Table 7-2. Simulated Malfunction Details (cont)

TM 55 6930-212-10 Table 7-2. Simulated Malfunction Details - Continued Method of Indications and effects on Effects sensed by trainee introduction related systems as presented if corrective action is Malfunction by instructor to the instructor and trainee not taken UTL hydraulic 679 Transmission (utility hydraulic Loss of utility pump transmission pump) does not operate. hydraulics. Auxiliary tank 701 (R FWD) AUX PRESS caution light illumi- AUX PRESS caution light boost pump fail 702 (R AFT) nates and fuel in affected tanks illuminates. Fuel in 704 (L FWD) cannot be used. Fuel quantity affected tanks cannot be 705 (L AFT) indication remains constant for used. Fuel quantity indi- affected tank. cation remains constant for affected tank. Main tank boost 703 (Right) L or R FUEL PRESS caution light If operations are being pump fail 706 (Left) illuminates. Fuel is supplied conducted above 6.000 feet (both pumps) to engines from each main tank pressure altitude, with through a bypass check as long as crossfeed fuel valve aircraft is operated below 6,000 closed, fuel starvation to feet pressure altitude. Auxiliary affected engine results. fuel tanks continue to transfer fuel to main tanks. Uneven fuel 707 (Left) Fuel quantity indicator shows un- Fuel quantity indicator consumption 708 (Right) even fuel distribution. Gradual shows uneven fuel distri- lateral CG shift occurs. This bution. Gradual lateral indicates loss of fuel from CG shift occurs. affected side and not an increase in fuel consumption caused by the engine (to simulate fuel leak and/or being pumped overboard). 7-22