Document ID: chunk:federal_register_of_legislation:F2007L04020:body:0:p4
Version: federal_register_of_legislation:F2007L04020
Segment Type: other
Provision Reference: 
Character Range: 10727–15632

trim actuator with a P/N DL5040M6, P/N DL5040M8, P/N 27-19008-006, P/N 27-19008-007, or 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.
   P/N DL5040M5pitch trim actuator installed that was overhauled and zero-timed where both nut assemblies, P/N AA56142, were not replaced with new assemblies during overhaul.
   (vi) For all affected aeroplane models (except for the Models SA227-CC and SA227-DC) that have a newly fabricated or overhauled and                                          Inspect in accordance with Requirement 2b of this AD before accumulating 500 hours total TIS on the pitch trim actuator or within 50 hours TIS after                                     Inspect in accordance with Requirement 2b 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 (vi) of the Repetitive Replacement column of this Table.  Replace the pitch trim actuator with a P/N DL5040M6, P/N DL5040M8, P/N 27-19008-006, P/N 27-19008-007, or 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.
   zero-timed pitch                                                                                                                                                             1 December 1997, whichever occurs later.
   trim actuator,
   P/N 27-19008-001, P/N 27-19008-002, P/N 27-19008-004, or P/N 27-19008-005.

   (vii) For the Models SA227-CC and SA227-DC that have a pitch                                                                 None.                                                                                                                                                                                          None.                                                                                                                                                                                                                                                                                                        Replace the pitch trim actuator with a P/N DL5040M8,
   trim actuator                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                            P/N 27-19008-006 P/N 27-19008-007, or an FAA-approved equivalent pitch trim actuator before accumulating 1,500 hours TIS on the pitch trim actuator or within 30 days after the effective date of this AD, whichever occurs later.
   P/N DL5040M5 or P/N DL5040M6 installed.
   (viii) For the Models SA227-CC and SA227-DC that have a newly fabricated or overhauled and zero-timed pitch trim actuator,   Inspect in accordance with Requirement 2b of this AD before accumulating 500 hours total TIS on the pitch trim actuator or within 50 hours TIS after 1 December 1997, whichever occurs later.  Inspect in accordance with Requirement 2b 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 (viii) of the Repetitive Replacement column of this Table.  Replace the pitch trim actuator with a P/N DL5040M8,
   P/N 27-19008-001, P/N 27-19008-002, P/N 27-19008-004, or P/N 27-19008-005.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                               P/N 27-19008-006, P/N 27-19008-007, or 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,