Document ID: chunk:federal_register_of_legislation:F2007L04020:body:0:p5
Version: federal_register_of_legislation:F2007L04020
Segment Type: other
Provision Reference: 
Character Range: 15356–19336

an FAA-approved equivalent pitch trim actuator before accumulating 5,000 hours TIS on the pitch trim actuator or within 30 days after the effective date of this AD, whichever occurs later.

   (ix) For all affected aeroplanes with a pitch trim actuator, P/N DL5040M8, installed.                   Inspect in accordance with Requirement 2a of this AD before accumulating 7,500 hours TIS on the pitch trim actuator or within the next 50 hours TIS after   Inspect in accordance with Requirement 2a of this AD before accumulating 300 hours TIS after the initial inspection and repetitively thereafter at intervals not to exceed 300 hours TIS until accumulating the hours TIS specified in paragraph (ix) of the Repetitive Replacement column of this Table.  Replace the pitch trim actuator with a P/N DL5040M8,
                                                                                                           April 10, 2000, whichever occurs later.                                                                                                                                                                                                                                                                                                                                                                                                                                P/N 27-19008-006 or P/N 27-19008-007, or an FAA-approved equivalent pitch trim actuator before accumulating 9,900 hours TIS on the pitch trim actuator or within 30 days after the effective date of this AD, whichever occurs later.
   (x) For all affected aeroplanes with a P/N 27-19008-006 or 27-19008-007 pitch trim actuator installed.  Overhaul following Requirement 2c of this AD before accumulating 2,000 hours TIS on the pitch trim actuator.                                                Overhaul following Requirement 2c of this AD before accumulating 2,000 hours TIS on the pitch trim actuator.                                                                                                                                                                                               No replacement requirements.

      3. For all aeroplanes - Replace the pitch trim actuator following the applicable maintenance manual.

      4. For all aeroplane models except Models SA227-CC and SA227-DC - Do not install as a replacement any of the following pitch trim actuators or FAA-approved equivalent P/Ns:

        a. P/N 27-19008-001;

        b. P/N 27-19008-002;

        c. P/N 27-19008-004;

        d. P/N 27-19008-005; or

        e. P/N DL5040M5.

                5. For all aeroplane Models SA227-CC and SA227-DC - Do not install as a replacement any of the following pitch trim actuators or FAA- approved equivalent P/Ns:

                  a. P/N 27-19008-001;

                  b. P/N 27-19008-002;

                  c. P/N 27-19008-004;

                  d. P/N 27-19008-005;

                  e. P/N DL5040M5; or

                  f. P/N DL5040M6.

             Note 2:  FAA AD 2007-16-03 Amdt 39-15142 dated 27 July 2007 refers.  This AD supersedes FAA AD 98-19-15R and AD 2000-03-17.
Compliance:     1. Remains unchanged as detailed in AD/SWSA 226/85 Amdt 1 as - Before further flight after 14 September 1998; or in the case of aircraft with actuators P/N
                27-19008-004, or P/N 27-19008-005, before further flight after 23 February 2000.

                Installation of any FAA-approved pitch trim actuator other than P/N
                27-19008-001, P/N 27-19008-002, P/ N 27-19008-004, or P/N 27-19008-005 terminates the actions detailed in Requirement 1 of this AD.

                2. As detailed in Table 2 of this AD.

                3. Before further flight when any of the following occurs:

                  a. The pitch trim actuator is inspected following Requirement 2 of this AD and the freeplay limitations