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Phoenix S-LSA Glider 02/U15 Operating Instructions Manual

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Phoenix S-LSA Glider
02/U15
Aircraft Operating
Instructions

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Summary of Contents for Phoenix S-LSA Glider 02/U15

  • Page 1 Phoenix S-LSA Glider 02/U15 Aircraft Operating Instructions...

  • Page 2: Table Of Contents

    Table of Contents Table of Contents ............1-4 Pilot operating handbook ..........5 General information ............5 Read this before your first flight! ..........7 Manufacturer................8 Warnings, cautions and notes ............. 9 Descriptive data ................ 10 2.4.1 Airplane description............10 2.4.2 Basic Technical data ............
  • Page 3 6.2.1 Takeoff distances ............... 31 6.2.2 Rate of climb ..............32 6.2.3 Climbing speeds ..............32 6.2.4 Maximum RPM ..............32 6.2.5 Time limit for the use of takeoff power ........ 33 6.2.6 Fuel consumption and total usable fuel volume ....33 6.2.7 Crosswind and wind limitations for takeoff and landing ..
  • Page 4 Before take-off ................. 56 Take-off ..................57 8.2.4 Engine extraction and retraction ......... 58 8.2.5 Best rate of climb ............... 58 8.2.6 In-flight starting of engine ........... 58 8.2.7 Ground shutdown of engine ..........58 Cruise ..................59 Approach .................. 59 Descent ..................
  • Page 5 10.3 Passenger warnings..............81 10.4 No intentionall spins ..............82 10.5 Empty weight ................82 10.6 Maximum takeoff weight............82 10.7 Maximum and minimum weight of crew ........82 10.8 Seat for solo operations of two seated gliders ......83 Supplementary Information .........

  • Page 6: H O E N I X S - L S A G L I D E R

    Pilot operating handbook In accordance with the specification F 2564 each U15 Phoenix in- cludes Aircraft Operating Instructions (AOI). The content and format here- with is defined by F 2564. Additions to F 2564 are considered where nec- essary. All flight speeds are given in terms of calibrated airspeeds (CAS).
  • Page 7 Read this before your first flight! ..........7 Manufacturer................8 Warnings, cautions and notes ............. 9 Descriptive data ................ 10 Three-view drawing ..............2-7 Date of Issue: 07/28/2010...

  • Page 8: Read This Before Your First Flight

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

  • Page 9: Manufacturer

    Manufacturer Lochmanova 64 562 01 Ústí nad Orlicí Czech Republic Date of Issue: 07/28/2010...

  • Page 10: 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 11: Descriptive Data

    Descriptive data 2.4.1 Airplane description U15 Phoenix is intended for recreational, sport, cross-country and training. It is not approved for aerobatic operation. The Phoenix is a single en- gine, carbon airplane with two side-by-side seats. The airplane is equipped with a fixed main wheel undercarriage with a steerable tail wheel. The fuse- lage is a carbon shell with carbon/kevlar seats integrated.

  • Page 12: Basic Technical Data

    2.4.2 Basic Technical data Wing Span/span with wing extension ......36/49.00 ft Area/area with wing extension ....... 100.9/138.5 ft MAC ............... 3.238 ft Aileron area ..............8.62 ft Fuselage length .............. 21.65 ft width ..............3.54 ft height ..............4.75 ft Horizontal tail unit span ..............
  • Page 13 Vertical tail unit height ..............3.93 ft area ..............11.84 ft rudder area ............4.73 ft Landing gear wheel track ............5.05 ft wheel base ............13.60 ft main wheel diameter.......... 1.31 ft tail wheel diameter ..........0.65 ft Date of Issue: 07/28/2010...

  • Page 14: Three-View Drawing

    Three-view drawing Date of Issue: 07/28/2010...

  • Page 15: Aircraft And Systems Descriptions

    Aircraft and systems descriptions Operating weights and loading ..........15 Propeller ................... 17 Fuel and fuel capacity ............... 18 Oil ..................... 19 Engine ..................20 Date of Issue: 07/28/2010...

  • Page 16: Operating Weights And Loading

    Operating weights and loading NOTE Actual empty weight is stated in SECTION 10.5 Minimum load solo ..........144 lb Maximum weight per seat ........242 lb Empty weight (standard)………………………………708 lb Max. take-off weight ..........1 320 lb Max. landing weight ..........1 320 lb Max.
  • Page 17 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: 07/28/2010...

  • Page 18: Propeller

    Propeller On-ground adjustable, 2 blade, composite propeller VARIA 1,6 is attached to the propeller flange with 6 bolts, and covered with a conic spinner. Date of Issue: 07/28/2010...

