Skip to main content

Technician’s Service Guide

CESSNA 170B · Training Manual

Free account — keep the POHs & checklists you reference in one place.

Overview

This document is a Technician’s Service Guide published by Parker Hannifin Corporation, specifically addressing maintenance and service procedures for Cleveland Wheels & Brakes. It includes detailed instructions on conditioning procedures for brake linings, wear limits for brake discs, and torque values for wheel assemblies. The guide is intended for technicians and maintenance personnel who are responsible for the upkeep of aircraft braking systems. It emphasizes the importance of using approved components and following specific maintenance protocols to ensure safety and performance.

  • Brake linings must be replaced if worn below 0.100 inch (2.54 mm).
  • Cumulative thickness of linings, disc, and pressure plate must be at least 1.00 inch (25.4 mm).
  • Brake discs should be replaced if coning exceeds 0.015 inch (0.381 mm).
  • Torque values for brake disc bolts range from 80 to 150 in-lbs depending on configuration.
  • Use only specified thread lubricants and do not mix different greases.

Document

Source

Originally published by www.parker.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

Report a problem or request removal

Document details

Type
Training Manual
Year
2022
Pages
28
File size
2.4 MB
Publisher
www.parker.com
How rare is it?
1,754CESSNA 170B registered worldwide · 1,496 active

Common. One of the most common aircraft types we track.

Documentation completeness
7/7

Full essential library on file for the CESSNA 170B.

More CESSNA 170Bmanuals & documents

See all 41
Similar aircraft

If you fly the CESSNA 170B, you may also be researching these.

In this document

Conditioning Procedures

The guide outlines specific conditioning procedures for both organic and metallic brake linings. For organic linings, the aircraft should be taxied for 1500 feet at 1700 RPM, applying brakes to achieve a speed of 5-10 mph. For metallic linings, two consecutive full-stop braking applications from 30 to 35 knots are required. Cooling periods of 10-15 minutes are necessary between applications to ensure proper conditioning.

Brake Lining Wear Limits

Brake linings must be replaced if worn below 0.100 inch (2.54 mm). The cumulative thickness of the linings, disc, and pressure plate should be measured, and if it is less than 1.00 inch (25.4 mm) with good linings, the brake disc should be replaced.

Brake Disc Minimum Thickness

The document specifies that brake discs should be inspected for wear, grooves, and pitting. Coning beyond 0.015 inch (0.381 mm) in either direction necessitates replacement. The minimum thickness for various part numbers is provided, ensuring that maintenance personnel can assess the condition of the discs accurately.

Wheel Assembly Torque Values

Torque values for wheel assembly tie bolts and nuts are specified, with dry and lube torque distinctions. For example, brake disc bolts should be dry torqued to 80 in-lbs or 150 in-lbs depending on the configuration. The guide emphasizes the importance of using the correct thread lubricant and not mixing different types of aviation wheel bearing greases.

Safety notes

  • Failure to follow maintenance procedures can lead to serious injury or death.
  • Improper selection or use of components can void warranties.

Full document text

1 Technician’s Service Guide AWBTSG0001-24 Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA i Reference Publication Number: AWBTSG0001-24/USA AWBTSG0001 Issue 24, Dated: April 08, 2022 IMPORTANT NOTE Use of other manufacturer’s components with original Cleveland wheel and brake assemblies will void the Cleveland Wheels & Brakes warranty. © 2022 Parker Hannifin Corporation CONTACT INFORMATION Cleveland Wheels & Brakes, 1160 Center Road • Avon, Ohio 44011 www.clevelandwheelsandbrakes.com www.parker.com E-mail: clevelandwbhelp@parker.com Customer Support Fax: 440-937-5409 Technical Service Hotline: 1-800-BRAKING (1-800-272-5464) Literature Requests: www.atp.com SAFETY WARNING FAILURE OR IMPROPER SELECTION OR IMPROPER USE OF THE PRODUCTS AND/OR SYSTEMS DESCRIBED HEREIN OR RELATED ITEMS CAN CAUSE DEATH, PERSONAL INJURY AND PROPERTY DAMAGE. This document and other information from Parker Hannifin Corporation, its subsidiaries and authorized distributors provide product and/or system options for further investigation by users having technical expertise. It is important that you analyze all aspects of your application, including consequences of any failure, and review the information concerning the product or system in the current product catalog. Due to the variety of operating conditions and applications for these products or systems, the user, through its own analysis and testing, is solely responsible for making the final selection of the products and systems and assuring that all performance, safety and warning requirements of the application are met. The products described herein, including without limitation, product features, specifications, designs, availability and pricing, are subject to change by Parker Hannifin Corporation and its subsidiaries at any time without notice. Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA ii Reference USAGE The procedures in this technician’s guide are applicable to external design wheels and brakes and auxilliary wheels only. Many wheel and brake assemblies have a manual expressly written for their overhaul and maintenance type activities. Before using this guide, consult the Cleveland Wheels & Brakes Technical Support Team for availability of those manuals. This guide is intended as a condensed version of specific data found in AWBCMM0001, the generic Component Maintenance Manual (external design wheels & brakes). AWBCMM0001 contains detailed maintenance/overhaul procedures for external design wheels & brakes that do not have a manual. In addition to this guide and AWBCMM0001, refer to AWBPC0001, Product Catalog for illustrated parts breakdown. These documents are intended to supplement, not replace, the airframe manufacturer’s instructions when Cleveland products are used. Consult the Aircraft Maintenance Manual and Airframe Log Books (for optional installations) to confirm the approved part numbers for the particular aircraft application. If any inconsistencies are observed in this data, please notify Cleveland Wheels & Brakes Customer Support. UPDATES The technician’s guide publication number will reflect the latest issue in effect with a suffix “-X” (X being the latest issue), e.g. AWBTSG0001-6. The publication number will advance numerically with each update issued. Each page will reflect the latest issue in effect. Refer to the Revisions Highlights Page in this publication for details of each update. Consult the Parker Hannifin website, www.parker.com, for current service publications. For additional information regarding publications on CD-Rom, please contact the Cleveland Wheels & Brakes Technical Support Team. Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA iii Revision Highlights Revision 24, dated April 08, 2022 Page Description of Change 14 F. Wheel Assembly Torque Valves updated Added 40-135B and 40-138C data to table 40-135B 150 D 16.9 M 40-138C 180 D 20.3 M Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA 1 Table of Contents SECTION PAGE A. Conditioning Procedures .................................................................. 2 B. Brake Lining Wear Limits ................................................................. 3 C. Brake Disc Minimum Thickness ....................................................... 4 D. Chrome Disc Maintenance............................................................... 7 E. Brake Lining Cross-Reference ......................................................... 7 F. Wheel Assembly Torque Values ..................................................... 11 G. Tire Inflation Valve Stem Torque .................................................... 16 H. Back Plate Tie Bolt Torque ............................................................. 17 I. Special Tools ................................................................................... 21 J. Elastomeric Compound Lubricants ................................................. 21 K. Lubricants....................................................................................... 21 L. Repair Materials ............................................................................. 22 M. Primers and Paints ........................................................................ 23 N. Chemical Stripping Agents ............................................................. 23 Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA 2 A. Conditioning Procedures When new linings have been installed, it is important to condition them properly to obtain the service life designed into them. The metallic and organic linings have different operating characteristics. Separate conditioning procedures are

