Document ID: chunk:federal_register_of_legislation:F2007L04020:body:0:p3
Version: federal_register_of_legislation:F2007L04020
Segment Type: other
Provision Reference: 
Character Range: 7950–10978

have a replacement                                          Inspect in accordance with Requirement 2a of this AD before accumulating 7,500 hours TIS on the pitch trim actuator or within 50 hours TIS after 17 April 1995, whichever occurs later.  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 (iii) 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 9,900 hours TIS on the pitch trim actuator or within 30 days after the effective date of this AD, whichever occurs later.
   pitch trim actuator, P/N DL5040M6, installed.  This part can be new, modified from a P/N DL5040M5 pitch trim actuator, or overhauled and
   zero-timed.
   (iv) For all affected aeroplane models (except for the Models SA227-CC and SA227-DC) that have a replacement pitch trim actuator,                      Inspect in accordance with Requirement 2a of this AD before accumulating 5,000 hours TIS on the pitch trim actuator or within 50 hours TIS after 17 April 1995, whichever occurs later.  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 (iv) 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 6,500 hours TIS on the pitch trim actuator or within 30 days after the effective date of this AD, whichever occurs later.
   P/N DL5040M5, installed that was overhauled and zero-timed where both nut assemblies, P/N AA56142, were replaced with new assemblies during overhaul.

   (v) For all affected aeroplane models (except for the Models SA227-CC and SA227-DC) that have a replacement                                                                  Inspect in accordance with Requirement 2a of this AD before accumulating 3,000 hours TIS on the pitch trim actuator or within 50 hours TIS after 17 April 1995, whichever occurs later.  Inspect in accordance with Requirement 2a of this AD before accumulating 250 hours TIS after the initial inspection and repetitively thereafter at intervals not to exceed 250 hours TIS until accumulating the hours TIS specified in paragraph (iv) 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