Orlican M-8 EAGLE 2022 Pilots Operating Manual
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Orlican M-8 EAGLE 2022 Pilots Operating Manual

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ORLIČAN M-8 EAGLE
REVISION NO. 05
PILOT'S OPERATING
DATE OF ISSUE: MAY 02,
an
Airplane Registration
Airplane
Serial Number
Number
N602TG
2022001
THIS MANUAL MUST BE ON THE AIRPLANE BOARD DURING OPERATION.
THIS AIRPLANE MUST BE OPERATED IN COMPLIANCE WITH THE INFORMATION
AND LIMITATIONS STATED IN THIS MANUAL.
ORLIČAN S.R.O.
PAGE
1
OF
2

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Summary of Contents for Orlican M-8 EAGLE 2022

  • Page 1 ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, Airplane Registration Airplane Serial Number Number N602TG 2022001 THIS MANUAL MUST BE ON THE AIRPLANE BOARD DURING OPERATION. THIS AIRPLANE MUST BE OPERATED IN COMPLIANCE WITH THE INFORMATION AND LIMITATIONS STATED IN THIS MANUAL.
  • Page 2 YOUR AIRPLANE SUPPLIER ORLIČAN M-8 EAGLE REVISION NO. 05 bervid@orlican.or PILOT'S OPERATING DATE OF ISSUE: MAY 02, www.orlican.or ORLIČAN Londýnská 120 00 Praha 2 – Czech Production ORLIČAN S.R.O. PAGE...
  • Page 3 ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, TABLE OF CONTENTS TABLE OF CONTENTS PAGE...

  • Page 4: Table Of Contents

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, TABLE OF CONTENTS LIST OF REVISIONS TERMINOLOGY 3.1. GENERAL AIRSPEED TERMINOLOGY AND SYMBOLS 3.2. METEOROLOGICAL TERMINOLOGY 3.3. ENGINE POWER TERMINOLOGY 3.4. AIRPLANE PERFORMANCE AND FLIGHT PLANNING TERMINOLOGY 3.5.
  • Page 5 ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 6.11. APPROVED MANEUVERS 6.12. MANEUVERING LOAD FACTORS 6.13. FLIGHT ENVELOPE 6.14. FLIGHT CREW 6.15. FUEL 6.16. OIL SPECIFICATION 6.17. COOLANT SPECIFICATION 6.18. KINDS OF OPERATION 6.19. FLIGHT SAFETY RESTRICTIONS 6.20.
  • Page 6 ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 7.14. OTHER EMERGENCY PROCEDURES 7.14.1. EXCEEDING MAXIMUM AIRSPEED 7.14.2. VIBRATIONS 7.14.3. CARBURETOR ICING NORMAL PROCEDURES 8.1. INTRODUCTION 8.2. PRE-FLIGHT INSPECTION 8.2.1. CABIN 8.2.2. FUSELAGE, WINGS AND TAIL SURFACES 8.2.3.
  • Page 7 ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 9.8. ENDURANCE AND RANGE 9.9. DEMONSTRATED CROSSWIND PERFORMANCE 9.10. OPTIMUM GLIDING SPEED 9.11. CEILING WEIGHT AND BALANCE 10.1. INTRODUCTION 10.2. AIRPLANE WEIGHING PROCEDURE AND DETERMINING THE LOCATION OF CG 10.2.1.
  • Page 8 ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 12.5. ASSEMBLY AND DISASSEMBLY OF THE AIRCRAFT 12.5.1. WING ASSEMBLY 12.5.2. HORIZONTAL STABILIZER (ELEVATOR) ASSEMBLY 12.5.3. WING DISASSEMBLY 12.5.4. HORIZONTAL STABILIZER (ELEVATOR) DISASSEMBLY 12.6. ROAD TRANSPORT 12.7. ENGINE COWLINGS 12.7.1.
  • Page 9 ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 13.1. INSTRUCTIONS: 13.2. CONTINUED OPERATIONAL SAFETY FEEDBACK FORM FLIGHT TRAINING SUPPLEMENT 14.1. INTRODUCTION 14.2. PILOT TRAINING 14.3. TRAINING SCHEDULE 14.4. PRACTICAL TRAINING FOR PILOT QUALIFICATION 14.4.1. LESSON 1: INTRODUCTORY FLIGHT 14.4.2.

  • Page 10: List Of Revisions

    Any changes to applicable regulations or to this aircraft's construction will be published in the form of a bulletin on http://orlican.com/bulletin/. It is the responsibility of each aircraft operator to keep all pages of this manual to the latest revision status, by exchanging the relevant pages when a new revision has been published.

  • Page 11: Terminology

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 3. TERMINOLOGY 3.1. GENERAL AIRSPEED TERMINOLOGY AND SYMBOLS Calibrated Airspeed is indicated airspeed corrected for position and instrument error. Calibrated airspeed is equal to true airspeed (TAS) in standard atmosphere at sea level. KCAS Calibrated Airspeed expressed in “knots”.

  • Page 12: Engine Power Terminology

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 3.3. ENGINE POWER TERMINOLOGY Maximum Continuous Power is the maximum power for abnormal or emergency operations. Brake Horsepower is the power developed by the engine. Revolutions Per Minute is engine speed. Static RPM Static RPM is engine speed attained during a full throttle engine run up when the airplane is on the ground and stationary.

