## KODI AK ® 

## 100 SB15- 01

Page 1 of 1 

### SUBJECT: YOKE ANTI-ROTATION GUIDE WEAR PAD UPGRADE REVISION: 00 DATE: 03 /26/2015 EFFECTIVITY: KODIAK® 100 series airplane serial numbers 100 -0001 thru 100- 01 49

SUMMARY The accompanying Field Service Instruction provides procedures for removing cushion edging, as installed from the factory or reinstalled in accordance with Quest® Aircraft Mandatory Service Bulletin SB14-07, Elevator Control System ─ Cushion Edging Inspection , and installing four wear pads on the pilot and co-pilot arms of the elevator bearing assemblies.

Document Number Document Title FSI

- 108 Yoke Anti

- Rotation Guide Wear Pad Upgrade



### COMPLIANCE Compliance with this service bulletin is RECOMMENDED. Installation of the modified design as detailed in FSI-108 negates the need for the initial and recurring inspections required by SB14-07.

FAA APPROVAL STATUS The instructions attached to this Service Bulletin have demonstrated compliance with all applicable Federal Aviation regulations and are approved by the Federal Aviation Administration.

SPECIAL INSTRUCTIONS If complied with, this Service Bulletin supersedes SB14- 07

.

CREDIT AND WARRANTY INFORMATION Quest will supply one service kit FSI-108 per airplane at no cost to owner, and for airplanes under factory warranty will reimburse up to three hours of labor costs associated with this Service Bulletin. Contact Quest Customer Service to order the kit. Refer to our web site at www.questaircraft.com for warranty reimbursement instructions.

Quest Customer Service Phone: (208) 263-1111 Toll Free: 1 (866) 263-1112 Email : customerservice@questaircraft.com



# RECOMMENDED SERVICE BULLETIN

Quest Aircraft Company, L.L.C., 1200 Turbine Drive, Sandpoint, ID 83864

__________________________________________________

CONFIDENTIALITY NOTICE: The information contained in this document and any attachments are the property of Quest Aircraft Design, L.L.C., and/or Ques t Aircraft Company, L.L.C., and may be used only by the intended recipient. In the event that this docume nt has been transmitted or forwarded to you in error, please notify the sender immediately by calling 208

- 263

- 1111. No person other than the intended recipient is authorized to read, print, retain, copy, and/or disseminate this document or any part of it. After notifying the sender of receipt, please destroy the document and any attachments. This document may contain information that is proprietary, privileged, confidential, and/or otherwise legally exempt from disclosure. Any erroneous transmission and /or receipt of this document shall not constitute waiver of any applicable protections against unauthorized use or disclosure of the information. QUEST ® , KODIAK ® , and logos are trademarks or registered trademarks of Quest Aircraft Design, L.L.C., and li censed to Quest Aircraft Company, L.L.C. English is the authoritative text of Quest Aircraft Design, L.L.C., and Quest Aircra ft Design, L.L.C., technical publications. If a technical publication is translated, then the English version will control.CONFIDENTIALITY NOTICE: The information contained in this document and any attachments are the property of Quest Aircraft Desi gn, L.L.C and/or Quest Aircraft Company, LLC. and may be used only by the intended recipient. In the event that this document has been transmitted or forwarded to you in error, please notify the sende r immediately by calling 208-263-1111. No person other than the intended recipient is authorized to read, print, retain, copy, and/or disseminate this document or any part of it. After notifying the sender of rec eipt, please destroy the document and any attachments. This document may contain information that is proprietary, privileged, confidential, and/or otherwise legally exempt from disclosure. Any erroneous transmission and/or receipt of this document shall not constitute waiver of any applicable protections against unauthorized use or disclosure of the information. QUEST ® , KODIAK ® , and logos are trademarks or registered trademarks of Quest Aircraft Design, L.L.C and licensed to Quest Aircraft Company, L. L.C. 