Show full text

given for metallic and organic linings. ORGANIC LININGS ORGANIC LININGS METALLIC LININGS METALLIC LININGS 1. Taxi aircraft for 1500 feet with engine at 1700 rpm applying brake pedal force as needed to develop a 5-10 mph taxi speed. 1. Perform two (2) consecutive full stop braking applications from 30 to 35 knots. Do not allow the brake discs to cool substantially between the stops. 2. Allow the brakes to cool for 10 to 15 minutes. 2. Allow the brakes to cool for 10 to 15 minutes. 3. Apply brakes and check for restraint at high static throttle. If brakes hold, conditioning is complete. 3. Apply brakes and check for restraint at high static throttle. If brakes hold, conditioning is complete. 4. If brakes cannot hold aircraft during static run-up, allow brakes to completely cool and repeat steps 1 through 3. 4. If brakes cannot hold aircraft during static run-up, allow brakes to cool completely and repeat steps 1 through 3. These conditioning procedures will wear off high spots and generate sufficient heat to create a thin layer of glazed material at the lining friction surface. Normal brake usage should generate enough heat to maintain the glaze throughout the life of the lining. Properly conditioned linings will provide many hours of maintenance free service. A visual inspection of the brake disc will indicate the lining condition. A smooth surface, one without grooves, indicates the linings are properly glazed. If the disc is rough (grooved), the linings must be reglazed. The conditioning procedure should be performed whenever the rough disc condition is observed. Light use, such as in taxiing, will cause the glaze to be worn rapidly and reduce the designed service life of the linings and discs. CAUTION: DUE TO THE EFFICIENCY OF THESE BRAKES, EXTREMELY HARD BRAKING ON AIRCRAFT WITH TAIL WHEELS COULD RESULT IN LIFTING THE TAIL FROM THE GROUND. Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA 3 B. Brake Lining Wear Limits For equipment used on Piper Aztec (using either 164-00206 or 164-03206 disc), see PRM19 or follow the procedure below: • First, measure linings as shown in Figure A1. Linings worn below .100 inch are cause for replacement. • If linings are still usable or are replaced, measure the cumulative thickness of two linings, disc and pressure plate as shown in Figure A1-1. If the stack measures less than 1.00 (1 inch) with good linings (linings above .100 inch) the brake disc is considered below minimum wear thickness and should be replaced. NOTE: On some designs the metallic lining is bonded directly to the pressure plate and back plate. In these cases, the part should be replaced when the lining material is worn to 0.030 inch (0.76 mm) thick. The minimum replacement thickness on metallic and organic linings is 0.100 inch (2.54 mm) except as noted below. Refer to Figure A1. Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA 4 C. Brake Disc Minimum Thickness Figure A2 – Disc Thickness Measurement Under average field conditions, a brake disc should give years of trouble free service. However, unimproved fields, standing water, heavy industrial pollution or infrequent use of the aircraft may necessitate more frequent inspection of discs to prolong the life of the brake lining. Generally, the disc faces should be checked for wear (Figure A2 Dim. “A”), grooves, deep scratches, excessive general pitting or coning of the brake disc. Coning beyond 0.015 inch (0.381 mm) in either direction would be cause for replacement. Single or isolated grooves up to 0.030 inch (0.76 mm) deep should not be cause for replacement, although general grooving of the disc faces will reduce lining life. Discs are plated for special applications only; therefore, rust in varying degrees can occur. If a powder rust appears, one or two braking applications during taxi should wipe the disc clear. Rust allowed to progress beyond this point may require removal of the disc from wheel assembly to properly clean both faces. Wire brushing followed by sanding with 220 grit sandpaper can restore the braking surface for continued use. Note: 164-1XXXX part numbers designate chrome plated discs. 464-XXXXX part numbers designate performace gold discs which are no longer manufactured. Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA 5 C. Brake Disc Minimum Thickness Part Number “A” in/mm 159-00104 0.225/5.715 159-00204 0.475/12.065 164-00206 See Page 3 164-00300 0.205/5.207 164-00400 0.162/4.115 164-00500 0.157/3.988 164-00700 0.345/8.763 164-00806 0.334/8.484 164-00900 0.227/5.766 164-01000 0.345/8.763 164-01100 0.345/8.763 164-01300 0.227/5.764 164-01406 0.334/8.484 164-01501 0.327/8.306 164-01506 0.327/8.306 164-01600 0.157/3.988 164-01700 0.167/4.242 164-01900 0.227/5.766 164-02000 0.205/5.207 164-02201 0.345/8.763 164-02300 0.345/8.763 164-02501 0.445/11.303 164-02502 0.445/11.303 164-02503 0.445/11.303 164-02504 0.445/11.303 164-02505 0.445/11.303 164-02601 0.205/5.207 164-02700 0.330/8.382 164-02701 0.340/8.636 164-02706 0.330/8.382 164-02707 0.330/8.382 164-02800 0.227/5.766 164-02900 0.580/14.732 164-03006 0.282/7.163 164-03106 0.163/4.140 164-03206 See Page 3 164-03300 0.235/5.969 164-03506 0.260/6.604 164-03600 0.327/8.306 164-03601 0.327/8.306 164-03700 0.345/8.763 164-03906 0.600/15.240 164-04000 0.205/5.207 Part Number “A” in/mm 164-04300 0.205/5.207 164-04406 0.334/8.484 164-04600 0.405/10.287 164-04700 0.345/8.763 164-04800 0.327/8.306 164-05006 0.475/12.065 164-05500 0.492/12.497 164-05606 0.395/10.033 164-05700 0.525/13.335 164-05806 0.395/10.033 164-06106 0.475/12.065 164-06306 0.465/11.81 164-06406 0.465/11.811 164-06506 0.240/6.096 164-06700 0.220/5.588 164-06900 0.205/5.207 164-07200 0.492/12.497 164-07306 0.395/10.033 164-07400 0.492/12.497 164-07500 0.205/5.207 