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AC 120-42B ETOPS and Polar Ops - Code7700

AC 120-42B ETOPS and Polar Ops - Code7700

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6/13/08 <strong>AC</strong> <strong>120</strong>-<strong>42B</strong>decisions successfully throughout the flight. The suitability of an en route alternate airport for anairplane that encounters an in-flight situation that necessitates a diversion during <strong>ETOPS</strong>operations is based on a determination that the airport still is suitable for the circumstances, <strong>and</strong>the weather <strong>and</strong> field conditions at that airport permit an instrument approach to be initiated <strong>and</strong>a l<strong>and</strong>ing completed.207. <strong>ETOPS</strong> IN-SERVICE EXPERIENCE REQUIREMENTS.a. When <strong>AC</strong> <strong>120</strong>-42 was first released in 1985, two-engine <strong>ETOPS</strong> was a new concept <strong>and</strong><strong>ETOPS</strong> approvals were sought on airframe-engine combinations that were already in service.Hence, it was logical to establish criteria for approvals based on in-service experience. At thatsame time, the FAA recognized the possibility that other approval methods could be developedwithout in-service experience, <strong>and</strong> accordingly, provided statements that recognized thoseoptions. The original two-engine <strong>ETOPS</strong> requirements for engine reliability were based on aworld fleet in-service experience of 250,000 hours. For <strong>120</strong>-minute <strong>ETOPS</strong>, the FAAadditionally required the certificate holder to have 12-consecutive months of operationalin-service experience with the airplane-engine combination (AEC). For 180-minute <strong>ETOPS</strong>, theFAA required the certificate holder to have previously gained 12 consecutive months ofoperational in-service experience with the specified AEC conducting <strong>120</strong>-minute <strong>ETOPS</strong>. Thesebasic, two-engine in-service requirements have been retained <strong>and</strong> are discussed in Appendix 3.Achieving these levels of experience, combined with the required levels of engine reliability, isan acceptable means of attaining <strong>ETOPS</strong> approval for operators of two-engine airplanes.b. At the time <strong>AC</strong> <strong>120</strong>-42A was drafted, the FAA recognized that a reduction oftwo-engine in-service experience requirements or substitution of in-service experience onanother airplane would be possible. Any reduction was to be based on an evaluation of thecertificate holder’s ability <strong>and</strong> competence to achieve the necessary reliability for the particularAEC in <strong>ETOPS</strong>. For example, a reduction in in-service experience would be considered for acertificate holder who could show extensive in-service experience with a related engine onanother airplane that had achieved acceptable reliability. The FAA also allowed certificateholders unable to initially fly <strong>ETOPS</strong> routes at the lesser thresholds to make use of <strong>ETOPS</strong>simulation or demonstration programs in their application for 180-minute <strong>ETOPS</strong>. Eventuallyspecific guidance material (<strong>AC</strong> <strong>120</strong>-42A, appendix 7, Accelerated <strong>ETOPS</strong> OperationalApproval) was developed by the FAA permitting <strong>ETOPS</strong> without accumulating in-serviceexperience in the airplane-engine combination. Most subsequent <strong>ETOPS</strong> approvals have beengranted under these guidelines <strong>and</strong> this method is retained in Appendix 3.208. OPERATIONAL RELIABILITY AND SYSTEMS SUITABILITYREQUIREMENTS.a. The safety of long-range operations such as <strong>ETOPS</strong> depends on the reliability of allairplane systems including the propulsion systems. Time-limited systems such as cargocompartment fire suppression/containment capability must be considered (§ 121.633). Thecertificate holder must also have an established program that monitors the reliability of systemssignificant to <strong>ETOPS</strong> (§ 121.374).Par 206 Page 11

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