### FIELD SERVIC E INSTRUCTION

- PAGE: 

### 1 of 8

TITLE: 

### Yoke Anti-Rotation Guide Wear Pad Upgrade REPORT NO.: 

### FSI-108

SERIAL RANGE: 100-0001 thru 100-0149 JASC CODE: 2701 REVISION: 

### 00

SUBJECT
This Field Service Instruction provides procedures for removing cushion edging, as installed from the factory or reinstalled in accordance with SB14-07, Elevator Control System - Cushion Edging Inspection , and installing four wear pads on the pilot and co-pilot link arms of the elevator bearing assemblies.

AFFECTED MANUALS AND PUBLICATIONS

None

INDUSTRY REFERENCES

None

WEIGHT AND BALANCE
Negligible

MANPOWER
The estimated man-hours and minimum number of persons required to perform this Field Service Instruction are listed below. The “Minimum Persons” refers only to maintena nce personnel or installers, and unless otherwise specified within this instruction does not include additional person nel that may be needed solely to comply with safety requirements (for example, safety observer s that are not performing tasks within this instruction). It is the responsibility of maintenance personnel to comply with safety requirements , including having a safety observer available as needed.
Estimated Man-hours: 3 hours

Minimum Persons: 1 person If more than the minimum personnel perform this instruction, the actual man-hours required may be reduced due to increased efficiencies. As appropriate, Quest encourages the use of additional personnel; man-hour estimates are based on the minimum personnel required.

RECORD OF COMPLETION
• Update the appropriate maintenance log books
• Ensure the KODIAK ® 100 Pilot’s Operating Handbook / Aircraft Flight Manual is up-to-date with the current revision (Rev 15 or later)
• Ensure the KODIAK ® 100 Aircraft Maintenance Manual is up-to-date with the current revision (Rev 16 or later)

Quest Aircraft Company, LLC 1200 Turbine Drive Sandpoint, ID 83864


## D D D I

I I S S S C

C C L

L L A

A A I

I I M M M E E E R

R R

The instructions / procedures presented herein are based upon the systems and components of the aircraft when it was delivered from the factory, or as modified by Quest Service Bulletins. Thirdparty modifications that have affected any component, system, or operating characteristic discussed by this document may invali date the instructions / procedures provided. Before performing the instructions / procedures herein, examine all Supplemental Type Certificate (STC), Suppl emental Type Authority (STA), or equiva lently authorized modifications to verify that the instructions/procedures presented in this document can be properly comple ted. If an aircraft has an ST C, STA, or equivalently authorized modification that affects any component, system, or operating characteristic also affected by this document, the operator is responsib le for obtaining appropriate regulatory appro val before performing the instructi ons / procedures herein. Quest Aircraft Company cannot be responsible for the quality of work performed in accomplishing the requirements of this document. If you have any questions as to the applicability of this document to your specific aircraft, contact Quest Customer Service by telephone at (208) 263-1111, toll-free at (866) 263-1112, or via email at CustomerService@QuestAircraft.com

### FIELD SERVIC E INSTRUCTION

- PAGE: 

### 2 of 8

TITLE: 

### Yoke Anti-Rotation Guide Wear Pad Upgrade REPORT NO.: 

### FSI-108

SERIAL RANGE: 100-0001 

### thru 100-0149 JASC CODE: 

### 2701 REVISION: 

### 00

CONFIDENTIALITY NOTICE: The information contained in this document and any attachments are the property of Quest Aircraft Desi gn, L.L.C and/or Quest Aircraft Company, LLC. and may be used only by the intended recipient. In the event that this document has been transmitted or forwarded to you in error, please notify the sende r immediately by calling 208-263-1111. No person other than the intended recipient is authorized to read, print, retain, copy, and/or disseminate this document or any part of it. After notifying the sender of rec eipt, please destroy the document and any attachments. This document may contain information that is proprietary, privileged, confidential, and/or otherwise legally exempt from disclosure. Any erroneous transmission and/or receipt of this document shall not constitute waiver of any applicable protections against unauthorized use or disclosure of the information. QUEST ® , KODIAK ® , and logos are trademarks or registered trademarks of Quest Aircraft Design, L.L.C and licensed to Quest Aircraft Company, L. L.C. 

