FAA-PMA

AIRCRAFT WHEEL & BRAKE DIVISION

PARKER HANNIFIN CORPORATION
AVON, OHIO

PARTS LIST

199-174 CONVERSION KIT

ROCKWELL AERO COMMANDER

PART NUMBER DRAWING REVISION DESCRIPTION QUANTITY

40-140 Rev. E dated 05-23-2008 Wheel Assembly 1

Publication Package (P/N PP199-17400)

199-174 P/L ----------------------------- Kit Parts List (This document)

50-130 Rev. A dated 10-23-1995 Installation Drawing
IM199-174 Rev. A dated 10-23-1995 Installation Manual
SA1457GL Issue date 03-15-1990 Supplemental Type Certificate
SA1458GL Issue date 03-15-1990 Supplemental Type Certificate
----------------------------- Pilot Operating Manual Inserts
----------------------------- Warranty Registration Card

NOTES:
1. This kit will convert one aircraft to Cleveland Nose Wheels.

REV. C
REV. B
REV. A
REV. NC
199-174
05-14-2009 (0384-81)
11-19-2007 (0377-29)
10-23-1995 (0318-79)
03-23-1989 (295-57)
 CLEVELAND WHEELS & BRAKES
IM199-174
INSTALLATION MANUAL
FOR
CONVERSION KIT
199-174
FOR
ROCKWELL AERO COMMANDER
MODELS SHRIKE 500 SERIES
AND COMMANDER SERIES

Cleveland
Wheels & Brakes Aerospace
PARKER HANNIFIN CORPORATION - AIRCRAFT WHEEL & BRAKE
1160 Center Road - Avon, Ohio 44011 - Customer Service 1-800-Braking
 STOP!
PLEASE TAKE A FEW MOMENTS TO COMPLETE AND RETURN THE
ATTACHED REGISTRATION CARD. IT IS IMPORTANT THAT ALL
INFORMATION IS LEGIBLY PRINTED. THIS DATA WILL ASSIST PARKER
HANNIFIN, AIRCRAFT WHEEL & BRAKE IN THE EVENT THAT
NOTIFICATION TO END USERS OF SPECIFIC AIRWORTHINESS
DOCUMENTS IS NECESSARY.
 IM199-174 INSTALLATION MANUAL FOR
CONVERSION KIT 199-174
Aerospace

TABLE OF CONTENTS

SECTION SUBJECT PAGE NO.

1.0 Introduction 1
1.1 Purpose 1
1.2 Kit Equipment 1
2.0 TSO Notice 1
3.0 Applicability 2
3.1 KIT 199-174 2
4.0 Safety 2
5.0 Product Registration 2
6.0 Order Information 3
7.0 Equipment Description 3
7.1 Wheel Assembly 3
8.0 Kit Installation 3
8.1 Remove Existing Equipment 3
8.2 Install Cleveland Equipment 4
9.0 Weight and Balance Computations 5
9.1 Weight and Balance Data 5
10.0 Pilot Operating Manual Inserts 5
11.0 Illustrated Parts List - 40-140 Wheel Assembly 6
12.0 Kit Parts List 7

Page i
 IM199-174 INSTALLATION MANUAL FOR
CONVERSION KIT 199-174
Aerospace

LIST OF REVISIONS

REVISION DATE PAGE DESCRIPTION APVD

N/C 03-27-89 ALL Initial Production Release BB

Cleveland Wheels & Brakes (295-57)
Conversion Kit 199-174

A 10-26-95 ALL Reformatted with changes as listed below

4 Sect. 8.2 (a.): “conforming to MIL-G-81322”

was
“Mobil grease 77, Mobilux EP2”

6 Sect. 11.0: Wheel P/N “40-140” was “40-140A”

Item 11: “153-00900 Qty 4”
was
“153-00300 Qty 2”
Item 12: “154-01400 Qty 2”
was
“154-01300 Qty 2”
Delete Item 13: “153-01500,
Ring - Grease Seal, Qty 2”

Figure: Pictorial revision to reflect above

7 Sect. 12.0: Item 1: ”40-140”

was
“40-140A”

Page ii
 IM199-174 INSTALLATION MANUAL FOR
CONVERSION KIT 199-174
Aerospace

1.0 INT RODUCT ION

The information herein addresses the installation of Cleveland Conversion Kit . It is published for
the guidance of qualified maintenance personnel responsible for the installation of Cleveland
Conversion Kit , manufactured by Parker Hannifin Corporation, Aircraft Wheel and Brake.

1.1 PURPOSE

This manual provides the necessary procedures to accomplish installation of Cleveland

Conversion Kit. For information regarding service limits, maintenance and component overhaul,
consult the Wheel and Brake Assemblies Component Maintenance Manual, published by Parker
Hannifin, Aircraft Wheel and Brake. This manual should be passed on to the owner or retained
by the maintenance facility for future reference.

