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I__. - International Military Testing Association

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Figure 2 shows temporal effects at auto mechanic test sites.<br />

Site A experienced a slight drop in agreement in the middle time<br />

period. The decline in reliability was noted at the time, so<br />

counselling and retraining were conducted, resulting in an<br />

increase during the final period. Site B agreement increased<br />

during all three periods. The overall increase in agreement at<br />

both sites is natural given increasing familiarity of the TAs<br />

with the scoring standards over time. The fact that the increase<br />

is relatively small indicates that the initial training program<br />

prepared the TAS very well. Again, this points to test effects<br />

as a likely cause of the differences in reliabilities.<br />

This same trend carries over into the helicopter mechanic<br />

t reliabilities despite some differences in their HOPTs. Whereas<br />

all automotive mechanics were given the same HOPT, each<br />

helicopter mechanic MOS had its own test. Helicopter MOSS were<br />

tested sequentially, so temporal effects are evident across<br />

aircraft type, as shown in Figure 3. Since test order varied<br />

across site, increased reliability is not indicated left to right<br />

for both sites. Test order for Site C was CH-53A/D, CH-46,<br />

CH-53E, and UH/AH-1. Site D order was UH/AH-1, CH-46, and CH-<br />

53E. No CH-53A/D were tested at Site D. Taking this test order<br />

into account we see that agreement increased over time at both<br />

sites, except for the CH-46 at Site C.<br />

Agasmcnt between +-7wy md shodor ted odnhistrotorr b y oicroft<br />

Fig. 3: Agreement by Aircraft Fig. 4: Agreement by Interview<br />

Ratings<br />

The drop in CH-46 agreement is explainable in terms of<br />

variation in test conditions. At Site D, all examinees in 2<br />

particular MOS were tested on the same aircraft. At Site C, each<br />

unit set up its own aircraft, resulting in changing conditi

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