## REVISION RECORD

REV PAGE CHANGE DESCRIPTION

00 All Initial Release

### FIELD SERVIC E INSTRUCTION

- PAGE: 

### 3 of 8

TITLE: 

### Yoke Anti-Rotation Guide Wear Pad Upgrade REPORT NO.: 

### FSI-108

SERIAL RANGE: 100-0001 

### thru 100-0149 JASC CODE: 

### 2701 REVISION: 

### 00

CONFIDENTIALITY NOTICE: The information contained in this document and any attachments are the property of Quest Aircraft Desi gn, L.L.C and/or Quest Aircraft Company, LLC. and may be used only by the intended recipient. In the event that this document has been transmitted or forwarded to you in error, please notify the sende r immediately by calling 208-263-1111. No person other than the intended recipient is authorized to read, print, retain, copy, and/or disseminate this document or any part of it. After notifying the sender of rec eipt, please destroy the document and any attachments. This document may contain information that is proprietary, privileged, confidential, and/or otherwise legally exempt from disclosure. Any erroneous transmission and/or receipt of this document shall not constitute waiver of any applicable protections against unauthorized use or disclosure of the information. QUEST ® , KODIAK ® , and logos are trademarks or registered trademarks of Quest Aircraft Design, L.L.C and licensed to Quest Aircraft Company, L. L.C. 

## TABLE OF CONTENTS

REVISION RECORD ............................................................................................................... .............2

TABLE OF CONTENTS ............................................................................................................. ..........3

1. Special Safety Instructions ...............................................................................................................4

1.1 Warnings ...................................................................................................................... ......4
1.2 Cautions ...................................................................................................................... ........4
1.3 Notes ......................................................................................................................... ..........4

2. Parts, Tools, and Equipment ............................................................................................................4

Table 2-1: Parts and Tools In cluded in the Service Kit......................................................................... .......... 4 Table 2-2: Consumables Incl uded in the Service Kit ............................................................................ .......... 4 Table 2-3: Serial-Numbe r-Specific Parts Included in the Serv ice Kit ........................................................... . 4 Table 2-4: Parts and Tools NOT Included in the Service Kit .................................................................... ..... 4



### 3. General ....................................................................................................................... ......................5
Figure 3-1: Overview .......................................................................................................... ............................ 5



### 4. Preparation ................................................................................................................... ....................5

5. Instructions .................................................................................................................. .....................5

5.1 Remove the Cushion Edging ..............................................................................................5 Figure 5-1: Remove cushion edging ............................................................................................. .................. 6 Figure 5-2: Detach Contro l Column Elev ator Link ............................................................................... .......... 6 

### 5.2 Prepare Holes for New Wear Pads .....................................................................................7 Figure 5-3: Correctly Positioned Dr ill Guide .................................................................................. ................ 7 

### 5.3 Install the Wear Pads ......................................................................................................... .7
5.4 Reassemble the Control Co lumn Elevator Link .................................................................8 Figure 5-4: Fina l Insta llation ................................................................................................ ........................... 8



### 6. Completion .................................................................................................................... ...................8

### FIELD SERVIC E INSTRUCTION

- PAGE: 

### 4 of 8

TITLE: 

### Yoke Anti-Rotation Guide Wear Pad Upgrade REPORT NO.: 

### FSI-108

SERIAL RANGE: 100-0001 

### thru 100-0149 JASC CODE: 

### 2701 REVISION: 

### 00

CONFIDENTIALITY NOTICE: The information contained in this document and any attachments are the property of Quest Aircraft Desi gn, L.L.C and/or Quest Aircraft Company, LLC. and may be used only by the intended recipient. In the event that this document has been transmitted or forwarded to you in error, please notify the sende r immediately by calling 208-263-1111. No person other than the intended recipient is authorized to read, print, retain, copy, and/or disseminate this document or any part of it. After notifying the sender of rec eipt, please destroy the document and any attachments. This document may contain information that is proprietary, privileged, confidential, and/or otherwise legally exempt from disclosure. Any erroneous transmission and/or receipt of this document shall not constitute waiver of any applicable protections against unauthorized use or disclosure of the information. QUEST ® , KODIAK ® , and logos are trademarks or registered trademarks of Quest Aircraft Design, L.L.C and licensed to Quest Aircraft Company, L. L.C. 

