9. ENGINE OUT PERFORMANCE

8369. If an engine failure occurs at an altitude above single-engine ceiling, what airspeed should be maintained?. VMC. VYSE. VXSE.

8370. What is the resulting performance loss when one engine on a twin-engine airplane fails?. Reduction of cruise airspeed by 50 percent. Reduction of climb by 80 to 90 percent. Reduction of all performance by 50 percent.

8371. Under what condition is VMC the highest?. Gross weight is at the maximum allowable value. CG is at the most rearward allowable position. CG is at the most forward allowable position.

9355. Which operational requirement must be observed by a commercial operator when ferrying a large, three-engine, turbojet-powered airplane from one facility to another to repair an inoperative engine?. The computed takeoff distance to reach V1 must not exceed 70 percent of the effective runway length. The existing and forecast weather for departure, en route, and approach must be VFR. No passengers may be carried.

9355-1. You are assigned to ferry a large, three-engine, turbojet-powered airplane from one facility to another to repair an inoperative engine. You know you are restricted to. VFR weather for takeoff, en route, and landing. flight crewmembers only aboard. a computed takeoff distance to reach V1 that cannot exceed 70 percent of the effective runway length.

9358. A commercial operator plans to ferry a large, four-engine, reciprocating-engine-powered airplane from one facility to another to repair an inoperative engine. Which is an operational requirement for the three-engine flight?. The gross weight at takeoff may not exceed 75 percent of the maximum certificated gross weight. Weather conditions at the takeoff and destination airports must be VFR. The computed takeoff distance to reach V1 must not exceed 70 percent of the effective runway length.

9359. Which operational requirement must be observed when ferrying an air carrier airplane when one of its three turbine engines is inoperative?. The weather conditions at takeoff and destination must be VFR. The flight cannot be conducted between official sunset and official sunrise. Weather conditions must exceed the basic VFR minimums for the entire route, including takeoff and landing.

9360. Which operational requirement must be observed when ferrying a large, turbine-engine-powered airplane when one of its engines is inoperative?. The weather conditions at takeoff and destination must be VFR. Weather conditions must exceed the basic VFR minimums for the entire route, including takeoff and landing. The flight cannot be conducted between official sunset and sunrise.

9361. When a turbine-engine-powered airplane is to be ferried to another base for repair of an inoperative engine, which operational requirement must be observed?. Only the required flight crewmembers may be on board the airplane. The existing and forecast weather for departure, en route, and approach must be VFR. No passengers except authorized maintenance personnel may be carried.

8678. (Refer to Figure 70.) How many minutes of dump time is required to reach a weight of 144,500 pounds? Initial weight................................................ 180,500 lb Zero fuel weight.......................................... 125,500 lb. 13 minutes. 15 minutes. 16 minutes.

8679. (Refer to Figure 70.) How many minutes of dump time is required to reduce fuel load to 25,000 pounds? Initial weight.................................................179,500 lb Zero fuel weight.......................................... 136,500 lb. 10 minutes. 9 minutes. 8 minutes.

8680. (Refer to Figure 70.) How many minutes of dump time is required to reach a weight of 151,500 pounds? Initial weight.................................................181,500 lb Zero fuel weight.......................................... 126,000 lb. 15 minutes. 14 minutes. 13 minutes.

8681. (Refer to Figure 70.) How many minutes of dump time is required to reduce fuel load to 16,000 pounds (at 2,350 lbs/min)? Initial weight.................................................175,500 lb Zero fuel weight.......................................... 138,000 lb. 9 minutes. 10 minutes. 8 minutes.

8682. (Refer to Figures 71 and 72.) What is the approximate level-off pressure altitude after drift-down under Operating Conditions D-1?. 19,400 feet. 18,000 feet. 20,200 feet.

8683. (Refer to Figures 71 and 72.) What is the approximate level-off pressure altitude after drift-down under Operating Conditions D-2?. 14,700 feet. 17,500 feet. 18,300 feet.

8684. (Refer to Figures 71 and 72.) What is the approxi- mate level-off pressure altitude after drift-down under Operating Conditions D-3?. 22,200 feet. 19,800 feet. 21,600 feet.

8685. (Refer to Figures 71 and 72.) What is the approximate level-off pressure altitude after drift-down under Operating Conditions D-4?. 27,900 feet. 22,200 feet. 24,400 feet.

8686. (Refer to Figures 71 and 72.) What is the approximate level-off pressure altitude after drift-down under Operating Conditions D-5?. 8,800 feet. 9,600 feet. 13,000 feet.