copert - alto-912. de

P92-J ILLUSTRATED

PARTS CATALOGUE REV. 1 – NOV. 2008

COSTRUZIONI AERONAUTICHE

TECNAM s.r.l.

COSTRUZIONI AERONAUTICHE TECNAM s.r.l.

P92-J P A R T S C A T A L O G

INTRODUCTION

ISSUED: November 2008

INTRODUCTION This illustrated Parts Catalog describes the spare parts concerning the P92 J aircraft ,manufactured by TECNAM S.r.l. di Casoria (NA) ITALY. 1) This illustrated Parts Catalog is divided into eight sections: - SECTION 1 - WING - SECTION 2 - FUSELAGE - SECTION 3 - TAIL SURFACES - SECTION 4 - LANDING GEAR - SECTION 5 - FLIGHT CONTROLS - SECTION 6 - POWER PLANT - SECTION 7 - SYSTEMS - SECTION 8 - FURNISHING 2) Enumeration is arranged in the following columns: a) “FIGURE & INDEX NO.” column. It includes the figure number and the index

numbers of the spare parts illustrated in the figure. b) "PART NUMBER (P/N)" column. It includes the number assigned to the spare

parts by the manufacturer, which have to be reported in the provisioning inquiries.

c) "NOMENCLATURE" column. It includes a brief description of the parts. d) "QUANTITY FOR ASSY" column. It includes the number showing the quantity

of each item illustrated on the figure to which the enumeration refers. e) "EFFECTIVITY CODE" column. It includes the codes assigned to the

production series having a different configuration or different P/N.

pag. I



INTRODUCTION


When no indication appears, it is recognized that the part can be used for any N.C. and that it maintains its inherent function regardless of any possible modification introduced during the manufacturing process.

3) Attachment parts, i.e. bolts, nuts, screws, etc., or parts that are available on the market are generally not supplied by Tecnam.

The catalog conveniently reports some of these parts identifying them by their

commercial code.

pag. II



INTRODUCTION


HOW TO IDENTIFICATE A "PART" IF YOU KNOW THE ASPECT AND WHERE IS LOCATED.

1) Refer to fig. 1 at page VII and determine the section in which the part is used. 2) Refer to the index (pag. IV , VI) and identify the section. Choose, among the figures describing the various subgroups, the one that

possibly contains the part to be identified and refer to the appropriate page. 3) Find the part on the drawing and write down the index number. NOTE: If the part cannot be found on the above mentioned drawing, pick a

different drawing from the same SECTION. 4) Refer to part-list “DRAWING” for a complete description of the part.

HOW TO ORDER PARTS Use the following procedure to order replacements: 1) Always specify the airplane manufacturing number. 2) Always specify P/N (Part Number), name and quantity required.

pag. III



INTRODUCTION


INDEX Figure Figure Page Number Title 1 Exploded view VII SECTION 1 - WING 1.1 Wing structure assembly 1-1 1.2 Wing box assembly 1-5 1.3 Leading edge and strut 1-7 1.4 Flap assembly 1-10 1.5 Aileron assembly 1-12 SECTION 2 - FUSELAGE 2.1 Aft fuselage assembly 2-1 2.2 Cabin structure 2-3 2.3 Fuselage skin installation 2-5 2.4 Cabin skin installation 2-8 2.5 Doors installation 2-11 2.6 Windows installation 2-14 SECTION 3 - TAIL SURFACES 3.1 Stabilator assembly 3-1 3.2 Fin assembly 3-4 3.3 Rudder assembly 3-6

pag. IV



INTRODUCTION


Figure Figure Page Number Title SECTION 4 - LANDING GEAR 4.1 Nose landing gear 4-1 4.2 Fairing - nose wheel 4-4 4.3 Main landing gear 4-6 SECTION 5 - FLIGHT CONTROLS 5.1 Stick installation 5-1 5.2 Aileron control installation 5-3 5.3 Flap control installation 5-6 5.4 Rudder control installation 5-8 5.5 Stabilator control installation 5-10 5.6 Elevator trim control installation 5-12 SECTION 6 - POWER PLANT 6-1 Power plant installation 6-1 6-2 Engine exhaust installation 6-3 6-3 Engine cowling installation 6-5 SECTION 7 - SYSTEMS 7.1 Fuel system 7-1 7.2 Brake system 7-4 7.3 Pitot and static press. system 7-6 7.4 Vacuum system 7-8 7.5 Throttle system control 7-10 7.6 Electric components 7-12

pag. V



INTRODUCTION


Figure Figure Page Number Title SECTION 7 - SYSTEM 7.7 Instruments panel installation 7-15 7.8 Heating system installation 7-18 7.9 Oil cooler system installation 7-20 7.10 Water cooler system installation 7-22 SECTION 8 - FURNISHING 8.1 Cabin interior finishing 8-1

pag. VI



INTRODUCTION


1

2

7

3

1

5

8

6

4

SECTION 1 - WING SECTION 2 - FUSELAGE SECTION 3 - TAIL SURFACES SECTION 4 - LANDING GEAR SECTION 5 - FLIGHT CONTROLS SECTION 6 - POWER PLANT SECTION 7 - SYSTEMS SECTION 8 - FURNISHING

Fig. 1 EXPLODED VIEW

pag. VII



INTRODUCTION


LIST OF EFFECTIVE PAGES

Rev. N.

PAGE DATE AMENDMENT

1 1

7-20 7-21

14/11/08 14/11/08

Definition of 3 assy on oil cooler system installation Definition of 3 assy on oil cooler system installation

pag. VIII



SECTION 1

WING

Fig. NO. P/N NOMENCLATURE Q.ty

assyEFF.

CODE


WING STRUCTURE ASSEMBLY

92-1-002-001 Wing structure assembly - Left 1

92-1-002-002 Wing structure assembly - Right 1

1 92-1-007-001 Spar assembly - front, left 1

92-1-007-002 Spar assembly - front, right 1

2 92-1-007-003 Spar assembly - rear, left 1

92-1-007-004 Spar assembly - rear, right 1

92-1-701-1 Web spar - front root, right 2

3 92-1-701-2 Web spar - front root, left 2

92-1-701-3 Web spar - front center, right 2

4 92-1-701-4 Web spar - front center, left 2

92-1-701-5 Web spar - front tip, right 2

5 92-1-701-6 Web spar - front tip, left 2

6 92-1-702-1 Doubler - Front spar attachment, center 2

7 92-1-702-2 Doubler - Front spar attachment, root 2

8 92-1-704-1 Angle - front spar, external 8

9 92-1-705-1 Stiffener 2

10 92-1-705-2 Spacer “L” 2

11 92-1-705-3 Plate with hole 2

12 92-1-705-4 Spacer 2

13 92-1-708-1 Stiffener - reinforcement, center 4

14 92-1-708-2 Angle - reinforcement, bottom 2

15 92-1-708-4 Angle - reinforcement, top 2

16 92-1-711-1 Channel - attachment strut, internal 2

17 92-1-714-2 Channel - attachment strut, external 2

18 UNI 5931 Bolt M4 cr8.8 L=62 mm 2

pag. 1-2



SECTION 1

WING


assyEFF.