### 1. Special Safety Instructions

1.1 Warnings Failure to comply with “Warnings” contained in this instruction may result in financial loss, significant delay in th e completion time, and/or se rious injury to personnel.

1.2 Cautions Failure to comply with “Cautions” containe d in this instruction may result in the destruction of components, unnecessary comp lications, the need to reverse completed work, and/or delays in the completion time.

1.3 Notes “Notes” are provided when additional informati on may lead to an increase in efficiency.

2. Parts, Tools, and Equipment The following tables describe the parts, tools, and equipment necessary to successfully complete this instruction. Where applicab le, reference to drawings provi ded with this instruction is provided.

Table 2-1: Parts and Tools Included in the Service Kit

Item # Part No. Qty Description Drawing No. Dwg Item # 2-1-1 100-619-0037 4 Wear Pad, FWD, Elevator Guide N/A N/A 2-1-2 CR3213-4-4 6 Rivet, Pulled N/A N/A 2-1-3 NAS1149FN532P 6 Washer N/A N/A 2-1-4 S100-619-4003 1 Link Arm Drill Guide, Elevator Bearing Assembly N/A N/A 2-1-5 MS24665-134 2 Cotter Pin N/A N/A



### Table 2-2: Consumables In cluded in the Service Kit

Item # Part No. Qty Description Drawing No. Dwg Item # 2-2-1 N/A - N/A N/A N/A
1: Consumables may be shipped separately from the primary kit.


### Table 2-3: Serial-Number-Specific Pa rts Included in the Service Kit

Item # Part No. Qty Description Drawing No. Dwg Item # 2-3-1 N/A - N/A N/A N/A



### Table 2-4: Parts and Tools NO T Included in the Service Kit

Item # Part No. Qty Description Drawing No. Dwg Item #

2-4-1 Cherry MAX Riveting tools 1 Cherry MAX Riveting tools N/A N/A
2-4-2 Emery Cloth AR Emery Cloth or sandpaper, 220 grit or finer N/A N/A

### FIELD SERVIC E INSTRUCTION

- PAGE: 

### 5 of 8

TITLE: 

### Yoke Anti-Rotation Guide Wear Pad Upgrade REPORT NO.: 

### FSI-108

SERIAL RANGE: 100-0001 

### thru 100-0149 JASC CODE: 

### 2701 REVISION: 

### 00

CONFIDENTIALITY NOTICE: The information contained in this document and any attachments are the property of Quest Aircraft Desi gn, L.L.C and/or Quest Aircraft Company, LLC. and may be used only by the intended recipient. In the event that this document has been transmitted or forwarded to you in error, please notify the sende r immediately by calling 208-263-1111. No person other than the intended recipient is authorized to read, print, retain, copy, and/or disseminate this document or any part of it. After notifying the sender of rec eipt, please destroy the document and any attachments. This document may contain information that is proprietary, privileged, confidential, and/or otherwise legally exempt from disclosure. Any erroneous transmission and/or receipt of this document shall not constitute waiver of any applicable protections against unauthorized use or disclosure of the information. QUEST ® , KODIAK ® , and logos are trademarks or registered trademarks of Quest Aircraft Design, L.L.C and licensed to Quest Aircraft Company, L. L.C. 

### 3. General

The instructions included in this document remove the existing Cushion Edging (P/N: M22529/3-2R-25) installed on the anti-rotation guid e and install a total of four (4) new wear pads attached to the elevator bearing assemb ly link arm. This document supersedes Quest Mandatory Service Bulletin SB14-07 which included FSI-105, Elevator Control System – Cushion Edging Inspection

.