164-07700 0.470/11.938 164-07800 0.450/11.43 164-07906 0.465/11.811 164-08100 0.450/11.43 164-08200 0.327/8.306 164-08300 0.327/8.306 164-08406 0.330/8.382 164-08500 0.325/8.255 164-08800 0.190/4.826 164-08900 0.330/8.382 164-09000 0.330/8.382 164-09100 0.492/12.497 164-09200 0.190/4.826 164-09300 0.190/4.826 164-09400 0.190/4.826 164-09500 0.325/8.255 164-09600 0.325/8.255 164-09700 0.325/8.255 164-09900 0.275/6.985 164-10500 0.157/3.988 164-10700 0.345/8.763 164-10900 0.227/5.766 164-11501 0.327/8.306 Part Number “A” in/mm 164-11700 0.164/4.166 164-11800 0.162/4.115 164-11900 0.227/5.766 164-12000 0.205/5.207 164-12300 0.345/8.763 164-12501 0.445/11.303 164-12502 0.445/11.303 164-12504 0.445/11.303 164-12505 0.445/11.303 164-12601 0.205/5.207 164-13300 0.235/5.969 164-13600 0.327/8.306 164-13601 0.327/8.306 164-14000 0.205/5.207 164-14300 0.205/5.207 164-14800 0.327/8.306 164-16700 0.220/5.588 164-17500 0.205/5.207 164-18300 0.327/8.306 164-18800 0.190/4.826 164-18900 0.330/8.382 164-19000 0.330/8.382 164-19200 0.191/4.826 164-19300 0.190/4.826 164-19400 0.190/4.826 164-19500 0.325/8.255 164-19600 0.325/8.255 164-19700 0.325/8.255 164-20100 0.250/6.350 164-20206 0.334/8.484 164-20306 0.465/11.811 164-20500 0.525/13.335 164-20600 0.455/11.557 164-20700 0.410/10.414 164-20806 0.475 /12.065 164-20900 0.410/10.414 164-21000 0.436/11.074 164-21100 0.492/12.497 164-21200 0.327/8.306 164-21406 0.334/8.484 164-21600 0.405/10.287 164-21700 0.475/12.065 164-21900 0.590/14.986 Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA 6 C. Brake Disc Minimum Thickness Part Number “A” in/mm 164-22000 0.360/9.144 164-22201 0.537/13.640 164-22202 0.537/13.640 164-22400 0.385/9.779 164-22900 0.410/10.414 164-23000 0.565/14.351 164-23001 0.582/14.783 164-23002 0.582/14.783 164-23100 0.345/8.763 164-23300 0.475/12.065 164-23400 0.205/5.207 164-23600 0.190/4.826 164-23900 0.325/8.255 164-24000 0.325/8.255 164-24100 0.325/8.255 164-24200 0.167/4.242 164-24400 0.290/7.366 164-24500 0.327/8.306 164-24501 0.327/8.306 164-24800 0.330/8.382 164-25200 0.312/7.925 164-25700 0.445/11.303 164-25800 0.459/11.659 164-30007 0.190/4.826 164-30195 0.190/4.826 164-30388 0.325/8.255 164-30398 0.325/8.255 164-30414 0.325/8.255 164-30440 0.190/4.826 164-30615-1 0.190/4.826 164-30615-2 0.330/8.382 164-30615-3 0.330/8.382 164-30804-1 0.190/4.826 164-30804-2 0.330/8.382 164-30804-3 0.330/8.382 464-11501 0.327/8.306 464-11700 0.164/4.166 464-12000 0.205/5.207 464-12601 0.205/5.207 464-13601 0.327/8.306 464-14000 0.205/5.207 464-14300 0.205/5.207 464-17500 0.205/5.207 464-18300 0.327/8.306 Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA 7 D. Chrome Disc Maintenance The primary purpose of chrome plated discs is to retard corrosion on the disc flange (rubbing surface) which, if pitted, will wear out linings rapidly. Chrome is a porous material which will allow moisture to penetrate and discolor, giving the appearance of corrosion. To restore the original luster of the cup surface, polish with common automotive chrome polish and a non-metallic abrasive pad (such as 3M Scotch Brite®) – DO NOT USE steel wool. The main area of concern should be the disc flange. As long as it is clean and corrosion-free, the disc will provide the service life designed into it. The plating will increase the life of a standard disc. When the plating wears off, which it eventually will, you then have a standard disc to wear down to the minimum thickness. The added benefit is the plating will be intact on the non- rubbing surfaces as opposed to the paint on a standard disc. This cross-reference identifies the proper brake lining for each of the brake assemblies listed. All linings require conditioning prior to use. Abbreviations: Pp = Pressure Plate Tp = Torque Plate N/A = Not Available Bp = Back Plate Cp = Carrier Plate Brake Assembly Lining Qty 30-23 066-06500 Pp 2 066-06200 Bp 2 30-23A 066-06500 Pp 2 066-06200 Bp 2 30-23B 066-06500 Pp 2 066-06200 Bp 2 30-23C 066-06500 Pp 2 066-06200 Bp 2 30-23D 066-06500 Pp 2 066-06200 Bp 2 30-24 066-10600 4 30-28B 066-03300 6 30-28C 066-03300 6 30-28D 066-03300 6 30-30 066-10500 2 30-31 066-11700 Tp 4 066-11900 Cp 4 066-11800 Bp 4 30-32 N/A 30-32A 066-10600 4 Brake Assembly Lining Qty 35-200A 066-11100 2 C2000 066-00504 2 C7000 066-00504 2 C7000A 066-00504 2 30-4 066-11100 2 30-5 N/A 30-6 066-11100 2 30-7 066-11100 2 37-200-2 066-10600 8 30-9 066-10600 2 30-9A 066-10600 2 30-9C 066-10600 2 30-9D 066-10600 2 30-9E 066-10600 2 3000-250 066-10600 2 3000-500 066-10600 2 30-18 066-10600 2 30-19 066-10600 2 30-19A 066-10600 2 30-21 066-10600 4 E. Brake Lining Cross-Reference Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA 8 E. Brake Lining Cross-Reference Brake Assembly Lining Qty 30-32B 066-10600 4 30-32C 066-10600 4 30-32D 066-10600 4 30-32E 066-10600 4 30-35 066-10600 4 30-40 066-10600 2 30-40A 066-10600 2 30-41 066-10600 4 30-41A 066-10600 4 30-41B 066-10600 4 30-45 066-11100 2 30-51 066-10600 4 30-51A 066-10600 4 30-51B 066-10600 4 30-52 066-10500 4 30-52A 066-10500 4 30-52B 066-10500 4 30-52D 066-10500 4 30-52E 066-10500 4 30-52F 066-10500 4 30-52G 066-10500 4 30-52H 066-10500 4 30-52K 066-10500 4 30-52L 066-10500 4 30-52M 066-10500 4 30-52N 066-10500 4 30-52P 066-10500 4 30-52Q 066-10500 4 30-52S 066-10500 4 30-52T 066-10500 4 30-52U 066-10500 4 30-52V 066-10500 4 30-52W 066-10500 4 30-52X 066-10500 4 30-52Y 066-10500 4 30-52Z 066-10500 4 30-52AA 066-10500 4 30-52AB 066-10500 4 30-52AC 066-10500 4 30-53 066-11200 2 30-53A 066-11200 2 30-54 066-10500 4 30-54A 066-10500 4 30-54B 066-10500 4 30-54C 066-10500 4 30-55 066-10500 2 30-55B 066-10500 2 30-56 066-10500 2 Brake Assembly Lining Qty 30-56A 066-10500 2 30-56B 066-10500 2 30-56C 066-10500 2 30-56D 066-10500 2 30-56F 066-10500 2 30-58A N/A 30-58B N/A 