Phoenix U-15 Flight Manual
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Phoenix U-15 Flight Manual

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FLIGHT MANUAL FOR ULTRALIGHT
U–15 Phoenix
Registration:
Serial number:
Producer address:
Lochmanova 64
562 01 Ústí nad Orlicí
CZECH REPUBLIC
www.phoenixair.cz
AEROPLANE
LN-YPV
03/U15

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  • Page 1 FLIGHT MANUAL FOR ULTRALIGHT AEROPLANE U–15 Phoenix LN-YPV Registration: 03/U15 Serial number: Producer address: Lochmanova 64 562 01 Ústí nad Orlicí CZECH REPUBLIC www.phoenixair.cz...

  • Page 2: Table Of Contents

    0. Table of Contents Table of Contents ............0-0 Pilot operating handbook ........... 1-0 General information........... 2-1 Read this before your first flight! ..........2-2 Manufacturer ................2-2 Warnings, cautions and notes ..........2-3 Descriptive data ............... 2-4 2.4.1 Airplane description ............2-4 2.4.2 Basic Technical data ............
  • Page 3 Powered gliders ............... 6-2 6.2.1 Takeoff distances .............. 6-2 6.2.2 Rate of climb ..............6-3 6.2.3 Climbing speeds ..............6-3 6.2.4 Maximum RPM..............6-3 6.2.5 Time limit for the use of takeoff power ....... 6-4 6.2.6 Fuel consumption and total usable fuel volume ....6-4 6.2.7 Crosswind and wind limitations for takeoff and landing..
  • Page 4 8.2.3 Normal takeoff ..............8-21 Before take-off ................8-21 Take-off ..................8-22 8.2.4 Engine extraction and retraction ........8-22 8.2.5 Best rate of climb ............8-23 8.2.6 In-flight starting of engine ..........8-23 8.2.7 Ground shutdown of engine ..........8-23 Cruise ..................
  • Page 5 10.3 Passenger warnings ............... 10-5 10.3 Passenger warnings ............... 10-5 10.4 No intentionall spins ............... 10-6 10.5 Empty weight ................. 10-7 10.6 Maximum takeoff weight ............10-7 10.7 Maximum and minimum weight of crew ........10-8 10.8 Seat for solo operations of two seated gliders ......10-8 Supplementary Information ........11-9 11.1 Familiarization flight procedures ..........

  • Page 6: Pilot Operating Handbook

    Section 1 1. Pilot operating handbook Each U15 Phoenix includes Aircraft Operating Instructions (AOI). The content and format herewith is defined by ultralight rules. All flight speeds are given in terms of indicated airspeeds (IAS). Date of Issue: 24/07/2010...

  • Page 7: General Information

    Section 2 2. General information Read this before your first flight! ..........2-2 Manufacturer ................2-2 Warnings, cautions and notes ..........2-3 Descriptive data ............... 2-4 Three-view drawing ..............2-7 Date of Issue: 24/07/2010...

  • Page 8: Read This Before Your First Flight

    VFR aircraft is extremely dangerous. As the owner or operator of an aircraft you are responsible for the safety of your passenger and your- self. Do not attempt to operate U15 Phoenix in any manner that would en- danger the aircraft, the occupants or persons on ground.

  • Page 9: Warnings, Cautions And Notes

    Warnings, cautions and notes The following definitions apply to warnings, cautions and notes in the flight manual. Warning Means that the non-observation of the corresponding proce- dure leads to an immediate or important degradation of the flight safety. Caution Means that the non-observation of the corresponding proce- dure leads to a minor or to a more or less long term degradation of the flight safety.

  • Page 10: Descriptive Data

    U15 Phoenix is intended for recreational, sport, cross-country and training. It is not approved for aerobatic operation. U15 Phoenix is a single engine, carbon airplane with two side-by- side seats. The aeroplane is equipped with fixed two main wheel undercar- riage with a steerable tail wheel.

  • Page 11: Basic Technical Data

    2.4.2 Basic Technical data Wing Span/span with wing extension ......34,77/49.21 ft Area/area with wing extension ....... 115/133 ft MAC ............... 3.238 ft Flaperon area ..............8.56 ft Fuselage length .............. 21.32 ft width ..............4,00 ft height ..............4.26 ft Horizontal tail unit span ..............
  • Page 12 Vertical tail unit height ..............3.93 ft area ..............11.84 ft rudder area ............4.73 ft Landing gear wheel track ............5.47 ft wheel base ............13.61 ft main wheel diameter .......... 1.18 ft tail wheel diameter ..........0.65 ft Date of Issue: 24/07/2010...