1.2 KIT EQUIPMENT

Each kit contains all materials needed to replace existing equipment with Cleveland Wheels and
Brakes. Kit 199-174 will completely retrofit one aircraft to Cleveland equipment. Refer to Kit
Parts List.

2.0 TSO NOTICE

The wheels used in this conversion kit carry a “TSO” marking which identifies them as having
been fully laboratory tested and qualified to meet the applicable Federal Aviation Agency (FAA)
specifications and requirements.

After final certification, substitution of critical parts or changes of processes or materials are not
permitted without requalification of the assemblies and resubmittal of the test data to the FAA for
approval.

FAA regulations subject both Parker Hannifin, Aircraft Wheel and Brake and the user to constant
surveillance to assure that uncompromising Quality Assurance materials and processing
controls are maintained in order to provide replacement parts that are the same as the parts
originally certified in the assembly.

Page 1
 IM199-174 INSTALLATION MANUAL FOR
CONVERSION KIT 199-174
Aerospace

3.0 APPLICABILITY

3.1 KIT 199-174

The equipment supplied under Kit No. 199-174 is applicable to the following aircraft.

TABLE I, APPLICABILITY

"KIT 199-174": MAKE MODELS

Rockwell Shrike 500 Series: 500, 500A, 500B,

500S, 500U, 560A, 560E
*Rockwell Commander Series: 560F, 680, 680E,
680FL, 680FL(P), 680T, 680V, 680W,
681, 685, 690, 690A, 690B, 690C,
690D, 695, 695A, 695B, 720

* NOTE:
This Kit not applicable to Models 680T, V, and W,
S/N’s 1473 thru 1725 which use 16 x 4.4, 4 ply nose tire.

4.0 SAFETY

Always follow proper safety precautions when handling or servicing any aircraft braking system
or component(s) of such systems.

CAUTIONS and WARNINGS are noted throughout this manual, where applicable. Follow them
when servicing aircraft wheel and brake equipment.

5.0 PRODUCT REGISTRATION

The product registration card is located at the front of this manual. The card is our way of
tracking the conversion kits and your guarantee of receiving any future airworthiness information
applicable to Conversion Kit No. 199-174. Please fill out the registration card completely and
return promptly. Postage is prepaid.

Page 2
 IM199-174 INSTALLATION MANUAL FOR
CONVERSION KIT 199-174
Aerospace

6.0 ORDER INFORMATION

To order spare parts, contact the nearest Parker Hannifin, Aircraft Wheel and Brake distributor in
your area, or contact Aircraft Wheel and Brake at the following address or numbers:

Parker Hannifin Corporation

Aircraft Wheel and Brake
Attn: Customer Service Dept.
1160 Center Road
Avon, Ohio 44011

Telephone: (216) 937-6211

1-800-272-5464

Fax: (216) 937-5409

NOTE: to order the Wheel and Brake Assemblies Component Maintenance Manual, contact
Aircraft Wheel and Brake.

7.0 EQUIPMENT DESCRIPTION

7.1 WHEEL ASSEMBLY

The wheel is cast magnesium and conforms to all tire and rim association standards for a
6.00-6 divided type wheel. It is a tube-type design only.

The wheel incorporates inboard and outboard halves which are fastened together with bolts,
washers, and nuts. The wheel rotates on two tapered roller bearings, which seat in bearing
cups in the wheel half hubs. Felt grease seals provide protection and lubricant retention for the
bearing.

8.0 KIT INSTALLATION

WARNING: Insure aircraft is secure and stable before beginning any work. Working under an
improperly stabilized aircraft could cause injury or death.

8.1 REMOVE EXISTING EQUIPMENT

a. Jack aircraft in accordance with Rockwell Service Manual until tire is clear of ground. Fully
deflate tire.

b. Remove nose wheel, retaining axle spacers, plugs, bolt and nut.

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 IM199-174 INSTALLATION MANUAL FOR
CONVERSION KIT 199-174
Aerospace

8.2 INSTALL CLEVELAND EQUIPMENT

a. The wheels are shipped from the factory as a complete assembly. The bearings are packed
with grease and installed in the wheel halves.

NOTE: Extended storage of lubricated bearings may require relubrication.

Use bearing grease conforming to MIL-G-81322.

b. Remove the following items from both the inboard and outboard side of wheel assembly:
snap rings, grease seals (rings and felts) and bearing cones. Place items on a clean
surface to avoid contamination.

c. Lightly coat/dampen grease seal felts with SAE 10 engine oil.

d. Re-assemble bearing cones, grease seals (rings and felts) and snap rings.