CODE



19 92-1-712-2 Angle - center 2

20 92-1-711-2 Spacer - center 2

21 92-1-707-2 Web spar - rear, root 2

22 92-1-707-4 Web spar - rear, center 2

23 92-1-707-6 Web spar - rear, tip 2

24 92-1-703-1 Doubler - rear spare 4

25 92-1-708-3 Stiffener - rear spar reinforcement 4

26 92-1-706-2 Plate - wing attachment 4

27 92-1-709-1 Spacer - wing attachment (trapezoid.) 2

28 92-1-705-4 Spacer - wing attachment (rectangular) 2

29 92-1-710-2 Reinforcement - rear wing attachment 2

30 92-1-104-1 Bulkhead - root side 2

31 92-1-104-2 Bulkhead - aileron control attachment, right 1

92-1-104-3 Bulkhead - aileron control attachment, left 1

32 92-1-104-4 Bulkhead - tip side 2

33 92-1-107-1 Rib - 1 hole, left 1

92-1-107-2 Rib - 1 hole, right 1

34 92-1-108-1 Rib - 4 holes, left 4

92-1-108-2 Rib - 4 holes, right 4

35 92-1-109-1 Rib - 5 holes, left 8

92-1-109-2 Rib - 5 holes, right 8

36 92-1-110-1 Rib - 3 holes, left 1

92-1-110-2 Rib - 3 holes, right 1

37 92-1-103-1 Plate - flap/aileron attachment 8

38 92-1-103-2 Hinge 8

pag. 1-3



SECTION 1

WING


assyEFF.

CODE



39 92-1-706-1 Plate - strut attachment 4

40 92-1-706-2 Plate - wing attachment 8

41 92-1-115-1 Plate - bottom, attachment lever, right 1

92-1-115-2 Plate - bottom, attachment lever, left 1

42 92-1-116-1 Plate - top, attachment lever, right 1

92-1-116-2 Plate - top, attachment lever, left 1

43 92-1-714-2 Spacer - plate attachment, internal right 1

92-1-714-1 Spacer - plate attachment, internal left 1

44 92-1-712-2 Spacer - plate attachment, external right 1

92-1-712-1 Spacer - plate attachment, external left 1

45 92-1-118-1 Stop - aileron travel 1

46 UNI 5739 Bolt M8 cr8.8 L=25 mm 4

47 UNI 6592 Washer d=8 4

48 UNI 7473 Self locking nut M8 4

49 UNI 5931 Bolt M6 cr8.8 L=62 mm 6





pag. 1-4



SECTION 1

WING


assyEFF.

CODE


WING BOX ASSEMBLY

1 92-1-111-1 Skin - top/root, left 1

92-1-111-2 Skin - top/root, right 1

2 92-1-111-3 Skin - top/center, left 1

92-1-111-4 Skin - top/center, right 1

3 92-1-111-5 Skin - top/tip, left 1

92-1-111-6 Skin - top/tip, right 1

4 92-1-111-7 Skin - bottom/root 2

5 92-1-111-8 Skin - bottom/center 2

6 92-1-111-9 Skin - bottom/tip 2

7 92-1-117-1 Nose - bottom skin 8

8 92-1-119-1 Cover - aileron lever access 2

9 92-1-310-1 Tip, left 1

92-1-310-2 Tip, right 1

10 UNI 6954 Screw self tapping L=13 mm 8

11 NAS 395 Nut “U” type M4 8

pag. 1-6



SECTION 1

WING


assyEFF.

CODE


WING LEADING EDGE and STRUT

1 92-1-009-001 Fuel tank, left 1

92-1-009-002 Fuel tank, right 1

2 92-9-220-000 Cap cover assembly - fuel tank access 2

92-1-003-001 Leading edge assembly, left 1

92-1-003-002 Leading edge assembly, right 1

3 92-1-300-1 Rib, left 11

92-1-300-2 Rib, right 11

4 92-1-301-1 Skin - root side, left 1

92-1-301-2 Skin - root side, DX 1

5 92-1-301-3 Skin - tip side, left 1

92-1-301-4 Skin - tip side, right 1

6 92-1-302-1 Stringer - root side 2

7 92-1-302-2 Stringer - center 2

8 92-1-302-3 Stringer - tip side 2

9 92-1-301-5 Cover - strut attachment access 2

92-1-011-001 Strut assembly, left 1

92-1-011-002 Strut assembly, right 1

10 92-1-880-1 Streamline strut tubing 2

11 92-1-845-000 Wing attachment fitting 2

12 92-1-840-000 Fuselage attachment fitting 2

13 UNI 5737 Bolt M8 cr8.8 L=75 mm 2



16 UNI 5737 Bolt M8 cr8.8 L=65 mm (fil. L=25 mm) 2


pag. 1-8



SECTION 1

WING


assyEFF.

CODE


WING LEADING EDGE and STRUT


19 92-9-502-1 Ground lead, cap filler tank 2

92-1-200-1 Fairing - upper, left - (Opt.) 1

20 92-1-200-2 Fairing - upper, right - (Opt.) 1

92-1-200-3 Fairing - lower, left - (Opt.) 1

21 92-1-200-4 Fairing - lower, right - (Opt.) 1

pag. 1-9



SECTION 1

WING


assyEFF.

CODE


FLAP ASSEMBLY

92-1-006-001 Flap assembly, left 1

92-1-006-002 Flap assembly, right 1

1 92-1-600-001 Rib with hinge, left 1

92-1-600-002 Rib with hinge, right 1

2 92-1-401-1 Rib, extremity left 1

92-1-401-2 Rib, extremity right 1

3 92-1-402-1 Rib 12

4 92-1-403-1 Nose - rib 4

5 92-1-404-1 Spar 2

6 92-1-601-1 Hinge 2

7 92-1-406-1 Skin 8

8 92-1-407-1 Hinge, MS20001-4 4

9 92-1-407-2 Spacer 4

10 92-1-408-1 Skin, leading edge 2

11 92-1-408-2 Skin, trailing edge 2

12 92-1-410-5 Angle, reinforcement hinge side, left 1

92-1-410-6 Angle, reinforcement hinge side, right 1

13 92-1-410-3 Angle, reinforcement, left 1

92-1-410-4 Angle, reinforcement, right 1

pag. 1-11



SECTION 1

WING


assyEFF.

CODE


AILERON ASSEMBLY

92-1-004-001 Aileron assembly, left 1

92-1-004-002 Aileron assembly, right 1

1 92-1-400-001 Rib with hinge, left 1

92-1-400-002 Rib with hinge, right 1

2 92-1-401-1 Rib, extremity left 1

92-1-401-2 Rib, extremity right 1

3 92-1-402-1 Rib 12

4 92-1-403-1 Nose - rib 4

5 92-1-404-1 Spar 2

6 92-1-405-1 Hinge 2

7 92-1-406-1 Skin 8

8 92-1-407-1 Hinge, MS20001-4 4

9 92-1-407-2 Spacer 4

10 92-1-408-1 Skin, leading edge 2

11 92-1-408-2 Skin, trailing edge 2

12 92-1-410-1 Angle, reinforcement hinge side, left 1

92-1-410-2 Angle, reinforcement hinge side, right 1

13 92-1-410-3 Angle, reinforcement, left 1

92-1-410-4 Angle, reinforcement, right 1

14 92-1-409-1 Strip, left 1

92-1-409-3 Strip, right 1

15 92-1-409-2 Sheet - adjustable trim 1

pag. 1-13



SECTION 2 FUSELAGE


assyEFF.