  • Page 13: Three-View Drawing

    Three-view drawing Date of Issue: 24/07/2010...

  • Page 14: Aircraft And Systems Descriptions

    Section 3 3. Aircraft and systems descriptions Operating weights and loading ..........3-1 Propeller .................. 3-3 Fuel and fuel capacity .............. 3-4 Oil .................... 3-5 Engine ..................3-6 Date of Issue: 24/07/2010...

  • Page 15: Operating Weights And Loading

    Operating weights and loading NOTE Actual empty weight is stated in SECTION 10.5 Minimum load per seat ......... 65 kg Maximum weight per seat ........110 kg Empty weight (standard)…………………………… 295 kg Max. take-off weight ..........472,5 kg Max. landing weight ..........472,5 kg Max.
  • Page 16 Weighing Put the airplane on three scales on a level surface. Make certain the plane is levelled using a bubble level put onto the canopy frame. Mark the wheel axle positions on the ground using a plumb. Date of Issue: 24/07/2010...

  • Page 17: Propeller

    Propeller Producer Sensenich. 2 blade, wooden propeller is attached to the propeller flange with 6 bolts, and covered with a conic spinner. Date of Issue: 24/07/2010...

  • Page 18: Fuel And Fuel Capacity

    Fuel and fuel capacity Fuel specification: Automotive Premium Unleaded per ASTM D 4814, minimum Oc- tane 95 for Jabiru 2200. For suitable fuel types refer to the original Jabiru Operator’s Man- ual. Warning Do not use fuel containing more than 10% ethanol. Fuel capacity: 2 x wing fuel tank 50 litters aech (100 liters total).

  • Page 19: Oil

    For suitable oil types refer to the original Jabiru Operator’s Manual. Date of Issue: 24/07/2010...

  • Page 20: Engine

    Engine Engine Manufacturer : Jabiru Australia Engine Model: Jabiru 2200 Power: Max. Take-off: 63 Kw / 85 hp at 3300 rpm Engine RPM: Max. Take-off: 3300 rpm. Max. Continuous: 3300 rpm Cruising: 2800 rpm Idling: 900 rpm ( set while engine is hot ) Cylinder head temperature: Maximum: 200 °C...
  • Page 21 (CHT) [°C] Temperature 65-95 95-100 [°C] 5.25 cold Pressure 0.8 at idle 2.2 – 4.0 4.0 – 5.0 engine [bar] starting NOTE TL engine instrument is installed in U15 Phoenix. Do not cross rec- ommended limits. Date of Issue: 24/07/2010...
  • Page 22 Description of design There is installed Jabiru 2200 engine in U15 Phoenix aeroplane. Jabiru 2200 is 4-stroke, 4 cylinder horizontally opposed, spark ignition en- gine. Ram air cooled cylinders and cylinder heads. Dry sump forced lubrication. Dual breaker less capacitor discharge ignition.

  • Page 23: Operating Limitations

    Section 4 4. Operating limitations Stalling speeds at maximum takeoff weight (v and v ) ... 4-1 Flap extended speed range (v and v ) ........4-1 Maximum maneuvering speed (v ) ........... 4-2 Never exceed speed (v ) ............4-2 Maximum aerotow speed (v ) ...........

  • Page 24: Stalling Speeds At Maximum Takeoff Weight

    Stalling speeds at maximum takeoff weight (v and v Vs1 = 40kts Vso = 35kts Flap extended speed range (v and v Vfe = 70kts Date of Issue: 24/07/2010...

  • Page 25: Never Exceed Speed

    Maximum maneuvering speed (v = 97 kts Up to speed V all control surfaces can be fully deflected Never exceed speed (v = 140 kts short wing span / 120 Kts long wing span From V to V only 1/3 of the maximum deflection of control sur- faces is allowed.

  • Page 26: Crosswind And Wind Limitations For Takeoff And Landing

    In gusty wind or wind speed more than 25 kts flight operations should be stopped. 4.10 Load factors From V up to V +4 g / -2 g 4.11 Prohibited maneuvers The U15 Phoenix is not certified for aerobatics or spins. Date of Issue: 24/07/2010...