  • Page 13: Electrical And Avionics Terminology

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 3.6. ELECTRICAL AND AVIONICS TERMINOLOGY Avionics Auxiliary Alternator BATT Battery Communication Crew Alerting System Emergency Locator Transmitter Engine monitoring system EFIS Electronic Flight Information System Global Positioning System Horizontal Situation Indicator Multi-Functional Display Navigation...

  • Page 14: Referenced Documents

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 4. REFERENCED DOCUMENTS The following documents are regarded as supporting documents to this Pilot Operating Handbook: 4.1. ASTM STANDARDS: • F 2245 - Specification for Design and Performance of a Light Sport Airplane •...

  • Page 15: General Information

    ATTENTION! THIS AIRCRAFT WAS MANUFACTURED IN ACCORDANCE WITH LIGHT SPORT AIRCRAFT ORLIČAN M-8 EAGLE REVISION NO. 05 AIRWORTHINESS STANDARDS AND DOES NOT CONFORM TO STANDARD CATEGORY PILOT'S OPERATING DATE OF ISSUE: MAY 02, AIRWORTHINESS REQUIREMENTS AND IT IS OPERATED ENTIRELY ON THE USER’S OWN RISK.

  • Page 16: Attentions, Cautions, Warnings

    WARNING! THIS TEXT BOX REPRESENTS A HAZARDOUS SITUATION. WARNINGS ARE USED ORLIČAN M-8 EAGLE REVISION NO. 05 TO CALL ATTENTION TO OPERATING PROCEDURES OR CONDITIONS WHICH, IF PILOT'S OPERATING DATE OF ISSUE: MAY 02, NOT STRICTLY OBSERVED, MAY RESULT IN PERSONAL INJURY OR DEATH. 5.3.

  • Page 17: Aircraft Description

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 5.4. AIRCRAFT DESCRIPTION CHARACTERISTICS The M-8 EAGLE aircraft is a two-seat, strut high-wing monoplane of all-composite structure designed for sport or recreational flying. Favorable flight characteristics make the aircraft suitable for flight training. The aircraft features spacious crew and baggage compartments.
  • Page 18 ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02,...

  • Page 19: Aircraft Dimensions

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, AIRCRAFT DIMENSIONS WING SPAN: 29,922 ft. 9,12 m LENGTH: 22,671 ft. 6,91 m HEIGHT, TOTAL: 8,924 ft. 2,72 m WING SURFACE: 116,09 sq 10,785 m2 WING ASPECT RATIO: 7,678 DEPTH OF MAC (MEAN AERODYNAMIC 47,36 in...
  • Page 20 ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, GENERAL INFORMATION PAGE 17 OF 99...

  • Page 21: Three-View Drawing

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, THREE-VIEW DRAWING...
  • Page 22 ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, GENERAL INFORMATION PAGE 18 OF 99...

  • Page 23: Aircraft Configuration

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 5.5. AIRCRAFT CONFIGURATION AIRCRAFT MANUFACTURER: ORLIČAN S.R.O. AIRCRAFT MODEL: M-8 EAGLE AIRCRAFT SERIAL NUMBER: 2022001 AIRCRAFT PLACE & YEAR OF ÚSTÍ NAD ORLICÍ - 2021 MANUFACTURE: ENGINE MANUFACTURER ROTAX ENGINE MODEL: 912 ULS 2...

  • Page 24: Powerplant

    WARNING! NEITHER OF THE ENGINES MENTIONED ABOVE IS CERTIFIED AS AN AIRCRAFT ORLIČAN M-8 EAGLE REVISION NO. 05 ENGINE. EVEN WITH UTMOST ATTENTION DURING ENGINE MANUFACTURE, PILOT'S OPERATING DATE OF ISSUE: MAY 02, ENGINE FAILURE MAY OCCUR AT ANY TIME DURING FLIGHT AND THE PILOT BEARS FULL RESPONSIBILITY FOR THE CONSEQUENCES.

  • Page 25: Propeller

    WARNING! THE PROPELLER SHALL BE SENT TO THE MANUFACTURER FOR INSPECTION IN ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, CASE OF EVEN THE SLIGHTEST DAMAGE OR IF CRACK IS FOUND. FLYING WITH DAMAGED PROPELLER MAY ENDANGER LIFE AND LIMB AND IS PROHIBITED. PROPELLER Three-blade ground-adjustable propeller is used on the aircraft.

  • Page 26: Aircraft Equipment

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 5.6. AIRCRAFT EQUIPMENT INSTRUMENTS TYPE MODEL MANUFACTURE SERIAL NO. Glass cockpit SV-HDX1100 10" SkyView HDX Dynon 14908 Glass cockpit SV-BAT-320 Dynon 53566 Glass cockpit SV-ADAHRS-200 Dynon 12141 SV-GPS-2020 Dynon 11379...
  • Page 27 YOU MUST FIRST REGISTER YOUR BEACON FOLLOWING THE REGISTRATION ORLIČAN M-8 EAGLE PROCEDURE OF THE COUNTRY WHERE THE AIRCRAFT IS BASED. YOU CAN ONLY REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, REGISTER THE ELT IN THE COUNTRY THE AIRCRAFT IS REGISTERED. 1.1.

