Airworthiness directives › 2005-22-14
AD 2005-22-14 Airworthiness Directives; GROB-WERKE Model G120A Airplanes
Models named: G120A. Read the applicability below — it usually turns on serial or part numbers too.
Applicability*9
(c) This AD affects Model G120A airplanes, all serial numbers, that are certificated in any category.
Required actions
(e) To address this problem, you must do the following: Actions Compliance Procedures (1) Inspect for: (i) Any signs of chafing damage to the attachment cables of switches below the switch panels of the left-hand instrument panel; Within the next 50 hours time-in-service (TIS) after December 19, 2005 (the effective date of this AD), unless already done Follow GROB Service Bulletin No. MSB1121-065, dated July 1, 2005 (ii) Any damaged switch on switch panels of the left-hand instrument panel; and (iii) Any damaged (that is, sharp) edge of the support tray for the attachment cables of switches below the switch panels of the left-hand instrument panel.. (2) Correct any damage found as a result of the inspection required by paragraph (e)(1) of this AD: (i) If you find any signs of chafing damage to the attachment cables of switches below the switch panels of the left-hand instrument panel, replace the attachment cables; (ii) If you find any damaged switch below the switch panels of the left-hand instrument panel, replace the switch; and (iii) If you find any damaged (that is, sharp) edge on the support tray for the attachment cables of switches below the switch panels of the left-hand instrument panel, grind off any sharp edges and clean thoroughly. Before further flight after the inspection required by paragraph (e)(1) of this AD Follow GROB Service Bulletin No. MSB1121-065, dated July 1, 2005. (3) Apply anti-rub (padding strips to the edge of the support tray for the attachment cables of switches below the switch panels of the left-hand instrument panel. Before further flight after the inspection required by paragraph (e)(1) of this AD. This modification is required even if damage is not found during the inspections Follow GROB Service Bulletin No. MSB1121-065, dated July 1, 2005.
Unsafe condition
(d) This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. The actions specified in this AD are intended to detect, correct, and prevent chafing of the cables against the rear lip of the tray that holds the switch panels. Chafing of the electrical cables could result in smoke or fire in the cockpit.
Affected ADs
(b) None.
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The directive text above is reproduced from the Federal Register, a work of the United States government and in the public domain. The separation into applicability, compliance and required actions is TrackAD's.*1