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Second Edition, Revision 0 – October, 2011 Revision 1 – January, 2015

Publication No. S2061A

SOLOY AVIATION SOLUTIONS

ILLUSTRATED PARTS CATALOG

SUPPLEMENT

FOR

CESSNA U206G/TU206G 206H/T206H AIRPLANES WITH SOLOY WING MOUNT CAMERA MODIFIED I/A/W SOLOY CONVERSION KIT

P/N 916-1000


CESSNA 206 WITH WING MOUNT CAMERA ILLUSTRATED PARTS CATALOG SUPPLEMENT

October, 2011

NOTICE

The use of parts listed herein may be restricted or prohibited by Soloy Aviation Solutions or Cessna Aircraft Company Service Bulletins. Accordingly, this manual must be used in conjunction with all applicable and effective Soloy and Cessna Aircraft Company Service Bulletins.

Soloy Aviation Solutions 450 Pat Kennedy Way S.W. Olympia, Washington 98501 USA Phone: 360-754-7000 Fax: 360-943-7659 Email: [email protected]

mailto:[email protected]


CESSNA 206 WITH WING MOUNT FLIR CAMERA ILLUSTRATED PARTS CATALOG SUPPLEMENT

January, 2015 i

NOTICE This data is furnished with the understanding that it will be used for operational service and maintenance purposes only, and not to manufacture or procure the manufacture of the part shown and/or described.

LIST OF EFFECTIVE PAGES Insert the latest revision pages; dispose of superseded pages.

NOTE

On a revised page, the portion of the text affected by the latest revision is indicated by a vertical line in the right hand margin.

First Edition: Revision 0 July 3, 2003 Second Edition: Revision 0 October, 2011 Revision 1 January, 2015

CHAPTER PAGE DATE

TITLE PAGE N/A 1/2015

NOTICE N/A 10/2011

LIST OF EFFECTIVE PAGES i 1/2015

INTRODUCTION ii 10/2011

iii 10/2011

iv 10/2011

TABLE OF CONTENTS v 10/2011

vi 10/2011

11-00-00 1 10/2011

2 1/2015

3 1/2015

4 10/2011

57-40-00 1 10/2011

2 1/2015

3 1/2015

4 1/2015

5 1/2015

6 10/2011

7 10/2011

8 1/2015

9 1/2015

57-60-00 0 10/2011

1 10/2011

2 10/2011

CHAPTER PAGE DATE

APPENDIX A A1 10/2011 A2 1/2015 A3 1/2015 A4 10/2011 APPENDIX B B1 10/2011 B2 1/2015 B3 1/2015 B4 10/2011



October, 2011 ii

INTRODUCTION

CONTENT AND ARRANGEMENT This publication applies to Cessna Model 206 aircraft modified in accordance with Soloy Aviation Solutions’ Supplemental Type Certificate SA02748AT. The purpose of this Illustrated Parts Catalog Supplement is to illustrate and identify replacement parts and assemblies necessary for the support of the model covered herein. The information in the catalog is based on data available at the time of publication. DO NOT USE this Illustrated Parts Catalog Supplement to determine removal and installation procedures, refer to the Maintenance Manual for the given part. The airplane operator, using applicable rules, is responsible for determining the status (or airworthiness) of the airplane. This Illustrated Parts Catalog Supplement is divided into chapters which correspond to equivalent chapters in the Maintenance Manual supplement and is prepared in accordance with the Air Transport Association 2200 Specification format. The catalog features an index system consisting of: 1. A TABLE OF CONTENTS located in the front of the catalog. 2. An ALPHABETICAL INDEX which appears in Appendix A. 3. A PART NUMBER INDEX which appears in Appendix B. A parts list is provided for each illustration throughout the supplement. The first line of each parts list contains information regarding the chapter, section, figure number, and description of the overall illustration. Any part associated with this installation can be ordered from Soloy Aviation Solutions; however, for convenience a supplier code is provided to source individual parts. Suppliers used in this installation include: S – Soloy Aviation Solutions C – Cessna HMS – Soloy Hardware/Material Substitution Report, Soloy publication 700-010 Blank – Multiple suppliers with a common part number

The catalog is a supplement to the existing Cessna Parts Catalog and when used in conjunction with that publication complete parts coverage is obtained.