  • Page 28: Equipment Layout

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, EQUIPMENT LAYOUT GENERAL INFORMATION PAGE 24 OF 99...

  • Page 29: Limitations

    CAUTION! LSA MAXIMUM SPEED FOR ALL OPERATIONS IS 120 ORLIČAN M-8 EAGLE REVISION NO. 05 KNOTS CAS, WHICH REPRESENTS 133 KNOTS IAS PILOT'S OPERATING DATE OF ISSUE: MAY 02, FOR M-8 EAGLE. 6. LIMITATIONS 6.1. INTRODUCTION This section contains operation limitation, instrument marking and basic placards necessary for safe operation of airplane and its engine, standard systems and equipment.

  • Page 30: Airspeed Indicator Markings

    CAUTION! LSA MAXIMUM SPEED FOR ALL OPERATIONS IS 120 ORLIČAN M-8 EAGLE REVISION NO. 05 KNOTS CAS, WHICH REPRESENTS 133 KNOTS IAS PILOT'S OPERATING DATE OF ISSUE: MAY 02, FOR M-8 EAGLE. 6.3. AIRSPEED INDICATOR MARKINGS KIAS MARKING MEANI [KNOTS [MPH] [KM/H] The flap operating range since its lower...

  • Page 31: Analog Airspeed Indicator Markings

    CAUTION! ALL SPEEDS IN THIS MANUAL ARE DETERMINED BY PRIMARY AIRSPEED INDICATOR ORLIČAN M-8 EAGLE REVISION NO. 05 DISPLAYED ON EFIS (DYNON SKYVIEW). PILOT'S OPERATING DATE OF ISSUE: MAY 02, ANALOG AIRSPEED INDICATOR, USED AS EMERGENCY ONE, MAY INDICATE SLIGHTLY DIFFERENT SPEEDS.

  • Page 32: Powerplant Limitations

    WARNING! NONCOMPLIANCE CAN RESULT IN SERIOUS INJURIES OR DEATH! EXCEEDING ORLIČAN M-8 EAGLE REVISION NO. 05 THE ADMISSIBLE VALUES CAN CAUSE ENGINE FAILURE. PILOT'S OPERATING DATE OF ISSUE: MAY 02, 6.4. POWERPLANT LIMITATIONS ENGINE MANUFACTURER: BOMBARDIER-Rotax-GmbH (Austria) ENGINE TYPE: Rotax 912 ULS 2 MAX.

  • Page 33: Powerplant Instrument Markings

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 6.5. POWERPLANT INSTRUMENT MARKINGS RED LINE YELLOW GREEN YELLOW RED LINE LOWER UPPER INSTRUMENT WARNING LOWER NORMAL UPPER WARNING CAUTION OPER. CAUTION RANGE TACHOMETER 0 - 1400 1400 - 5500 5500 - 5800 5800...

  • Page 34: Weight Limits

    WARNING! PAY SPECIAL ATTENTION TO LUGGAGE AND FUEL WEIGHT, THESE APPLICABLE ORLIČAN M-8 EAGLE REVISION NO. 05 MASSES INFLUENCE PILOT'S OPERATING DATE OF ISSUE: MAY 02, THE CENTER OF GRAVITY. EXCEEDING BAGGAGE WEIGHT LIMITS CAN SHIFT 6.7. WEIGHT LIMITS WEIGHT POUNDS MAXIMUM TAKE-OFF WEIGHT 1 320...

  • Page 35: Centre Of Gravity

    TAILWIND TAKE-OFF AND LANDING SHOULD BE AVOIDED. ORLIČAN M-8 EAGLE REVISION NO. 05 REMEMBER: FAR 61.315, (B), (11) STATES THAT SPORT PILOT LICENSE PRIVELEGES DO PILOT'S OPERATING DATE OF ISSUE: MAY 02, 6.8. CENTRE OF GRAVITY % MAC XT [INCH] XT [MM] EMPTY AIRPLANE C.G.

  • Page 36: Approved Maneuvers

    ATTENTION! THE DATA FOR BANK ANGLES 45° AND 60° ARE ORLIČAN M-8 EAGLE REVISION NO. 05 CALCULATED VALUES, THEY HAVE NOT BEEN VERIFIED PILOT'S OPERATING DATE OF ISSUE: MAY 02, BY A TEST FLIGHT. 6.11. APPROVED MANEUVERS M-8 Eagle airplane is approved to perform the following maneuvers: •...

  • Page 37: Flight Envelope

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 6.13. FLIGHT ENVELOPE 6.14. FLIGHT CREW Minimum crew: 1 pilot Maximum crew: 1 pilot + 1 passenger Minimum weight of crew: unlimited Maximum weight of crew: 440 lb (200 kg) Maximum weight per seat: 242 lb (110 kg) LIMITATIONS...

  • Page 38: Fuel

    ATTENTION! ORLIČAN M-8 EAGLE USE ONLY FUEL SUITABLE FOR THE RESPECTIVE CLIMATIC ZONE. REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 6.15. FUEL Fuel specifications, the following fuels can be used: • min RON 95 • min. AKI 91 •...

