AIRCRAFT ASSEMBLY MANUALCR-AAM-1-0-00 . Revision No.: - Date of issue: 2011-03-01 1 - 10 . 13. Slip wing into fuselage. Do not pinch wires / hoses between fuselage to wing cover and

CR-AAM-1-0-00 PS-28 Cruiser

SportCruiser

Revision No.: 1 i Date of issue: 2019-01-11

PS-28 Cruiser / SportCruiser

AIRCRAFT ASSEMBLY MANUAL

Copy No.:

PS-28 Cruiser

SportCruiser

CR-AAM-1-0-00

Date of issue: 2019-01-11 ii Revision No.: 1

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SportCruiser

Revision No.: 1 iii Date of issue: 2019-01-11

PS-28 Cruiser / SportCruiser

AIRCRAFT ASSEMBLY

MANUAL

PPSS--2288 CCrruuiisseerr // SSppoorrttCCrruuiisseerr aaiirrccrraafftt iiss ddeessiiggnneedd aanndd mmaannuuffaaccttuurreedd bbyy

Czech Sport Aircraft a. s.. Na Záhonech 212, 686 04 Kunovice

Czech Republic

www. czechsportaircraft.com; [email protected] Fax: +420 576 519 394, Phone: +420 576 514 034 (Sales Dept.)

PS-28 Cruiser

SportCruiser

CR-AAM-1-0-00

Date of issue: 2019-01-11 iv Revision No.: 1

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SportCruiser RECORD OF REVISIONS

Date of issue: 2019-01-11 Revision No.: 1 0 - 1

Rev.No. Revision name Changed pages Issue date

Date and signature

1

Updated pictures, descriptions of pictures and list of the hardware. Information about torque moments added.

i to iv RoR: 0-1, LoEP: 0-1, 1-1, 1-4, 1-6, 1-7, 1-11

2019-01-11 2019-01-11 Konečný

PS-28 Cruiser

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CR-AAM-1-0-00

RECORD OF REVISIONS

Revision No.: - Date of issue: 2011-03-01 0 - 2

Rev.No. Revision name Changed pages Issue date

Date and signature


SportCruiser LIST OF EFFECTIVE PAGES

Date of issue: 2019-01-11 Revision No.: 1 0 - 1

Chapter Page Date Chapter Page Date

Title i 2019-01-11

Page ii 2019-01-11

iii 2019-01-11

iv 2019-01-11

RoR 0-1 2019-01-11

RoR 0-2 2011-03-01

LoEP 0-1 2019-01-11

LoEP 0-2 2011-03-01

1 1-1 2019-01-11

1-2 2011-03-01

1-3 2011-03-01

1-4 2019-01-11

1-5 2011-03-01

1-6 2019-01-11

1-7 2019-01-11

1-8 2011-03-01

1-9 2011-03-01

1-10 2011-03-01

1-11 2019-01-11

1-12 2011-03-01

1-13 2011-03-01

1-14 2011-03-01

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LIST OF EFFECTIVE PAGES

Revision No.: - Date of issue: 2011-03-01 0 - 2

Chapter Page Date Chapter Page Date


SportCruiser

Date of issue: 2019-01-11 Revision No.: 1

1 - 1

Procedure of aircraft assembly:

Carefully remove aircraft from the container and unpack it.

Place fuselage on the flat suitable place for assembly (take into consideration aircraft dimension).

Hardware for installation (bolts, nuts, washers, cotter pins and cable ties) is located in the paper box or plastic bag in the cockpit.

Tools are not delivered with the aircraft.

Do not use force while connecting parts.

For bolt joints the following torque moments shall be used (see AC 43x13-1B - Chapter 7-40, page 7-9):

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Hardware for wheel fairings installation

1.....Bolt AN525-10R7 Front part of nose wheel fairing

2.....Bolt AN525-10R9 Rear part of nose wheel fairing

3.....Bolt AN525-10R9 Right main wheel fairing

4.....Bolt AN525-10R9 Left main wheel fairing

5….Washer SG0029N below by all the bolt

A.....Phillips screwdriver No.2


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Date of issue: 2011-03-01 Revision No.: -

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A/ Wheel fairings installation

1. Prepare the front wheel fairing.

2. Prepare main wheels fairings.

3. Screw the rear part of the nose wheel fairing.

4. Screw the front part of the nose wheel fairing.

5. Screw the inner side of the left main wheel fairing (repeat it for the right wheel fairing).

6. Screw the outer side of the left main wheel fairing (repeat it for the right wheel fairing).

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Hardware for stabilizer installation

