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On the Design of Flight-Deck Procedures - Intelligent Systems ...

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5.7.3 Technique and PoliciesAny given technique may indeed conform to <strong>the</strong> written procedure, and thus not add to “∆,” but couldstill entail an unnecessary risk or inefficiency. Consider <strong>the</strong> example mentioned earlier (Section 3.2.1) <strong>of</strong>leveling <strong>of</strong>f at FL 250 during a climb to a higher cruise altitude for <strong>the</strong> sake <strong>of</strong> avoiding <strong>the</strong> use <strong>of</strong> <strong>the</strong>oxygen mask. If this technique is evaluated from a procedural stand point, <strong>the</strong>re is no “∆.” Thetechnique is in full conformity with <strong>the</strong> FAR and company procedures. Yet, if <strong>the</strong> companypolicy/philosophy includes a statement about efficiency <strong>of</strong> operations, <strong>the</strong>n it is non-conformity.Therefore, it is not enough for <strong>the</strong> technique to conform to <strong>the</strong> procedure; it must also be consistent with<strong>the</strong> policies.In some cases <strong>the</strong>re is no procedure for a given task and related procedures do not help in solving <strong>the</strong>problem. At this point policies are <strong>the</strong> only guidance to <strong>the</strong> crew on how <strong>the</strong>y may use a technique. It ishere where <strong>the</strong> structure <strong>of</strong> policies and philosophy pays <strong>of</strong>f. Figure 9 depicts this relationship between<strong>the</strong> technique and <strong>the</strong> policy.PoliciesProcedureTechniqueSub-TasksSub-TasksFigure 9. Framework <strong>of</strong> technique and policy.For example, one <strong>of</strong> <strong>the</strong> many auto-level<strong>of</strong>f techniques we observed involved placing a 300-knotairspeed in <strong>the</strong> autothrottle while climbing in vertical speed mode below 10,000 feet. The purpose wasto provide a smoo<strong>the</strong>r acceleration to an intermediate speed when leveling at or above 10,000 feet.During <strong>the</strong> level<strong>of</strong>f <strong>the</strong> pilot would switch to airspeed mode and <strong>the</strong> aircraft would smoothly accelerate asit leveled. The potential hazard is that it would not be difficult to switch inadvertently to airspeed modebelow 10,000 feet and thus violate <strong>the</strong> speed restriction.Properly applied, <strong>the</strong> technique should work well, provide a smoo<strong>the</strong>r flight for <strong>the</strong> passengers, andremain in conformity with <strong>the</strong> 250 knots restriction. And although “∆” is not increased, time after timewhen <strong>the</strong> technique is employed, <strong>the</strong> seeds <strong>of</strong> a latent error may have been planted. The following ASRSreport illustrates a similar technique for <strong>the</strong> same task and <strong>the</strong> potential for an error:Our departure clearance <strong>of</strong> out Atlanta included instructions to maintain 10,000 feet. <strong>On</strong> this flight <strong>the</strong> captaindecided to delete <strong>the</strong> 250 knots restriction from <strong>the</strong> FMS climb page in order to eliminate <strong>the</strong> throttle burstassociated with leveling <strong>of</strong>f at 10,000. He planned to follow <strong>the</strong> flight director pitch bar up to 300 AGL [duringtake<strong>of</strong>f] and <strong>the</strong>n decrease pitch to allow <strong>the</strong> aircraft to accelerate to 250 knots <strong>On</strong>ce at 250 knots his plan was26

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