  • Page 39: Oil Specification

    ATTENTION! OBEY THE LATEST EDITION OF ROTAX SERVICE INSTRUCTION SI-912-016, FOR THE ORLIČAN M-8 EAGLE REVISION NO. 05 SELECTION OF THE CORRECT COOLANT. PILOT'S OPERATING DATE OF ISSUE: MAY 02, CAUTION! ENGINE OIL SHOULD BE REPLACED EVERY 100 HOURS FLOWN! 6.16.

  • Page 40: Kinds Of Operation

    DAYLIGHT FLIGHTS UNDER VFR CONDITIONS ARE ALLOWED ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, WARNING! NIGHT FLIGHTS UNDER VFR CONDITIONS ARE ALLOWED ONLY WITH APPROVED POSITION AND ANTI- COLLISION LIGHTS PRIVATE PILOT CERTIFICATE IS REQUIRED! 6.18.

  • Page 41: Placards

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, PLACAR PLACAR PLACAR PLACARD 1 6.20. PLACARDS Placards affixed to the aircraft contain warnings, operating limitations, and reference information. The FAA-accepted ASTM consensus standard specifies placard lettering is to be clearly printed, large enough, and positioned so it is legible to the user.

  • Page 42: Placard Light Sport Aircraft

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, ORLIČAN s.r.o. 2022001 N602TG PLACARD LIGHT SPORT AIRCRAFT Location: left side of the middle panel. (PLACARD 1) Location: left part of instrument panel - at the bottom, on the left. (PLACARD 2) VFR - Visual Flight Rules VMC - Visual Meteorological Conditions IFR - Instrument Flight...
  • Page 43 ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, LIMITATIONS PAGE...

  • Page 44: Registration Placard

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, REGISTRATION PLACARD Location: left side of the middle panel. (PLACARD 5) AIRCRAFT IDENTIFICATION PLATE Location: either adjacent to and aft of the entrance door or on the fuselage surface near the tail surfaces. FUEL PLACARD Location: Near fuel filler cup, top wing surface.
  • Page 45 ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02,...

  • Page 46: Emergency Procedures

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 7. EMERGENCY PROCEDURES 7.1. INTRODUCTION This section describes recommended procedures for resolving emergency situations, which could occur during airplane operation, and should be committed to memory. Procedures provide instructions that must be executed in the given sequence, as far as possible without interruption.

  • Page 47: Engine Failure

    WARNING! DURING A LANDING IT IS VITAL FOR THE PILOT TO CONTINUE TO FLY THE ORLIČAN M-8 EAGLE REVISION NO. 05 AIRCRAFT. DAMAGE AND/OR INJURIES CAN BE MINIMIZED IF THE PILOT IS PILOT'S OPERATING DATE OF ISSUE: MAY 02, FULLY CONCENTRATING ON CONTROLLING THE AIRCRAFT UNTIL IT COMES TO COMPLETE STOP.

  • Page 48: During Take-Off Run

    WARNING! IF OBSTRUCTIONS, LENGTH OF LANDING AREA OR TERRAIN DON’T PERMIT A ORLIČAN M-8 EAGLE REVISION NO. 05 SUCCESSFUL PILOT'S OPERATING DATE OF ISSUE: MAY 02, EMERGENCY LANDING – USE THE EMERGENCY PARACHUTE! DURING TAKE-OFF RUN • Throttle → idle •...

  • Page 49: Flying Without Engine Power (Gliding Flight)

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 7.4.1 FLYING WITHOUT ENGINE POWER (GLIDING FLIGHT) • If the engine fails, it is necessary to maintain best glide speed – 65 knot (120 km/h) 7.5. PRECAUTIONARY LANDING Precautionary landing is generally made in case of loss of orientation, worsening of weather, low fuel, engine vibration or engine roughness is present and/or sudden incapacitation of pilot.

  • Page 50: Fire On Ground, During Take-Off

    WARNING! DO NOT TRY TO RESTART THE ENGINE IN THIS SITUATION. ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, FIRE ON GROUND, DURING TAKE-OFF • Airspeed → 65 knots (120 km/h) • Fuel valve selector → OFF •...

  • Page 51: High Oil Pressure

    WARNING! KEEP THE CONTROL YOKE CENTERED ALONG ITS LATERAL AXIS (NO AILERON ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, DEFLECTIONS THROUGHOUT THE RECOVERY PHASE)! DO NOT ATTEMPT TO STOP THE AIRCRAFT FROM SPINNING USING AILERONS INSTEAD OF RUDDER! WARNING! PROLONGED USE OF HIGH POWER SETTINGS AFTER LOSS OF OIL PRESSURE WILL LEAD TO ENGINE MECHANICAL DAMAGE AND TOTAL ENGINE FAILURE,...

  • Page 52: Stall Recovery

    WARNING! DO NOT USE MAXIMUM ENGINE POWER WITHOUT RPM INDICATION! ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, WARNING! PAY VERY CLOSE ATTENTION TO KEEP THE AIRSPEED WELL ABOVE STALL WARNING! DURING THE SPIN RECOVERY, THE AIRSPEED WILL BUILD VERY RAPIDLY WITH A NOSE LOW ATTITUDE.

