Shark UL Specifiche tecniche

Flight manual UL aircraft

FLIGHT MANUAL

UL airplane

SHARK.AERO s.r.o

SHARK.AERO CZ s.r.o.

Version: AFM Shark-EN 60_2017-05-17_final

created from Czech original version :

AFM_Shark-CZ_60_2017-04-22_certifikat.doc

Flight manual UL aircraft

Airplane Type / version:SHARK UL

Serial number:

Registration:

Date of issue:

LAA - Approval number and date:

ULL - 05 / 2013

1.3. 2013 / 20.12. 2016

Manufacturer –stamp and signature :

The airplane must be operated according to informations and

limitations presented in this handbook.

This handbook must be available to pilot at any time of the

flight.

Flight manual UL aircraft

LIST OF THE REVISIONS AND THE EPAIRS

Ordinal

No.

Number of

document -

bulletin

It concerns to pages No.

Date of

issue

Signature

1/13

2-1,2-2,2-6,2-9,

3-1 to 3-3, 3-6 to 3-8

4-1 to 4-11

5-1 to 5-5

6-2

7-8 to 7-10

appendix 3-3

format editing

5.3.2013

V.Pekár

2/13

2-6,2-7,6-1 to 6-7

15.3.2013

V.Pekár

3/13

2-6, 5-1,5-2,6-4,6-5,6-6

4.4.2013

V.Pekár

4/15

2-4, 2-6, 7-10, 7-18, 8-6

28.4.2015

J. Skočej

5/16

57-00

1-2,2-3,2-4,2-6, 3-6, 4-3,

4-7, 4-11,4-12, 5-2 to 5-6,

6-6, 7-1, 7-10, 7-11, 7-12,

7-14, 7-15, 7-18 to 7-27,

8-6

19.5.2016

V.Pekár

6/16

57-02

4-13

17.7.2016

V.Pekár

7/16

57-03

3-6 to 3-9, 5-2, 5-3, 7-1,

7-7, 7-14,7-19 to 7-29

22.8.2016

V.Pekár

8/16

57-04

4-15, 6-7 to 6-9

22.12.2016

V.Pekár

9/17

57-05

1-2, 2-1, 2-8, 2-9, 4-15,

6-2, 6-4, 6-5

1.2.2017

V.Pekár

10/17

57-06

Rewritten as a part of the

LAA type certification

requirements

1.4.2017

J.Dostál

Flight manual UL aircraft

Content

1. General........................................................................ 1-1

1.1. Introduction.................................................................. 1-1

1.2. Certification bases ....................................................... 1-1

1.3. Warnings, cautions and notes ..................................... 1-1

1.4. Airplane basic description............................................ 1-2

1.5. Three view drawing...................................................... 1-3

2. Limitations.................................................................... 2-1

2.1. Airspeed....................................................................... 2-1

2.2. Airspeed indicator markings ....................................... 2-1

2.3. analog airspeed indicator markings............................. 2-2

2.4. Engine.......................................................................... 2-3

2.5. Engine instrument marking.......................................... 2-4

2.6. Weight limits ................................................................ 2-5

2.7. Center of gravity (CG).................................................. 2-6

2.8. Approved maneuvers................................................... 2-6

2.9. Maneuvering load factor G .......................................... 2-6

2.10. Flight crew ................................................................... 2-6

2.11. Kind of operation.......................................................... 2-7

2.12. Fuel.............................................................................. 2-7

2.12.1. Approved fuel types..................................................... 2-7

2.12.2. Fuel tanks capacity...................................................... 2-7

2.13. Other limitations........................................................... 2-8