Figure 3-1: Overview

4. Preparation

1. Remove the crew seats in accordance with the KODIAK ® 

### 100 Airplane Maintenance Manual

. 2. Protect the floor area under th e control yoke with a drop clot h or equivalent to prevent debris from falling into th e floor of the aircraft.

5. Instructions Repeat these instructions for both the pilot and co-pilot yoke.

5.1 Remove the Cushion Edging

1. Detach the existing cushion edging (P/N M 22529/2-3R-25), 2x on the pilot side and 2x on the co-pilot side, and re move from the aircraft.

### FIELD SERVIC E INSTRUCTION

- PAGE: 

### 6 of 8

TITLE: 

### Yoke Anti-Rotation Guide Wear Pad Upgrade REPORT NO.: 

### FSI-108

SERIAL RANGE: 100-0001 

### thru 100-0149 JASC CODE: 

### 2701 REVISION: 

### 00

CONFIDENTIALITY NOTICE: The information contained in this document and any attachments are the property of Quest Aircraft Desi gn, L.L.C and/or Quest Aircraft Company, LLC. and may be used only by the intended recipient. In the event that this document has been transmitted or forwarded to you in error, please notify the sende r immediately by calling 208-263-1111. No person other than the intended recipient is authorized to read, print, retain, copy, and/or disseminate this document or any part of it. After notifying the sender of rec eipt, please destroy the document and any attachments. This document may contain information that is proprietary, privileged, confidential, and/or otherwise legally exempt from disclosure. Any erroneous transmission and/or receipt of this document shall not constitute waiver of any applicable protections against unauthorized use or disclosure of the information. QUEST ® , KODIAK ® , and logos are trademarks or registered trademarks of Quest Aircraft Design, L.L.C and licensed to Quest Aircraft Company, L. L.C. 

### Figure 5-1: Remove cushion edging

2. Using a fine grit sandpaper or emery cloth, cl ean up the slot edge of the anti-rotation guide to remove any burrs or other sharp edges. 3. Remove the cotter pin; remove and retain the bolt, nut, and two (2) washers securing the bearing assembly to the control column elevator link. Discard the cotter pin. See Figure 5-2

.

Figure 5-2: Detach Contro l Column Elevator Link

4. Move the elevator link down and away from control column elevator bearing assembly. Cushion Edging Cushion Edging

Bearing Assembly Ea r Anti-rotation guide Guide Slot

### FIELD SERVIC E INSTRUCTION

- PAGE: 

### 7 of 8

TITLE: 

### Yoke Anti-Rotation Guide Wear Pad Upgrade REPORT NO.: 

### FSI-108

SERIAL RANGE: 100-0001 

### thru 100-0149 JASC CODE: 

### 2701 REVISION: 

### 00

CONFIDENTIALITY NOTICE: The information contained in this document and any attachments are the property of Quest Aircraft Desi gn, L.L.C and/or Quest Aircraft Company, LLC. and may be used only by the intended recipient. In the event that this document has been transmitted or forwarded to you in error, please notify the sende r immediately by calling 208-263-1111. No person other than the intended recipient is authorized to read, print, retain, copy, and/or disseminate this document or any part of it. After notifying the sender of rec eipt, please destroy the document and any attachments. This document may contain information that is proprietary, privileged, confidential, and/or otherwise legally exempt from disclosure. Any erroneous transmission and/or receipt of this document shall not constitute waiver of any applicable protections against unauthorized use or disclosure of the information. QUEST ® , KODIAK ® , and logos are trademarks or registered trademarks of Quest Aircraft Design, L.L.C and licensed to Quest Aircraft Company, L. L.C. 

### 5.2 Prepare Holes for New Wear Pads

1. Position the link arm drill guide (P/N S100-619-4003) against the control column elevator bearing assembly, aligning the la rge bolt hole in the drill guide with the existing bolt hole in the bearing assembly. Ali gn the lower edges of the drill guide with the outside edge of the bearing assembly ear.