October, 2011 iii

LOCATION OF PARTS 1. WHEN THE PART NUMBER IS KNOWN:

A. Locate the part number in the PART NUMBER INDEX in the rear of the catalog. B. Record the chapter and figure number. C. Turn to the chapter and locate the figure number. D. Locate the part number in the parts index and note the index number. E. Locate the part on the component illustration noting the index number in the

illustration. F. Confirm correct part.

2. WHEN THE PART NOMENCLATURE IS KNOWN:

A. Locate the part number in the ALPHABETICAL INDEX in the rear of the catalog. B. Record the chapter and figure number. C. Turn to the chapter and locate the figure number. D. Locate the part number in the parts index and note the index number. E. Locate the part on the component illustration noting the index number in the

illustration. F. Confirm correct part.

3. FOR ALL OTHER CASES:

A. Refer to the TABLE OF CONTENTS and find an appropriate section. B. Select the figure covering the part in question. C. Turn to the figure and locate the part by reference to the illustration and

determine its index number. D. Locate the index number on the adjacent parts callout page, confirming both part

number and description.



October, 2011 iv

INSTRUCTIONS FOR ORDERING Order parts by part number and nomenclature as indicated in this publication. Specify quantity, required method of shipment and P.O. number if applicable. Do not order by nomenclature alone. Soloy Aviation Solutions reserves the right to supply substitute parts interchangeable with the part ordered wherein design change, later specifications, conditions of supply or product improvement make such substitution necessary. All orders for parts will be filled in the shortest possible time, with parts of any emergency nature given special attention. Items not in stock will be placed on backorder and the customer notified as to the date when shipment will be made. Parts are shipped on open account to all customers having an approved credit rating with Soloy Aviation Solutions. All other orders are shipped C.O.D. Method of transportation on shipments will be designated by the customer. When no such designation is made, method of transportation will be by the most expeditious means, at the discretion of Soloy Aviation Solutions. When shipping charges are prepaid, as on parcel post, the amount of the charges will be added to the customer’s invoice. Orders for spare parts should be addressed to: SOLOY AVIATION SOLUTIONS 450 Pat Kennedy Way SW Olympia, Washington 98501 U.S.A. Attention; Spare Parts Department or call direct Phone: 360-754-7000 Fax: 360-943-7659 Email: [email protected] Website: www.soloy.com

mailto:[email protected]

http://www.soloy.com/



October, 2011 v

TABLE OF CONTENTS FIGURE DESCRIPTION CHAPTER PAGE GENERAL LIST OF EFFECTIVE PAGES........................................................... i INTRODUCTION .............................................................................. v TABLE OF CONTENTS .................................................................... viii PLACARDS AND MARKINGS 11-30-00 1 INTERIOR PLACARDS..................................................................... 1 WINGS 57-40-00 1 SPAR BLOCKS ................................................................................ 1 2 INTERCOSTAL WEB AND INTERCOSTAL BLOCKS ...................... 3 3 WING ACCESS HOLES ................................................................... 5 4 DOVETAIL MOUNT .......................................................................... 7 57-60-00 1 AILERON TRIM TABS ...................................................................... 1 INDEX ALPHABETICAL INDEX ................................................................... A1 PART NUMBER INDEX .................................................................... B1



October, 2011 vi

This Page Intentionally Left Blank

CHAPTER

11 PLACARDS AND

MARKINGS


CESSNA 206 WITH WING MOUNT CAMERA MAINTENANCE MANUAL SUPPLEMENT

PLACARDS AND MARKINGS 11-00-00 PLACARDS – COMPONENT INSTALLATION October, 2011

Page 1




PLACARDS AND MARKINGS 11-00-00 PLACARDS – COMPONENT INSTALLATION January, 2015

Page 2

PLACARDS – COMPONENT INSTALLATION

Figure Item

Manufacturer’s Part Number Description Qty

Supplier Code

11-00-00-1 Interior Placards Ref.