2.14. Placards ....................................................................... 2-9

3. Emergency procedures................................................ 3-1

3.1. Engine failure and emergency landing........................ 3-1

3.1.1. Engine failure during take-off run ................................ 3-1

3.1.2. Engine failure during take-off....................................... 3-1

3.1.3. In-flight engine failure .................................................. 3-2

3.1.4. Carburettor icing.......................................................... 3-2

3.2. In-flight engine restart.................................................. 3-2

3.3. Fire............................................................................... 3-3

3.3.1. Engine fire on the ground ............................................ 3-3

3.3.2. Engine fire during take-off............................................ 3-3

3.3.3. Engine fire in flight....................................................... 3-3

3.3.4. Cockpit / electrical fire.................................................. 3-4

3.4. Gliding.......................................................................... 3-4

3.5. Precautionary Landing................................................. 3-4

3.6. Blown-Out Tire Landing............................................... 3-4

3.7. Landing with Damaged Landing Gear......................... 3-5

3.8. Landing gear retraction malfunction............................ 3-5

3.9. Landing gear opening malfunction .............................. 3-5

3.10. Vibrations from engine or other engine problem ........ 3-6

Flight manual UL aircraft

3.11. Inadvertent icing encounter......................................... 3-6

3.12. Extreme turbulence encounter .................................... 3-6

3.13. Electrical system malfunctions .................................... 3-7

3.14. Inadvertent Stall and spin recovery............................. 3-8

3.14.1. Stall recovery............................................................... 3-8

3.14.2. Spin recovery............................................................... 3-8

3.15. USe of Rescue system................................................ 3-9

4. Normal procedures...................................................... 4-1

4.1. Pre-flight inspection..................................................... 4-1

4.1.1. Cockpit......................................................................... 4-1

4.1.2. Wing............................................................................. 4-2

4.1.3. Landing gear................................................................ 4-2

4.1.4. Powerplant................................................................... 4-2

4.1.5. Control cables.............................................................. 4-3

4.1.6. Tail unit and fuselage .................................................. 4-3

4.1.7. Turning on of electric devices...................................... 4-3

4.2. Engine starting............................................................. 4-3

4.2.1. Engine warm-up and test............................................. 4-4

4.3. Before taxiing............................................................... 4-4

4.4. Taxiing......................................................................... 4-6

4.5. Check on holding line .................................................. 4-6

4.6. normal take off............................................................. 4-7

