Airworthiness Directive · Amendment 39-14719 · B-N Group Ltd. BN-2, BN-2A, BN-2B, BN-2T, and BN-2T-4R Series (All Individual Models Included in Type Certificate Data Sheet (TCDS) A17EU, Revision 16, Dated December 9, 2002) Airplanes
B-N Group Ltd. BN-2, BN-2A, BN-2B, BN-2T, and BN-2T-4R Series (All Individual Models Included in Type Certificate Data Sheet (TCDS) A17EU, Revision 16, Dated December 9, 2002) Airplanes
This AD applies to all BN-2, BN-2A, BN-2B, BN-2T, and BN-2T-4R Series (all individual models included in Type Certificate Data Sheet (TCDS) A17EU, Revision 16, dated December 9, 2002) airplanes; certificated in any U.S. category.
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) issued by an airworthiness authority of another country to identify and correct an unsafe condition on an aviation product. We are issuing this AD to require actions to correct the unsafe condition on these products.
Unless already done, do the following except as stated in paragraph (f) below.
(1) Within the next 50 hours time-in-service or one month after the effective date of this AD, whichever occurs first, inspect the internal surface of the elevator system final drive control rod, in accordance with B-N Group Ltd. Britten-Norman Service Bulletin SB number 303, Issue 1, dated May 14, 2004.
(2) If corrosion is found, the elevator control rod must be replaced before further flight.
When complying with this AD, repeat the actions in paragraphs (e)(1) and (e)(2) of this AD at intervals not to exceed 12 months.