  • Page 19: Fuel And Fuel Capacity

    Fuel and fuel capacity Fuel specification: Automotive Premium Unleaded per ASTM D 4814, minimum Oc- tane 89 for Rotax 912 UL and minimum Octane 91 for Rotax 912 ULS. For suitable fuel types refer to the original Rotax Operator’s Man- ual.

  • Page 20: Oil

    For suitable oil types refer to the original Rotax Operator’s Manual. Oil type: Automotive engine oil of registered brand with gear additives, but not aircraft oil (refer to engine Operator’s Manual). API classification „SF“ or „SG“. Honda GN-4 10-40 motorcycle oil highly recommended. Date of Issue: 07/28/2010...

  • Page 21: Engine

    Engine Engine Manufacturer : Bombardier-Rotax GMBH Rotax 912 ULS Engine Model: Power: Max. Take-off: 73.5 kW (100hp) at 5800rpm Max. Continuous: 69 kW (95 hp) at 5500rpm Cruising: 59 kW / 79 hp at 4800 rpm Engine RPM: Max. Take-off: 5800 rpm, max.
  • Page 22 Fuel pressure (if the fuel gauge and sensor are installed): Maximum: 0.40 bar (5.8 psi) Minimum: 0.15 bar (2.2 psi) Warning The Rotax 912 ULS has not been certified as an aircraft engine and its failure may occur at any time. The pilot is fully responsi- ble for consequences of such a failure.
  • Page 23 Note Original Rotax analog engine instruments are installed in U15 Phoenix. Do not cross recommended limits. Description of design 4-stroke, 4 cylinder horizontally opposed, spark ignition engine, one central camshaft – pushrods – OHV Liquid cooled cylinder heads, ram air cooled cylinders, dry sump forced...

  • Page 24: Operating Limitations

    Operating limitations Stalling speeds at maximum takeoff weight (v and v ) ... 24 Flap extended speed range (v and v ) ........24 Maximum maneuvering speed (v ) ..........25 Never exceed speed (v ) ............25 Maximum aerotow speed (v ) ............

  • Page 25: Stalling Speeds At Maximum Takeoff Weight

    Stalling speeds at maximum takeoff weight and v Vs1 = 42kts Vso = 40kts Flap extended speed range (v and v Vfe = 80kts Date of Issue: 07/28/2010...

  • Page 26: Flap Extended Speed Range (V Maximum Maneuvering Speed (V )

    Maximum maneuvering speed (v = 97 kts Up to speed V all control surfaces can be fully deflected Never exceed speed (v = 120 kts From V to V only 1/3 of the maximum deflection of control surfaces is allowed. Maximum aerotow speed (v Maximum winch tow speed (v Maximum landing gear extended operating...

  • Page 27: 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: 07/28/2010...

  • Page 28: Weight And Balance Information

    Weight and Balance Information Installed equipment list Phoenix has the following cockpit installation: 1. Pilot control stick 7. Throttle 2. Wheel brake 8. Rescue system handle 3. Pedals 9. Co-pilot stick 4. Spoiler control lever 10. Fuel valve 5. Flap lever 11.
  • Page 29 Instrument panel 1. Master switch 14. Switches 2. Ignition key 15. 12V power socket 3. Slip/skid 16. Fuel switch 4. Compass 17. Throttle 5. Altimeter 18. Choke 6. Airspeed 19. Cowl flap 7. VSI 20. Air vent 8. Parachute handle 21.

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

    Center of gravity (CG) range and determination Date of Issue: 07/28/2010...

  • Page 31: Performance

    Performance Performance ........30 Gliders ..................31 Powered gliders ................ 31 6.2.1 Takeoff distances ..............31 6.2.2 Rate of climb ................32 6.2.3 Climbing speeds ............... 32 6.2.4 Maximum RPM ................. 32 6.2.5 Time limit for the use of takeoff power ........33 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 Rotax 912ULS and VARIA 1.6 propeller the best rate-of-climb at MTOW is 1000 feet/min. 6.2.3 Climbing speeds The best rate of climb speed is 55 kts CAS The best angle of climb speed is 50kts CAS 6.2.4 Maximum RPM All information is for Rotax 912ULS.

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

    6.2.5 Time limit for the use of takeoff power The limit for takeoff power if RPM is 5 800 rpm, and if all tempera- tures are in Engine Operating Manual limits is 5 minutes. 6.2.6 Fuel consumption and total usable fuel volume Fuel consumption at takeoff power 6.88 gal/h Fuel consumption at cruising power...

  • Page 35: Emergency Procedures

    Emergency procedures Emergency procedures ............. 34 Engine failure ................35 7.1.1 Engine failure during take-off run..........35 7.1.2 Engine failure immediately after take-off ........35 7.1.3 Engine failure in flight (Forced landing) ........36 In-Flight start ................37 Smoke and fire ................37 7.3.1 Fire on ground ................