CODE


AFT FUSELAGE ASSEMBLY

92-3-004-000 Aft fuselage assembly 1

1 92-3-410-000 Frame assembly No. 1 1

2 92-3-420-000 Frame assembly No. 2 1

3 92-3-430-1 Frame No. 3 1

4 92-3-440-1 Frame No. 4 1

5 92-3-450-1 Frame No. 5 1

6 92-3-500-1 Stiffener, left 1

7 92-3-500-2 Stiffener, right 1

8 92-3-510-4 Channel - reinforcement 2

9 92-3-520-1 Angle 2

10 92-3-520-2 Bracket - stabilator rod control 1

11 92-3-530-1 Hinge stabilator, left 1

12 92-3-530-2 Hinge stabilator, right 1

13 92-3-530-3 Bearing SKF GE10 E 2

14 92-3-531-1 Bushing 4

15 92-3-440-2 Stiffener on frame 4 1

16 92-3-440-3 Reinforcement on frame 4 1

17 Grommet d=48 mm 1

18 UNI 5739 Bolt M4 cr8.8 L=20 mm 8



pag. 2-2



SECTION 2 FUSELAGE


assyEFF.

CODE


CABIN STRUCTURE

1 92-2-008-000 Cabin structure assembly 1

2 92-11-942-000

Firewall assembly 1

3 92-11-941-1 Plate - reinforcement 1

4 92-11-942-2 Angle, right 1

5 92-11-942-3 Angle, left 1

pag. 2-4



SECTION 2 FUSELAGE


assyEFF.

CODE


FUSELAGE SKIN INSTALLATION

1 92-3-460-1 Skin - front, left 1

2 92-3-460-2 Skin - front, right 1

3 92-3-460-3 Skin - rear, left 1

4 92-3-460-4bis Skin - rear, right (batt. access) 1

5 92-3-460-5 Skin - top, front 1

6 92-3-460-6 Skin - top, center 1

7 92-3-460-7 Skin - top, rear 1

8 92-3-460-8 Skin - bottom, front 1

9 92-3-460-9 Skin - bottom, center 1

10 92-3-460-10 Skin - bottom, rear 1

11 92-3-510-5 Stringer - skin reinforcement, left 3

12 92-3-510-6 Stringer - skin reinforcement, right 2

13 92-3-510-7 Stringer - skin reinforcement with batt. access 1

14 92-3-510-8 Stringer - lower skin 2



17 92-3-511-1 Stringer - lower tail skin 1

18 92-3-511-2 Stringer- lower tail skin 1

19 92-3-511-3 Stringer - lower tail skin 1

20 92-1-119-1 Cover - inspection hole 2

21 92-3-510-2 Stiffener - side skin 2

22 92-3-510-3 Stiffener - side skin 2

23 92-3-540-000 Box assembly - battery 1

24 92-3-542-000 Drain tube assembly 1

25 92-3-541-000 Adapter - battery vent 1

pag. 2-6



SECTION 2 FUSELAGE


assyEFF.

CODE


FUSELAGE SKIN INSTALLATION

26 92-3-543-000 Adapter - battery vent 1

27 Clamp - Serflex 12-20 2

28 Hose L=700 mm - d=12.8 mm 1

29 92-3-540-3 Cover - access battery box 1

30 92-3-540-4 Hinge - tail side 1

31 92-3-540-5 Hinge - cover side 1

32 92-3-540-6 Pin 1

33 92-9-909-1 Tail spring 1

34 92-3-540-1 Fairing - tail fuselage 1

35 92-3-544-1 Spacer - fin attachment 1

36 92-2-114-2 Spacer - tail attachment 2

37 92-3-461-1 Ring - flap hole reinforcement 1




41 UNI 5739 Bolt M6 cr8.8 L=20 mm 2



44 UNI 7688 Bolt M4 L=12 mm 7

45 Anchor nut M4 7

pag. 2-7



SECTION 2 FUSELAGE


assyEFF.

CODE


CABIN SKIN INSTALLATION

1 92-2-100-1 Skin - side left 1

92-2-100-2 Skin - side right 1

2 92-2-101-1 Skin - side left 1

92-2-101-2 Skin - side right 1

3 92-2-122-1 Skin - side lower left 1

92-2-122-2 Skin - side lower right 1

4 92-2-122-3 Skin - side upper left 1

92-2-122-4 Skin - side upper right 1

5 92-2-102-3 Skin - window, left 1

92-2-102-4 Skin - window, right 1

6 92-2-100-3 Skin - upper cockpit 1

7 92-2-123-1 Angle - panel reinforcement 1

8 92-2-124-1 Channel - reinforcement 1

9 92-2-103-1 Skin - floor, aft 1

10 92-2-103-2 Skin - floor, rear 1

11 92-2-104-1 Stiffener - floor 3

12 92-2-104-2 Stiffener - floor 1

13 92-2-106-2 Channel - upper skin reinforcement 2

14 92-2-106-1 Top skin 1

15 92-2-112-1 Rubber seal 2

16 92-2-110-1 Hole - outer reinforcement 2

17 92-2-110-2 Hole - inner reinforcement 2

18 92-2-125-1 Plate door, left 1

92-2-125-2 Plate door, right 1

19 92-9-906-2 Bracket - spring attachment, right 1

pag. 2-9



SECTION 2 FUSELAGE


assyEFF.

CODE


CABIN SKIN INSTALLATION

20 92-2-906-1 Bracket - spring attachment, left 1

21 92-5-906-1 Plate guard, left 2

22 92-5-906-2 Plate guard, right 1

23 92-5-906-3 Plate in Lexan, left 1

24 92-5-906-4 Plate in Lexan, right 2

25 92-2-104-5 Bracket - floor panel 2

26 92-2-104-4 Bracket - lateral panel 2

27 92-2-111-1 Plate with ashlar 2

28 92-12-609-1 Stinger - lateral carpet 2


30 92-1-105-1 Track - cover cockpit, left 1

92-1-105-2 Track - cover cockpit, right 1

31 92-2-114-5 Spacer for lateral panel 2

pag. 2-10



SECTION 2 FUSELAGE


assyEFF.

CODE


DOORS INSTALLATION

92-2-002-001 Door assembly, left 1

92-2-002-002 Door assembly, right 1

1 92-2-200-1 Door - structure, left 1

92-2-200-2 Door - structure, right 1

2 92-2-201-1 Hinge - half, door element 2

3 92-2-201-2 Hinge - half, cabin element 2

4 92-2-113-3 Spacer for hinge 2

5 92-2-201-3 Pin 2

6 92-2-301-1 Skin - outer, left 1

92-2-301-2 Skin - outer, right 1

7 92-2-301-7 Window in Lexan, left 1

92-2-301-8 Window in Lexan, right 1

8 92-2-203-1 Air intake - cabin ventilation 2

9 92-2-301-3 Molding - upper, left 1

92-2-301-4 Molding - upper, right 1

10 92-2-301-5 Molding - lower, left 1

92-2-301-6 Molding - lower, right 1

11 92-2-301-8 Upholstery panel with pocket, left 1

92-2-301-9 Upholstery panel with pocket, right 1

12 92-9-910-1 Safety lock in Teflon 2

13 92-2-304-1 Plate for safety lock 2

14 92-2-303-1 Retainer - window, left 1

92-2-303-2 Retainer - window, right 1

15 92-2-303-3 Retainer - window 2


pag. 2-12



SECTION 2 FUSELAGE


assyEFF.

CODE


DOORS INSTALLATION


18 92-2-303-6 Rib - door molding, left 1

92-2-303-7 Rib - door molding, right 1

19 92-2-302-3 Handle - door 2

20 92-2-304-1 Plate 2

21 92-9-905-1 Pin 2

22 92-9-911-1 Spring 2

23 92-9-905-4 Case for pin 2

24 92-9-912-1 Tie rod - control lock 2

25 92-2-302-8 Handle -, with lock 1

92-2-302-3 Handle - outside 2

26 92-2-302-8 Cable - door lock control 2

27 92-2-302-4 Lever 2

28 92-2-302-7 Knob 2

29 92-2-302-001 Bracket - handle, left 1

92-2-302-002 Bracket - handle, right 1

30 92-3-302-6 Bushing 2

31 Lock assembly 1

32 92-2-305-1 Bracket - door end travel, left 1

92-2-305-2 Bracket - door end travel, left 1

33 92-2-305-3 Cable - door stop 2

pag. 2-13



SECTION 2 FUSELAGE


assyEFF.