  • Page 53: Aileron Or Rudder Failure

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, CAUTION! USE WING FLAPS WITH CAUTION, AS THEY WILL AFFECT PITCH ATTITUDE AND AIRSPEED. AILERON OR RUDDER FAILURE In the event of failure of the rudder or ailerons, control may still be maintained with the remaining control surface (if the ailerons are lost, flight is capable with rudder control / if the rudder is lost, flight is capable with aileron control).
  • Page 54 ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02,...

  • Page 55: Normal Procedures

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 8. NORMAL PROCEDURES 8.1. INTRODUCTION Section 8 provides checklist for the pre-flight inspection and recommended procedures for normal operation of the airplane. Normal procedures following from system installation and optional equipment, which require supplementation of this Manual, are shown in section 15 - Supplements.

  • Page 56: Cabin

    WARNING! DO NOT FLY THE AIRCRAFT IF YOU FIND ANY DAMAGE OR PROBLEMS DURING ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, A PREFLIGHT INSPECTION. ALWAYS CONSULT AUTHORIZED PERSONNEL FOR REPAIRS. CABIN • Ignition off •...

  • Page 57: Engine Starting

    CAUTION! DO NOT PERFORM THE ENGINE TEST WITH THE AIRCRAFT PLACED ON THE LOOSE ORLIČAN M-8 EAGLE REVISION NO. 05 GROUND. LOOSE MATERIAL, IF DRAWN IN BY THE PROPELLER, MAY CAUSE PERSONAL PILOT'S OPERATING DATE OF ISSUE: MAY 02, INJURY AND/OR DAMAGE TO PROPELLER. ENGINE STARTING •...

  • Page 58: Taxiing

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 8.5. TAXIING Be aware of the entire area around the aircraft to ensure that the aircraft will clear all obstructions and other aircraft. When first beginning to taxi, the brakes should be tested for proper operation as soon as the aircraft is put in motion.

  • Page 59: Climbing

    CAUTION! IF CYLINDER HEAD OR OIL TEMPERATURE EXCEED LIMITS, REDUCE THE ANGLE OF ORLIČAN M-8 EAGLE REVISION NO. 05 CLIMB TO INCREASE AIRSPEED AND ALLOW BETTER COOLING. PILOT'S OPERATING DATE OF ISSUE: MAY 02, WARNING! DO NOT TAKE OFF WHEN: ENGINE DOES NOT RUN SMOOTHLY ENGINE INSTRUMENT VALUES ARE NOT WITHIN PRESCRIBED...

  • Page 60: Descent

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, CAUTION! IN CASE OF TURBULENCE: IN STRONG TURBULENCE, WE RECOMMEND MAINTAINING FLIGHT SPEED ABOVE 60 KNOTS (110 KM/H) BUT LESS THAN 90 KNOTS (170 KM/H) WHEN MAKING A TURN, DO NOT BANK MORE THAN 30°. DO NOT USE MORE THAN 1/3 RUDDER DEFLECTION AT SPEED ABOVE 95 KNOTS (175 KM/H);...

  • Page 61: Landing

    CAUTION! IF CROSSWIND → ADJUST APPROACH AND TOUCHDOWN SPEEDS AS NECESSARY ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, ACCORDING TO THE CROSSWIND VECTOR. WARNING! IF THE CRAB METHOD OF DRIFT CORRECTION HAS BEEN USED THROUGHOUT THE FINAL APPROACH AND ROUNDOUT, THE CRAB MUST BE RECOVERED BEFORE THE TOUCHDOWN BY APPLYING RUDDER TO ALIGN THE AIRCRAFT’S...

  • Page 62: Short Field Takeoff

    CAUTION! ALL LANDING SPEEDS WITH 15 ° / 30 ° / 40 ° FLAPS MUST BE INCREASED BY 5.4 KNOTS ORLIČAN M-8 EAGLE REVISION NO. 05 (10 KM/H) IN TURBULENT WEATHER. PILOT'S OPERATING DATE OF ISSUE: MAY 02, 8.14. SHORT FIELD TAKEOFF Short field take-off is a demanding procedure, utilized when it is necessary to get off the ground in the minimum distance and sometimes to climb relatively steeply to clear obstacles.

  • Page 63: Soft Field Landing

    CAUTION! ALL LANDING SPEEDS WITH 15 ° / 30 ° / 40 ° FLAPS MUST BE INCREASED BY 5.4 KNOTS ORLIČAN M-8 EAGLE REVISION NO. 05 (10 KM/H) IN TURBULENT WEATHER. PILOT'S OPERATING DATE OF ISSUE: MAY 02, 8.17. SOFT FIELD LANDING Landing on fields that are rough or have soft surfaces, such as snow, sand, mud, or tall grass, require unique procedures.

  • Page 64: Performance

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 9. PERFORMANCE 9.1. INTRODUCTION This section provides data for airspeed calibration, stall speeds and take-off performance and additional information. The stated performance data has been computed from actual flight tests with the M-8 EAGLE airplane and ROTAX 912 ULS 2 engine in good condition and using average piloting techniques.

  • Page 65: Stall Speeds

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 9.3. STALL SPEEDS HIGHT FLAP CONDITIONS: MAX. LOSS TOW, ENGINE AT [KNOTS] [KM/H] DURING IDLE DEFLEC RECOVER TION Y [FT] 0° 15° HORIZONTAL 30° FLIGHT 40° 0° TURN WITH 30°...

