“Application of Brakes During Backward Movement is Prohibited”

3. Inspect the MLG Main Fittings in accordance with the Accomplishment Instructions of Messier-Dowty (SB) F100-32-104, dated 22 August 2002, or later UK CAA approved revision.

4. Whenever a hard or overweight landing is reported and subsequently confirmed by inspection in accordance with the Aircraft Maintenance Manual Chapter 05- 51-01, Table A, inspect the MLG Main Fittings in accordance with the Accomplishment Instructions of Messier-Dowty SB F100-32-104 Revision 2, dated 30 October 2003, or later UK CAA approved revision.

5. After each occasion when braking has been applied during aircraft backward movement in push-back or power-back operation, inspect the MLG Main Fittings in accordance with the Accomplishment Instructions of Messier-Dowty SB F100- 32-104 Revision 2, or later UK CAA approved revision.

6. When cracks are found, determine whether and for how many, flights may be continued before repair or replacement; in accordance with the crack size and location thresholds as listed in Fokker Services SB F100-32-137 Revision 2, dated 9 February 2004, or later CAA-NL approved revision.

7. Irrespective of the results, report all inspection findings to Fokker Services.

Note: CAA-NL AD 2002-115/2 refers.