CODE


WINDOWS INSTALLATION

1 92-2-102-5 Window - lateral 2

2 92-2-108-2 Window - rear 1

3 92-2-108-3 Windshield in Perspex 1

4 92-2-111-1 Fairing 1

5 92-2-126-1 Retainer - window, rear 1

6 92-2-121-1 Retainer - window, left 1

7 92-2-121-2 Retain - window, right 1

8 92-12-101-4 Strip - windshield 1

pag. 2-15



SECTION 2 FUSELAGE


assyEFF.

CODE




SECTION 3

TAIL SURFACES


assyEFF.

CODE


STABILATOR ASSEMBLY

92-7-001-001 Stabilator assembly - half, left 1

92-7-001-002 Stabilator assembly - half, right 1

1 92-7-101-1 Rib - root side 2

2 92-7-102-1 Rib 6

3 92-7-103-1 Tip - stabilator 2

4 92-7-104-1 Spar 2

5 92-7-105-1 Skin - leading edge 2

6 92-7-105-2 Skin - trailing edge 2

7 92-7-106-1 Torque tube 2

8 92-7-107-1 Nose 2

9 92-7-108-2 Panel - upper 2

10 92-7-108-1 Panel - lower 2

11 92-7-109-1 Hinge - half, trim/tab 4

12 92-7-110-1 Collar - torque tube 2

13 92-7-111-1 Plate - coupling 2

14 92-7-002-001 Tab assembly, left 1

92-7-002-002 Tab assembly, right 1

15 92-7-003-000 Torque Tube assembly 1

16 92-7-303-1 Spacer 2

17 92-7-112-1 Strip for rib 12

18 92-7-202-3 Pin 4

19 92-5-905-1 Spacer trim 1

20 92-5-907-1 End travel 1

21 92-5-907-2 End travel 1

22 UNI 5737 Bolt M6 cr8.8 L=70 mm 2

pag. 3-2



SECTION 3

TAIL SURFACES


assyEFF.

CODE


STABILATOR ASSEMBLY



pag. 3-3



SECTION 3

TAIL SURFACES


assyEFF.

CODE


FIN ASSEMBLY

92-6-500-000 Fin assembly 1

1 92-6-511-1 Rib - upper 1

2 92-6-512-1 Flange - rudder bracket 1

3 92-6-800-2 Bushing 1

4 92-6-520-1 Spar, front 1

5 92-6-520-2 Spar, rear 1

6 92-6-580-1 Rib, lower 1

7 92-6-580-2 Rib, center 1

8 92-6-580-3 Rib, upper 1

9 92-6-540-1 Plate - fin fuselage attachment 1

10 92-6-550-1 Stiffener - rear spar 2

11 92-6-550-2 Stiffener - front spar 2

12 92-6-560-1 Skin - leading edge 1

13 92-6-570-1 Skin - lateral fin 2

14 92-6-530-4 Stringer - skin reinforcement 6

15 92-6-700-1 Tip - fin 1

16 92-6-530-1 Angle - rib reinforcement 1


18 92-6-530-3 Angle - fitting reinforcement 1


20 UNI 5739 Bolt M5 cr8.8 L=20 mm 9



pag. 3-5



SECTION 3

TAIL SURFACES


assyEFF.

CODE


RUDDER ASSEMBLY

92-6-600-000 Rudder assembly 1

1 92-6-610-1 Torque tube 1

2 92-6-620-1 End tube 2

3 92-6-630-1 Rib 3

4 92-6-650-1 Rib - upper 1

5 92-6-640-1 Skin, left 1

6 92-6-640-2 Skin, right 1

7 92-6-801-1 Bellcrank - rudder control 1

8 92-6-800-2 Bushing 1

9 92-6-800-1 Bracket 1

10 92-6-651-1 Sheet - adjustable trim 1

11 UNI 5737 Bolt M6 cr8.8 L=30 mm 2



pag. 3-7



SECTION 4

LANDING GEAR


assyEFF.

CODE


NOSE LANDING GEAR

92-8-001-000 Nose landing gear assembly 1

1 92-8-100-000 Nose gear strut assembly 1

2 92-8-240-3 Bushing 4

3 92-8-240-2 Spacer 2

4 92-8-120-1 Fork, left 1

5 92-8-120-2 Fork, right 1

6 92-8-130-1 Wheel centering 2

7 92-8-130-2 Washer 2

8 92-8-240-1 Axle 1

9 92-8-220-000 Rod assembly - absorber 1

10 92-8-240-4 Bushing 1

11 92-8-210-1 Plate, upper 1

12 92-8-200-1 Solid rubber element - Shock absorber 7

13 92-8-210-3 Aluminium element - Shock absorber 2

14 92-8-210-2 Plate, lower 1

15 92-8-230-000 Rod assembly - absorber 1

16 92-8-242-1 Chain - end travel 1

17 92-8-240-5 Bushing 4

18 92-8-130-3 Washer 4

19 UNI 5737 Bolt M8 cr8.8 L=110 mm 2



22 UNI 5737 Bolt M8 cr8.8 L=45 mm 1



pag. 4-2



SECTION 4

LANDING GEAR


assyEFF.

CODE


NOSE LANDING GEAR


26 UNI 5931 Bolt M8 L=72 mm 2

27 UNI6592 Washer d=8 2

28 UNI 5593 Castle nut M8 2

29 UNI 1336 Cotter pin 2

pag. 4-3



SECTION 4

LANDING GEAR


assyEFF.

CODE


FAIRING - NOSE WHEEL

1 92-8-420-2 Fairing - front (Opt.) 1

2 92-8-420-1 Fairing - rear (Opt.) 1

3 SAVA Tire 4.00-6 1

4 SAVA Tube 1

5 92-8-242-1 Wheel 1

6 UNI 7688 Screw M4 cr8.8 L=12 mm 6

7 UNI 5739 Bolt M6 cr8.8 L=12 mm 2


pag. 4-5



SECTION 4

LANDING GEAR


assyEFF.

CODE


MAIN LANDING GEAR

92-8-002-000 Main landing gear assembly 2

1 92-8-300-1 Leaf spring 2

2 92-8-202-1 Axle 2

3 92-12-301-3 Bracket - wheel attachment 2

4 92-12-301-2 Support - fairing (Opt.) 2

5 UNI 5737 Bolt cr8.8 M8 L=150 mm 2



8 92-12-301-4 Support fairing 2

9 92-8-410-1 Fairing, left (Opt.) 1

92-8-410-2 Fairing, right (Opt.) 1

10 92-12-301-1 Washer - fairing attachment (Opt.) 2


12 UNI 5739 Bolt M6 cr8.8 L=16 mm 2

13 UNI 5737 Bolt M4 cr8.8 L=35 mm 2



16 AIR-TRAC Tire 5.00-5 2

17 AIR-TRAC Tube 2

18 157-00800 Dust cover 2

19 102-00600 Screw M3.16 L=6 mm 6

20 92-8-204-1 Rod - leaf attachment 2

21 92-8-206-1 Spacer - composite 4

22 92-8-205-1 Spacer 2

23 UNI 5737 Bolt M8 cr8.8 L=120 mm 2

pag. 4-7



SECTION 4

LANDING GEAR


assyEFF.

