Airworthiness Directive · Amendment 39-14698 · Fokker Model F.28 Mark 0070 and 0100 Airplanes
Fokker Model F.28 Mark 0070 and 0100 Airplanes
This AD applies to all Fokker Model F.28 Mark 0070 and 0100 airplanes, certificated in any category.
The FAA is adopting a new airworthiness directive (AD) for all Fokker Model F.28 Mark 0070 and 0100 airplanes. This AD requires modification of the wiring distribution of the alternating current bus transfer power system and the right-hand and left-hand windshield anti- icing system, as necessary. This AD results from a report of electrical sparks coming out of the flight deck from a panel behind the left seat. We are issuing this AD to prevent failure of the sliding window heating element(s), due to electrical overload, which could result in smoke and fire in the cockpit.
You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done.
Within 36 months after the effective date of this AD, modify the wiring distribution of the alternating current bus transfer power system and the right-hand and left-hand windshield anti-icing system, by accomplishing all of the actions specified in the Accomplishment Instructions of Fokker Service Bulletin SBF100-30-027, dated May 9, 2005, as applicable; including Fokker Manual Change Notification—Maintenance Documentation MCNM F100-098, dated May 9, 2005, and the drawings listed in Table 1 of this AD. (To conform to certain Office of the Federal Register requirements for incorporating these materials by reference, the table identifies the date of the service bulletin for undated drawings.)
| Fokker drawing | Sheet | Issue | Date |
|---|---|---|---|
| W41043 | 007 | H | May 9, 2005. |
| W41043 | 008 | H | May 9, 2005. |
| W41249 | 006 | F | May 9, 2005. |
| W41249 | 007 | F | May 9, 2005. |
| W41249 | 008 | F | May 9, 2005. |
| W41249 | 009 | G | May 9, 2005. |
| W41249 | 010 | G | May 9, 2005. |
