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I__. - International Military Testing Association

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TABLE 2. Ranking, Weighting, and Scoring for Troubleshooting Evaluation Factors<br />

Rank Factor Weight Scoring Scale<br />

(Max Points)<br />

Scoring<br />

(Per event)<br />

1<br />

2<br />

3<br />

4<br />

Solution<br />

Cost (Incorrect Sol)<br />

Time<br />

Proof Points<br />

42.78<br />

13.13<br />

11.80<br />

9.88<br />

‘EZ<br />

20:62<br />

17.23<br />

-100 For Fail to find<br />

-0.5 X ea NFR LRU<br />

-0.5 X ea Minute<br />

- % X ea Proof Pt missed<br />

i<br />

Illogical<br />

Invalid<br />

Approach<br />

Checks<br />

6.87<br />

4.68<br />

12.01<br />

8.18<br />

-6.0 X ea Illogical App<br />

-0.8 X ea Invalid Check<br />

5<br />

Out of Sounds<br />

Tests Points<br />

4.00<br />

3.21<br />

8.99<br />

5.61<br />

-0.6 X ea Out of Sounds<br />

4.5 X # of Tests<br />

Q<br />

10<br />

Checks<br />

Redundant Checks<br />

3.08<br />

tbd<br />

5.38<br />

tbd<br />

-0.5 X # of Checks<br />

to be analyzed<br />

Scoring is designed to discriminate between levels of troubleshooting proficiency: failure to solve the<br />

roblem results in a score of 0, while solving the problem results in a score of 100. There is no partial score<br />

Por factor 1. Ability to discriminate between levels of troubleshooting proficiency is in scoring of the remaining<br />

factors. Wei hts for the factors were converted into a scale equaling 100 points. The final score for each<br />

subject equa Bs<br />

100 points minus the sum of points lost for each factor. The minimum score is 0: that is, no<br />

ne atfve scores. The scoring criteria for each factor, also shown in Table 2, are the wei hts that were used<br />

In tfe TAE epfsodes to evaluate and diagnose troubleshooting proficiency levels. The cost9actor<br />

was changed<br />

to incorrect solutions to more accurately describe the actual behavior.<br />

Once we had determined factors and scoring scheme, we selected and constructed practical<br />

troubleshooting episodes that provided a valid representation tionof the hardware system being used in the<br />

study. Our hardware system was the U.S. Navy s communications system, the Navy Modular Automated<br />

Communications System/Satellite Communications (NAVMACS/SATCOM). To construct TAE<br />

troubleshooting episodes, we focused on the fault diagnosis/problem solving behaviors (Table 3) that military<br />

schools have identified in their six step troubleshooting process (Conner 1986,1987).<br />

\<br />

TABLE 3. Six Step Troubleshooting Process<br />

1. Symptom Recognition<br />

2. Symptom Elaboration<br />

3. Probable Faulty Functions<br />

4. Localizing Faulty Function(s)<br />

5. Isolating Faulty Circuit<br />

6. Failure Analysis.<br />

Although the design and delivery of the troubleshooting episodes did not require a computer, the amount<br />

of data made it obvious that the only efficient and cost effective approach would be utilization of microcomputer<br />

delivery and data gathering. Also, to keep developmental and hardware costs down, we limited ourselves to<br />

using off-the-shelf technology. We also reduced the “troubleshooting universe” of the episodes so that a<br />

standard microcomputer memory could handle data.<br />

The model developed for the troubleshooting actlviiy on a iven piece of hardware (shown in Fi ure 2)<br />

9<br />

provides a TAE Factors Model for “System Troubleshooting.” he modd works as follows: Once a8ystem is determined to be inoperative, the fault symptoms reduce the universe of type and location of tests to be<br />

made to a reasonable spectrum for further Investigation; that is the symptoms bound the problem and<br />

establishes what is in or out of bounds. This bounding of the problem reduces the number of tests in the<br />

spectrum to reasonable number and limits the amount of computer memory necessary. We called the “in<br />

bounds” checks that are not logical for the fault symptoms “illogrcal approach.” For a given set of symptoms<br />

for a given fault, there is an optimum troubleshooting path to determine the problem. To prove a component,<br />

or unit, is bad a number of tests must be performed; this requires testing of the “proof points.”<br />

. .<br />

IroubleshootlW<br />

-!+DrK~<br />

Jrcub @shoctlna<br />

f Faull 0 llbgi~l Approach<br />

0 Optimum Path 0 Out Of Bounds<br />

0 Proof Points 0 In Bounds<br />

Figure 2. TAE Factors Model<br />

373

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