  • Page 27: Weight And Balance Information

    Section 5 5. Weight and Balance Information Installed equipment list Phoenix has the following cockpit installation: Date of Issue: 24/07/2010...
  • Page 28 1. Wheel brake 6. Trim lever 2. Pilot control stick 7. Throttle 3. Pedals 8. Co-pilot stick 4. Spoiler control lever 9. Fuel valve 5. Flap lever Date of Issue: 24/07/2010...
  • Page 29 Instrument panel 14 15 16 17 1. Master switch 12. Magnetos 2. Slip/skid 13. VSI 3. Airspeed 14. Rescue sys. handle 4. Altmeter 15. Choke 5. TL engine instrument 16. Switches 6. Cockpit ventilation 17. Throttle 7. Radio 18. Carburettor heating 8.

  • Page 30: Center Of Gravity (Cg) Range And Determination

    Center of gravity (CG) range and determination Date of Issue: 24/07/2010...

  • Page 31: Performance

    Section 6 6. Performance Performance ........6-1 Gliders ..................6-2 Powered gliders ............... 6-2 6.2.1 Takeoff distances ..............6-2 6.2.2 Rate of climb ................6-3 6.2.3 Climbing speeds ..............6-3 6.2.4 Maximum RPM ................ 6-3 6.2.5 Time limit for the use of takeoff power ........6-4 6.2.6 Fuel consumption and total usable fuel volume......

  • Page 32: Gliders

    Gliders Powered gliders 6.2.1 Takeoff distances Take-off distances stated in the following table are valid at sea level and for MTOW. Take-off run Take-off distance over distance 15 m obstacle [feet] [feet] Grass Paved Landing distances stated in the following table are valid at sea level and for MTOW.

  • Page 33: Rate Of Climb

    6.2.2 Rate of climb For Jabiru 2200 and Sensenich propeller is the best rate-of-climb 1000 feet/min. 6.2.3 Climbing speeds The best climbing speed is 70 kts IAS 6.2.4 Maximum RPM All information is for Jabiru 2200. Takeoff performance 3 300 rpm Max.

  • Page 34: Time Limit For The Use Of Takeoff Power

    6.2.5 Time limit for the use of takeoff power There is no limit for takeoff power if RPM is not over 3 300 rpm, and if all temperatures are in Engine Operating Manual limits. 6.2.6 Fuel consumption and total usable fuel volume Fuel consumption at takeoff power 25 l/h Fuel consumption at cruising power...

  • Page 35: Speeds For Extracting And Retracting Powerplant

    6.2.8 Speeds for extracting and retracting powerplant Date of Issue: 24/07/2010...

  • Page 36: Emergency Procedures

    Section 7 7. Emergency procedures Emergency procedures ............7-0 Engine failure ................7-1 7.1.1 Engine failure during take-off run ..........7-1 7.1.2 Engine failure immediately after take-off ........7-1 7.1.3 Engine failure in flight (Forced landing) ........7-2 In-Flight start ................7-3 Smoke and fire .................

  • Page 37: Engine Failure

    Section 7 provides checklist and amplified procedures for coping with emergencies that may occur. Emergencies caused by airplane or engine malfunctions are ex- tremely rare if proper pre-flight inspections and maintenance are practised. However, should an emergency arise, the basic guidelines de- scribed in this section should be considered and applied as necessary to correct the problem.

  • Page 38: Engine Failure In Flight (Forced Landing)

    9. Master key - switch off position before landing 10. Land Note Skip 6-10 if necessary. 7.1.3 Engine failure in flight (Forced landing) 1. Speed - keep gliding speed at 55 kts - sink rate 180 feet/min 2. Altitude - below 100 feet: land in take-off direction - over 150 feet: choose landing area 3.

  • Page 39: In-Flight Start

    In-Flight start 1. Speed - keep speed a bit higher at 65 kts 2. Altitude - check 3. Landing area - choose according to altitude (safest area) 4. Master switch - on 5. Fuel valve - open 6. Choke - closed initially, then as needed 7.

  • Page 40: Fire During Take-Off

    7.3.2 Fire during take-off 1. Fuel valve - off 2. Throttle - full 3. Speed - 55 kts 4. Master switch - off 5. Ignition - off 6. Land and brake 7. Abandon the airplane 8. Extinguish fire if possible or call fire department. Date of Issue: 24/07/2010...

  • Page 41: Fire In Flight

    7.3.3 Fire in flight 1. Fuel valve - off 2. Throttle - full 3. Master switch - off 4. Ignition - off after using up fuel in carburettors then engine stops 5. Choose of area - heading to the nearest airport or choose emergency landing area 6.