1 916-9008-7 Placard, autopilot use with camera 1 S

2 916-9008-5 Placard, maximum airspeed/flap

extension with camera installed. 1 S



PLACARDS AND MARKINGS 11-00-00 PLACARDS – COMPONENT INSTALLATION January, 2015

Page 3

INSTRUMENT PANEL

1

1.

2.

Figure 1: Interior Placards

1 2

AUTOPILOT USE WITH CAMER INSTALLED IS LIMITED TO:

DAY/NIGHT VFR ONLY

AIRSPEED: 90 - 120 KIAS

MAXIMUM FUEL IMBALANCE: 60 LBS

MAXIMUM FLAP EXTENSION: 10°

NO FLAP MOVEMENT WITH AUTOPILOT ON

WITH CAMERA INSTALLED:

MAXIMUM AIRSPEED: 140 KIAS

MAXIMUM FLAP EXTENSION: 20°



PLACARDS AND MARKINGS 11-00-00 PLACARDS – COMPONENT INSTALLATION October, 2011

Page 4


CHAPTER

57 WINGS



WINGS 57-40-00 LEADING EDGE AND LEADING EDGE DEVICES – October, 2011 COMPONENT INSTALLATION Page 1




WINGS 57-40-00 LEADING EDGE AND LEADING EDGE DEVICES – January, 2015 COMPONENT INSTALLATION Page 2

LEADING EDGE AND LEADING EDGE DEVICES – COMPONENT INSTALLATION

Figure Item


Supplier Code

57-40-00-1

Spar Blocks Ref.

1 916-1321-1 Spar Block Assembly 2 S

2 916-1325-1 Shim 4 S

3 916-1326-1 Shim 1 S

4 HL18PB70-6-9 Hi-Lok 2

5 HL18PB70-6-8 Hi-Lok 6

6 HL18PB70-6-6 Hi-Lok 12




Figure 1: Spar Blocks

1

2

5

3

1

5

6 4 5




Figure Item


Supplier Code

57-40-00-2

Intercostal Web and Intercostal Blocks

Ref.

21 916-1311-1 Intercostal Block Assembly 2 S

22 916-1312-1 Shim Pack 2 S

23 916-1314-1 Intercostal Web 1 S

24 CR3243 4-3 Rivet, Blind 5

HL18PB70-5-3 Hi-Lok - Alternate ALT

25 CR3243-4-4 Rivet, blind 5

HL18PB70-5-4 Hi-Lok - Alternate ALT

26 MS20426AD4-4 Rivet 14

27 MS20470AD4-5 Rivet 13

28 MS20470AD4-7 Rivet 20

HL18PB70-5-4 Hi-Lok – Alternate ALT




Figure 2: Intercostal Web and Intercostal Blocks

22

23 21

25

24

28

27

26




Figure Item


Supplier Code

57-40-00-3

Wing Access Holes Ref.

31 916-1330-1 Doubler Assembly 1 S

32 MS21049L08K Nutplate 12

33 916-1331-1 Cover 1 S

34 1220116-1 Doubler Assembly 1 C

916-1339-1 Doubler Assembly - Alternate ALT S

35 MS21059L08K Nutplate 8

36 916-1340-1 Cover, Cable Entry 1 S

37 MS21266-1N Grommet 1

38 916-1341-1 Cover * S

120117-1 Cover - Alternate *ALT C

39 MS24694-S3 Screw 20

* Cover without cable entry hole. Used when camera is not installed.




Figure 3: Wing Access Holes

31

32

34

35

39 33 39 36

38

37




Figure Item


Supplier Code

57-40-00-4

Dovetail Mount Ref.

