump - located on the engine (auxiliary electrical fuel pump can be installed), distribution pipe of fuel with, return branch of fuel, fuel gauges and fuel tanks draining valves.

  • Page 112: Fuel Filter

    Section 7 Airplane and System Description AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS can be freely moved between LEFT and RIGHT position. Safety button prevents unintentionally switch the selector to OFF position. To move selector to OFF (closed) position it is necessary pull the safety button on the fuel selector, turn the handle to the OFF position and then release safety button.
  • Page 113 Section 7 Airplane and System Description AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Figure 7–4 Scheme of fuel system 7-15 June 01, 2011...

  • Page 114: Lighting

    Section 7 Airplane and System Description AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 7.13 Electrical system The airplane is equipped with 14 DC electrical installation. A generator with power of 250 W is the primary source of electrical energy. The secondary source of energy is the accumulator 12V/16Ah that is located in the engine compartment on the firewall.
  • Page 115 Section 7 Airplane and System Description AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS switch and anticollision beacon by BEACON switch. Landing headlight is switched by LDG LIGHT switch. Night VFR and IFR versions are equipped with the landing light, position lights & anticollision beacons. There is also a cockpit light installed for these versions.

  • Page 116: Pitot-Static System

    Section 7 Airplane and System Description AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 7.14 Pitot-static system Pitot-static tube for sensing static and total pressure is located under the left half of the wing. Total pressure is sensed through the opening in the Pitot-static tube face. Static pressure is sensed through openings on the tube circumference.

  • Page 117: Supplementary Equipment

    Section 7 Airplane and System Description AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS 7.15 Supplementary equipment 7.15.1 Ventilation and heating system Cockpit ventilation is ensured by 2 eye–ball vents located on the left and right of the tip-up canopy frame. Vents are connected to the NACA scoops through tip-up canopy frame front flaps.
  • Page 118 Section 7 Airplane and System Description AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Intentionally left blank 7-20 June 01, 2011...

  • Page 119: Airplane Handling, Servicing And Maintenance

    Section 8 Airplane Handling, Servicing and AIRCRAFT OPERATING INSTRUCTIONS Maintenance Doc. No. HARMAOIUS SECTION 8 8. AIRPLANE HANDLING SERVICING AND MAINTENACE Introduction ..............8-3 Airplane inspection period ..........8-5 Modifications or airplane repairs ........8-5 Road transport ...............8-6 8.4.1 Airplane towing ..............8-6 8.4.2 Airplane parking..............
  • Page 120 Section 8 Airplane Handling, Servicing and AIRCRAFT OPERATING INSTRUCTIONS Maintenance Doc. No. HARMAOIUS Intentionally left blank June 01, 2011...

  • Page 121: Introduction

    The airplane serial number is shown on the title sheet of these Instructions and on the Manufacturer’s plate below stabilizer on the left side of the fuselage. The manufacturer delivers along with aircraft HARMONY LSA the “Aircraft Operating Instructions (AOI)“...

  • Page 122: Supplements

    Section 8 Airplane Handling, Servicing and AIRCRAFT OPERATING INSTRUCTIONS Maintenance Doc. No. HARMAOIUS Owner/Operator Responsibilities: Each owner/operator of an LSA airplane shall read and comply with the maintenance and continued airworthiness information and instructions provided by the manufacturer. Each owner/operator of an LSA airplane shall be responsible for providing the manufacturer with current contact information where the manufacturer may send the owner/operator supplemental notification bulletins.

  • Page 123: Airplane Inspection Period

    100 ± 5 hours of operation or at least annual inspection annual inspection Details on periodical inspections are provided in the Aircraft Maintenance and Inspection Procedures of HARMONY LSA. Refer to the Rotax 912 Operator’s Manual for engine maintenance. Refer to the Propeller Maintenance Manual for propeller maintenance.

  • Page 124: Road Transport

    Section 8 Airplane Handling, Servicing and AIRCRAFT OPERATING INSTRUCTIONS Maintenance Doc. No. HARMAOIUS Road transport 8.4.1 Airplane towing It is possible to move the airplane on a short distance by holding the fuselage end in the position before the fin, eventually by holding the root part of wings.

  • Page 125: Airplane Anchoring

    Section 8 Airplane Handling, Servicing and AIRCRAFT OPERATING INSTRUCTIONS Maintenance Doc. No. HARMAOIUS 8.4.3 Airplane anchoring The airplane is anchored at parking out of hangar after termination of flight day or according to need. Anchoring of the airplane is necessary for its protection against possible damage, caused by wings and gusts.

  • Page 126: Leveling

    8.4.5 Leveling Leveling procedure is described in the Aircraft Maintenance and Inspection Procedures for HARMONY LSA airplane. 8.4.6 Road transport The airplane can be transported on communication after its loading on an appropriate trail. It is necessary to dismount wings. The airplane must be secured against possible movement.

  • Page 127: Cleaning And Care

    Section 8 Airplane Handling, Servicing and AIRCRAFT OPERATING INSTRUCTIONS Maintenance Doc. No. HARMAOIUS Cleaning and care Always use appropriate cleaning agents when cleaning airplane surface. Residuum of oil and fat can be removed form the airplane surface (excluding the canopy) by suitable detergents, possibly by petrol.
  • Page 128 Section 8 Airplane Handling, Servicing and AIRCRAFT OPERATING INSTRUCTIONS Maintenance Doc. No. HARMAOIUS Intentionally left blank 8-10 June 01, 2011...
  • Page 129 Section 9 Supplements AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS SECTION 9 9. SUPPLEMENTS Introduction ..............9-2 List of inserted supplements.........9-2 Supplements inserted............9-4 June 01, 2011...
  • Page 130 Section 9 Supplements AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Introduction This section contains the appropriate supplements necessary to safely and efficiently operate the airplane when equipped with various optional systems and equipment not provided with the standard airplane. List of inserted supplements Inst.
  • Page 131 Section 9 Supplements AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Inst. Date Doc. No. Title of inserted supplement June 01, 2011...
  • Page 132 Section 9 Supplements AIRCRAFT OPERATING INSTRUCTIONS Doc. No. HARMAOIUS Supplements inserted June 01, 2011...

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