  • Page 66: Climbing Performance

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 9.6. CLIMBING PERFORMANCE CONDITIONS: IDEAL CLIMBING SPEED/RATE MAX. CONTINUOUS POWER 5500RPM, AIRCRAFT WEIGHT KNOTS IAS FT/MIN [M/S] 1320 LB 1500 FT ISA 994 [5,05] 4000 FT ISA 970 [4,93] 8000 FT ISA 919 [4,67]...
  • Page 67 ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, PERFORMANCE PAGE...

  • Page 68: Endurance And Range

    PAGE 60 OF 99 PERFORMANCE ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 9.8. ENDURANCE AND RANGE Range and endurance were calculated for 23.5 US gal of fuel. The 2.9 US gal of fuel not included in the calculation were left as a 30 min flight reserve. ALTITUDE [FT ISA] 1500 ft...

  • Page 69: Optimum Gliding Speed

    CAUTION! REMEMBER: FAR 61.315, (B), (11) STATES THAT SPORT PILOT LICENSE PRIVELEGES DO ORLIČAN M-8 EAGLE REVISION NO. 05 NOT ALLOW FLIGHT AT AN ALTITUDE OF MORE THAN 10,000 FEET MSL OR 2,000 FEET PILOT'S OPERATING DATE OF ISSUE: MAY 02, AGL, WHICHEVER IS HIGHER.

  • Page 70: Weight And Balance

    WARNING! IT IS THE RESPONSIBILITY OF THE PILOT TO MAKE SURE THE AIRPLANE IS ORLIČAN M-8 EAGLE REVISION NO. 05 LOADED PROPERLY. OPERATION OUTSIDE OF PRESCRIBED WEIGHT AND PILOT'S OPERATING DATE OF ISSUE: MAY 02, BALANCE LIMITATIONS COULD RESULT IN AN ACCIDENT AND SERIOUS OR FATAL INJURY.

  • Page 71: Weight And Balance Record Of The Aircraft

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, WEIGHT AND BALANCE RECORD OF THE AIRCRAFT AIRCRAFT ENGINE PROPELLER TYPE M8-EAGLE ROTAX 912 ULS 2 SR 200 SERIAL NUMBER 2022001 9 573 673 1900921 �� ���� = 28,82 ��...
  • Page 72 ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 218,7 1093,9 1312,6 34,4 Calculated position of C.G. is within a permitted range of 23 - 37 % bSAT. WEIGHT AND BALANCE PAGE...

  • Page 73: Determination Of Pre-Flight Cg

    WARNING! MAKE SURE THAT THE BAGGAGE IS PLACED FIXED INSIDE THE BAGGAGE ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING AREA. MOVEMENTS OF BAGGAGE IN-FLIGHT WILL CAUSE SHIFTS OF DATE OF ISSUE: MAY 02, CENTER OF GRAVITY! DETERMINATION OF PRE-FLIGHT CG To calculate weight and balance for an actual flight, follow the process shown in the Sample Loading Problem shown below.

  • Page 74: Permitted Payload Range

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 10.3. PERMITTED PAYLOAD RANGE WEIGHT AND BALANCE PAGE 65 OF 99...

  • Page 75: Description Of Airplane And Systems

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 11. DESCRIPTION OF AIRPLANE AND SYSTEMS 11.1. INTRODUCTION This section provides description and operation of the airplane and its systems. Some optional equipment, primarily avionics, may not be described in this section. More detailed information on optional systems and equipment are available in section 15 - Supplements.

  • Page 76: Controls In Cockpit

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 11.4. CONTROLS IN COCKPIT 1. Control yokes 2. Main switch 3. Engine throttle 4. Choke 5. Fuel valve selector / Starter (under fuel valve selector) 6. Ruder control pedals 7.

  • Page 77: Seats And Safety Harnesses

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 11.6. SEATS AND SAFETY HARNESSES The seats are made of aramid-carbon composite and upholstered. To set the optimal distance from the pedals and the instrument panel, the seats are sliding on a rail and can be folded down for easier access to the luggage compartment.

  • Page 78: Cabin Doors

    WARNING! INTENTIONAL FLIGHT WITH DOOR(S) OPEN IS PROHIBITED. ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, locking WARNING! 11.7. CABIN DOORS Cabin doors have two locking pins for closing at the bottom: one on the left side (lock 1) and one on the right side (lock 2).

  • Page 79: Landing Gear And Brake System

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 11.9. LANDING GEAR AND BRAKE SYSTEM The airplane is equipped with a tricycle landing gear with steerable nose wheel. Main wheels size 14 x 4 - 6 - are provided with hydraulic disc brakes. These are carried on an all- composite leg.

  • Page 80: Power Unit

    WARNING! NEITHER OF THE ENGINES MENTIONED ABOVE IS CERTIFIED AS AN AIRCRAFT ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, ENGINE. EVEN WITH UTMOST ATTENTION DURING ENGINE MANUFACTURE, ENGINE FAILURE MAY OCCUR AT ANY TIME DURING FLIGHT AND THE PILOT BEARS FULL RESPONSIBILITY FOR THE CONSEQUENCES.

