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This form is used for recording and calculating takeoff data for the KC-135R aircraft, including thrust settings, weight, and environmental conditions.
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How to fill out kc-135r takeoff data

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How to fill out KC-135R TAKEOFF DATA

01
Begin by setting up the aircraft's flight management system.
02
Enter the aircraft's weight and balance data, including fuel and cargo.
03
Input the current weather conditions at the departure airport.
04
Determine and enter the field elevation and runway length.
05
Calculate the required takeoff thrust settings based on aircraft performance charts.
06
Fill in the V1, V2, and VR speeds as per the aircraft's performance data.
07
Review and verify all entered data for accuracy before finalizing.

Who needs KC-135R TAKEOFF DATA?

01
Pilots operating the KC-135R for accurate flight planning.
02
Flight planners involved in mission coordination.
03
Maintenance crews needing to understand aircraft readiness.
04
Air traffic control for safe departure management.
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People Also Ask about

With necessary runway requirements at just over 6000 feet, the 737-200 is able to access a great number of additional airports in comparison to its competition in the class. The average hourly rental rate of the Boeing 737-200 is around 18,300 USD per hour.
Four turbofans, mounted under 35-degree swept wings, power the KC-135 to takeoffs at gross weights of up to 322,500 pounds. A cargo deck above the refueling system can hold a mixed load of passengers and cargo. Depending on fuel storage configuration, the KC-135 can carry up to 83,000 pounds of cargo.
The only external difference between a KC-135R and a KC-135T is the presence of a clear window on the underside of the empennage of the KC-135T where a remote controlled searchlight is mounted.
For example, at ambient temperature of 60°F, pressure altitude of 3000 feet and a headwind of 3 knots, the KC-135 with a gross weight of 220,000 pounds has a runway roll of about 6300 feet as compared to the C-141 with the same gross weight which has a runway roll of about 2600 fePt.
Our SOP is 6000' runways minimum, I could see theirs being 6500'.
Fuel use is typically around 10,000 lbs per hour at 530 mph (4500 kg at 850 km/h). So a straightforward bit of arithmetic tells us that the aircraft could stay aloft for 20 hours, during which it would travel about 10,600 miles. In fact, the ferry range is given variously online as between 9500–11,000 miles.
The refueling pods are required to provide and offload rate of 355 gallons per minute (gpm) to receiver aircraft (Boeing, 1995).
For example, the takeoff distance at a normal maximum takeoff weight of 155,000 pounds (70,305 kg) is 3,290 ft (1,003 m) for the C-130J model and 3,586 feet (1,093 m) for the C-130H model.

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KC-135R TAKEOFF DATA refers to the specific information recorded prior to the takeoff of a KC-135R aircraft, which includes parameters such as weight, balance, and environmental conditions necessary for a safe takeoff.
Pilots and aircrew members of the KC-135R are required to file KC-135R TAKEOFF DATA as part of the pre-flight procedures to ensure safety and compliance with operational standards.
To fill out KC-135R TAKEOFF DATA, the pilot must enter specific flight parameters including aircraft weight, fuel load, runway length, and environmental conditions. This ensures all necessary data is recorded accurately for a safe takeoff.
The purpose of KC-135R TAKEOFF DATA is to ensure that the aircraft is within safe operational limits for takeoff, providing critical information for performance calculations that help mitigate risks during the flight.
The information that must be reported on KC-135R TAKEOFF DATA includes aircraft weight, center of gravity, fuel load, engine performance data, and environmental conditions such as temperature and wind speed.
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