CODE


MAIN LANDING GEAR



26 UNI 5931 Bolt M8 cr8.8 L=47 mm 4



29 UNI 5737 Bolt M6.35 cr8.8 L=39 mm 8


31 UNI 7473 Self locking nut M6.35 8

32 KIT 199-102 Brake assembly 2

33 “ Lining 2

34 “ Back plate 2

35 “ Bolt-lock 4

36 “ Washer 4

pag. 4-8



SECTION 5

FLIGHT CONTROLS


assyEFF.

CODE


STICK INSTALLATION

1 92-4-002-000 Aileron/stabil. control assembly 1

2 92-4-200-000 Stick attachment assembly 2

3 92-4-210-000 Shaft 1

4 92-4-203-2 Pulley 2

5 92-4-203-3 Spacer 2

6 92-4-203-4 Bushing 4

7 92-4-300-000 Stick 2

8 Grip with push-button 2

9 UNI 5737 Bolt M6 cr8.8 L=50 mm 2





14 UNI 5737 Bolt M6 cr8.8 L=25 mm 2

15 UNI 5737 Bolt M6 cr8.8 L=40 mm 2

pag. 5-2



SECTION 5

FLIGHT CONTROLS


assyEFF.

CODE


AILERON CONTROL INSTALLATION

1 92-4-002-000 Stick assembly (See Fig. 5.1) 1

2 MS 24566-3B Pulley 6

3 92-9-917-1 Guard - cable 6

4 92-5-903-2 Cable - Carbon Steel 5/32” 2

5 92-5-903-3 Cable - Carbon Steel 5/32” 2

6 MS 21251 Turnbuckle barrel 2

7 MS 21255 Turnbuckle - cable eye 2

8 92-5-005-000 Rod assembly (Cabin) 1

9 92-5-400-2 Rod (Wing) 2

10 92-5-400-1 Rod end, side cabin 2

11 92-5-400-3 Rod end, side wing 2

12 Saka C6M Bearing 6

13 92-1-112-1 Lever 2

14 92-1-112-2 Bearing BC4W10 (AN218-4) 2

15 92-1-112-3 Spacer 4

16 92-5-903-1 Spacer - rods attachment 2

17 92-5-901-1 Rod - aileron control 2

18 UNI 5737 Bolt M6 cr8.8 L=65 mm 2



21 UNI 5737 Bolt M6.5 cr8.8 L=50 mm 2

22 UNI 7474 Self locking nut, thin M6 2

23 UNI 5737 Bolt M5 cr8.8 L=55 mm 2



pag. 5-4



SECTION 5

FLIGHT CONTROLS


assyEFF.

CODE


AILERON CONTROL INSTALLATION

26 UNI 5737 Bolt M6 cr8.8 L=30 mm 2

27 UNI 5737 Bolt M6 cr8.8 L=25 mm 4

28 UNI 5737 Bolt M6 cr8.8 L=30 mm 2

pag. 5-5



SECTION 5

FLIGHT CONTROLS


assyEFF.

CODE


FLAP CONTROL INSTALLATION

1 92-5-001-000 Tube assembly - flap control 1

2 92-5-902-1 Push-pull rod - flap control 2


4 92-9-610-000 Rod assembly - actuator 1

5 92-9-610-5 Gudgeon pin 1

6 Clamp - Serflex 2

7 92-9-612-3 Flap transmitter arm 1

8 92-9-612-2 Flap transmitter arm 1

9 92-9-612-1 Bracket 1

10 92-9-630-2 Transmitter - flap position 1

11 Switch - flap end travel 2

12 33x150/C/12A Electric actuator "SKF" 1

13 92-9-610-4 Bushing 1

14 UNI 5737 Bolt M6 cr8.8 L=40 mm 1



17 UNI 5737 Bolt M6 cr8.8 L=30 mm 1

18 UNI 5737 Bolt M6 cr8.8 L=35 mm 2

19 UNI 5737 Bolt M6 cr8.8 L=20 mm 2



pag. 5-7



SECTION 5

FLIGHT CONTROLS


assyEFF.

CODE


RUDDER CONTROL INSTALLATION

1 92-5-003-001 Pedal structure assembly, left 1

2 92-5-003-002 Pedal structure assembly, right 1

3 92-5-310-4 Bushing 4

4 MS 21252 Turnbuckle - fork end 2

5 MS 21251 Turnbuckle - barrel 2

6 MS 21255 Turnbuckle - cable eye 2

7 92-5-904-1 Cable Carbon Steel 5/32” - left 1

8 92-5-904-2 Cable Carbon Steel 5/32” - right 1

9 92-9-917-1 Guard - cable control 2

10 AN 210-3A Pulley 2

11 AN 115-21 Cable shackles 2

12 92-9-908-1 Spring - rudder return 2

13 92-9-913-1 Link - spring attachment 2

14 92-5-700-002 Steering tube, right 1

15 92-5-700-001 Steering tube, right 1


17 UNI 5737 Bolt M6 cr8.8 L=40 mm 4



20 92-5-310-7 Bolt - pedal attachment 4


22 UNI 5737 Bolt M6 cr8.8 L=40 mm 2

23 Bolt M4.75 L=22 mm 4

24 UNI 5593 Castle nut 4


pag. 5-9



SECTION 5

FLIGHT CONTROLS


assyEFF.

CODE


STABILATOR CONTROL INSTALLATION

1 92-4-002-000 Stick assembly (See Fig. 5.1) 1


3 92-5-008-000 Push-pull rod assembly - front 1

4 92-5-600-1 Lever, left 1

5 92-5-600-4 Lever, left 1

6 92-5-600-2 Bushing 2

7 92-5-600-3 Spacer 1

8 92-5-090-1 Push-pull rod assembly - rear 1

9 92-5-091-1 Rod - end attachment 2

10 92-5-091-2 Bearing - GE 10E - 2

11 92-5-092-2 Spacer 1

12 92-5-092-1 Spacer 2

13 UNI 5737 Bolt M6 cr8.8 L=20 mm 2



16 UNI 5737 Bolt M6 cr8.8 L=25 mm 3

17 UNI 5737 Bolt M6 cr8.8 L=40 mm 1

pag. 5-11



SECTION 5

FLIGHT CONTROLS


assyEFF.

CODE


STABILATOR TRIM CONTROL INSTALL.

1 92-9-310-000 Bracket assembly - actuator unit 1

2 11-02058 Electric servo actuator MAC 6A 1

3 92-9-304-1 Rod - safe guard 1

4 92-9-303-1 Link 1

5 92-9-302-1 Spacer 1

6 92-9-320-000 Lever 1

7 92-9-330-3 Spacer 1

8 92-9-330-000 Rod assembly - stab. trim control 1

9 92-9-331-1 Spacer - actuator 1

10 UNI 5737 Bolt M4 cr8.8 L=25 mm 2

11 Bolt M4.75 L=22 mm 2

12 UNI 6592 Washer 2

13 UNI 5593 Castle nut 2


15 UNI 5737 Bolt M4 cr8.8 L=20 mm 4



18 UNI 5737 Bolt M6 cr8.8 L=60 mm 1



21 UNI 5737 Bolt M6 cr8.8 L=30 mm 1

22 UNI 5737 Bolt M6 cr8.8 L=25 mm 1


pag. 5-13



SECTION 6

POWER PLANT


assyEFF.

