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AD/SWSA226/91 Amdt 1 - Improved Wheel Well Fire Protection
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(ii) Fairchild Aircraft Service Bulletin (SB) No. 227-26-002, incorporating the following pages:
| Pages | Date |
|---|---|
| 1, 2, 8, and 9 | Issued: 1 March, 2000. |
| 7 | Issued: 1 March, 2000, Revised: 27 June, 2000. |
| 3, 4, 5, and 6 | Issued: 1 March, 2000, Revised: 2 October,2000. |
For all applicable aeroplanes, except those equipped with an anti-skid/power brake system, replace each brake shuttle valve with part number (P/N) MS28767- 4 brake shuttle valve in accordance with the ACCOMPLISHMENT INSTRUCTIONS section of Fairchild Aircraft SB No. 226-26-003 Revision 4, or Fairchild Aircraft SB No. 227-26-002, as applicable.
For all applicable aeroplanes, install a shield over the hydraulic lines in accordance with the ACCOMPLISHMENT INSTRUCTIONS section of Fairchild Aircraft Service Bulletin No. 226-26-003 Revision 4, or Fairchild Aircraft SB No. 227-26-002, as applicable.
3. For all aeroplane models within the SA226 series, replace the rubber fuel hose with a metal device in accordance with the ACCOMPLISHMENT INSTRUCTIONS section of Fairchild Aircraft SB No. 226-26-003 Revision 4.
4. No person shall install any brake shuttle valve that is not a P/N MS28767-4 brake shuttle valve or a fuel hose that is made of rubber.
Note: FAA AD 2002-08-02 refers superseding FAA AD 2001-20-14.
Compliance: For Requirement 1, 2 and 3: Unless already complied with in accordance with the original issue of this Directive; within 500 hours time- in-service (TIS) from the effective date of this Directive, or within 6 months from the effective date of this Directive, whichever occurs first.
For Requirement 4: From 6 March 2002, the date of original issue of this Directive. This Amendment becomes effective on 3 July 2002.