  • Page 81: Propeller

    WARNING! THE PROPELLER SHALL BE SENT TO THE MANUFACTURER FOR INSPECTION IN ORLIČAN M-8 EAGLE REVISION NO. 05 CASE OF EVEN THE SLIGHTEST DAMAGE OR IF CRACK IS FOUND. FLYING WITH PILOT'S OPERATING DATE OF ISSUE: MAY 02, DAMAGED PROPELLER MAY ENDANGER LIFE AND LIMB AND IS PROHIBITED. 11.11.PROPELLER SR 200 Wooden propeller blades, that are equipped with leading edges made of highly resistant composite...

  • Page 82: Fuel System

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 11.12.FUEL SYSTEM Scheme of fuel system DESCRIPTION OF AIRPLANE AND PAGE SYSTEMS...

  • Page 83: Electrical System

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 11.13.ELECTRICAL SYSTEM DESCRIPTION OF AIRPLANE AND PAGE SYSTEMS...

  • Page 84: Pitot-Static System

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 11.14.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 85: Lights

    CAUTION! INSTRUMENT, NAVIGATION AND ANTI-COLLISION LIGHTS HAS TO BE ORLIČAN M-8 EAGLE REVISION NO. 05 CHECKED FOR ASTM F2245 COMPLIANCE IF THE AIRCRAFT IS OPERATED PILOT'S OPERATING DATE OF ISSUE: MAY 02, UNDER NIGHT VFR CONDITIONS. 11.15.LIGHTS Exterior lighting consists of navigation and strobe lights located on the wing tips, a position light at the top of the vertical tail leading edge and a headlight in the lower engine cover.

  • Page 86: Handling And Servicing

    FOR MORE INFORMATION AND INSPECTION CHECKLIST REFER TO M-8 EAGLE MAINTENANCE MANUAL! ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 12. HANDLING AND SERVICING 12.1. INTRODUCTION This section defines periodical inspections and prerequisites for the required performance and reliability of aircraft.

  • Page 87: Airplane Modifications Or Repairs

    CAUTION! WHEN PARKING OUTSIDE HANGAR, IT IS NECESSARY TO USE ANCHORS, SO THAT THE ORLIČAN M-8 EAGLE REVISION NO. 05 AIRCRAFT CANNOT BE DAMAGED BY WIND GUSTS. PILOT'S OPERATING DATE OF ISSUE: MAY 02, 12.3. AIRPLANE MODIFICATIONS OR REPAIRS Only qualified personnel are permitted to accomplish repairs and modifications of airplane in an approved service center.

  • Page 88: Towing Instructions

    CAUTION! TOWING THE AIRCRAFT BEHIND AN AUTOMOBILE IS PROHIBITED. ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, ATTENTION! ANCHORING The aircraft is not equipped with anchoring lugs. If necessary (parking outside hangar), the aircraft can be anchored by the landing gear legs.

  • Page 89: Assembly And Disassembly Of The Aircraft

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 12.5. ASSEMBLY AND DISASSEMBLY OF THE AIRCRAFT WING ASSEMBLY • Check and grease strut and wing connecting bolts. • Grasp the wing and insert flap and aileron control rods into the fuselage. •...

  • Page 90: Horizontal Stabilizer (Elevator) Assembly

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, Figure 6 - stabilizer mounting points HORIZONTAL STABILIZER (ELEVATOR) ASSEMBLY • Check condition of elevator hinges (Figure 5), stabilizer mounting (Figure 6) and elevator coupling (Figure 6). •...

  • Page 91: Wing Disassembly

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, WING DISASSEMBLY • Drain all fuel (see section - Draining of fuel tanks and refueling) • Remove cabin ceiling trim panel and disconnect the ceiling light. • Unscrew connecting pins of the aileron and flap control rods.

  • Page 92: Horizontal Stabilizer (Elevator) Disassembly

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, HORIZONTAL STABILIZER (ELEVATOR) DISASSEMBLY Horizontal stabilizer is removed and transported complete with both halves of elevator, including mounting baffle. • Disassemble horizontal stabilizer mounting cover. • Disconnect trim cable connector. •...

  • Page 93: Engine Cowlings

    WARNING! DURING MAINTENANCE ENGINE IGNITION MUST BE SWITCHED OFF. ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 12.7. ENGINE COWLINGS Engine compartment is covered by upper (Figure 14) and lower (Figure 12) cowling. They are made of carbon fiber composite.
  • Page 94 ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, Figure 13 - Lower cowling inner Figure 14 - Upper cowling HANDLING AND SERVICING PAGE...

  • Page 95: Engine Cowlings Removal And Installation

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 12.7.1 ENGINE COWLINGS REMOVAL AND INSTALLATION TYPE OF Line MAINTENANCE: LEVEL OF Owner CERTIFICATION: LSA Repairman Inspection LSA Repairman Maintenance A&P Mechanic TOOLS REQUIRED: Standard metric tool set PARTS REQUIRED: METHOD TO TEST/ INSPECT:...

  • Page 96: Draining Of Fuel Tanks And Refueling

    ATTENTION! THERE IS ALWAYS A CERTAIN INEXHAUSTIBLE AMOUNT OF FUEL LEFT IN THE TANKS. ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 12.8. DRAINING OF FUEL TANKS AND REFUELING When draining or refueling, check that master switch is set to off position. DRAINING OF FUEL TANKS Draining the fuel tanks is necessary before each wing disassembly.