CODE


POWER PLANT INSTALLATION

1 92-10-002-000 Mount structure assembly - engine 1

2 92-11-912-1 Bracket, left 1

92-11-912-2 Bracket, right 1

3 92-11-912-3 Washer - shock mount 8

4 786021 Shock mount 70 SH 2

5 786021 Shock mount 70 SH 2

6 92-11-910-2 Spacer 6

7 92-11-910-1 Prop hub 1

8 92-11-101-1 Bulkhead 1

9 GT-2/166/145-FW100/1 SRTC Propeller “F.lli Tonini” 1

10 827 835 Prop flange 1

11 92-11-100-1 Spinner 1

12 UNI 7688 Screw M4 L=12 mm 8

13 UNI 5737 Bolt M8 cr8.8 L=120 mm 6


15 UNI 5739 Bolt M10 cr8.8 L=35 mm 4


17 UNI 5737 Bolt M8 cr8.8 L=75 mm 2

18 UNI 5737 Bolt M8 cr8.8 L=80 mm 2


20 UNI 5737 Bolt M6 cr8.8 L=70 mm 2



23 UNI 5737 Bolt M6 cr8.8 L=80 mm 2

pag. 6-2



SECTION 6

POWER PLANT


assyEFF.

CODE


ENGINE EXHAUST INSTALLATION

1 978-480 Muffler 1

2 92-11-750-002 Stack assembly - rear, right 1

3 92-11-750-001 Stack assembly - rear, left 1

4 92-11-750-004 Stack assembly - front, right 1

5 92-11-750-003 Stack assembly - front, left 1

6 938-795 Spring 8

7 92-11-830-1 Heat exchanger 1

8 92-11-830-2 Retainer - heat exchanger 2

pag. 6-4



SECTION 6

POWER PLANT


assyEFF.

CODE


ENGINE COWLING INSTALLATION

1 92-11-960-1 Cowling - lower 1

2 92-11-960-2 Cowling - upper 1

3 92-11-960-3 Panel cowl 1

4 92-11-903-1 Peg 4

5 92-11-915-1 Lock - upper element 4

6 92-11-915-4 Pin 4

7 92-11-915-2 Lever - latch 4

8 2600-4 Stud "Camlock" 6

9 2600-LW Ring 6

10 212-12N Receptacle 6

11 92-11-915-3 Lock - lower element 4

12 92-11-916-1 Pin - hinge 2

13 92-11-916-2 Hinge - fuselage side 2

14 92-11-916-3 Hinge - cowling side 2

pag. 6-6



SECTION 7 SYSTEMS


assyEFF.

CODE


FUEL SYSTEM

1 92-9-980-1 Flange 2

2 92-9-980-3 Finger strainer 2

3 5/8 19fil. Nut 2

4 92-9-980-4 Hose 2

5 Union 2

6 O-Ring 2

7 Shut-off valve 1/8” 2

8 AN816-4D Nipple 2

9 AN819-4D Sleeve 2

10 AN818-4D Nut

11 92-9-981-1 Line - valve to filter, left 1

12 92-9-981-2 Line- valve to filter, right 1

13 AN824-4D Tee 1

14 Nut M16 1

15 Hose - fuel drain 1

16 92-9-402-1 Bracket 1

17 10560 Gascolator 1

18 Adapter -tube to filter 1

19 92-11-103-1 Fire shield for filter 1

20 92-9-404-1 Fuel drain cup, left 1

92-9-404-2 Fuel drain cup, right 1

21 92-9-405-000 Fuel drain cup 1

22 92-9-401-000 Bracket valve 1

23 92-9-400-000 Bypass valve assembly 1

24 92-9-409-000 Tee with nut 2

pag. 7-2



SECTION 7 SYSTEMS


assyEFF.

CODE


FUEL SYSTEM

25 92-11-950-1 Tee 1

26 92-11-951-1 Hose - line: tee to carb., left 1

27 92-11-951-2 Hose - line: tee to carb., right 1

28 92-11-951-3 Hose - line: valve to filter 1

29 92-11-951-4 Hose - line: valve to pump 2

30 92-11-951-5 Hose - line: tank to valve 2

31 Clamp - Serflex 12

32 Hose - fuel drain 2

33 Hose - filter drain 1

34 92-9-411-1 Union 1

pag. 7-3



SECTION 7 SYSTEMS


assyEFF.

CODE


BRAKE SYSTEM

1 92-9-100-000 Lever 1

2 Knob lever 1

3 92-9-110-3 Bushing 2

4 92-9-111-1 Push-rod 1

5 Brake cylinder 1

6 AN818-4D Nut 8

7 AN819-4D Sleeve 7

8 AN822-4D Elbow 3

9 AN816-4D Nipple 2

10 AN824-4D Tee 1

11 92-9-904-1 Flange 1

12 92-9-904-2 Washer 1

13 92-9-904-3 Brake fluid reservoir 1

14 92-9-926-1 Clamp 2

15 Valve 1/8" - parking brake 1

16 92-9-923-1 Tube - line: cylinder to valve 1

17 92-9-923-2 Tube - line: valve to tee 1

18 92-9-923-3 Tube - line: tee to brake assy, left 1

19 92-9-923-4 Tube - line: tee to brake assy, left 1

20 92-9-918-1 Bracket 4

21 92-5-310-7 Bolt - lever attachment 2


23 UNI 5737 Bolt M6 cr8.8 L=25 mm 1



pag. 7-5



SECTION 7 SYSTEMS


assyEFF.

CODE


PITOT and STATIC PRESS. SYSTEM

1 Airspeed indicator (See fig. 7.7) 1

2 Altitude indicator (See fig. 7.7) 1

3 Rate of Climb indicator (See fig. 7.7) 1

4 92-9-920-000 Pitot tube assembly 1

5 92-9-903-1 Static source 2

6 Tee 2

7 Adapter 2

8 Tee (all tube) 1

9 Connector (tube to tube) 1

10 Hose - airspeed to altitude 1

11 Hose - airspeed to R/C 1

12 Hose - Tee to static 1

13 Hose - airspeed to connector 1

14 Hose - Pitot to connector 1

15 Hose - tee to static, right 1

16 Hose - tee to static, left 1

pag. 7-7



SECTION 7 SYSTEMS


assyEFF.

CODE


VACUUM SYSTEM

1 Hose - Vacuum pump to valve 1

2 Relief valve 1

3 Nut 1

4 Hose 1

5 92-8-408-1 Union end “Y” for valve (P/N 2H3-6) 1

92-8-408-2 Union end “Y” for valve SIGMA-TEK 1

6 Hose - valve to horizontal gyro 1

7 Hose - horizontal to suction gage 1

8 Hose - valve to directional gyro 1

9 Hose - horizontal to air filter 1

10 Hose - directional to air filter 1

11 1J7-1 Air filter 1


pag. 7-9



SECTION 7 SYSTEMS


assyEFF.

CODE


THROTTLE SYSTEM CONTROL

1 92-5-232-1 Knob 2

2 92-5-232-2 Push-pull rod 2

3 92-5-230-1 Fitting 2

4 UNI 8842 Lock washer (internal teeth) 2

5 UNI EN24035 Nut M16 2

6 92-5-400-001 Throttle link rod, left 1

7 92-5-400-002 Throttle link rod, right 1

8 92-5-020-000 Rod - link control 1

9 92-5-213-000 Lever 1

10 92-5-239-2 Friction lock rod 1

11 92-5-239-1 Friction 2

12 92-9-471-001 Cable - engine control, left 1

13 92-9-471-002 Cable - engine control, left 1

14 92-9-470-001 Cable - choke control, left 1

15 92-9-470-002 Cable - choke control, right 1

16 Lever - choke control 1

17 UNI 5737 Bolt M6 cr8.8 L=35 mm 1



20 MS20392-2C17 Clevis pin L=18 mm 4


22 UNI 5737 Bolt M4 cr8.8 L=25 mm 1



pag. 7-11



SECTION 7 SYSTEMS


assyEFF.

