Document ID: chunk:federal_register_of_legislation:F2007L04020:body:0:p2
Version: federal_register_of_legislation:F2007L04020
Segment Type: other
Provision Reference: 
Character Range: 3279–8236

27-19008-002, P/N 27-19008-004, or P/N 27-19008-005 - Do a functional inspection of the pitch trim actuator using the INSTRUCTIONS section of Fairchild Aircraft SA226 Series SL 226-SL-014, Fairchild Aircraft SA227 Series SL 227-SL-031, or Fairchild Aircraft SA227 Series SL
        CC7-SL-021; all Revised: 1 February 1999; as applicable.

        c. For aeroplanes equipped with a pitch trim actuator P/N 27-19008-006 or
        P/N 27-19008-007 - Overhaul the pitch trim actuator following the applicable maintenance manual.

   Table 2. - Inspection/Overhaul and Replacement
   Requirements for Pitch Trim Actuators

   Condition                                                                                                      Initial Inspection or Overhaul                                                                                                                                                          Repetitive                                                                                                                                                                                                                                                                                                 Repetitive
                                                                                                                                                                                                                                                                                                          Inspection or Overhaul                                                                                                                                                                                                                                                                                     Replacement
   (i) For all affected aeroplane models (except for the Models SA227-CC and SA227-DC) that have an original      Inspect in accordance with Requirement 2a. of this AD before accumulating                                                                                                               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 (i) 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, 500 hours TIS after the initial inspection, or within 30 days after effective date of this AD, whichever occurs later.
   pitch trim actuator, P/N DL5040M5,                                                                             3,000 hours time-in-service (TIS) on the pitch trim actuator or within 50 hours TIS after 17 April 1995, whichever occurs later, unless previously accomplished.
   installed.
   (ii) 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 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 (ii) 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
   pitch trim actuator, P/N DL5040M5 installed.                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                                      6,500 hours TIS on the pitch trim actuator or within 30 days  of the effective date of this AD, whichever occurs later.

   (iii) 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 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