Figure 5-3: Correctly Positioned Drill Guide

2. Temporarily secure the drill guide to the bearing assembly ear with the nut and bolt removed previously. Stack sufficient washers on the bolt to provide a tight fit of the drill guide against the bearing assembly ear. 3. Match drill two (2) holes into the elevator bearing assembly ear with a # 40 drill bit. 4. Remove the drill guide. 5. Deburr the newly drilled holes.

5.3 Install the Wear Pads

1. Position one (1) wear pad (P/N 100-619-0037) on each side of the bearing assembly ear aligning the two (2) holes in each wear pa d with the holes just drilled through the bearing assembly ear. 2. Temporarily secure the wear pads in place with one (1) #40 cleco. 3. Upsize the open hole in the wear pads and b earing assembly ear with a #30 drill bit. 4. Temporarily secure the wear pads in place with a second #30 cleco and remove the first cleco. 5. Upsize the open hole in the wear pads and b earing assembly ear with a #30 drill bit. 6. Remove the cleco and wear pads from the bearing assembly ear. 7. Deburr the upsized holes in th e bearing assembly ear and ensure the wear pads are free of any aluminum debris. 8. Position the wear pads on both sides of the bearing assembly aligning the mounting holes just prepared and secure th em in place with one (1) #30 cleco. 9. Insert one (1) pulled rivet through the open mounting hole and place one (1) washer (P/N NAS1149FN532P) over th e tail of the rivet. Align Bolt Holes Align Edges

### FIELD SERVIC E INSTRUCTION

- PAGE: 

### 8 of 8

TITLE: 

### Yoke Anti-Rotation Guide Wear Pad Upgrade REPORT NO.: 

### FSI-108

SERIAL RANGE: 100-0001 

### thru 100-0149 JASC CODE: 

### 2701 REVISION: 

### 00

CONFIDENTIALITY NOTICE: The information contained in this document and any attachments are the property of Quest Aircraft Desi gn, L.L.C and/or Quest Aircraft Company, LLC. and may be used only by the intended recipient. In the event that this document has been transmitted or forwarded to you in error, please notify the sende r immediately by calling 208-263-1111. No person other than the intended recipient is authorized to read, print, retain, copy, and/or disseminate this document or any part of it. After notifying the sender of rec eipt, please destroy the document and any attachments. This document may contain information that is proprietary, privileged, confidential, and/or otherwise legally exempt from disclosure. Any erroneous transmission and/or receipt of this document shall not constitute waiver of any applicable protections against unauthorized use or disclosure of the information. QUEST ® , KODIAK ® , and logos are trademarks or registered trademarks of Quest Aircraft Design, L.L.C and licensed to Quest Aircraft Company, L. L.C. 

### 10. Permanently secure the wear pads in place with the rivet and washer. 11. Remove the cleco and repeat the rivet and washer installation through the second hole in the wear pads and bearing assembly ear.

5.4 Reassemble the Control Column Elevator Link

1. Raise the elevator link into position and thr ead the bolt removed previously through the hole in the end of the link a nd the bearing assembly ear. 2. Secure the elevator link to the bearing asse mbly ear with the nut and washers removed previously, torque the nut to 5 in-l b and then back off one castellation.

N N N O

O O T

T T E

E E Ensure the nylon (self-locking) f eature of the nut is in good cond ition. Replace the nut if needed.



### 3. Install a new cotter pin (P/N MS 24665-134) through the nut and bolt. 4. Check the control yoke for smooth freedom of movement through the full range of normal motion and verify minimum wear pad extension beyond the anti-rotation guide. See Figure 5-4

.

Figure 5-4: Final Installation

5. Repeat Section 5 for the opposite control yoke.

6. Completion

1. Clean up all chips and all ot her foreign object debris. 2. Reinstall the crew seat s in accordance with the KODIAK ® 

### 100 Airplane Maintenance Manual

. 3. Record all work performed in the appropriate mainte nance records.

---END--- Anti Rotation Guide Wear Pads

0.010" Minimum