CODE


ELECTRIC COMPONENTS

1 945 345 Voltage regulator 1

2 Holder - fuse 1

3 40A 12V 2NA Relay overvoltage 1

4 OS75-14 Overvoltage sensor 1

5 992 819 Relay starter 1

6 92-9-410-1 Bracket 1

7 105-408 Condenser electrolytic (22000μF 25V) 1

8 073-0141 Strobe Light 2

9 152-0007 Power supply - anticollision light 1

10 W1285-PR Position light - tail 1

11 W1285-PR Position light - green, right wing 1

Position light - red, left wing 1

12 FIAMM 6H4P Battery 1

13 111-226-5 Relay - battery 1

14 GE 4509 Landing light 1

15 OAT gauge 1

16 164R Avvisatore acustico di stallo 1

17 164r Stall detector 1

18 Speaker - radio 2

19 Antenna VHF 1

20 Antenna VOR 1

21 Antenna G.P.S. (Opt.) 1

22 Antenna Transponder 1

23 92-9-501-1 Bus bar - breakers 1

24 UNI 5737 Bolt M6 cr8.8 L=20 mm 2

pag. 7-13



SECTION 7 SYSTEMS


assyEFF.

CODE


ELECTRIC COMPONENTS



27 UNI 5737 Bolt M6 cr8.8 L=16 mm 4

28 UNI 5737 Bolt M4 cr8.8 L=16 mm 3



4

pag. 7-14



SECTION 7 SYSTEMS


assyEFF.

CODE


INSTRUMENTS PANEL INSTALLATION

1 92-12-105-1 Instrument panel 1

2 92-12-113-1 Angle 2

3 92-9-907-4 Bracket - compass 1

4 Airspeed indicator 1

5 Attitude gyro (Opt.) 1

6 Gyro pressure gauge (Opt.) 1

7 Altitude indicator 1

8 301C Gauge - Outside air temp. 1

9 MAC 6A Trim position indicator 1

10 VOR indicator (Opt.) 1

11 Compass - magnetic 1

12 11-103 Switch “trim disconnect” 1

13 MX 2 Switch trim 1

14 Tachometer gauge 1

15 310.274/83/1 Flap position indicator 1

16 565 197 Dash light - Generator 1

17 310.274/81/1 Cylinder Head Temperature gauge 1

18 350.271/31/7 Oil temperature gauge 1

19 310.274/81/1 Oil pressure gauge 1

20 AT 420100 Digital clock 1

21 471 Amps indicator 1

22 486 Volts indicator 1

23 MS 22073-x Breakers 13

24 Transponder (Opt.) 1

25 VHF COM/NAV radio (Opt.) 1

pag. 7-16



SECTION 7 SYSTEMS


assyEFF.

CODE


INSTRUMENTS PANEL INSTALLATION

26 Lever switch - Master avionics (Opt.) 1

27 92-11-104-3 Knob - flap control 1

28 Rate of Climb indicator 1

29 AC10-2 FAA-PMA Keyed ignition switches 1

30 Directional gyro indicator (Opt.) 1

31 S-1994-1 Master switch 1

32 11-103 Switch - position lights (Opt.) 1

33 11-103 Switch - Strobe Light (Opt.) 1

34 11-103 Switch - Landing light (Opt.) 1

35 1394T100-72 Turn & bank indicator 1

36 92-12-111-1 Cover - large 1

92-12-111-2 Cover - small 1

37 92-12-123-1 Cover - radio box 1

38 92-9-907-4 Reinforcement 1

39 92-9-907-3 Bracket 2

40 92-12-113-2 Bracket - radio 2

41 92-12-125-1 Cover - instrument panel (ABS) 1

42 Handle 1

43 92-12-113-3 Plate - handle attachment 1

44 UNI 5737 Bolt M4 cr8.8 L=20 mm 2


pag. 7-17



SECTION 7 SYSTEMS


assyEFF.

CODE


HEATING SYSTEM INSTALLATION

1 92-11-850-000 Manifold assembly 1

2 Duct 1

3 Clamp - Serflex 50-60 3

4 92-11-870-000 Box assembly - valve, heating system 1

5 Duct 1

6 92-9-705-000 Air intake assembly 1

7 Duct - inlet 1

8 Duct - outlet 1

9 92-11-890-000

Cabin heat box assembly 1

10 92-11-840-000

Air filter assembly 1

11 92-11-104-1 Knob - cabin hot air 1

12 92-11-104-2 Knob - engine hot air 1

13 Duct - inlet cool air 1

14 92-11-820-000

Air intake assembly 1

15 Duct 1

16 92-11-860-000

Box assembly - hot air outlet 1

pag. 7-19



SECTION 7 SYSTEMS


assyEFF.

CODE


OIL COOLER SYSTEM INSTALLATION A 92-11-920-001 ASSY TUBE RADIATOR-TANK

1 92-11-990-3 COOPER WASHER 2 2 157256 CLAMP 2 3 92-11-920-1 FLEXIBLE TUBE RADIATOR TANK 1 4 92-11-922-1 ANTIFIRE PAINT SHEATH 1 5 956580 TUBE CONNECTOR 1

B 92-11-920-002 ASSY TUBE LINETANK ENGINE 5 956580 TUBE CONNECTOR 1

6 157256 CLAMP 1

7 92-11-920-2 FLEXIBLE LINE TANK ENGINE 1 8 92-11-922-2 ANTIFIRE PAINT SHEATH 1

9 92-11-908-4 WASHER 2

10 92-11-908-000 RADIATOR STIFFENING CLAMPER 1 11 NUT 2 12 HOSE CLAMP 2

13 92-11-990-5 OIL PASSAGE PIN 2 14 92-11-990-2 TUBE ATTACHMENT 1 C 92-11-920-003 ASSY RADIATOR TUBE 15 157256 CLAMP 1

16 92-11-920-3 FLESSIBLE TUBE 1 17 92-11-922-3 RADIATOR TUBE ANTIFIRE PAINT SHEAT 1 18 92-11-990-3 COOPER WASHER 1

19 92-11-990-000 METALLIC ELBOW 1

20 NUT 1 21 PUMP REDUCTION 1 22 92-11-920-4 BREATHER PIPE 1 23 92-11-100-001 LH RADIATOR SUPPORT 1 24 92-11-100-002 RH RADIATOR SUPPORT 1 25 HOSE CLAMP 1 26 TANK SUPPORT TIE 2 27 956-137 OIL TANK 1 28 92-11-913-1 TANK SUPPORT 1



SECTION 7 SYSTEMS


assyEFF.

CODE


WATER COOLER SYSTEM INSTALLATION

1 Hose 1

2 92-11-102-2 Tube 1

3 Hose 1

4 92-11-880-000 Flanged tube 1

5 Hose 1

6 92-11-102-1 Tube 1

7 Hose 1

8 Clamp - Serflex 8

9 Clamp - water cooler 2

10 92-9-926-1 Bracket - water cooler 2

11 Bottom - tank 1

12 Tank 1

13 Hose 1


15 UNI 5739 Bolt M6 cr8.8 L= 25 mm 4


17 UNI 5737 Screw M4 L=12 mm 2


pag. 7-23



SECTION 8

FURNISHING


assyEFF.