  • Page 42: Landing Emergencies

    Landing emergencies 7.5.1 Emergency landing 1. An emergency landing may be carried out due to engine fail- ure and when the engine cannot be restarted. 2. Speed - 55 kts 3. Trim - trim the airplane 4. Safety harness - tighten 5.

  • Page 43: Precautionary Landing

    7.5.2 Precautionary landing A precautionary landing may be carried out due to low fuel and/or bad weather conditions. 1. Choose landing area, determine wind direction 2. If a COMM is installed - report your plan to land and land area location to nearest ATC 3.

  • Page 44: Landing With A Defective Landing Gear

    7.5.4 Landing with a defective landing gear 1. If the main landing gear is damaged, perform touch-down at the Lowest speed possible and maintain direction during land- ing run, if possible 2. If the tail wheel is damaged perform touch-down at the lowest possible speed and maintain direction during landing run, if possible.

  • Page 45: Recovery From Unintentional Spin

    Recovery from unintentional spin Warning Intentional spins are prohibited! There is no tendency of spontaneous uncontrollable spin entry if normal pilot techniques are used. Should an inadvertent spin occur, the following recovery procedure should be used: 1. Throttle retard to idle 2.

  • Page 46: Other Emergencies

    Other emergencies 7.7.1 Vibration If vibrations appear: 1. Set engine speed to power setting where the vibrations are the lowest. 2. Land at the nearest airfield or perform a precautionary landing according to 3.6.2 7.7.2 Carburetor icing Carburetor icing mostly occurs when getting into an area of humid- ity formation.

  • Page 47: Normal Procedures

    Section 8 8. Normal Procedures Normal Procedures ..............8-11 Pre-flight check ..............8-12 Powered glider normal procedures ......... 8-17 8.2.1 Groung engine starting ............8-17 8.2.2 Taxiing ................... 8-20 8.2.3 Normal takeoff................ 8-21 8.2.4 Engine extraction and retraction ..........8-22 8.2.5 Best rate of climb ..............

  • Page 48: Pre-Flight Check

    Pre-flight check The pre-flight inspection is very important because an incomplete or careless inspection could allow airplane failure. The following pre-flight inspection procedure is recommended by the airplane Manufacturer: Date of Issue: 24/07/2010 8-12...
  • Page 49 ⇒ Check if ignition is switched off in the cockpit 1. Wing • Wing surface condition • Leading edge condition • Wing flaps free movement 2. Wing tips • Surface condition • Check of tips attachment • (if installed) Condition and attachment of position lights 3.
  • Page 50 6. Horizontal tail • Surface condition • Attachment • Play • Free movement • 7. see. 5 8. see. 4 9. see. 3 10. see. 2 11. see. 1 12. Landing gear • Check of main landing gear and tail wheel attachment •...
  • Page 51 13. Engine • Engine cowlings condition • Oil flap condition and check of movement • Engine mount condition • Engine attachment check • Oil quantity check (after burping the engine) • Cooling liquid quantity check • Fuel and Electrical system visual check •...
  • Page 52 • Controls - visual check check for proper function check of plays check of flaps extension check of free movement up to the stops • Check for loose items - secure papers • Canopy Condition attachment, cleanliness Date of Issue: 24/07/2010 8-16...

  • Page 53: Powered Glider Normal Procedures

    Powered glider normal procedures 8.2.1 Ground engine starting Before entering cockpit 1. Airplane surface - check for damage 2. Cockpit - items inside the cockpit 3. Ignition - off 4. Master switch - off After entering cockpit 1. Rudder control - free movement check - Correct? 2.

  • Page 54: Before Engine Starting And Engine Starting

    Before engine starting and Engine starting 1. Fuel valve - on 2. Ignition key - off 3. Circuit breakers - in 4. Throttle - set for idling 5. Choke - according to engine temperature 6. Control stick - fully pulled 7.

  • Page 55: Engine Warm Up, Engine Check

    Caution The starter should be activated for max.10 sec., then 2 min. pause for engine cooling. After engine starting adjust the throttle for smooth running at 1500 rpm. Check oil pressure which should increase within 10 sec. Increase engine speed after oil pressure reaches2 bars and is steady.

  • Page 56: Taxiing

    8.2.2 Taxiing The maximum recommended taxiing speed is 8 kts. The direction of taxiing can be controlled by the steerable rear wheel – rudder. Use the lever on the control stick to operate the brakes intermittently. Do not ride the brakes which can cause overheating of the brake pads and possible locking of the brakes.