  • Page 36: Engine Failure

    Engine failure 7.1.1 Engine failure during take-off run 1. Throttle - retard to idle 2. Ignition - off 7.1.2 Engine failure immediately after take-off 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 37: Engine Failure In Flight (Forced Landing)

    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. Wind - evaluate direction and velocity 4.

  • Page 38: In-Flight Start

    In-Flight start 1. Speed - 60 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. Throttle - closed 8.

  • Page 39: 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: 07/28/2010...

  • Page 40: 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 area - head to the nearest airport or choose emergency landing area 6.

  • Page 41: 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 42: Precautionary Landing

    7.5.2 Precautionary landing A precautionary landing may be carried out due to low fuel and/or bad weather conditions. It is best to land at an airport whenever possible. But if an airport is not available, a landing may be made in a field or on a road.

  • Page 43: Landing With A Flat Tire

    7.5.3 Landing with a flat tire 1. Approach Normal 2. Touch down - good tire first, keep the damaged wheel above ground as long as possible using ailerons 3. Maintain the direction at landing run, applying braking control Date of Issue: 07/28/2010...

  • 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 3. Note that if unbalanced wheel spins in flight, vibration may result.

  • Page 47: Normal Procedures

    Normal Procedures Normal Procedures ..............46 Pre-flight check ................. 47 Powered glider normal procedures ..........52 8.2.1 Ground engine starting .............. 52 8.2.2 Taxiing ..................55 8.2.3 Normal takeoff ................56 8.2.4 Engine extraction and retraction ..........58 8.2.5 Best rate of climb ..............58 8.2.6 In-flight starting of engine ............

  • 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: 07/28/2010...
  • Page 49 ⇒ Check if ignition is switched off in the cockpit 1. Wing Wing surface condition • Leading edge condition • Pitot tube inspection • Wing flaps free movement • 2. Wing tips Surface condition • Check of tips attachment • (if installed) Condition and attachment of position lights •...
  • Page 50 6. Horizontal tail Surface condition • Attachment • Play • Free movement • Tail wheel tire and steering • 7. see. 5 8. see. 4 9. see. 3 10. see. 2 11. see. 1 12. Landing gear Check of main landing gear •...
  • Page 51 13. Engine Engine cowlings condition • Engine mount condition • Engine attachment check • (after burping the engine) Oil quantity check • Cooling liquid quantity check • Fuel and Electrical system visual check • Fuel system drain • Caution It is advisable to turn the propeller by hand with ignition off if the engine has been out of operation for a long time.
  • Page 52 15. Cockpit Ignition key - off • Master switch - on • Instruments check of condition • Fuel gauge fuel quantity check • Master switch - off • Controls - visual check • check for proper function check for play check for flap operation check for free movement up to the stops...

  • 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

    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. Check of free area - clear 8.

  • 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 2500 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 (CCCCIGAAR – Lights, Camera, Action) 1. Controls - check of free movement 2. Canopy -closed and locked 3. Choke - off 4. Cowl flap -open 5. Instruments - set and in the green 6. Gas - fuel valve on left tank 7.

  • Page 58: H O E N I X S - L S A G L I D E R

    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: Engine Extraction And Retraction

    8.2.4 Engine extraction and retraction 8.2.5 Best rate of climb For Rotax 912UL and VARIA 1.6 propeller the best rate-of-climb speed is 1000 feet/min. 1. Throttle - Max. continuous power (5 500 rpm) 2. Speed - 55 kts 3. Trim - adjust as needed to reduce stick pressure 4.

  • Page 60: Cruise

    6. Master switch - off 7. Fuel valve - off 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!

  • Page 61: Check Before Landing

    Check before landing – GPS-FUSTALL 1. Gas - fuel on left tank 2. Pump -fuel pump on 3. Straps -tight 4. Flaps -0° or +10° 5. Undercarriage - down 6. Speed - 60kts 7. Trim - adjust as required 8. Airbrakes - unlocked and operational 9.

  • 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: Information On Stalls, Spins And Any Other Usefull Pilot Info

    Information on stalls, spins and any other useful pilot info Recovery from unintentional spin and stall 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.

  • Page 65: Flight In Rain

    Flight in rain When flying in the rain, no additional steps are required. Airplane qualities and performance are not substantially changed. Feathering of the propeller 1. Shut off engine with ignition key (off position) Engine restarting Follow same engine start procedures as in 8.2.1 Caution After extended soaring flight, the engine could be cooled down.

  • Page 66: Airplane Ground Handling And Servicing

    Airplane Ground Handling and Servicing Airplane Ground Handling and Servicing........65 Servicing fuel, oil, coolant ............66 Towing and tie-down instructions ..........69 Date of Issue: 07/28/2010...