51 916-1220-1 Upper Dovetail Mount Assembly

1 S

52 MS16556-842 Pin 1

Not Shown DT-1 Lower Dovetail Mount 1

53 916-1240-1 Bushing 4 S

54 AN5H-13A Bolt 4

55 NAS1149F0563P Washer 4

56

MS15795-712 Washer – Optional 1

MS9321-11 Washer – Alternate ALT

NAS1149D0563J Washer – Alternate ALT




Figure 4: Dovetail Mount

55

51

53

54

52

56



WINGS 57-60-00 AILERONS AND ELEVONS – October, 2011 COMPONENT INSTALLATION Page 0

Figure Item


Supplier Code

57-60-00-1

Aileron Trim Tabs Ref.

61 916-1610-1 Tab Assembly, LH 1 S

62 916-1621-1 Inboard Tab Rib 1 S

63 916-1622-1 Outboard Tab Rib 1 S

64 916-1623-1 Intercostal Frame Assy, LH 1 S

65 MS21047L08 Nutplate 4

66 AN525-832R6 Screw 8

67 CR3213-4-2 Rivet, Blind 8

68 MS20470AD3-3 Rivet 12

71 916-1610-2 Tab Assembly, RH 1 S

72 916-1621-1 Inboard Tab Rib 1 S

73 916-1622-1 Outboard Tab Rib 1 S

74 916-1623-2 Intercostal Frame Assy, RH 1 S

75 MS21047L08 Nutplate 4

76 AN525-832R6 Screw 8

77 CR3213-4-2 Rivet, Blind 8

78 MS20470AD3-3 Rivet 12




Figure 1: Aileron Trim Tabs

64

65

72 74

75 76 71

68 67

62

61

63 66

73

78

77

RIGHT AILERON TRIM TAB

LEFT AILERON TRIM TAB



ALPHABETICAL INDEX October, 2011

Page A1

ALPHABETICAL INDEX



ALPHABETICAL INDEX January, 2015

Page A2

Description Part Number Section Figure

Bolt AN5H-13A 57-40-00 4

Bushing 916-1240-1 57-40-00 4

Cover 916-1331-1 57-40-00 3

Cover 916-1341-1 57-40-00 3

Cover - Alternate 120117-1 57-40-00 3

Cover, Cable Entry 916-1340-1 57-40-00 3

Doubler Assembly 1220116-1 57-40-00 3

Doubler Assembly 916-1330-1 57-40-00 3

Doubler Assembly 916-1339-1 57-40-00 3

Dovetail Mount Assembly 916-1220-1 57-40-00 4

Grommet MS21266-1N 57-40-00 3

Hi-Lok HL18PB70-5-3 57-40-00 2

Hi-Lok HL18PB70-5-4 57-40-00 2

Hi-Lok HL18PB70-6-6 57-40-00 1

Hi-Lok HL18PB70-6-8 57-40-00 1

Hi-Lok HL18PB70-6-9 57-40-00 1

Inboard Tab Rib 916-1621-1 57-60-00 1

Intercostal Block Assembly 916-1311-1 57-40-00 2

Intercostal Frame Assy, LH 916-1623-1 57-60-00 1

Intercostal Frame Assy, RH 916-1623-2 57-60-00 1

Intercostal Web 916-1314-1 57-40-00 2

Nutplate MS21047L08 57-60-00 1

Nutplate MS21049L08K 57-40-00 3

Nutplate MS21059L08K 57-40-00 3

Outboard Tab Rib 916-1622-1 57-60-00 1

Pin MS16556-842 57-40-00 4

Placard, Max airspeed/Max flap 916-9008-5 11-00-00 1

Placard, Autopilot 916-9008-7 11-00-00 1

Rivet MS20426AD4-4 57-40-00 2

Rivet MS20470AD3-3 57-60-00 1

Rivet MS20470AD4-5 57-40-00 2

Rivet MS20470AD4-7 57-40-00 2

Rivet, Blind CR3243-4-3 57-40-00 2

Rivet, Blind CR3243-4-4 57-40-00 2