CAUTION: Do not use impact or power wrenches to remove wheel nuts and bolts.

e. Remove all six nuts, twelve washers and six bolts to separate wheel halves.

f. Position inner wheel half sub-assembly on a flat surface with the register side up.

g. Place serviceable tire and tube over inner wheel half sub-assembly and then place outer
wheel half sub-assembly in tire, making sure to properly align inner and outer registers.

h. Slide bolts through the wheel assembly. Install washers and nuts onto bolts. Torque to 150
in-lbs (dry).

i. Inflate tire to airframe manufacturers recommended pressure in a safety cage.

WARNING: Place the wheel/tire in an inflation cage for initial inflation, to

prevent injury to personnel from possible explosion.

j. Install nose wheel / tire assembly and original axle spacers in gear fork and insert axle
through fork spacers and nose wheel.

k. Ins tall axle plugs and axle bolt and nut. Tighten axle bolt until wheel bearings begin to bind,
then bac k off until bearings are free.

Page 4
 IM199-174 INSTALLATION MANUAL FOR
CONVERSION KIT 199-174
Aerospace

9.0 WEIGHT AND BALANCE COMPUTATIONS

Weigh existing nose wheel. Subtract from new weights to derive weight increase created by the
kit installation. Multiply weight increase by applicable aircraft moment and revise weight and
balance information in log book.

9.1 WEIGHT AND BALANCE DATA

New installed (nose gear leg)

Wheel assy........ 5.5 lbs.

Complete form 337 and make appropriate log book entries.

10.0 PILOT OPERATING INSERTS

Inserts are located in front with conversion kit documentation.

Attach label in pilot operating manual as close as possible to the original section labeled Nose
Wheel Assembly. Enter the correct arm and moment in blocks provided. Zero items out for the
original nose wheel that has been removed.

Inserts are reprinted below for reference:

x One 6.00-6 Type III Wheel Assembly, 5.5 ea.

Cleveland P/N 40-140

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 IM199-174 INSTALLATION MANUAL FOR
CONVERSION KIT 199-174
Aerospace

11.0 WHEEL ASSEMBLY IPL

ITEM PART NUMBER DESCRIPTION QTY

1 40-140 Wheel Assembly 1
2 161-08200 Inner Wheel Half Assembly 1
3 151-07900 Inner Wheel Half 1
4 214-00100 Cup-Bearing 1
5 162-07700 Outer Wheel Half Assembly 1
6 152-07800 Outer Wheel Half 1
4 214-00100 Cup-Bearing 1
7 103-20400 Bolt AN5-35A 6
8 095-10500 Washer AN960-516 12
9 094-10400 Nut MS21044-N5 6
10 214-00200 Cone-Bearing 2
NOTES: 11 153-00900 Ring-Grease Seal 4
(1) NOT ILLUSTRATED 12 154-01400 Felt-Grease Seal 2
14 155-00100 Snap Ring 2
15 166-09600 (1) Nameplate 1
16 166-09700 (1) Nameplate 1

FIGURE 1
ILLUSTRATED PARTS LIST (IPL) FOR 40-140 WHEEL ASSEMBLY

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 IM199-174 INSTALLATION MANUAL FOR
CONVERSION KIT 199-174
Aerospace

12.0 KIT PARTS LIST

199-174 KIT

SEE
NOTE PART NUMBER DESCRIPTION QUANTITY

(1) 40-140 Wheel Assembly 1

IM199-174 Installation Manual for 1

Conversion Kit 199-174

50-130 Installation Drawing 1

SA1457GL STC 1
SA1458GL STC 1
------- Pilot Operating Manual Inserts 1
------- Product Registration Card 1

(1) For Subassembly and Parts identification: See Fig 1; 40-140 IPL

Page 7
Parker Hannifin Corporation
Aerospace/Aircraft Wheel & Brake
1160 Center Road
Avon, OH 44011

Date: _ _/_ _/20_ _

Subject: Letter of Authorization for Installation of STC’d Conversion Kits

To whom it may concern:

Parker Hannifin Corporation, Aircraft Wheel & Brake Division, hereby states that
the following item(s):

KIT NUMBER: 199-___________

FAA APPROVAL: 1) STC # ________________________

NO OTHER APPROVALS NECESSARY

AUTHORIZATION TO INSTALL: With the sale of this STC KIT, OWNER of the
Supplemental Type Certificate agrees to permit the buyer or buyer’s agent or
agency to use the certificate to alter the product under the terms and
conditions of this STC.

A/C MAKE: ______________________

A/C MODEL______________________

TAIL # __________________________

Regards,

Technical Support Team

Technical Hotline (800) 272-5464
Clevelandwbhelp@parker.com
Web-site: www.clevelandwheelandbrake.com
Manufacturer of Cleveland Wheels & Brakes