Aircraft Wheels & Brakes
Goodrich Corporation
                                              PO Box 340            Troy, Ohio 45373
                                              Tel: (937) 339-3811 FAX: (937) 440-2055
  These commodities, software, or technology are controlled by the Export Administration Regulations (EAR). They
  are subject to the export control laws of the U.S. Government. They are not to be placed in the public domain,
  exported from the U.S., or given to any foreign person in the U.S., without prior, specific written authorization of
  Goodrich Corporation and the U.S. Department of Commerce.
SUBJECT:             LANDING GEAR - WHEELS AND BRAKES
                     WARNINGS ON INSTALLATION OF PARTS THAT ARE NOT APPROVED BY
                     GOODRICH
USED ON:             Aircraft that use Goodrich wheels and brakes
REFERENCE:           Goodrich Component Maintenance Manuals (CMM’s)
PURPOSE:             This Service Letter gives warnings to not use parts that are not approved by
                     Goodrich for installation in specified assemblies.
DISCUSSION:          The Federal Aviation Administration (FAA) has approved replacement parts that
                     are different from specified parts in applicable Goodrich publications. Goodrich
                     has not done tests on these FAA-approved parts and does not give approval for
                     the installation of these parts.
                     Goodrich uses proprietary design procedures and rigorous tests to show that
                     Goodrich assemblies give specified performance or better-than-specified
                     performance. Tests were done with Goodrich-approved parts in each assembly
                     to show that related subsystems correctly work together as a system for
                     qualification and certification. Some examples of related subsystems include:
                     landing gear, brake control (anti-skid), wheels, brakes, and tires.
                     Goodrich makes wheel assemblies and brake assemblies to aircraft
                     manufacturer specifications, to FAA requirements, and to all other applicable
                     regulations. Goodrich design procedures also use data on wear distribution,
                     thermal balance, dynamic stability, reliability, endurance, torque sensitivity, and
                     environmental exposure. The environmental exposure includes: humidity, icing,
                     salt fog, shock, and vibration. Installation of parts that do not have equivalent
                     design procedures or test results can decrease the performance of wheel
                     assemblies, brake assemblies, or related subsystems.
                     FAA approval of replacement parts in Goodrich assemblies usually is given
                     after tests that are less extensive than performance tests by the aircraft
                     manufacturer and by Goodrich. The Aircraft Flight Manual, Component
                     Maintenance Manuals, and warranties are based on performance tests by the
                     aircraft manufacturer and by Goodrich. The operation of each subsystem
                     depends on all related subsystems to give safe and reliable take-offs and
                     landings. When equivalent tests with FAA-approved parts are not done,
                     Goodrich cannot make sure that the assemblies give safe and reliable
                     performance. Goodrich has policies that follow:
Issued: Dec 18/01                                    SL1914                                           Page 1 of 2
Revision No. 1: Feb 3/06
                                     Aircraft Wheels & Brakes
                                     Goodrich Corporation
                                     PO Box 340            Troy, Ohio 45373
                                     Tel: (937) 339-3811 FAX: (937) 440-2055
    WARNING:     THE USE OF REPLACEMENT PARTS THAT ARE NOT APPROVED BY
                 GOODRICH FOR INSTALLATION IN A SPECIFIED ASSEMBLY WILL
                 AUTOMATICALLY VOID ALL WARRANTIES EXTENDED BY GOODRICH.
    WARNING:     REGARDLESS OF ANY FAA APPROVALS OR DEMONSTRATED
                 COMPLIANCE WITH AIRFRAME MANUFACTURER'S ORIGINAL
                 EQUIPMENT REQUIREMENTS, GOODRICH DOES NOT WARRANT OR
                 ASSUME THE RISK OF THE INSTALLATION OF REPLACEMENT PARTS
                 THAT ARE NOT APPROVED BY GOODRICH FOR INSTALLATION IN A
                 SPECIFIED ASSEMBLY. OPERATORS WHO USE REPLACEMENT
                 PARTS THAT ARE NOT APPROVED BY GOODRICH DO SO AT THEIR
                 OWN RISK AND TAKE FULL RESPONSIBILITY FOR ALL PROPERTY
                 DAMAGE, PERSONAL INJURY, OR DEATH CAUSED BY SUCH
                 REPLACEMENTS PARTS. USE ONLY GOODRICH-APPROVED
                 REPLACEMENT PARTS THAT ARE GIVEN IN THE ILLUSTRATED
                 PARTS LIST OF THE COMPONENT MAINTENANCE MANUAL OR IN
                 SERVICE BULLETINS OR SERVICE LETTERS THAT ARE ISSUED BY
                 GOODRICH.
    WARNING:     GOODRICH ASSUMES NO LIABILITY WHATSOEVER, WHETHER
                 CONTRACTUAL, WARRANTY, TORT OR OTHERWISE, FOR ANY
                 FEDERAL AVIATION ADMINISTRATION SANCTIONS, PRODUCT
                 MALFUNCTIONS, PROPERTY DAMAGE, PERSONAL INJURIES, OR
                 SIMILAR INCIDENTS THAT OCCUR AFTER SUBSTITUTION OF PARTS
                 THAT ARE NOT APPROVED BY GOODRICH, OR SUBSTITUTION OF
                 PARTS WITH ALTERATIONS THAT ARE NOT APPROVED BY
                 GOODRICH MANUALS OR OTHER WRITTEN PROCEDURES THAT ARE
                 ISSUED BY GOODRICH.
         This document is subject to the controls and restrictions on the first page.
Issued: Dec 18/01                           SL1914                                 Page 2 of 2
Revision No. 1: Feb 3/06