CTHIn ForceLegislation
AD/BEECH 36/53 - Chafing of Wire Harness/Connector and Fuel Line
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AD/BEECH 36/53 - Chafing of Wire Harness/Connector and Fuel Line
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| AD/BEECH 36/53 | Chafing of Wire Harness/Connectorand Fuel Line | 9/2009 DM |
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| Applicability: | Model G36 aeroplanes, serial numbers E- 3630, E-3636 through E-3817, E-3819 through E-3834, E-3836 through E-3887, E-3889 through E-3896, E-3898 andE-3899. |
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| Requirement: | 1. Inspect for the following in accordance with Hawker Beechcraft Mandatory Service Bulletin SB 28-3967, dated June 2009: |
| a. Improper installation of the P60 / J60 electrical connector, associated wiring and fuel line, and | |
| b. Chafing damage of the electrical wiring and fuel line. | |
| 2. If, as a result of the Requirement 1 inspections any of the following discrepancies are found accomplish corrective actions following in accordance with SB28-3967: | |
| a. Improper installation of the P60 / J60 electrical connector, associated wiring or fuel line, correct the installation of the P60 / J60 electrical connector, associated wiring and fuel line. | |
| b. Chafing damage of the electrical wiring or fuel line, replace or repair the damaged parts. | |
| Later revisions of the above SB, approved by the United States Federal Aviation Administration (FAA) as an Alternate Method of Compliance (AMOC) to FAA AD 2009-15-01 are considered acceptable for compliance with the equivalent Requirements of this Directive. | |
| Note: FAA AD 2009-15-01 Amdt 39-15964 refers. | |
| Compliance: | For Requirement 1 - Within 10 hours time-in-service (TIS) after 27 July 2009 (the effective date of this Directive) or 6 calendar months after 27 July 2009, whichever occurs first. |
| For Requirement 2 - Before further flight after the Requirement inspection. | |
| This Airworthiness Directive becomes effective on 27 July 2009. |
| Background: | This Directive results from reports of chafing between the wire harness/connector(s) and fuel line. The directive is issued to detect and correct improper installation and/or chafing between the wire harness/connector(s) and fuel line. This chafing could lead to fuel leaking into the cockpit and fire in the cockpit if wiring arcs through the fuel line. |
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James Coyne
Delegate of the Civil Aviation Safety Authority
17 July 2009