Airworthiness Directive · Amendment 39-15394 · Fuselage
Fokker Model F.28 Mark 0070 and 0100 Airplanes
Superseded. A later AD replaced this one: AD 2009-02-10. Comply with the one in force.
This AD applies to Fokker Model F.28 Mark 0070 and 0100 airplanes, certificated in any category, all serial numbers.
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) originated 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 12 months after the effective date of this AD, inspect the wing-to-fuselage fairings for indications of incorrect fit, damage or wear, in accordance with the Accomplishment Instructions of Fokker Service Bulletin SBF100-53-101, dated September 30, 2005.
(i) If no indications of incorrect fit, damage or wear are found, no further action is required by this AD.
(ii) If any incorrect fit, damage or wear is found, before next flight, do related investigative actions and applicable corrective actions in accordance with the Accomplishment Instructions of the service bulletin.
(2) When incorrect fit, damage or wear is found, within 30 days after the inspection or within 30 days after the effective date of the AD, whichever occurs later, report the findings to Fokker Services B.V., Technical Services Dept., P.O. Box 231, 2150 AE Nieuw-Vennep, The Netherlands.
Note: This AD differs from the MCAI and/or service information as follows: No differences.