  • Page 67: Servicing Fuel, Oil, Coolant

    Servicing fuel, oil, coolant Fuel check 2 x wing fuel tanks (13.2 gal each, 26.4 gal total) are an integral part of the wings, and fuel quantity sensors are lo- cated inside the wings. In addition, a coarse filter, fuel valve, and fine filter are parts of the fuel system.
  • Page 68 Oil quantity check To service oil one person is required. Remove top cowling Make sure the ignition and both magnetos are OFF Open the oil tank cap Turn the prop 3-4 times counter- clockwise standing in the front of aircraft until burp is heard Check the level of the oil by the dipstick Oil level on land of dipstick Add oil if necessary –...
  • Page 69 Coolant quantity check To service the coolant one person is needed Remove the top cowling Open the cap of the coolant tank and add coolant to fill up the tank Make sure the ignition and both magnetos are OFF Turn the prop 3-4 times counter- clockwise standing in the front of aircraft Make sure that there is no air inside...

  • Page 70: 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 airplane is relatively low. Suitable surfaces to hold the airplane airframe are the rear part of the fuselage before the fin, wing roots, and cockpit forward frame.

  • Page 71: Tie-Down

    Tie-down The airplane is usually tied-down after a flight day or when needed. This is necessary to protect the airplane 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 72: Jacking

    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. It is neces- sary to dismantle airplane before loading to avoid damage to roadway signs.

  • Page 73: 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 gripping.
  • Page 74 • Wing Installation: Set the left wing on the pins and check automatic connection of control rods. Connect the fuel lines and fuel sensor. Then secure the rear auxiliary pin. Follow with the right wing, insert the wing in automatic connection device and secure the rear auxiliary pin.
  • Page 75 Insert the main eccentric pin, turn it 180 ° to tighten both halves of the wing together. Then secure the main pin with a bolt through the handle and at the rear with a safety pin. Check control system and fuel gauge function. Use an adhesive tape to cover the gap between the center section and the wing root.

  • Page 76: Airplane Disassembly

    Airplane Disassembly Follow the Assembly steps in reverse order. Date of Issue: 07/28/2010...
  • Page 77 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. Boating supply companies such as West Marine carry a large supply of cleaners and wax cleaners such as Maguiers which are designed for use on gel coat surfaces.

  • Page 78: 10.0 Required Placards And Markings

    10.0 Required Placards and Markings Required Placards and Markings ..........77 10.1 Airspeed indicator range markings ..........78 10.2 Operating limitations on instrument panel ........81 10.3 Passenger warnings..............81 10.4 No intentional spins ..............82 10.5 Empty weight ................82 10.6 Maximum takeoff weight............

  • Page 79: 10.1 Airspeed Indicator Range Markings

    10.1 Airspeed indicator range markings Airspeed indicator system calibration V IAS V CAS δ δ δ δ V [kts] [kts] [kts] -2.7 -1.6 -1.1 -0.5 Date of Issue: 07/28/2010...
  • Page 80 Airspeed limitations Airspeed limitations and their operational significance are shown below: Airspeed Remarks [kts] Never exceed Do not exceed this speed in speed any operation. Maximum Do not exceed this speed structural except in smooth air, and cruising speed then only with caution. Do not make full or abrupt control movement above Maneuvering...
  • Page 81 Airspeed indicator markings Airspeed indicator markings and their colour-code significance are shown below: Range or value Marking Significance [IAS kts] Green 42-96 Normal Operating Range Maneuvering must be con- Yellow 97-119 ducted with caution and only in smooth air. Maximum speed for all opera- tions.

  • Page 82: Operating Limitations On Instrument Panel

    10.2 Operating limitations on instrument panel See 10.3 and 10.4 for required instrument panel placards. 10.3 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.” is placed on co- pilot side of instrument panel.

  • Page 83: No Intentionall Spins

    10.5 Empty weight Empty weight …………………………………… ..708 lb 10.6 Maximum takeoff weight Maximum takeoff weight of U-15 Phoenix is 1320 lb. The follow- ing placard is to be placed in a visible area of the cockpit. Empty weight 708 lbs Never exceed 1320 lbs Max.

  • Page 84: Seat For Solo Operations Of Two Seated Gliders

    Max. weight of crew if…. ¼ fuel tank (6.9 gal) 576 lb ½ fuel tank (13.2 gal) 536 lb ¾ fuel tank (20 gal) 497 lb full fuel tank (26.5 gal) 458 lb 10.8 Allowable weight of the load in any luggage area The following placard is to be placed in the baggage area.

  • Page 85: 11.0 Supplementary Information

    11.2 Pilot operating advisories No any other pilot operating advisories. 12.0 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: 07/28/2010...

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