Document ID: chunk:federal_register_of_legislation:F2008L03774:body:0:p2
Version: federal_register_of_legislation:F2008L03774
Segment Type: other
Provision Reference: 
Character Range: 2921–7071

Bombardier Aerospace for disposition.

             SB 700-1A11-27-025 or 700-27-067 may be accomplished in lieu of Requirements 1a, 1b and 1c of this AD.

             The Units listed below have been lubricated by the vendor and are not required to accomplish the instructions detailed in Requirements 1a, 1b and 1c of this AD.

             Table 1:
             P/N GT411-3800-7 units sent to vendor for maintenance have been returned as greased bearings
             0030                                                                                          0092  0141  0179  0206  0296  0427  0506
             0031                                                                                          0097  0145  0181  0208  0301  0429  0513
             0033                                                                                          0101  0156  0183  0210  0310  0430  0533
             0041                                                                                          0105  0161  0188  0214  0323  0431  0536
             0046                                                                                          0108  0163  0190  0218  0365  0433  0586
             0060                                                                                          0109  0164  0191  0222  0369  0435
             0062                                                                                          0110  0165  0197  0223  0406  0438
             0066                                                                                          0111  0171  0198  0240  0407  0453
             0081                                                                                          0119  0173  0199  0262  0408  0491
             0083                                                                                          0130  0174  0202  0265  0413  0495
             0087                                                                                          0138  0178  0205  0281  0420  0504

             Note 1:  Units listed in the above table must comply with Requirement 2.

                2. For all other elevator PCU P/N GT411-3800-7 that are not covered in Requirement 1 of this AD, complete a disassembly with inspection and lubrication of the PCU attachment joint components in accordance with SB 700 1A11 27 025 basic issue dated 9 October 2008 or later revisions approved by the Chief, Continuing Airworthiness, or SB 700-27-067 basic issue dated 9 October 2008 or later revisions approved by the Chief, Continuing Airworthiness, Transport Canada, as applicable.

                3. Report all findings to Bombardier Aerospace as defined in the applicable SB.

             Terminating Action

             Incorporation of Bombardier SB 700-1A11-27-025 or 700-27-067 constitutes terminating action for this AD.

             Note 2:  Transport Canada Urgent AD CF-2008-31 dated 9 October 2008 refers.
Compliance:  For Requirement 1a - Within 10 flight cycles or 50 flight hours, whichever comes first after the effective date of this AD.

             For Requirement 1b - Within 90 days or 200 flight hours, whichever comes first, following the successful completion of Requirement 1a.

             For Requirement 1c - Within 45 days or 100 hours air time, whichever comes first, following the successful completion of Requirement 1b.

             For Requirement 1d - Within 45 days or 100 hours air time, whichever comes first, following the successful completion of Requirement 1c.

             For Requirement 1e - Prior to further flight after the effective date of this AD.

             For Requirement 2 - Within 180 days or 400 flight hours after the effective date of this directive, whichever comes first.

             For Requirement 3 - Within 14 days after completion of each inspection detailed in Requirements 1 and 2 of this AD.
             This Airworthiness Directive becomes effective on 13 October 2008.
Background:  During scheduled maintenance inspection, a bolt which connects the PCU to the elevator surface was found fractured in