30-59 066-11200 2 30-59A 066-11200 2 30-59D 066-11200 2 30-59E 066-11200 2 30-60 066-10600 4 30-60A 066-10600 4 30-60B 066-10600 4 30-61 066-10500 4 30-61A 066-03600 4 30-61B 066-03600 4 30-61D 066-10500 4 30-61E 066-10500 4 30-61F 066-10500 4 30-63 066-10500 2 30-63A 066-10500 2 30-63B 066-10500 2 30-63D 066-10500 2 30-63E 066-10500 2 30-63F 066-10500 2 30-63J 066-10500 2 30-63K 066-10500 2 30-63M 066-10500 2 30-63P 066-10500 2 30-63Q 066-10500 2 30-63S 066-10500 2 30-65 066-10500 4 30-65A 066-10500 4 30-65E 066-10500 4 30-66 066-04400 4 30-66A 066-11000 4 30-66B 066-11000 4 30-66C 066-02200 4 30-66D 066-02200 4 30-66F 066-04400 4 30-66G 066-09700 4 30-66H 066-02200 4 30-67 066-10800 4 30-67A 066-10800 4 30-67B 066-10800 4 30-67C 066-10800 4 30-67D 066-10800 4 Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA 9 E. Brake Lining Cross-Reference Brake Assembly Lining Qty 30-67E 066-10800 8 30-67X 066-10800 4 30-68 066-03300 6 30-68A 066-03300 6 30-68B 066-03300 6 30-69A 066-02200 4 30-69B 066-02200 4 37-200A 066-06500 Pp 4 066-06200 Bp 4 30-74B 066-06700 4 30-75 066-10500 2 30-75A 066-10500 2 30-75B 066-10500 2 30-75X 066-10500 2 30-79 066-10500 2 30-79A 066-10500 2 30-79B 066-10500 2 30-83 066-06200 4 30-83A 066-06200 4 30-84 066-10800 8 30-88 066-02200 8 30-89 066-10800 6 30-89A 066-10800 6 30-89B 066-10800 6 30-89C 066-10800 6 30-89E 066-10800 6 30-91 066-11300 12 30-93 066-04400 6 30-93A 066-02200 6 30-93B 066-04400 6 30-93C 066-09700 6 30-93D 066-04400 6 30-93E 066-04400 6 30-94 066-10800 8 30-95 066-03300 8 30-95A 066-06600 8 30-95B 066-06600 8 30-96 066-06200 8 30-97 066-06400 8 30-98 066-10800 12 30-98A 066-10800 12 30-98B 066-10800 12 30-98C 066-10800 12 30-98D 066-10800 12 30-99 066-06600 8 30-99A 066-06600 8 30-100 066-06600 8 30-103 066-11300 16 Brake Assembly Lining Qty 30-106 066-06800 16 30-107 066-09000 8 30-107A 066-09000 8 30-107B 066-09000 8 30-107C 066-09000 8 30-107D 066-09000 8 30-107E 066-09000 8 30-111 066-10800 8 30-113 066-06400 8 30-113A 066-06400 8 30-123 066-06800 12 30-127 066-06200 4 30-127A 066-06200 4 30-127C 066-06200 4 30-127D 066-06200 4 30-129 066-06200 4 30-131 066-09000 8 30-133 066-10500 2 30-138 066-06800 6 30-139 066-06200 8 30-141 066-07300 8 30-142 066-07300 8 30-143 066-07300 8 30-144 066-09000 8 30-144A 066-09000 8 30-144B 066-09000 8 30-145 066-09700 6 30-146 066-09100 Pp 2 066-09200 Bp 2 30-146A 066-09100 Pp 2 066-09200 Bp 2 30-148 066-11300 16 30-149 066-06600 12 30-158 066-06800 8 30-159 066-09000 8 30-159A 066-09000 8 30-159B 066-09000 8 30-159C 066-09000 8 30-163 066-03300 8 30-164 066-06200 2 30-170 066-10000 8 30-176 066-10800 4 30-181A 066-10600 2 30-182 066-03300 8 30-182A 066-15300 8 30-184 066-10800 8 30-195 066-10800 4 30-195A 066-10800 4 Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA 10 E. Brake Lining Cross-Reference Brake Assembly Lining Qty 30-208 N/A 30-208A 066-12901 2 30-210 066-13100 16 30-210A 066-13100 16 30-210C 066-13100 16 30-214 066-10500 2 30-214B 066-10500 2 30-220 066-13500 Pp 2 066-13700 Bp 2 30-224 066-10500 2 30-231 066-06600 12 30-233 066-06200 4 30-233A 066-06200 4 30-233B 066-06200 4 30-233C 066-15100 4 30-233E 066-15500 4 30-233E RH 066-15500 4 30-236 066-10500 2 30-239 066-14100 2 30-239A 066-14100 2 30-239B 066-14100 2 30-241 066-10500 4 30-269 066-04400 4 30-280 066-10800 4 30-290 066-09100 Pp 1 066-09200 Bp 1 30-293 066-09100 Pp 1 066-09200 Bp 1 30-293 RH 066-09100 Pp 1 066-09200 Bp 1 30-308 066-14800 2 30-312 066-09100 Pp 1 066-09200 Bp 1 C-30018 066-30026 2 C-30018-1 066-30026 2 C-30018-2 066-30026 2 C-30018-3 066-30026 2 C-30018-4 066-30026 2 C-30018-5 066-30026 2 C-30018-6 066-30026 2 C-30018-7 066-30026 2 D-30118-3 066-30026 4 D-30118-4 066-30026 4 D-30118-5 066-30026 4 D-30118-6 066-30026 4 D-30118-7 066-30026 4 D-30118-8 066-30026 4 D-30118-9 066-30026 4 D-30118-10 066-30026 4 C-30764-5 066-30026 2 C-30764-6 066-30026 2 C-30764-7 066-30026 2 D-30793-3 066-30026 4 D-30793-4 066-30026 4 D-30793-5 066-30026 4 D-30793-6 066-30026 4 Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA 11 F. Wheel Assembly Torque Values All wheel assembly tie bolt and nut torque values listed are to be applied to the nut only. A “D” shown adjacent to the torque value indicates the value to be a “Dry” torque only. An “L” shown adjacent to the torque value indicates a “Lube” torque only. Lube requires the application of a thread lubricant to all friction surfaces of the hardware prior to torquing. Only use the thread lubricant specified for your wheel assembly. [A5-#] = Code for inflation valve stem torque. See appropriate dash number, -#, in Table G for torque value. Included in this section is wheel bearing grease information. Beginning March, 2007 all active wheel assemblies listed in the torque values table, except those noted for amphibious application, will be shipped from the Cleveland Wheels & Brakes facility with the bearings packed with Mobil Aviation Grease SHC 100, the approved preferred grease for all Parker Hannifin wheel assemblies. If your non-amphibious wheel assembly was shipped prior to March 2007 it may contain other approved bearing grease. To change to the Mobil Aviation Grease SHC 100, you must completely remove the contained grease and clean the bearings. You must also replace any felt grease seals which were previously lubricated with other approved grease. Refer to Cleveland Wheels & Brakes Component Maintenance Manual, AWBCMM0001, latest issue for additional information and grease packing instructions. Torque Values Bearing Grease CAUTION: DO NOT MIX AVIATION WHEEL BEARING GREASES WITH EACH OTHER. IF USING OTHER APPROVED GREASE, COMPLETE REMOVAL OF CONTAINED GREASE AND BEARING CLEANING IS REQUIRED. REPLACEMENT OF PREVIOUSLY LUBRICATED FELT SEALS IS ALSO REQUIRED. CAUTION: DO NOT LUBRICATE ANY HARDWARE THAT IS SPECIFIED AS A “DRY” TORQUE VALUE. IF THERE IS A CONFLICT OR QUESTION REGARDING TORQUE METHODS OR VALUES ON YOUR ASSEMBLY, PLEASE CONTACT CLEVELAND CUSTOMER SUPPORT FOR RESOLUTION. Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA 12 F. Wheel Assembly Torque Values Table Flag Note Legend: Material Column Designations: “A” Aluminum “M” Magnesium (1) For assistance contact the Technical Services Hotline (page i). Thread Lubricant: (2) Use SAE AMS2518 (ref MIL-T-5544). (3) Use MIL-PRF-83483 (Molydisulphide). Wheel Bearing Grease: All active wheel assemblies listed are shipped with Mobil Aviation Grease SHC 100 except: (4) Wheel uses BG Products HCF Grease P/N 605 (Amphibious) (8) Wheel uses OMNI Waterproof Green Grease, No. 2 (Amphibious). (9) Wheel uses Mobil Aviation Grease SHC 100 ONLY. Torque Values: (5) Dry torque brake disc bolts to 80 in-lbs. (6) Dry torque brake disc bolts to 150 in-lbs. (7) Torque value is dependent on hardware configuration. PRM’s are in development to release the hardware upgrade for the following assemblies. In the interim, follow the wheel assembly nameplate for torque value. The table below is for reference only. For assistance contact the Technical Services Hotline (Page i). Wheel Assembly Nut / Washer Torque in-lb (N-M) 40-87C, 40-110, 40-168 094-01200 / 095-10400 75 D (8.5) 094-10300 / 095-10200 90 D (10.2) 40-87 094-01200 / 095-10400 qty-6 75 D (8.5) 094-10300 / 095-10400 qty-3 90 D (10.2) 40-151, 40-151A, 40-230 094-01200 / 095-10200 75 D (8.5) 094-10300 / 095-10200 90 D (10.2) 40-87A, 40-87D, 40-87F, 40-110B, 40-152 094-01200 / 095-10400 75 D (8.5) 094-10300 / 095-10400 90 D 10.2) Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA 13 F. Wheel Assembly Torque Values Wheel Assembly Bolt Torque Wheel Matl in-lb N•m 27-100D 90 D 10.2 A 21-100D 90 D 10.2 M 3080A 90 D 10.2 M 3080B 90 D 10.2 M 3070 90 D 10.2 M 3040 90 D 10.2 A 3050 90 D 10.2 A 3050A 90 D 10.2 A 38501 90 D 10.2 M 40-12 90 D 10.2 M 40-12A 90 D 10.2 M 40-18 90 D 10.2 M 40-19 90 D 10.2 A 40-19A 90 D 10.2 A 40-21 90 D 10.2 A 40-24 90 D 10.2 A 40-28 90 D 10.2 M 40-28D 90 D 10.2 M 40-30A 90 D 10.2 A 40-32 90 D 10.2 A 40-34 90 D 10.2 M 40-37 90 D 10.2 A 40-40A 135-145 D 15.3-16.4 M 40-40B 135-145 D 15.3-16.4 M 40-40C 90 D 10.2 M 40-40D 150 D 16.9 M 40-41 150 D 16.9 M 40-46 90 D 10.2 A 40-47 150 D 16.9 A 40-50 90 D 10.2 A 40-55 90 D 10.2 A 40-56 150 D 16.9 M 40-56B 150 D 16.9 M 40-56C 150 D 16.9 M 40-57 90 D 10.2 A 40-57A 90 D 10.2 A 40-58 90 D 10.2 M 40-59 150 D 16.9 M 40-59A 150 D 16.9 M 40-59B 150 D 16.9 M 40-59D 150 D 16.9 M 40-59E 150 D 16.9 M 40-60 90 D 10.2 M 40-60A 90 D 10.2 A 40-61 90 D 10.2 M 40-66 90 D 10.2 A 40-67 90 D 10.2 A 40-74 90 D 10.2 A 40-74A 90 D 10.2 A 40-74B 90 D 10.2 A 40-75B 150 D 16.9 M 40-75D 150 D 16.9 M 40-75E 150 D 16.9 M 40-75F 150 D 16.9 M Wheel Assembly Bolt Torque Wheel Matl in-lb N•m 40-75G 150 D 16.9 M 40-75H 150 D 16.9 M 40-75J 150 D 16.9 M 40-75P 150 D 16.9 M 40-75S 150 D 16.9 M 40-75T 150 D 16.9 M 40-75W 150 D 16.9 M 40-75Z 150 D 16.9 M 40-75AA 150 D 16.9 M 40-76A 150 D 16.9 M 40-76B 150 D 16.9 M 40-76C 150 D 16.9 M 40-76D 150 D 16.9 M 40-76E 150 D 16.9 M 40-76F 150 D 16.9 M 40-76G 150 D 16.9 M 40-76H 150 D 16.9 M 40-76P 150 D 16.9 M 40-76-1 150 D 16.9 (1) 40-77 Refer to PRM86 M 40-77A Refer to PRM94 M 40-77B Refer to PRM94 M 40-77C Refer to PRM83 M 40-77D 90 D 10.2 M 40-77E Refer to PRM83 M 40-77F Refer to PRM94 M 40-77G 90 L (2) 10.2 M 40-77H 90-100 L (2) 10.2-11.3 M 40-78 Refer to PRM96 M 40-78A Refer to PRM96 A 40-78B Refer to PRM96 M 40-78E Refer to PRM96 M 40-78J Refer to PRM96 A 40-79 150 D 16.9 M 40-83 150 D 16.9 M 40-83A 150 D 16.9 M 40-83B 150 D 16.9 M 40-84 150 D 16.9 M 40-84A 150 D 16.9 M 40-84B 150 D 16.9 M 40-86 150 D 16.9 M 40-86A 150 D 16.9 M 40-86B 150 D 16.9 M 40-86E 150 D 16.9 M 40-86F 150 D 16.9 M 40-87 (7) M 40-87A (7) M 40-87C (7) A 40-87D (7) M 40-87F (7) M 40-87G 115-135 D 13.0-15.3 M 40-87H 75 D 8.5 A 40-88C 150 D 16.9 M 40-90 150 D 16.9 M Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA 14 F. Wheel Assembly Torque Values Wheel Assembly Bolt Torque Wheel Matl in-lb N•m 40-127 300 L (2) 33.9 A 40-128 180 D 20.3 M 40-128A 180 D 20.3 M 40-128C 180 D 20.3 M 40-128D 180 D 20.3 M 40-128E 180 D 20.3 M 40-129 90 D 10.2 A 40-130 90 D 10.2 M 40-131 (5) 90 D 10.2 M 40-132 [A5-1] 150 D 16.9 M 40-133 150 D 16.9 A 40-134 [A5-2] 150 D 16.9 M 40-134A [A5-2] 150 D 16.9 M 40-135 135-145 D 15.3-16.4 M 40-135A 150 D 16.9 M 40-135B 150 D 16.9 M 40-137 180 D 20.3 A 40-138A 150 D 16.9 M 40-138B 150 D 16.9 M 40-138C 180 D 20.3 M 40-139 150 D 16.9 A 40-140 150 D 16.9 M 40-140A 150 D 16.9 M 40-140B 150 D 16.9 M 40-140C 150 D 16.9 M 40-141 150 D 16.9 M 40-142 150 D 16.9 M 40-142A 150 D 16.9 M 40-143 150 D 16.9 M 40-148 [A5-3] 300 D 33.9 M 40-151 (7) M 40-151A (7) A 40-152 (7) M 40-162 150 D 16.9 M 40-163 150 D 16.9 M 40-166 [A5-1] (6) 300 D 33.9 M 40-167 (6) 300 D 33.9 M 40-168 (7) A 40-169 [A5-1] (6) 150 D 16.9 M 40-170 [A5-3] 300 L (2) 33.9 M 40-170A [A5-3] 300 L (2) 33.9 A 40-170B [A5-3] 300 L (2) 33.9 M 40-171 180 D 20.3 M 40-172 180 D 20.3 M 40-174 300 L (2) 33.9 A 40-175 150 D 16.9 A 40-176 [A5-1] 300 D 33.9 A 40-176A [A5-1] 300 D 33.9 A 40-177A (9) 150 D 16.9 M 40-179 (9) 150 D 16.9 A 40-179A 150 D 16.9 A 40-181B [A5-1] 180 D 20.3 A 40-181C [A5-1] 180 D 20.3 A 40-193 150 D 16.9 A Wheel Assembly Bolt Torque Wheel Matl in-lb N•m 40-90A 150 D 16.9 M 40-90B 150 D 16.9 M 40-90D 150 D 16.9 M 40-90E 150 D 16.9 M 40-90F 150 D 16.9 M 40-96E 150 D 16.9 M 40-97A 150 D 16.9 M 40-97B 150 D 16.9 M 40-97C 150 D 16.9 M 40-97D 150 D 16.9 M 40-97E 150 D 16.9 M 40-97F 150 D 16.9 M 40-98 150 D 16.9 M 40-98A 150 D 16.9 M 40-98D 150 D 16.9 M 40-98E 150 D 16.9 M 40-98F 150 D 16.9 M 40-98G 150 D 16.9 M 40-98H 150 D 16.9 M 