Figure 1 of Docket No. 97-CE-67-AD
Compliance Table
Letters in ( ) correspond with AD paragraphs | | | | | | | Throughout the |
Actions of Docket No. 97-CE-67-AD | Visually inspect the exhaust system. | Remove the tailpipes and visually inspect for any crack, corrosion, holes, or distortion. | Visually inspect the outboard engine beams, firewalls, and canted bulkheads. | Inspect and pressure test the exhaust system. | Replace the multi-segment V-band clamps. | Remove the exhaust system from the slip joints aft to all turbo-charger components. | If any damage is found on any component or part, repair or replace the damaged component or part in accordance with this AD. |
Initial Compliance Time | Within the next 50 hours TIS after the effective date of this AD or within the next 30 calendar days, whichever occurs later. | Upon the accumulation of 5 years since installing a new or overhauled exhaust system or within the next 100 hours TIS after the effective date of this AD, whichever occurs later. | Within the next 100 hours TIS after the effective date of this AD. | Upon the accumulation of 5 years since installing a new or overhauled exhaust system or within the next 100 hours TIS after the effective date of this AD, whichever occurs later. | Within 500 hours TIS after the last replacement required by AD 75-23-08 R5 or within the next 500 hours TIS after the effective date of this AD, whichever occurs first. | At whichever occurs later: - At the next engine overhaul that occurs after the accumulation of 2,500 hours TIS since installing a new or overhauled exhaust system;or - Within the next 100 hours TIS after the effective date of this AD. | Prior to further flight after damage is found. |
Repetitive Compliance Times | Thereafter at intervals not to exceed 50 hours TIS or 30 calendar days, whichever occurs later. | Thereafter at intervals not to exceed 12 calendar months. | Thereafter at intervals not to exceed 500 hours TIS. | Thereafter at intervals not to exceed 12 calendar months. | Thereafter at intervals not to exceed 500 hours TIS. | Thereafter at intervals not to exceed 2,500 hours TIS or 12 years, whichever occurs first. These inspection intervals are established to coincide with each regularly scheduled engine overhaul. | Prior to further flight after damage is found. |