CODE


CABIN INTERIOR FINISHING

1 92-12-124-1 Panel - Head (ABS) 1

2 92-12-124-2 Panel - side right (ABS) 1

92-12-124-3 Panel - side left (ABS) 1

3 92-12-102-1 Strip - external, left 1

92-12-102-2 Strip - external, right 1

4 92-12-101-1 Retainer - windshield, left 1

92-12-101-2 Retainer - windshield, right 1

5 92-12-102-3 Strip - internal, left 1

92-12-102-4 Strip - internal, right 1

6 92-12-101-3 Retainer - windshield, upper 1

7 92-12-107-1 Plate - top attachment 2

8 92-12-608-1 Angle - Carpet 1

9 92-12-101-3 Retainer - head panel 1

10 92-9-927-1 Plate - jack headphone 1

11 92-12-601-1 Bulkhead - vertical, left 1

12 92-12-601-2 Bulkhead - vertical, right 1

13 92-12-602-1 Panel - baggage compartment 1

14 92-12-602-2 Panel - lower baggage 1

15 92-12-605-1 Retainer - panel baggage 2

16 92-12-605-2 Retainer - panel baggage 1

17 92-12-607-1 Retainer 1

18 92-12-606-1 Rib panel 4

19 92-9-912-2 Bracket - belt attachment 2

20 92-9-912-1 Bracket - belt attachment 2

21 92-12-103-2 Cover tunnel, rear 1

pag. 8-2



SECTION 8

FURNISHING


assyEFF.

CODE


CABIN INTERIOR FINISHING

22 92-12-103-1 Cover tunnel, front 1

23 92-12-114-1 Plate label - parking brake 1

24 92-12-104-2 Panel - floor, right 1

25 92-12-104-1 Panel - floor, left 1

26 92-12-121-1 Angle - bulkhead attachment, long 1

27 92-12-121-2 Angle - bulkhead attachment, short 1

28 92-2-120-1 Cover - stick compartment, left 1

92-2-120-2 Cover - stick compartment, right 1

29 92-2-120-3 Flange - sleeve attachment 2

30 92-12-121-4 Angle - Bulkhead attachment, right 1

31 92-12-121-3 Angle - Bulkhead attachment, left 1

32 92-12-122-2 Cover- seat compartment, right 1

33 92-12-122-3 Cover - seat compartment, left 1

34 92-12-122-1 Cover - seat compartment, center 2

92-12-500-000

Seat structure assembly 2

35 92-12-005-000

Seat assembly 2

36 92-9-902-1 Seat track 8

37 92-12-502-1 Lever - seat catch release, left 1

92-12-502-2 Lever - seat catch release, right 1

38 92-12-502-3 Bracket - lever 2

39 92-12-502-5 Spring 2

40 92-12-502-4 Plunger 2

41 92-12-114-2 Plate label - brake lever

pag. 8-3



SECTION 8

FURNISHING


assyEFF.

CODE




SECTION 1

WING


Fig. 1.1 WING STRUCTURE ASSEMBLY

pag. 1-1



SECTION 1

WING


Fig. 1.2 WING BOX ASSEMBLY

pag. 1-5



SECTION 1

WING


Fig. 1.3 LEADING EDGE and STRUT

pag. 1-7



SECTION 1

WING


Fig. 1.4 FLAP ASSEMBLY

pag. 1-10



SECTION 1

WING


Fig. 1.5 AILERON ASSEMBLY

pag. 1-12



SECTION 2 FUSELAGE


2.1 AFT FUSELAGE ASSEMBLY

pag. 2-1



SECTION 2 FUSELAGE


2.2 CABIN STRUCTURE

pag. 2-3



SECTION 2 FUSELAGE


Fig. 2.3 FUSELAGE SKIN INSTALLATION

pag. 2-5



SECTION 2 FUSELAGE


Fig. 2.4 CABIN SKIN INSTALLATION

pag. 2-8



SECTION 2 FUSELAGE


Fig. 2.5 DOORS INSTALLATION

pag. 2-11



SECTION 2 FUSELAGE


2.6 WINDOWS INSTALLATION

pag. 2-14



SECTION 3

TAIL SURFACES


1

2

3

4

5

6

7

89

10

11

16

13

14

12

15

Fig. 3.1 STABILATOR ASSEMBLY

pag. 3-1



SECTION 3

TAIL SURFACES


Fig. 3.2 FIN ASSEMBLY

pag. 3-4



SECTION 3

TAIL SURFACES


Fig. 3.3 RUDDER ASSEMBLY

pag. 3-6



SECTION 4

LANDING GEAR


Fig. 4.1 NOSE LANDING GEAR

pag. 4-1



SECTION 4

LANDING GEAR


Fig. 4.2 FAIRING - NOSE WHEEL

pag. 4-4



SECTION 4

LANDING GEAR


Fig. 4.3 MAIN LANDING GEAR

pag. 4-6



SECTION 5

FLIGHT CONTROL


Fig. 5.1 STICK INSTALLATION

pag. 5-1



SECTION 5

FLIGHT CONTROL


Fig. 5.2 AILERON CONTROL INSTALLATION

pag. 5-3



SECTION 5

FLIGHT CONTROL


Fig. 5.3 FLAP CONTROL INSTALLATION

pag. 5-6



SECTION 5

FLIGHT CONTROL


Fig. 5.4 RUDDER CONTROL INSTALLATION

pag. 5-8



SECTION 5

FLIGHT CONTROL


Fig. 5.5 STABILATOR CONTROL INSTALLATION

pag. 5-10



SECTION 5

FLIGHT CONTROL


Fig. 5.6 ELEVATOR TRIM CONTROL INSTALLATION

pag. 5-12



SECTION 6

POWER PLANT


Fig. 6.1 POWER PLANT INSTALLATION

pag. 6-1



SECTION 6

POWER PLANT


Fig. 6.2 ENGINE EXHAUST INSTALLATION

pag. 6-3



SECTION 6

POWER PLANT


Fig. 6.3 ENGINE COWLING INSTALLATION

pag. 6-5



SECTION 7 SYSTEMS


Fig. 7.1 FUEL SYSTEM

pag. 7-1



SECTION 7 SYSTEMS


Fig. 7.2 BRAKE SYSTEM

pag. 7-4



SECTION 7 SYSTEMS


Fig. 7.3 PITOT and STATIC PRESSURE SYSTEM

pag. 7-6



SECTION 7 SYSTEMS


Fig. 7.4 VACUUM SYSTEM

pag. 7-8



SECTION 7 SYSTEMS


Fig. 7.5 THROTTLE SYSTEM CONTROL

pag. 7-10



SECTION 7 SYSTEMS


Fig. 7.6 ELECTRIC COMPONENTS

pag. 7-12



SECTION 7 SYSTEMS


Fig. 7.7 INSTRUMENTS PANEL INSTALLATION

pag. 7-15



SECTION 7 SYSTEMS


Fig. 7.8 HEATING SYSTEM INSTALLATION

pag. 7-18



SECTION 7 SYSTEMS


Fig. 7.9 OIL COOLER SYSTEM INSTALLATION

pag. 7-20



SECTION 7 SYSTEMS


Fig. 7.10 WATER COOLER SYSTEM INSTALLATION

pag. 7-22



SECTION 8

FURNISHING


Fig. 8.1 CABIN INTERIOR FINISHING

pag. 8-1



SECTION 8

FURNISHING


Fig. 8.2 LABELS INSTALLATION

pag. 8-4

copert - alto-912. de

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