40-98N 150 D 16.9 M 40-98P 150 D 16.9 M 40-99 90 D 10.2 M 40-101 90 D 10.2 A 40-101A 90 D 10.2 A 40-101D 90 D 10.2 A 40-101E 90 D 10.2 A 40-101F 90 D 10.2 A 40-102 90 D 10.2 M 40-102A 90 D 10.2 M 40-103 90 D 10.2 A 40-103A 90 D 10.2 A 40-106 150 D 16.9 M 40-106A 150 D 16.9 M 40-107A [A5-3] 300 L (2) 33.9 M 40-110 (7) M 40-110B (7) M 40-111 150 D 16.9 M 40-111A 150 D 16.9 M 40-112 90 D 10.2 A 40-113 90 D 10.2 A 40-113A 90 D 10.2 A 40-113B 90 D 10.2 A 40-113C 90 D 10.2 A 40-113X 90 D 10.2 A 40-115 90 D 10.2 M 40-115A 115-135 D 13.0-15.3 M 40-115B 115-135 D 13.0-15.3 M 40-115C 115-135 D 13.0-15.3 M 3080D (5) 90 D 10.2 M 40-117A 150 D 16.9 M 40-120 150 D 16.9 M 40-120A 150 D 16.9 M 40-120C 150 D 16.9 M 40-124 180 D 20.3 M Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA 15 F. Wheel Assembly Torque Values Wheel Assembly Bolt Torque Wheel Matl in-lb N•m 40-195 150 D 16.9 M 40-196 90 D 10.2 A 40-198 [A5-3] 300 L (2) 33.9 A 40-199 90 D 10.2 A 40-199A 90 D 10.2 A 40-202 [A5-1] 300 L (1) 33.9 A 40-203 [A5-4] 290-300 L (2) 32.8-33.9 A 40-204 [A5-4] 290-300 L (2) 32.8-33.9 A 40-205 [A5-1] 180 D 20.3 M 40-210 [A5-6] 150 L (2) 16.9 M 40-211 [A5-3] 300 D 33.9 M 040-21101 [A5-3] 300 L (2) 33.9 M 40-212 [A5-1] 150 L (2) 16.9 M 40-223 90 D 10.2 A 40-230 (7) M 40-234 90 D 10.2 A 40-239 [A5-6] 300 L (2) 33.9 A 040-23901 [A5-6] 300 L (2) 33.9 A 40-240A [A5-6] 125 L (2) 14.1 M 40-255 [A5-1] 90-100 L (2) 10.2-11.3 M 40-256 135-145 D 15.3-16.4 M 40-258 300 D 33.9 (1) 40-259 [A5-1] 95-105 L (2) 10.7-11.8 M 40-260 [A5-1] 95-105 L (2) 10.7-11.8 M 40-262A [A5-6] 90 L (2) 10.2 M 40-262AA [A5-6] 90-100 L (2) 10.2-11.3 M 40-270 [A5-6] 115-135 L (2) 13.0-15.3 M 40-273 [A5-5] 300 L (2) 33.9 A 40-273A [A5-4] 290-300 L (2) 32.8-33.9 A 40-273B [A5-4] 290-300 L (2) 32.8-33.9 A 40-276 [A5-6] 90-100 L (2) 10.2-11.3 M 40-279 [A5-3] 300 L (2) 33.9 M 40-279A 300 L (3) 33.9 M 40-281 90 D 10.2 M 40-289 [A5-1] 300 L (2) 33.9 M 40-293 [A5-6] 180-190 L (2) 20.3-21.5 M 40-307 75 D 8.5 M 40-308 75 D 8.5 M 40-403 150 D 16.9 A 40-406 150 D 16.9 M 40-406A 150 D 16.9 M 40-406B 150 D 16.9 M 40-406C 150 D 16.9 M 40-407 150 D 16.9 M 40-414 150 D 16.9 M 40-414A 150 D 16.9 M 40-417 [A5-7] 115-125 L (3) 13.0-14.1 A 40-418 (4) 150 D 16.9 A 40-418A (4) 150 D 16.9 A 40-418B (8) 150 D 16.9 A 40-418C (4) 150 D 16.9 A 40-423 [A5-8] 170-190 L (3) 19.2-21.5 A 40-426 (4) 150 D 16.9 A 40-426A (8) 150 D 16.9 A Wheel Assembly Bolt Torque Wheel Matl in-lb N•m 40-426B 150 D 16.9 A 40-426C 150 D 16.9 A 40-432 [A5-1] 115-125 L (3) 13.0-14.1 A 40-434 [A5-6] 315-325 L (3) 35.6-36.7 A 40-450 105-115 L (2) 11.9-13.0 A 40-455 150 D 16.9 A 40-459 150 D 16.9 M 040-46900 [A5-1] 115-125 L (3) 13.0-14.1 M 40-481 [A5-1] 290-300 L (2) 32.8-33.9 A 40-483 [A5-1] 290-300 L (3) 32.8-33.9 M C-30174-1 95 D 10.7 (1) C-30179 95 D 10.7 (1) D-30204 95 D 10.7 (1) D-30255 195 D 22.0 (1) D-30260 195 D 22.0 (1) D-30260-1 195 D 22.0 (1) D-30291-1 195 D 22.0 A D-30291-2 195 D 22.0 A D-30291-3 195 D 22.0 A D-30291-4 195 D 22.0 A D-30291-5 195 D 22.0 A D-30291-6 195 D 22.0 A D-30380 95 D 10.7 A C-30480 195 D 22.0 (1) D-30500 145 D 16.4 A D-30500-1 145 D 16.4 A D-30570 195 D 22.0 A D-30580 195 D 22.0 (1) D-30585 195 D 22.0 (1) D-30660-1 145 D 16.4 A D-30660-2 145 D 16.4 A D-30660-3 145 D 16.4 A D-30660-4 145 D 16.4 A D-30660-5 145 D 16.4 A D-30660-6 145 D 16.4 A D-30660-7 145 D 16.4 A D-30660-8 145 D 16.4 A D-30660-9 145 D 16.4 A D-30660-10 145 D 16.4 A D-30665 145 D 16.4 A D-30665-1 145 D 16.4 A Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA 16 F. Wheel Assembly Torque Values G. Tire Inflation Valve Stem Torque Inflation Valve Code Dash No. [A5-#] Inflation Valve P/N Recommended Torque in-lb N•m A5-1 160-00700 50-60 5.7-6.8 A5-2 160-00900 165-200 18.7-22.6 A5-3 160-01100 75-100 8.4-11.3 A5-4 160-01200 35-45 4.0-5.1 A5-5 160-01500 70-80 7.9-9.0 A5-6 160-01900 50-60 5.7-6.8 A5-7 160-02000 25-35 2.8-4.0 A5-8 160-01900 45-55 5.08-6.21 Table G. Tire Inflation Valve Stem Torque provides the recommended torque value for the applicable inflation valve of listed wheel assemblies in section F. A code following the P/N, e.g. [A5-#] will correspond to the code in Table G. Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA 17 H. Back Plate Tie Bolt Torque A “D” shown adjacent to the torque value indicates the value to be a “Dry” torque only. An “L” shown adjacent to the torque value indicates a “Lube” torque only. Lube requires the application of a thread lubricant to all friction surfaces of the hardware prior to torquing. Only use the thread lubricant specified for your brake assembly. A flag note will specify which thread lubricant to use. Overtorquing (exceeding these values) could cause depressions in the brake cylinder, which result in dragging or bound up brakes. Use a torque wrench when installing back plate bolts to ensure the proper torquing values are attained. Replace the back plate tie bolts with approved bolts as shown in the Cleveland Product Catalog. Depressions in the brake cylinder (surface A) exceeding 0.005 inch (0.127 mm) deep require replacement of the brake cylinder. BACK PLATE BOLTS BACK PLATE BOLTS SURFACE A Figure A3 – Back Plate Tie Bolts Table Flag Note Legend: Material Column Designations: “A” Aluminum “M” Magnesium “S” Steel (1) For assistance contact the Technical Services Hotline (page i). Thread Lubricant: (2) Use SAE AMS2518 (ref MIL-T-5544). (3) Use MIL-PRF-83483 (Molydisulphide). Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA 18 H. Back Plate Tie Bolt Torque Brake Assembly Bolt Torque Matl in-lb N•m Housing Torque Plate 35-200A 60 D 6.8 A S 30-4 60 D 6.8 A S 30-5 60 D 6.8 A S 30-6 60 D 6.8 A S 30-7 60 D 6.8 A S 30-4 60 D 6.8 A S 37-200-2 90 D 10.2 A S 30-9 75-80 D 8.5-9.0 A S 30-9A 75-80 D 8.5-9.0 A S 30-9C 75-80 D 8.5-9.0 A S 30-9D 75-80 D 8.5-9.0 A S 30-9E 75-80 D 8.5-9.0 A S 3000-250 90 D 10.2 A S 3000-500 90 D 10.2 A S 30-18 75-80 D 8.5-9.0 A S 30-19 75-80 D 8.5-9.0 A S 30-19A 75-80 D 8.5-9.0 A S 30-21 65-75 D 7.3-8.5 A S 30-23 65-75 D 7.3-8.5 A N/A 30-23A 65-75 D 7.3-8.5 A N/A 30-23B 65-75 D 7.3-8.5 A N/A 30-23C 65-75 D 7.3-8.5 A N/A 30-23D 65-75 D 7.3-8.5 A N/A 30-24 65-75 D 7.3-8.5 A S 30-28B 80-90 D 9.0-10.2 M M 30-28C 80-90 D 9.0-10.2 M M 30-28D 80-90 D 9.0-10.2 M M 30-30 90 D 10.2 M S 30-31 1/4-28 85-90 D 9.6-10.2 A S 3/8-24 125-150 D 14.0-17.0 30-32 65-75 D 7.3-8.5 A S 30-32A 65-75 D 7.3-8.5 A S 30-32B 65-75 D 7.3-8.5 A S 30-32C 65-75 D 7.3-8.5 A S 30-32E 65-75 D 7.3-8.5 A S 30-35 65-75 D 7.3-8.5 A S 30-40 60 D 6.8 A S 30-40A 75-80 D 8.5-9.0 A S 30-41 65-75 D 7.3-8.5 A N/A 30-41A 90 D 10.2 A S 30-41B 65-75 D 7.3-8.5 A N/A 30-45 60 D 6.8 A S 30-51 65-75 D 7.3-8.5 A S 30-51A 65-75 D 7.3-8.5 A S 30-51B 65-75 D 7.3-8.5 A S 30-52 90 D 10.2 M S 30-52A 90 D 10.2 M S 30-52B 90 D 10.2 M S 30-52D 90 D 10.2 M S 30-52E 90 D 10.2 M S 30-52F 90 D 10.2 M S Brake Assembly Bolt Torque Matl in-lb N•m Housing Torque Plate 30-52G 90 D 10.2 M S 30-52H 90 D 10.2 M S 30-52K 90 D 10.2 M S 30-52L 75-80 D 8.5-9.0 M N/A 30-52M 90 D 10.2 M S 30-52N 90 D 10.2 M S 30-52P 90 D 10.2 M S 30-52Q 90 D 10.2 M S 30-52S 90 D 10.2 M S 30-52T 90 D 10.2 M S 30-52U 90 D 10.2 M S 30-52V 90 D 10.2 M S 30-52W 90 D 10.2 M S 30-52X 90 D 10.2 M S 30-52Y 90 D 10.2 M S 30-52Z 90 D 10.2 M S 30-52AA 90 D 10.2 M S 30-52AB 90 D 10.2 M S 30-52AC 90 D 10.2 M S 30-53 75-80 D 8.5-9.0 M S 30-53A 75-80 D 8.5-9.0 M S 30-54 90 D 10.2 M A 30-54A 90 D 10.2 M A 30-54B 90 D 10.2 M S 30-54C 85-90 D 9.6-10.2 M A 30-55 75-80 D 8.5-9.0 M S 30-55A 75-80 D 8.5-9.0 (1) (1) 30-55B 75-80 D 8.5-9.0 M S 30-56 75-80 D 8.5-9.0 M S 30-56A 75-80 D 8.5-9.0 M S 30-56B 75-80 D 8.5-9.0 M S 30-56C 75-80 D 8.5-9.0 M S 30-56D 75-80 D 8.5-9.0 M S 30-56F 75-80 D 8.5-9.0 M S 30-58A 75-80 D 8.5-9.0 (1) (1) 30-58B 75-80 D 8.5-9.0 M (1) 30-59 75-80 D 8.5-9.0 M S 30-59A 75-80 D 8.5-9.0 M S 30-59E 75-80 D 8.5-9.0 M S 30-60 75-80 D 8.5-9.0 A S 30-60A 65-75 D 7.3-8.5 A S 30-60B 65-75 D 7.3-8.5 A S 30-61 90 D 10.2 M S 30-61A 90 D 10.2 M S 30-61B 65-75 D 7.3-8.5 M S 30-61D 90 D 10.2 M S 30-61E 90 D 10.2 M S 30-61F 90 D 10.2 M S 30-63 75-80 D 8.5-9.0 M S 30-63A 75-80 D 8.5-9.0 M S 30-63B 75-80 D 8.5-9.0 M S 30-63D 75-80 D 8.5-9.0 M S 30-63E 75-80 D 8.5-9.0 M S Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA 19 H. Back Plate Tie Bolt Torque Brake Assembly Bolt Torque Matl in-lb N•m Housing Torque Plate 30-93E 90-100 D 10.2-11.3 M M 30-94 80-90 D 9.0-10.2 A A 30-95 60 D 6.8 (1) (1) 30-95A 60 D 6.8 M M 30-95B 60 D 6.8 M M 30-96 60 D 6.8 M S 30-97 80-90 D 9.0-10.2 A M 30-98 80-90 D 9.0-10.2 A A 30-98A 80-90 D 9.0-10.2 A A 30-98B 80-90 D 9.0-10.2 A A 30-98C 80-90 D 9.0-10.2 A A 30-98D 80-90 D 9.0-10.2 A A 30-99 75-80 D 8.5-9.0 M A 30-99A 75-80 D 8.5-9.0 M M 30-100 75-80 D 8.5-9.0 M M 30-106 80-90 D 9.0-10.2 M M 30-107 85-90 D 9.6-10.2 A M 30-107A 85-90 D 9.6-10.2 A M 30-107B 85-90 D 9.6-10.2 A M 30-107C 85-90 D 9.6-10.2 A M 30-107D 85-90 D 9.6-10.2 A M 30-107E 80-95 D 9.0-10.7 A M 30-111 80-90 D 9.0-10.2 A A 30-113 80-90 D 9.0-10.2 A M 30-113A 80-90 D 9.0-10.2 A M 30-123 80-90 D 9.0-10.2 M M 30-127 90 D 10.2 M S 30-127A 90 D 10.2 M S 30-127C 90 D 10.2 M S 30-127D 90 D 10.2 M S 30-129 75-90 D 8.5-10.2 M S 30-131 80-90 D 9.0-10.2 A M 30-133 75-80 D 8.5-9.0 M S 30-138 80-90 D 9.0-10.2 M M 30-139 75-80 D 8.5-9.0 M S 30-141 150 D 16.9 A M 30-142 150 D 16.9 A M 30-143 150 D 16.9 A M 30-144 85-90 D 9.6-10.2 A M 30-144A 85-90 D 9.6-10.2 A M 30-144B 85-90 D 9.6-10.2 A M 30-145 80-90 D 9.0-10.2 M M 30-146 85-90 D 9.6-10.2 A M 30-146A 85-90 D 9.6-10.2 A A 30-149 80-90 D 9.0-10.2 A A 30-158 80-90 D 9.0-10.2 M M 30-159 85-90 D 9.6-10.2 A M 30-159A 85-90 D 9.6-10.2 A M 30-159B 85-90 D 9.6-10.2 A M 30-159C 85-90 D 9.6-10.2 A M 30-163 85-90 D 9.6-10.2 M A 30-164 75-80 D 8.5-9.0 M S 30-170 80-85 D 9.0-9.6 A A Brake Assembly Bolt Torque Matl in-lb N•m Housing Torque Plate 30-63F 75-80 D 8.5-9.0 M S 30-63J 75-80 D 8.5-9.0 M S 30-63K 75-80 D 8.5-9.0 M S 30-63M 75-80 D 8.5-9.0 M S 30-63P 75-80 D 8.5-9.0 M S 30-63Q 75-80 D 8.5-9.0 M S 30-63S 75-80 D 8.5-9.0 M S 30-65 75-90 D 8.5-10.2 M S 30-65A 75-90 D 8.5-10.2 M S 30-65E 75-90 D 8.5-10.2 M S 30-66 90 D 10.2 M A 30-66A 90 D 10.2 M M 30-66B 90 D 10.2 M A 30-66C 90 D 10.2 M A 30-66D 90 D 10.2 M (1) 30-66F 90 D 10.2 M M 30-66G 80-90 D 9.0-10.2 M A 30-66H 75-90 D 8.5-10.2 M S 30-67 85-90 D 9.6-10.2 A A 30-67A 85-90 D 9.6-10.2 A A 30-67B 85-90 D 9.6-10.2 A A 30-67C 85-90 D 9.6-10.2 A A 30-67D 85-90 D 9.6-10.2 A A 30-67E 85-90 D 9.6-10.2 A A 30-67X 85-90 D 9.6-10.2 A A 30-68 75-80 D 8.5-9.0 M M 30-68A 75-80 D 8.5-9.0 M M 30-68B 75-80 D 8.5-9.0 M M 30-69A 85-95 D 9.6-10.7 M M 30-69B 90 D 10.2 M M 37-200A 65-70 D 7.3-7.9 A S 30-74B 60-75 D 6.8-8.5 M M 30-75 75-80 D 8.5-9.0 A S 30-75A 75-80 D 8.5-9.0 A S 30-75B 75-80 D 8.5-9.0 A S 30-75X 75-80 D 8.5-9.0 A S 30-79 90 D 10.2 A S 30-79A 90 D 10.2 A S 30-79B 90 D 10.2 A S 30-83 90 D 10.2 M S 30-83A 90 D 10.2 M S 30-84 80-90 D 9.0-10.2 A N/A 30-88 75-80 D 8.5-9.0 M A 30-89 80-90 D 9.0-10.2 A A 30-89A 80-90 D 9.0-10.2 A A 30-89B 80-90 D 9.0-10.2 A A 30-89C 80-90 D 9.0-10.2 A A 30-89E 80-90 D 9.0-10.2 A A 30-93 80-90 D 9.0-10.2 M M 30-93A 80-90 D 9.0-10.2 M M 30-93B 80-90 D 9.0-10.2 M M 30-93C 80-90 D 9.0-10.2 M M 30-93D 80-90 D 9.0-10.2 M M Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA 20 H. Back Plate Tie Bolt Torque Brake Assembly Bolt Torque Matl in-lb N•m Housing Torque Plate 30-176 85-90 D 9.6-10.2 A A 30-181A 75-80 D 8.5-9.0 A S 30-182 85-90 D 9.6-10.2 M A 30-182A 85-90 D 9.6-10.2 M A 30-184 80-90 D 9.0-10.2 A A 30-195 85-90 D 9.6-10.2 A A 30-195A 85-90 D 9.6-10.2 A A 30-210 80-85 L (2) 9.0-9.6 A A 30-210A 80-85 L (3) 