  • Page 57: Normal Takeoff

    8.2.3 Normal takeoff Before take-off (CCCIGAAR – Lights, Camera, Action) 1. Controls - check of free movement 2. Canopy -closed and locked 3. Choke - off 4. Instruments - set and in the green 5. Gas - fuel valve on left tank 6.

  • Page 58: Take-Off

    Take-off Gradually increase the throttle (max. power) to set the airplane into motion. The direction of take-off run can be controlled by steerable tail wheel and rudder. Place the stick 2 inches forward of the rear stop. The airplane takes-off at a speed above 38 kts, then slightly push forward the stick to reach climb speed of 55 kts.

  • Page 59: Best Rate Of Climb

    8.2.5 Best rate of climb For Jabiru 2200 and Sensenich propeller is the best rate-of-climb 1000 feet/min. 1. Throttle - Max. 2. Speed - 70 kts 3. Trim - adjust as needed to reduce stick pressure 4. Instruments - CHT, Oil temp. and pressure within limits. Caution If cylinder head or oil temperature exceed limits, reduce the angle of climb to increase airspeed and allow better cooling.

  • Page 60: Cruise

    Cruise The airplane flight characteristics are very forgiving within permit- ted limits of airspeeds, configurations and C/G range. The airplane can be controlled very easily. Refer to the Section 5 par. 5.3.1 . Warning Never remove your feet from rudder pedals during flight! Your feet are making tension in rudder control line! Approach Descent...

  • Page 61: Check Before Landing

    Check before landing – GPS-USTALL 1. Gas - fuel on left tank 2. Pump -fuel pump on 3. Straps -tight 4. Undercarriage - down 5. Speed - 55kts 6. Trim - adjust as required 7. Airbrakes - unlocked and operational 8.

  • Page 62: Normal Landing

    Normal landing Landing The airspeed during final is slowly reduced, so that the touchdown speed is about 38 kts. Gradually pull the stick after touchdown. The landing run can be shortened by braking. Caution If the airplane rebounds 2 or 3 feet hold the control stick fully pulled.

  • Page 63: After Landing

    After landing 1. Engine speed - set as necessary for taxiing 2. Fuel pump - off Engine shutdown 1. Instruments - engine instruments within limits 2. COMM + intercom - off 3. Ignition key - off 4. Circuit breakers - off 5.

  • Page 64: Flight In Rain

    Should an inadvertent spin occur, the following recovery procedure should be used: 1. Throttle retard to idle 2. Control stick hold ailerons neutralized 3. Rudder pedals apply full opposite rudder 4. Control stick forward elevator control as required to break the spin 5.

  • Page 65: Engine Restarting

    Engine restarting Follow same engine start procedures as in 8.2.1 Caution After extended soaring flight, the engine could be cooled down. Use the choke if engine fails to start initially. Date of Issue: 24/07/2010 8-29...

  • Page 66: Airplane Ground Handling And Servicing

    Section 9 9. Airplane Ground Handling and Servicing Airplane Ground Handling and Servicing ......... 9-0 Servicing fuel, oil, coolant ............9-1 Towing and tie-down instructions ..........9-3 Date of Issue: 24/07/2010...

  • Page 67: Servicing Fuel, Oil, Coolant

    Servicing fuel, oil, coolant Fuel check 2 x wing fuel tanks (50 l each, 100 l total) are an integral part of the wings, and fuel quantity sensors are located inside the wings. In addition, a coarse filter, fuel valve, and fine filter are parts of the fuel system. For draining use the drain valve located on the bottom of the wing.
  • Page 68 Oil quantity check To service oil one person is required. Ø Remove top cowling Ø Make sure the ignition and both magnetos are OFF Ø Open the oil tank cap Ø Turn the prop 3-4 times counter-clockwise standing in the front of aircraft until burp is heard Ø...

  • Page 69: Towing And Tie-Down Instructions

    Towing and tie-down instructions Towing It is easy to tow the airplane a short distance by holding the blade root because the empty weight of this aeroplane is relatively low. Suitable surfaces to hold the airplane airframe are the rear part of the fuselage before the fin and wing roots..
  • Page 70 Tie-down The airplane is usually tied-down after a flight day or when needed. This is necessary to protect the aeroplane against possible dam age caused by wind gusts. The airplane is equipped with tie-down bolts on the wing tips. Procedure: Check: Fuel valve off, Circuit breakers and Master switch off, Ignition key off.

  • Page 71: Jacking

    To lift the wings, push on the wings lower surface at the main spar. Do not lift by the wing tips. Levelling Refer to the Operating, Maintenance and Repair Manual for U-15 Phoenix for more details about levelling. Road transport The airplane may be transported in a suitable trailer.

