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

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We envision a term “∆” -- delta, or <strong>the</strong> degree <strong>of</strong> difference between procedures and practices (Figure 4).This “∆,” not to be taken as a quantitative value by any means, expresses symbolically <strong>the</strong> amount <strong>of</strong>deviation from a specified procedure. This term has two components: (1) <strong>the</strong> magnitude <strong>of</strong> deviationfrom <strong>the</strong> procedure, and (2) <strong>the</strong> frequency <strong>of</strong> such deviations during actual line operations. The goal <strong>of</strong>flight management is to minimize “∆.” When “∆” is large (flight crews constantly deviate from SOPand/or deviate in a gross manner), <strong>the</strong>re is a problem. This “∆” may be due to a crew's deviation and/ora problem in using this procedure.<strong>Procedures</strong>CrewPractices"∆" = | Practices - <strong>Procedures</strong> |Figure 4. The quantity “∆” - deviation from procedures.The human operator in this situation is analogous to a filter. From <strong>the</strong> above, standards and trainingdepartments dictate and teach <strong>the</strong> way procedures should be performed. However, in daily lineoperations (and not under <strong>the</strong> watchful eye <strong>of</strong> a check-airman), <strong>the</strong> individual pilot may adjust <strong>the</strong> gauge<strong>of</strong> <strong>the</strong> filter. This gauge will determine <strong>the</strong> degree to which <strong>the</strong> SOPs actually will be observed,modified, misused, or completely ignored. The purpose <strong>of</strong> standardization is to bias <strong>the</strong> filter towardprevention <strong>of</strong> deviations.The consequences <strong>of</strong> <strong>the</strong> failure to conform to a procedure can be seen in <strong>the</strong> following report fromNASA's Aviation Safety Reporting System (ASRS) 5 :Our flight departed late PM local time for <strong>the</strong> 4:30 plus flight to SFO. F/O was PF. En-route discussednecessity to request lower altitudes with both OAK Center and Bay Approach when approaching SFO due totendency to be “caught high" on arrival in this aircraft type. Area arrival progressed smoothly and we werecleared for <strong>the</strong> QUIET BRIDGE visual to 28R. Good speed control and vertical descent planning until vicinity<strong>of</strong> BRIJJ LOM. When changing radio frequency from approach to tower (head down), F/O selected "opendescent" to 400 feet MSL. Autopilot was <strong>of</strong>f, both flight directors were engaged, and autothrust was on. Whilecontacting SFO tower I became aware that we were below <strong>the</strong> glideslope, that airspeed was decaying, and that wewere in an "open descent." Instructed <strong>the</strong> F/O to engage <strong>the</strong> “vertical speed” mode in order to stop our descent,restore <strong>the</strong> speed mode for <strong>the</strong> autothrust, and continue <strong>the</strong> approach visually once above <strong>the</strong> 28R ILSglideslope. Company procedures explicitly prohibit selecting an altitude below 1500 feet AGL for an opendescent, since this places <strong>the</strong> aircraft close to <strong>the</strong> ground with engines at idle. (ASRS Report No. 149672)5ASRS reports are quoted here verbatim.9

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