Airworthiness Directive · Amendment 39-14970 · REIMS AVIATION S.A. Model F406 Airplanes
REIMS AVIATION S.A. Model F406 Airplanes
This AD applies to Model F406 airplanes, all serial numbers, certificated in any 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 aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Unless already done, do the following actions:
(1) Within 3 months or 100 hours time-in-service (TIS) after April 11, 2007 (the effective date of this AD), whichever occurs first:
(i) For airplanes with Teijin Seiki Nose Landing Gear (NLG) P/N 9910139-9: inspect the NLG for conformity with the key lock system installation description in Figure 1 of the REIMS AVIATION INDUSTRIES Service Bulletin No. F406-56, dated April 12, 2005;
(ii) For airplanes with Cessna NLG P/N 9910139-9: inspect the NLG for conformity with the key lock system installation description in Figure 2 of the REIMS AVIATION INDUSTRIES Service Bulletin No. F406-56, dated April 12, 2005;
(iii) For airplanes with Teijin Seiki Main Landing Gear (MLG) P/N 9910136-8: inspect the MLG for conformity with the key lock system installation description in Figure 3 of the REIMS AVIATION INDUSTRIES Service Bulletin No. F406-56, dated April 12, 2005; and
(iv) For airplanes with Cessna MLG P/N 9910136-8: inspect the MLG for conformity with the key lock system installation description in Figure 4 of the REIMS AVIATION INDUSTRIES Service Bulletin No. F406-56, dated April 12, 2005.
(2) Before further flight after any inspection from (e)(1) of this AD where the key lock system does not conform to the appropriate installation description, install a key lock system that conforms to the appropriate installation description.
Note: This AD differs from the MCAI and/or service information as follows: No differences.
