e made. Consider, also, <strong>the</strong> following example: <strong>On</strong>e company, providing mostly short-haul flightswith fast turn-around, required all its pilots to avoid hard braking and fast turns in an attempt to make <strong>the</strong>nearest high-speed turn<strong>of</strong>f. Passengers' complaints to <strong>the</strong> company public relations <strong>of</strong>fice could not beignored. Efficiency <strong>of</strong> operations yielded to passenger comfort.5.5.2 Resource Conservation <strong>Procedures</strong>Fuel conservation is a major consideration in development <strong>of</strong> airline procedures. Because <strong>the</strong>“multipliers” in airline operations over <strong>the</strong> fleets over time are so great, a procedural change yielding, onany given leg, a seemingly small saving can result in a very considerable dollar savings annually. Thishas brought about a host <strong>of</strong> fuel conservation procedures: single engine taxiing, delayed engine start,delayed lowering <strong>of</strong> landing gear and flaps, reduced use <strong>of</strong> <strong>the</strong> APU, and recalculation <strong>of</strong> fuelrequirements. All have important procedural implications.Fuel is not <strong>the</strong> only consideration. Wear on equipment may lead to procedures such as derated take<strong>of</strong>fsto reduce engine wear, lower flap extension speeds to reduce wear, and use <strong>of</strong> autobrakes for landing toreduce brake and tire wear. An example <strong>of</strong> <strong>the</strong> impact <strong>of</strong> equipment conservation on procedures isreduction <strong>of</strong> APU starts. <strong>On</strong>e airline has <strong>the</strong> following procedure: on taxi-in, if <strong>the</strong> taxi time is estimated(by <strong>the</strong> crew) to be less than nine minutes on a B-757, <strong>the</strong>y taxi on both engines and do not start <strong>the</strong>APU (two engines provide two generators) 9 .5.6 AUTOMATIONOur observations suggest that increased automation reduces <strong>the</strong> number <strong>of</strong> procedures on <strong>the</strong> fight deck.It appears that as systems become more autonomous (engaged in higher levels <strong>of</strong> automation) <strong>the</strong>re isless need for procedures. It is not that <strong>the</strong> procedure evaporates as soon as <strong>the</strong> system is automated -- <strong>the</strong>point is that <strong>the</strong> procedure is simply written in s<strong>of</strong>tware, and <strong>the</strong>refore <strong>the</strong> machine takes over someaspects <strong>of</strong> <strong>the</strong> procedure execution. For example, consider <strong>the</strong> task <strong>of</strong> rolling out <strong>of</strong> a turn. When handflying an aircraft, a useful rule <strong>of</strong> thumb (or procedure), is to start leveling <strong>the</strong> wings several degreesprior to <strong>the</strong> assigned heading. The time-honored rule <strong>of</strong> thumb is to lead <strong>the</strong> rollout heading by <strong>the</strong>number <strong>of</strong> degrees equal to half <strong>of</strong> <strong>the</strong> angle <strong>of</strong> bank (e.g., for a bank angle <strong>of</strong> 10 degrees to turn right toa heading <strong>of</strong> 090, rollout will be initiated at 085). <strong>On</strong> <strong>the</strong> o<strong>the</strong>r hand, when <strong>the</strong> autopilot is engaged, <strong>the</strong>flight crew will dial 090 in <strong>the</strong> heading window and <strong>the</strong> plane will turn and level <strong>of</strong>f by itself. Again, itis not that <strong>the</strong> procedure has vanished, but it is simply concealed in <strong>the</strong> autopilot computer code (in amore precise control algorithm, <strong>of</strong> course). In a previous paper (Degani and Wiener, 1991), wedescribed procedures as a bridge between <strong>the</strong> crew and <strong>the</strong> machine. With increased automation, dutiesand procedures that were previously assigned to <strong>the</strong> human are now usurped by <strong>the</strong> machine.Conversely, when <strong>the</strong>re is a need for a reduction in level <strong>of</strong> automation, a procedure must be instituted.For example, consider <strong>the</strong> following situation. When a glass cockpit aircraft is intercepting <strong>the</strong> glideslope and localizer while HEADING SELECT mode is