1.....Bolt AN4-5A Rear stabilizer suspension

2.....Washer AN960-416 Rear stabilizer suspension

3.....Nut AN365-428 Rear stabilizer suspension

4.....Bolt AN174-10A Connection elevator control rod with lever

5.....Washer AN960-416L Connection elevator control rod with lever

6.....Nut AN365-428 Connection elevator control rod with lever

7.....Bolt MS35207-245 Stabilizer fairing

8.....Bolt MS35207-245 Rear cover of fuselage

9.....Cable tie 100mm Connector

10...Cable tie 200mm Cable

A.....Nippers

B.....Phillips screwdriver No.2

C.....Aluminum hammer

D.....Wrench No.7/16“


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B/ Stabilizer installation

1. For stabilizer installation are requested three persons.

2. Rear part of fuselage with suspension pins prepared for stabilizer installation. Lubricate the pins with grease.

3. Front part of the stabilizer with holes for suspension pins.

4. Stabilizer bottom side with trim tab control connector and rear suspensions.

5. Turn rudder up to stop to left or right position during stabilizer installation.

6. Two persons hold stabilizer and slip it on two pins on the rear part of the fuselage. Slip stabilizer up to stop.

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7. Insert bolt into rear suspension, slip washer and screw nut. Repeat it for the right side. Tighten nuts of both suspensions.

8. Interconnect connector and secure it with tightening strips.

9. Tight cable to the right suspension with cable tie.

10. Connect elevator control rod and tighten nut. Bolt head is on the left side with flight direction. Washer is on the nut side.

11. Install rear cover of the fuselage. The lower bolt screw at first.

12. Screw stabilizer fairing.


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Hardware for wing installation

1.....Bolt AN5-21A Fuselage center section

2.....Washer AN960-516 Fuselage center section

3.....Nut AN365-524 Fuselage center section

4.....Nut AN365-428 Aileron control rod

5.....Washer AN960-416L Aileron control rod

6.....Bolt AN4-7A Aileron control rod

7.....Nut AN365-524 Rear wing suspension

8......Washer AN960-516 Rear wing suspension

9......Bolt AN5-5A Rear wing suspension

10.....Bolt MS35207-243 Rear wing suspension cover

11.....Bolt AN525-10R7 Cover under seat

12.....Cable tie 100mm Connector

13.....Hose clamp 9-15 Fuel hose

A.....Nippers D.....Flat tip screwdriver

B.....Aluminum hammer E.....Wrench No.1/2“

C.....Phillips screwdriver No.2 F.....Wrench No.7/16“

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C/ Wings installation

1. For wings installation are requested at least three persons. If you have no supports additional person is necessary for wing assembly.

2. Lay down the wings on suitable (soft) supports. The support must be situated under the wing rib (to avoid damage of the skin).

3. The ideal distance between the wing and the fuselage for easy connection of all hoses and wirings is about 30cm (12inches).

4. Connect fuel hoses. On the left wing is situated the vapor return line. Connect the same marked hoses.

5. Fuel hoses secure with hose clamps.

6. Connect hoses of the pitot static system in the left wing. Connect the hoses marked “S” together. As well as for “T” marked hoses.


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7. Secure it with cable tie.

8. Connect wiring of the position light and connect fuel sender wiring. Connect aileron trim tab wiring (in the right wing only).

9. Secure all connectors with cable tie.

10. After making all connections on left side check all systems (NAV/STROBE lights, left fuel indicator by switching on Master, Instrument and Avionics switch) are operating properly.

11. After making all connections on right side check all systems (NAV/STROBE lights, right fuel indicator by switching on Master, Instrument and Avionics switch, Aileron trim tab by buttons on control stick) are operating properly.

12. Flaps secured in closed (cruise) position with cable tie.

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13. Slip wing into fuselage. Do not pinch wires / hoses between fuselage to wing cover and wing. Watch out for damaging the wing fairings

14. Rear wing suspension must be in front of the rear fuselage suspension.

15. Insert flap drive pin to the flap slot during wing to fuselage slipping.

16. While assembling the left wing move the control stick to right stop. Repeat it for right wing.

17. Use the special tools for secure the connection of wing with fuselage centre section. Use two for upper line of bolts and at least one for the lower line.

18. Before rear suspension bolting removes the flap securing cable tie and set flap into down position.


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19. Install bolt, washer and nut into rear suspension and screw it to rear wing spar by hand. Bolt head must be oriented opposite to the flight direction. Tighten it by socket wrench.

20. The rear wing suspension cover with bolts. Shorter one is for the hole next to flap.

21. Install rear suspension attachment covers.

22. Connect pull rods of the ailerons behind the seats and tighten nuts. Bolt head must be oriented opposite to the flight direction.

23. Insert bolts into remaining holes. Slip one washer on the less protruding bolt and two washers on the other bolts and screw nuts on all bolts.

24. Tighten all nuts.

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25. Check space behind seats for lost things and tools.

26. Check space under seats for lost things and tools.

27. Install the cover of the access hole under the seat.

28. Insert seats to the cockpit.


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Assembled PIPERSPORT aircraft

Recommendation:

After aircraft assembly check control surfaces deflections and proper function of all aircraft control system. Also fuel system tightness test and pitot-static system leak test should be done. Short engine test is also highly recommended.

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Documents

AIRCRAFT ASSEMBLY MANUALCR-AAM-1-0-00 . Revision No.: - Date of issue: 2011-03-01 1 - 10 . 13. Slip wing into fuselage. Do not pinch wires / hoses between fuselage to wing cover and