  • Page 72: Airplane Assembly

    Airplane Assembly Note No special qualification needed for assembling/disassembling. Degrease and clean all connecting parts and grease again using suitable lubricants. • Horizontal Tail Unit (HTU) Installation: Set the HTU on the two main pins and at the same time insert the elevator control bell into automatic grip- ping.

  • Page 73: Airplane Disassembly

    • Wing Installation: Set the left half of the wing on the pins and check automatic con- nection of control rods. Then secure the rear auxiliary pin. Follow with the right half of the wing, insert the wing in automatic connection device and secure the rear auxiliary pin.
  • Page 74 Cleaning and care Use cleaning detergents to clean airplane surface. Oil spots on air- plane surface (except the canopy!) may be cleaned with appropriate de- greasers. The canopy should be cleaned only by washing it with lukewarm water and mild detergents, using clean, soft cloth sponge or deerskin. Then use suitable polishers to clean the canopy.

  • Page 75: Required Placards And Markings

    Section 10 Required Placards and Markings Required Placards and Markings ..........10-0 10.1 Airspeed indicator range markings.......... 10-1 10.2 Operating limitations on instrument panel ....... 10-4 10.3 Passenger warnings ............... 10-5 10.3 Passenger warnings ............... 10-5 10.4 No intentionall spins ............... 10-6 10.5 Empty weight .................

  • Page 76: Airspeed Indicator Range Markings

    10.1 Airspeed indicator range markings Airspeed indicator system calibration δV V IAS V CAS [kts] [kts] [kts] -2.7 -1.6 -1.1 -0.5 Date of Issue: 24/07/2010 10-1...
  • Page 77 Airspeed limitations Airspeed limitations and their operational significance are shown below: Airspeed Remarks [kts] Never exceed Do not exceed this speed in 140/120 speed any operation. Maximum Do not exceed this speed structural except in smooth air, and cruising speed then only with caution.
  • Page 78 Airspeed indicator markings Airspeed indicator markings and their colour-code significance are shown below: Range or value Marking Significance [IAS kts] Green 35-97 Normal Operating Range Maneuvering must be con- Yellow 97-120 ducted with caution and only in smooth air. Maximum speed for all opera- 140 / 120 tions.

  • Page 79: Operating Limitations On Instrument Panel

    10.2 Operating limitations on instrument panel Date of Issue: 24/07/2010 10-4...

  • Page 80: Passenger Warnings

    PRODUCER: Phoenix Air s.r.o. MADE IN: CZECH REPUBLIC TYPE: U-15 Phoenix YEAR OF PRODUCTION: 2010 SERIAL NUMBER: 03/U15 REGISTR. NUMBER: LN-YPV MTOW: 472,5 kg Passenger warnings The warning placard: “This aircraft was manufactured in accor- dance with Light Sport Aircraft airworthiness standards and does not con- form to standard category airworthiness requirements.”...

  • Page 81: No Intentionall Spins

    Photo of instrument panel 10.3 No intentional spins The placard: “No intentional spins” is placed on co-pilot side of in- strument panel. Date of Issue: 24/07/2010 10-6...

  • Page 82: Empty Weight

    Warning No intentional spins! 10.4 Empty weight Empty weight …………………………………… ..297 kg 10.5 Maximum takeoff weight Maximum takeoff weight of U-15 Phoenix is 472,5 kg. Warning Never exceed 472,5 kg MTOW. Date of Issue: 24/07/2010 10-7...

  • Page 83: Maximum And Minimum Weight Of Crew

    10.6 Maximum and minimum weight of crew Max. weight of crew if…. ¼ fuel tank (25 l) 148 kg ½ fuel tank (50 l) 130 kg ¾ fuel tank (75 l) 112 kg full fuel tank (100 l) 94 kg 30 min flight 158 kg 10.7...

  • Page 84: Supplementary Information

    Section 11 Supplementary Information 11.1 Familiarization flight procedures For familiarization flight procedure, refer to the Flight Training Supplement. 11.2 Pilot operating advisories No any other pilot operating advisories. Date of Issue: 24/07/2010 11-9...

  • Page 85: Maintenance Manual

    Section 12 Maintenance Manual Maintenance manual containing routine, inspection and repair maintenance procedures for the aircraft and engine and propeller is pro- vided with each U15 Phoenix. Date of Issue: 24/07/2010 12-10...

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