engaged, and subsequently selecting APPROACHmode before <strong>the</strong> “localizer” and “glide slope” are captured, <strong>the</strong>re is a possibility for a false capture: The“glide slope” will capture and <strong>the</strong> plane will start to descend while maintaining <strong>the</strong> heading displayed in<strong>the</strong> HEADING SELECT window (and not <strong>the</strong> LOCALIZER course). The concern is obvious -- <strong>the</strong> aircraftwill descend, but not to <strong>the</strong> runway. The only feedback available to <strong>the</strong> flight crews is on <strong>the</strong> ADI: <strong>the</strong>LOCALIZER symbol will be armed (white), as opposed to being engaged (green) 10 . To counter this, onecompany's SOP states: “to prevent a false capture, do not arm <strong>the</strong> APPROACH mode until <strong>the</strong> localizerand glide slope pointers have appeared on <strong>the</strong> ADI.”9 This is due, in part, to <strong>the</strong> fact that <strong>the</strong> APU uses more fuel to start than running an engine. Ano<strong>the</strong>r benefit <strong>of</strong> thisprocedure is <strong>the</strong> reduction in <strong>the</strong> number <strong>of</strong> APU start sequences.10 This information can not be obtained from <strong>the</strong> mode control panel (MCP) -- because according to <strong>the</strong> MCP logic, onceAPPROACH mode is armed, <strong>the</strong> button is lit (regardless <strong>of</strong> whe<strong>the</strong>r <strong>the</strong> “localizer” has been captured or not).22
The above example shows how automation and procedures are inversely related. To “fix” a problemwith automation, one must go one step down in <strong>the</strong> level <strong>of</strong> automation. Subsequently, this requires anincrease in procedurization -- <strong>the</strong> pilots <strong>of</strong> this company may only engage <strong>the</strong> APPROACH mode afterseeing <strong>the</strong> “localizer” and “glide slope” pointers on <strong>the</strong> ADI.It appears that increased level <strong>of</strong> automation eliminates <strong>the</strong> need for some procedures. Also, automationmakes it more difficult to mandate a large set <strong>of</strong> stringent procedures. We believe several factors lead tothis.1. Some tasks that were previously assigned to <strong>the</strong> pilot have been completely automated. Forexample, <strong>the</strong> engine start sequence <strong>of</strong> an Airbus A-320 has been automated. This has resulted inone less engine control (<strong>the</strong> “fuel control” switch), reduction in task requirement (positioning <strong>the</strong>“fuel control” switch to “run”), and elimination <strong>of</strong> associated procedures (“Aborted Engine Startsor Excessive EGT on Ground”), as <strong>the</strong> system provides all limit protection as well as automaticengine crank after start abort.2. Since most modern automation is controlled by some type <strong>of</strong> digital processor, <strong>the</strong> interfacebetween human and machine is usually some form <strong>of</strong> computer input device. The most commonform is a keyboard. Using <strong>the</strong> CDU, simple tasks, such as position initialization, can beperformed as a set <strong>of</strong> procedures. Never<strong>the</strong>less, tasks that must be conducted in real time, requirefar more complex interaction with <strong>the</strong> computer, and hence are not amenable to simpleprocedurization. For instance, many crews build approaches that are not available in <strong>the</strong> FMC.The FMC routing and STARs will guide <strong>the</strong>m to a certain point short <strong>of</strong> <strong>the</strong> airport. If <strong>the</strong>y wishFMC guidance <strong>the</strong> rest <strong>of</strong> <strong>the</strong> way, <strong>the</strong>y have to build it, and this is too complex to be reduced tostep-by-step procedures and sub-tasks.3. Many aircraft systems, such as <strong>the</strong> aut<strong>of</strong>light system, operate in a dynamic and sometimesunpredictable environment and <strong>the</strong>refore cannot be completely pre-programmed. In <strong>the</strong>se cases,<strong>the</strong> aut<strong>of</strong>light system provides <strong>the</strong> pilot with several semi-automatic modes to choose from. Anexample is <strong>the</strong> various modes available to perform a level change: <strong>the</strong>re are at least five