9.0-9.6 A A 30-210C 80-85 L (3) 9.0-9.6 A A 30-214 75-80 D 8.5-9.0 M S 30-214B 75-80 D 8.5-9.0 M S 30-220 85-90 D 9.6-10.2 A M 30-224 75-80 D 8.5-9.0 M S 30-231 80-90 D 9.0-10.2 A A 30-233 90 D 10.2 M S 30-233A 90 D 10.2 M S 30-233B 90 D 10.2 M S 30-233C 90 D 10.2 M S 30-233E 85-95 D 9.6-10.2 M S 30-233E RH 85-95 D 9.6-10.2 M S 30-236 75-80 D 8.5-9.0 M N/A 30-239 75-80 D 8.5-9.0 M S 30-239A 75-80 D 8.5-9.0 M S 30-239B 75-80 D 8.5-9.0 A S 30-241 90 L (3) 10.2 A S 30-269 90 D 10.2 M A 30-280 85-90 D 9.6-10.2 A A 30-290 85-90 D 9.6-10.2 A S 30-293 85-90 D 9.6-10.2 A S 30-293 RH 85-90 D 9.6-10.2 A S 30-308 75-80 D 8.5-9.0 M S 30-312 85-90 D 9.6-10.2 A S C-30018 120-130 D 13.6-14.7 A S C-30018-1 120-130 D 13.6-14.7 A S C-30018-2 120-130 D 13.6-14.7 A S C-30018-3 120-130 D 13.6-14.7 A S C-30018-4 120-130 D 13.6-14.7 A S C-30018-5 120-130 D 13.6-14.7 A S C-30018-6 120-130 D 13.6-14.7 A S C-30018-7 120-130 D 13.6-14.7 A S D-30118-3 100-110 D 11.3-12.4 A S D-30118-4 100-110 D 11.3-12.4 A S D-30118-5 100-110 D 11.3-12.4 A S D-30118-6 100-110 D 11.3-12.4 A S D-30118-7 100-110 D 11.3-12.4 A S D-30118-8 100-110 D 11.3-12.4 A S D-30118-9 100-110 D 11.3-12.4 A S D-30118-10 100-110 D 11.3-12.4 A S C-30764-5 120-130 D 13.6-14.7 A S C-30764-6 120-130 D 13.6-14.7 A S C-30764-7 120-130 D 13.6-14.7 A S D-30793-3 100-110 D 11.3-12.4 A S Brake Assembly Bolt Torque Matl in-lb N•m Housing Torque Plate D-30793-4 100-110 D 11.3-12.4 A S D-30793-5 100-110 D 11.3-12.4 A S D-30793-6 100-110 D 11.3-12.4 A S Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA 21 I. Special Tools J. Elastomeric Compound Lubricants K. Lubricants Wheel Bearing Grease – Refer to Topic F, Bearing Grease paragraph MIL-PRF-81322, Grade 2 or DOD-G-24508A (Aeroshell Grease 22) Shell Oil Company, Metairie, LA Mobil Aviation Grease SHC 100 ExxonMobil Oil Corp., Beaumont, TX HCF Grease P/N 605 (Amphibious) BG Products, Wichita, KS OMNI Waterproof Green Grease, No. 2 (Amphibious) OMNI Lubricants, Lewisville, TX Bolts/Nuts Thread Lubricant – Only use the thread lubricant specified for your assembly per SAE-AMS2518 (ref MIL-T-5544) Armite Laboratories, Costa Mesa, CA Royco 44 - Royal Lubricant, East Hanover, NJ per MIL-PRF-83483 (Molydisulphide) Moly-50 P/N 51094 – Fel-Pro Chemical Products L.P., Skokie, IL Pneumatic Applications Grease per MIL-G-4343 Royco 43 – Royal Lubricants Co., East Hanover, NJ Aeroshell 43 – Royal Lubricants Co., Inc., East Hanover, NJ Cosmolube 615 – Houghton International, Inc., Fogelsville, PA Other: 55 O-Ring Lubricant - Dow Corning Corp., Midland, MI Hydraulic Applications - Use fluids compatible with the system MIL-H-5606 / MIL-H-83282 (Red Oils) Skydrol – Only compatible with itself Item Part No. Description Parker O-Ring Extractor Kit 199-18 Consists of Multi-hook, Multi-ramp & Case Brake Line Bleeder 087-00500 The brake line bleeder can be used to service all Cleveland hydraulic brake assemblies or any other brake assembly utilizing the 079-00300 FC6446) Bleeder Screw. Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA 22 L. Repair Materials K. Lubricants Aluminum - Conversion Coating per MIL-C-5541, Class 1A, (Alodine) Magnesium - For parts surface pretreated per AMS-M-3171 (MIL-M-3171) (dull bronze to bright gold appearance) • Surface pretreament per AMS-M-3171 (MIL-M-3171) Type III (dip), Type VI (brush on), or Type VIII (dip) • IRIDITE 15, MacDermid Inc., Waterbury, CT (800-325-4158) (use instructions furnished by Mfr. for AZ81 & AZ91 magnesium) For parts pretreated with Oxsilan® (clear to iridescent appearance) • Oxsilan® MG 0610, Chemetall Oakite, www.chemetall.com Pipe Threads (Brake Cylinder Inlet Fittings) - Apply to first 3 threads Lubon #404EU - Oil Center Research (Balmar LLC), Lafayette, LA Loctite 567 Thread Sealant - Henkel Corp., Rocky Hill, CT Loctite 592 Thread Sealant w/PTFE - Henkel Corp., Rocky Hill, CT PPG JC5A Jointing Compound - PPG Aerospace PRC-DeSoto, Sylmar, CA Anchor Bolts/Torque Plate Bushings Amphibious Environment Lubriplate X-357 Extreme Pressure Moly Lubricant Non-Amphibious Environment Silicone Spray Dri-Slide® Multi-Purpose Lubricant LPS Force 842® Dry Moly Lubricant Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Guide AWBTSG0001-24/USA 23 M. Primers and Paints N. Chemical Stripping Agents For Magnesium alloys AZ81 and AZ Turco Products (Carson, CA) www.hstna.com/turco/aviation.cfm • Spray or brush on application: Water Based Environmentally Advantaged Paint Remover P/N T-6813 or T-6840S • Tank type stripping application: Diphase Hot Tank Paint Remover P/N T-6813 or T-5668 Color Sherwin Williams, Cleveland, OH www.sherwin-williams.com White Paint Primer: P60G2, P60G10, or PSE2130-WHITE Topcoat: F63W13 (White) Silver Paint Primer: P60G2, P60G10, or PSE2130-WHITE Topcoat: F63BXS58-4337 (Silver) Silver Paint (brake discs) Primer: P60G2, P60G10, or PSE2130-WHITE Topcoat: F63BXS58-4337 (Silver) ZRC Products www.zrcworldwide.com • ZRC Galvilite Cold Galvanizing Compound (per MIL-P-26915A) – P/N 11011-10014 Return to Table of Contents Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE Return to Table of Contents Parker Hannifin Corporation • Aircraft Wheel & Brake Division 1160 Center Road • Avon, Ohio 44011 Web site: www.clevelandwheelsandbrakes.com or www.parker.com E-mail: clevelandwbhelp@parker.com • Fax (440) 937-5409 Technical Services Hotline: 1-800-BRAKING (1-800-272-5464) • (440) 937-1213 AWBTSG0001-24 Released: 4/18/2022 Delivered from Parker Vault - VERIFY REVISION BEFORE USE

Type certificate, explained

What's in the CESSNA 170B TCDS

A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.

TCDS A-799Rev 54· Issued 2004
Read the full TCDS

261 CESSNA 170B parts for sale

See all →

Parts listed for sale by vetted eBay sellers — confirmed on eBay at checkout.