Division Dornier 228 Series Aeroplanes - AD/DO 228/15 - Aileron Trim Actuator and Rod Spring Lever Attachment Bracket - Dornier 228 Series Aeroplanes

Dornier 228 Series AeroplanesDornier 228 Series Aeroplanes

Start here

Get a plain-English read of Dornier 228 Series Aeroplanes

Turn the raw legal text into a practical explanation grounded in AD/DO 228/15 - Aileron Trim Actuator and Rod Spring Lever Attachment Bracket.

AD/DO 228/15	Aileron Trim Actuator and RodSpring Lever Attachment Bracket	2/2009 DM

Applicability:	Model 228-100, -101, -200, -201, -202, and -212 aircraft, all serial numbers.
Requirement:	1. Accomplish inspection for “unequal aileron steering wheel force” in accordance with paragraphs A(1) through A(3) of the Accomplishment Instructions of RUAG Aerospace Service Bulletin (SB) No. SB-228-275 original issue, or later EASA approved revision.If a defect is evident or suspected, before further flight, modify the attachment bracket riveting in accordance with paragraph B of the Accomplishment Instructions of SB No. SB-228-275 original issue, or later EASA approved revision.2. Modify the attachment bracket riveting in accordance with paragraph B of the Accomplishment Instructions of SB No. SB-228-275 original issue, or later EASA approved revision.Note: EASA AD 2008-0217 refers.
Compliance:	1. Within 10 flight hours after 24 December 2008.2. Unless already accomplished, within 300 flight hours after 24 December 2008.
	This Airworthiness Directive becomes effective on 24 December 2008.
Background:	Reports were received of loose rivets on the aileron trim actuator and rod spring lever attachment bracket between frame 18 and 19 left hand. This condition, unless detected and corrected, could lead to separation of the attachment bracket which could result in loss of aileron trim and loss of artificial force feedback; and consequent reduced controllability of the aircraft.

Image unavailable in extracted text
David Punshon
Delegate of the Civil Aviation Safety Authority

12 December 2008