differentmethods to conduct this task. Therefore, any attempts to completely procedurize such tasks bymandating one method, would usually fail (and lead to non-compliance). <strong>On</strong>e major U.S.company attempted to procedurize <strong>the</strong> descent pr<strong>of</strong>ile <strong>of</strong> its B-737-EFIS fleet. The result wasnon-compliance. The project was quietly abandoned.To conclude, we argue that automation requires a new dimension in <strong>the</strong> design <strong>of</strong> flight deck procedures.As we have noted previously, a procedure that is ponderous and is perceived as increasing workloadand/or interrupting smooth cockpit flow will probably be ignored on <strong>the</strong> line. Even worse, <strong>the</strong>re couldbe a spreading <strong>of</strong> this effect, since a rejected procedure may lead to a more general distrust <strong>of</strong>procedures, resulting in non-conformity in o<strong>the</strong>r areas.Guideline #2: When designing procedures for automated cockpits, <strong>the</strong> designer shouldrecognize that many tasks that involve <strong>the</strong> use <strong>of</strong> automation are too complex and interactive toallow a stringent set <strong>of</strong> SOPs to be mandated.5.6.1 Lack <strong>of</strong> Automation PhilosophyMost airlines that fly glass cockpit aircraft have attempted to develop an operational doctrine for operating<strong>the</strong>se aircraft. Those that have failed to articulate a clear philosophy (and hence policies) have probablydone so because <strong>the</strong>y jumped immediately into policies, and in some cases straight into procedureswithout a governing philosophy.<strong>On</strong>e <strong>of</strong> <strong>the</strong> problems with not developing and publishing a philosophy <strong>of</strong> operations is that policies,decisions, and ultimately procedures are put into place without an explanatory basis. The philosophybehind <strong>the</strong>se decisions is not articulated nor understood. What is more, philosophies change from timeto time. Because <strong>the</strong>se changes in philosophy are not made public, <strong>the</strong>y can lead to confusion and to acompliance problem. For example, one airline's early automation doctrine was to fly an automatedaircraft, to <strong>the</strong> extent possible, as if it were a B-727, and <strong>the</strong>reby minimizing <strong>the</strong> use <strong>of</strong> advancedfeatures. Then, following a change in management, it switched to a philosophy <strong>of</strong> “use <strong>the</strong> automationas much as possible” (in order to save fuel, wear, etc.). Recently, as indicated by <strong>the</strong> vice president <strong>of</strong>23
- Page 2 and 3: TABLE OF CONTENTSSUMMARY ..........
- Page 4 and 5: 1. INTRODUCTIONWhen we try to pick
- Page 6 and 7: Hendrick (1987) states that human f
- Page 8 and 9: influenced by the individual philos
- Page 10 and 11: 3. THE FOURTH P: PRACTICES3.1. AN E
- Page 12 and 13: To summarize, the ultimate factor t
- Page 14 and 15: Humor. Humor is closely related to
- Page 16 and 17: technical deficiencies, induce work
- Page 18 and 19: operations and the philosophy of th
- Page 20 and 21: 5.3 MERGERS AND ACQUISITIONSMergers
- Page 22 and 23: Figure 7. A Boeing B-757 checklist
- Page 26 and 27: flight operations, the philosophy m
- Page 28 and 29: 5.7.3 Technique and PoliciesAny giv
- Page 30 and 31: For example, one company constantly
- Page 32 and 33: 6. ISSUES IN PROCEDURE DESIGN6.1 CO
- Page 34 and 35: solution involves “anchoring” a
- Page 36 and 37: On August 19, 1980, a Saudi Arabian
- Page 38 and 39: 3. The procedures allow the other a
- Page 40 and 41: coordination of tasks between agent
- Page 42 and 43: Similarly, it has been a common pra
- Page 44 and 45: 7.1.3 Structure of ProceduresAs men
- Page 46 and 47: mission simulation (see Wiener et a
- Page 48 and 49: felt that this is an efficient tech
- Page 50 and 51: esponse. The PF, therefore, can con
- Page 52 and 53: 7.5.1 Cross-fleet StandardizationCr
- Page 54 and 55: 1. Training department (for both pi
- Page 56 and 57: REFERENCESAviation Week and Space T
- Page 58 and 59: Perrow, C. (1986). Complex organiza
- Page 60 and 61: APPENDICESAppendix 1 - Guidelines f
- Page 62 and 63: 14. In managing automated cockpits,
- Page 64 and 65: APPENDIX 3 - QUESTIONS ASKED OF FLI
- Page 66 and 67: APPENDIX 5 - QUESTIONS ASKED DURING
- Page 68 and 69: 8. Change in operational environmen