Document ID: chunk:federal_register_of_legislation:F2006B07187:body:0:p2
Version: federal_register_of_legislation:F2006B07187
Segment Type: other
Provision Reference: 
Character Range: 3041–6172

2 inches to the oxygen tubing. Add additional support or reroute as necessary to prevent wire contact or chafing, which may damage the wire insultation, and clean any contamination from the bundles.

                   M.     Before further flight, correct all discrepancies and remove any hydraulic fluid contamination found during inspections.

                 Para 2. Inspect electrical cables and terminals within and below the generator control junction box (J-box), install phenolic insulator on side of J-box and spiral wrap on cables in accordance with Fairchild Service Bulletin SB No 24-021 (SA226) and SB24-03 (SA227).

                 Para 3. On aircraft models SA226-T s/nos T201 to T287; SA226-AT s/nos AT001 to AT066; SA226-TC s/nos TC201 to TC247, in which MIL-H-5606 hydraulic fluid is used, drain and purge the main hydraulic fluid. Change the placards on both reservoirs to specify MIL-H-83282.

                 Para 4. On aircraft models SA226-T (S/Nos. T201 to T275, T277 to T291), SA226- AT (S/Nos AT001 to AT074); SA226-TC (S/Nos. TC201 to TC419);
                 SA226-T (B) (S/Nos T(B)276, T(B)292 to T(B)417) modify the hydraulic system in accordance with Fairchild Service Bulletin SB No. 226-29-005 revised 19 July 1985.

           Note: inspect condition of cushion clamps when changing hydraulic lines and replace as necessary.

                 Para 5. On aircraft models SA226-T (S/Nos. T249 to 275, 277 to 291), SA226-AT (S/Nos. AT001 to AT074), SA226TC (S/Nos. TC201 to 397), SA226-T(B)
                 (S/Nos. T(B)276, T(B)292 to T(B)417) modify the oxygen system in accordance with Fairchild Service Bulletin S.B. No. 226- 35-003 Revised 19 July 1985.

                 Para 6. Inspect "sceet" hoses in side consoles for condition and security, and re- route, repair or replace hoses as necessary in accordance with Fairchild Service Note 226- SN-145 dated 2 July 1985 for the SA226 and Fairchild Service Note 227-SN-052 dated 2 July 1985 for the SA227.

           Note: FAA AD 83-19-02 Amdt 39-4728 and FAA AD 84-05-01 Amdt 39-4822 and
           FAA AD 85-04-01 Amdt 39-5005 refer.

                 Compliance: Para 1. Within 65 hours time in service after 31 May 1984, unless already accomplished IAW original AD/SWSA226/47, and thereafter at intervals not exceeding 260 hours time in service.

                       1. For aircraft modified in accordance with paras 4 and 5 of the requirements and equipped with anti-skid brake system, the inspections of Para 1 of the requirements are not applicable.

                      b.    For aircraft modified in accordance with paras 4 and 5 of the requirements and NOT equipped with an anti-skid brake system, only inspection D of Para 1 of the Requirements applies.

                    Para 2. Within 65 hours time in service after 31 May 1984 unless already accomplished.

               Para 3.  Within 30 hours time in service after 12 November 1983.

               Para 4.  Before further flight after 31 December 1985.

               Para 5.  Before further flight after 31 December 1985.

                    Para 6. Within 65