4.7. Climb............................................................................ 4-7

4.8. Cruise .......................................................................... 4-8

4.9. Approach ..................................................................... 4-8

4.9.1. Descent........................................................................ 4-8

4.10. Downwind.................................................................... 4-9

4.11. Normal landing ............................................................ 4-9

4.11.1. On Base Leg................................................................ 4-9

4.11.2. On Final....................................................................... 4-9

4.11.3. Landing........................................................................ 4-9

4.11.4. After landing............................................................... 4-10

4.11.5. Engine shut down...................................................... 4-10

4.11.6. Post-Flight Check ...................................................... 4-10

4.12. Short field take-off and landing procedures.............. 4-10

4.13. Balked landing procedures........................................ 4-10

4.14. Fuel SYSTEM use..................................................... 4-11

4.15. REPEATED TAKE OFF............................................. 4-11

4.16. High speed flights...................................................... 4-12

4.16.1. Turbulences............................................................... 4-12

4.16.2. Maneuvering.............................................................. 4-12

4.16.3. Landing gear opening................................................ 4-12

4.16.4. Propeller, engine RPM .............................................. 4-13

Flight manual UL aircraft

4.16.5. Flaps.......................................................................... 4-13

4.16.6. Landing gear retraction.............................................. 4-13

4.16.7. Flutter, high altitude flights......................................... 4-13

5. Performance................................................................ 5-1

5.1. Airspeed indicator system calibration.......................... 5-1

5.2. Stall speed................................................................... 5-2

5.3. TAKE-OFF Distance.................................................... 5-2

5.3.1. In flight adjustable prop. NEUFORM TXR2-V-70....... 5-2

5.3.2. In flight adjustable prop. Woodcomp SR3000/2WN.... 5-3

5.3.3. On ground adjustable prop. DUC SWIRL 1680........... 5-3

5.4. Landing distance.......................................................... 5-4

5.5. Rate of climb................................................................ 5-4

5.6. Cruise, endurance, range............................................ 5-5

6. Airplane empty weight and COG determination.......... 6-1

6.1. Weight and center of gravity determination for flight.. 6-3

7. Technical Description of the airplane .......................... 7-1

7.1. AIRFRAME .................................................................. 7-2

7.1.1. Fuselage...................................................................... 7-2

7.1.2. Cockpit canopy............................................................ 7-2

7.1.3. Engine cowlings........................................................... 7-2

7.1.4. Wing............................................................................. 7-3

7.1.5. Ailerons........................................................................ 7-3

7.1.6. Flaps............................................................................ 7-3

7.1.7. Horizontal stabilizer ..................................................... 7-3

7.1.8. Elevator........................................................................ 7-3

7.1.9. Rudder......................................................................... 7-3

7.1.10. Airplane exterior surface painting................................ 7-4

7.2. Landing gear................................................................ 7-4

7.2.1. Front undercarriage..................................................... 7-4

7.2.2. Main undercarriage...................................................... 7-5

7.2.3. Undercarriage retraction and extension ...................... 7-6

7.3. CONTROL SYSTEMS................................................. 7-8

7.3.1. Elevator control............................................................ 7-8

7.3.2. Aileron control.............................................................. 7-8

7.3.3. Rudder control............................................................. 7-9

7.3.4. Flaps............................................................................ 7-9

7.3.5. Elevator trim tab control............................................... 7-9

7.4. ELECTRIC SYSTEM................................................. 7-10

7.5. Fuel system ............................................................... 7-10

7.6. COCKPIT - interior and instruments.......................... 7-12

7.7. POWER UNIT.............................................................. 7-16

7.7.1. Technical data ........................................................... 7-17

7.8. PROPELLER ............................................................. 7-18

Flight manual UL aircraft

7.8.1. DUC SWIRL 3 blade, on the ground adjustable

propeller, diameter 1680 mm..................................... 7-18

7.8.2. Woodcomp SR 3000 2W two blade in flight electrically

adjustable propeller ................................................... 7-19

7.8.3. Woodcomp KW 20W - two blade hydraulically in flight

adjustable .................................................................. 7-20

7.8.4. Neuform TXR2-V-70.................................................. 7-21

7.9. Rescue system.......................................................... 7-22

7.9.1. Description of rescue system Stratos/Junkers Magnum

501............................................................................. 7-22

7.9.2. The activation mechanism......................................... 7-23

7.9.3. Rescue system installation........................................ 7-24

7.10. Towing system........................................................... 7-25

7.11. Position lights............................................................. 7-26

7.12. Landing Light............................................................. 7-26

7.13. ELT Unit..................................................................... 7-27

7.14. Autopilot..................................................................... 7-28

8. Airplane handling, care and maintenance................... 8-1

8.1 Wing Dismounting ....................................................... 8-1

8.1.1. Remove flaps............................................................... 8-1

8.1.2. Disconnect aileron controls ......................................... 8-2

8.1.3. Disconnect rear wing spar pin..................................... 8-2

8.1.4. Disassemble the main wing spar pins......................... 8-2

8.1.5. Disconnect fuel hoses and fuel sensors sockets......... 8-3

8.1.6. Remove wing spars out of center-wing....................... 8-3

8.1.7. Disconnect pitostatic system hoses ............................ 8-3

8.1.8. Secure wings by hangaring (transport) jigs................. 8-3

8.2. Stabilizer disassembly................................................. 8-3

8.3. Parking and mooring ................................................... 8-4

8.3.1. General........................................................................ 8-4

8.3.2. Cover of pitot tube ....................................................... 8-4

8.3.3. Mooring........................................................................ 8-4

8.4. Hangaring, Ground Handling....................................... 8-5

8.5. Towing......................................................................... 8-6

8.6. Tire pressure................................................................ 8-6

9. Supplements................................................................ 9-1

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