  • Page 97: Refueling

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, REFUELING • Rotax 912 engines are designed for automotive lead-free gasoline (AKI 91, RON 95 unleaded). Temporary limited use of AVGAS is possible. See Rotax 912 UL, Rotax 912 ULS 2 Operating manual for more details.

  • Page 98: Long-Term Storage

    CAUTION! ORLIČAN M-8 EAGLE TO AVOID SOLUTION DRIPPING ONTO DISPLAY AND POSSIBLY MIGRATING INTO REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, COMPONENT, APPLY THE CLEANING SOLUTION TO CLOTH FIRST, NOT DIRECTLY TO THE DISPLAY SCREEN. USE ONLY A LENS CLOTH OR NONABRASIVE COTTON CLOTH TO CLEAN DISPLAY SCREENS.

  • Page 99: Continued Operational Safety

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 13. CONTINUED OPERATIONAL SAFETY 13.1. INSTRUCTIONS: • The aircraft owner is responsible to provide current contact information to the manufacturer that is suitable for delivery of COS Notices. Contact information can be provided via phone call, letter, email, or manufacturers Feedback Form.

  • Page 100: Continued Operational Safety Feedback Form

    NOTICE DATE: AIRCRAFT MODEL: AIRCRAFT S/N: ISSUE DESCRIPTION: ORLIČAN S.R.O. - LONDÝNSKÁ 376/57, 120 00 PRAGUE 2, CZECH REPUBLIC BERVID@ORLICAN.ORG, PHONE: +420 605 231 920, WWW.ORLICAN.ORG THE AIRCRAFT OWNER IS RESPONSIBLE TO PROVIDE CURRENT CONTACT INFORMATION TO THE MANUFACTURER THAT ARE...
  • Page 101 ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, CONTINUED OPERATIONAL PAGE 91 OF 99 SAFETY...

  • Page 102: Flight Training Supplement

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 14. FLIGHT TRAINING SUPPLEMENT 14.1. INTRODUCTION THE FLIGHT TRAINING DATA SUPPLIED HERE IS PRESENTED FOR INFORMATION ONLY. FLIGHT TRAINING FOR THE SPORT PILOT CERTIFICATE OR ANY OTHER CERTIFICATE MUST BE COMPLETED ACCORDING TO THE APPROPRIATE FAA REGULATIONS ADMINISTERED BY A COMMERCIAL FLIGHT INSTRUCTOR, CFI, WHO IS LEGALLY ACTIVE AND CURRENT.

  • Page 103: Practical Training For Pilot Qualification

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 14.4. PRACTICAL TRAINING FOR PILOT QUALIFICATION LESSON 1: INTRODUCTORY FLIGHT Minimum flight level is 1000ft / 300m AGL Training methodology: The instructor shows aircraft handling during traffic pattern flight and in the practice area to the student. He also introduces the shape of airfield traffic pattern, its size, and major orientation landmarks in the vicinity.

  • Page 104: Lesson 5: Side Slips, Slow Flight, Flight At Max Cruise Speed And Approach To Astall

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, LESSON 5: SIDE SLIPS, SLOW FLIGHT, FLIGHT AT MAX CRUISE SPEED AND APPROACH TO A STALL Flight level is 1000ft / 300m AGL – 1600ft / 500m AGL Training methodology: The instructor shows side slip maneuver, slow flight, approach to a stall in a level flight, approach to a stall in turns with 30 degrees bank angle, and a flight at maximum speed to the student.

  • Page 105: Lesson 8: Precautionary Landing

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, LESSON 8: PRECAUTIONARY LANDING Training methodology: The instructor practices approach to suitably selected area, with engine operating. The instructor assesses student’s selection of area for landing, and performance of the maneuver by the student. During this practice, it is allowed to review the area, having assessed the slope and obstacles in the vicinity, from at least 150 ft AGL.

  • Page 106: Blocked Flight Instruments / Instrument Failure

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, BLOCKED FLIGHT INSTRUMENTS / INSTRUMENT FAILURE Training methodology: The instructor reviews with the student the behavior of the aircraft at different air speeds and performs the flight with the student with the instruments covered. Even without the help of instruments, the student must keep the speed in a safe range, especially to maintain safe speed during descent and landing.

  • Page 107: Lesson 16: Side Slips And Approach To A Stall

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, according to compass, and flying figure-eight in the practice area, outside the airfield, but under instructor’s supervision. Two-way radio communication between the instructor and the student is recommended. LESSON 16: SIDE SLIPS AND APPROACH TO A STALL Flight level is 1000ft / 300m AGL –...
  • Page 108 ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, km, minimum flight time 1hr. All conditions must be met. Training methodology: The instructor defines flight route with landing at different airfield. Definition is the same as in Lesson 18.

  • Page 109: Supplements

    ORLIČAN M-8 EAGLE REVISION NO. 05 PILOT'S OPERATING DATE OF ISSUE: MAY 02, 15. SUPPLEMENTS 15.1. INTRODUCTION This section contains the appropriate supplements necessary to operate the airplane safely and efficiently when equipped with various optional systems and equipment not provided with the standard airplane. 15.2.

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