McFarlane Aviation Products - APS66-09000

Part Number: APS66-09000

BRAKE LINING, Metallic (Adherent)

Eligibility Notice

Please verify that this product is eligible for your aircraft before adding it to your cart.

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Product Details

Please note:
Eligibility depends on the wheel, brake, and aircraft make, model, and serial number. Please see the current catalog information or click "View Eligible Aircraft" and read any applicable comments to verify and/or determine eligibility.

 

APS Brake Linings  
Improve braking performance

 

             

 

Metallic and Semi-Metallic Brake Linings
Two types of brake linings are available: semi-metallic/organic (abrasive) and metallic (adherent). The part number of the brake assembly as determined by the OEM dictates which type of lining is to be used.

 

The semi-metallic linings are made with Kevlar fibers integrated into the material, providing the greatest stopping power and long lining life. The optimal operating temperature of the semi-metallic linings is 600-900 deg F.

 

The main ingredient in the metallic linings is iron. In an adherent system, a thin layer of lining material transfers and adheres to the disc during break-in. The optimal operating temperature range of the metallic linings is 950-1200 deg F.

 

Brake discsrivets and pins also sold separately. APS linings can be used with any OEM or PMA discs.

 

Warning: 
One of the most important factors in disc and lining performance and safety margins is proper break-in. In order for any brake system to work optimally, the disc and linings must be properly bedded. Please follow the break-in procedures upon installation.

 

Lining Break-In Procedures 

 

Brake bleed valveswheel bearing cups and cones, and wheel grease seals also available.

Supersedures

Eligibility Notice

Please verify that this product is eligible for your aircraft before adding it to your cart.

Click here to view product eligibility.
OEM Part Number McFarlane Part Number Comment
066-09000 APS66-09000
APS066-09000 APS66-09000

Eligible Aircraft

Make Series Model Beginning S/N Ending S/N Quantity Per Aircraft Comment Eligibility Chart
Aero Commander (Rockwell/Gulfstream) 500 500 500-618 500-852 8 With conversion kit # 199-122 or 199-122A. Wheel Assembly P/N 40-198, Brake Assembly P/N 30-159B or 30-159C.
Aero Commander (Rockwell/Gulfstream) 500 500-A 500-A-875 500-A-1276 8 With conversion kit # 199-122 or 199-122A. Wheel Assembly P/N 40-198, Brake Assembly P/N 30-159B or 30-159C.
Aero Commander (Rockwell/Gulfstream) 500 500-B 500-B-893 500-B-1631 8 With conversion kit # 199-122 or 199-122A. Wheel Assembly P/N 40-198, Brake Assembly P/N 30-159B or 30-159C.
Aero Commander (Rockwell/Gulfstream) 500 500-S 500-S-1755 500-S-1756 8 With conversion kit # 199-122 or 199-122A. Wheel Assembly P/N 40-198, Brake Assembly P/N 30-159B or 30-159C.
Aero Commander (Rockwell/Gulfstream) 500 500-S 500-S-1781 500-S-1876 8 With conversion kit # 199-122 or 199-122A. Wheel Assembly P/N 40-198, Brake Assembly P/N 30-159B or 30-159C.
Aero Commander (Rockwell/Gulfstream) 500 500-S 500-S-3050 500-S-3323 8 With conversion kit # 199-122 or 199-122A. Wheel Assembly P/N 40-198, Brake Assembly P/N 30-159B or 30-159C.
Aero Commander (Rockwell/Gulfstream) 500 500-U 500-U-1635 500-U-1780 8 With conversion kit # 199-122 or 199-122A. Wheel Assembly P/N 40-198, Brake Assembly P/N 30-159B or 30-159C.
Beechcraft 18 JRB-6 39763 67381 With STC SA788GL installed
Beechcraft 65 65 L-1 L-6 With STC SA673GL installed
Beechcraft 65 65 LC-1 LC-239
Beechcraft 65 65 LF-7 LF-8
Beechcraft 65 65 (L-23F) L-1 LF-9999
Beechcraft 90 65-90 LJ-1 LJ-113
Beechcraft 90 65-A90 LJ-76 LJ-317
Beechcraft 90 65-A90-1 (U-21A,D; JU-21A; RU-21A,D) LM-1 LM-9999
Beechcraft 90 65-A90-4 (RU-21E,H) LU-1 LU-9999
Beechcraft 90 C90GT LJ-1727 LJ-1852
Beechcraft 90 C90GTi LJ-1769 LJ-9999
Beechcraft 90 C90GTi LJ-1847 LJ-9999
Beechcraft 90 H90 (T-44A) LL-1 LL-9999 With STC SA619GL installed
Fairchild (M7 Aerospace) SA26 SA26-AT 0 ZZZZZZZZZZZZZZZ With STC SA1009GL installed
Fairchild (M7 Aerospace) SA26 SA26-T 0 ZZZZZZZZZZZZZZZ With STC SA1009GL installed
Mitsubishi MU-2B MU-2B-26A 0 ZZZZZZZZZZZZZZZ With STC SA648GL or SA652GL installed

Related Documents

PMA Lists

Aviation Products Systems PMA Supplement 36

Non-Reference Documents

APS Minimum Wear Dimensions

Installation, Use, and Maintenance Instructions

APS Break-In Procedures

Related Product Catalog Pages

APS Catalog Information

Related Items

Please verify product details for suitability for your application.

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