Rivet, Blind CR3213-4-2 57-60-00 1

Screw AN525-832R6 57-60-00 1

Screw MS24694-S3 57-40-00 3

Shim 916-1325-1 57-40-00 1

Shim 916-1326-1 57-40-00 1

Shim Pack 916-1312-1 57-40-00 2

Spar Block Assembly 916-1321-1 57-40-00 1



ALPHABETICAL INDEX January, 2015

Page A3

Description Part Number Section Figure

Tab Assembly, LH 916-1610-1 57-60-00 1

Tab Assembly, RH 916-1610-2 57-60-00 1

Washer MS9321-11 57-40-00 4

Washer MS15795-712 57-40-00 4

Washer NAS1149D0563J 57-40-00 4

Washer NAS1149F0563P 57-40-00 4



ALPHABETICAL INDEX October, 2011

Page A4




PART NUMBER INDEX October, 2011 Page B1

PART NUMBER INDEX



PART NUMBER INDEX January, 2015

Page B2

Part Number Description Section Figure

120117-1 Cover - Alternate 57-40-00 3

1220116-1 Doubler Assembly 57-40-00 3

916-1220-1 Dovetail Mount Assembly 57-40-00 4

916-1240-1 Bushing 57-40-00 4

916-1311-1 Intercostal Block Assembly 57-40-00 2

916-1312-1 Shim Pack 57-40-00 2

916-1314-1 Intercostal Web 57-40-00 2

916-1321-1 Spar Block Assembly 57-40-00 1

916-1325-1 Shim 57-40-00 1

916-1326-1 Shim 57-40-00 1

916-1330-1 Doubler Assembly 57-40-00 3

916-1331-1 Cover 57-40-00 3

916-1339-1 Doubler Assembly - Alternate 57-40-00 3

916-1340-1 Cover, Cable Entry 57-40-00 3

916-1341-1 Cover 57-40-00 3

916-1610-1 Tab Assembly, LH 57-60-00 1

916-1610-2 Tab Assembly, RH 57-60-00 1

916-1621-1 Inboard Tab Rib 57-60-00 1

916-1622-1 Outboard Tab Rib 57-60-00 1

916-1623-1 Intercostal Frame Assy, LH 57-60-00 1

916-1623-2 Intercostal Frame Assy, RH 57-60-00 1

916-9008-5 Placard, Autopilot 11-00-00 1

916-9008-7 Placard, Max airspeed/Max flap 11-00-00 1

AN525-832R6 Screw 57-60-00 1

AN5H-13A Bolt 57-40-00 4

CR3213-4-2 Rivet, Blind 57-60-00 1

CR3243-4-3 Rivet, Blind 57-40-00 2

CR3243-4-4 Rivet, Blind 57-40-00 2

HL18PB70-5-3 Hi-Lok 57-40-00 2

HL18PB70-5-4 Hi-Lok 57-40-00 2

HL18PB70-6-6 Hi-Lok 57-40-00 1

HL18PB70-6-8 Hi-Lok 57-40-00 1

HL18PB70-6-9 Hi-Lok 57-40-00 1

MS9321-11 Washer 57-40-00 4

MS15795-712 Washer 57-40-00 4

MS16556-842 Pin 57-40-00 4

MS20426AD4-4 Rivet 57-40-00 2

MS20470AD3-3 Rivet 57-60-00 1

MS20470AD4-5 Rivet 57-40-00 2

MS20470AD4-7 Rivet 57-40-00 2

MS21047L08 Nutplate 57-60-00 1



PART NUMBER INDEX January, 2015

Page B3

Part Number Description Section Figure

MS21049L08K Nutplate 57-40-00 3

MS21059L08K Nutplate 57-40-00 3

MS21266-1N Grommet 57-40-00 3

MS24694-S3 Screw 57-40-00 3

NAS1149D0563J Washer 57-40-00 4

NAS1149F0563P Washer 57-40-00 4



PART NUMBER INDEX October, 2011

Page B4


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