Air temperature drops an average of 6.5 degrees Celsius per every 1000 feet. One of the central reasons behind aircraft altitude is that, as the air gets thinner with every foot climbed, planes can travel more easily and therefore move faster and burn less fuel, saving money. Note that the dew point temperature remains constant until saturation is reached. 6.5°C per 1,000 m – or about 3.5°F (2°C) per 1,000 ft. – from sea level to 11,000 meters (approximately 36,000 ft.) From 11,000 meters (approximately 36,000 ft.) up to 20,000 meters (approximately 65,600 ft.), constant temperature is -56.5°C (-69.7°F), and this is also the lowest assumed temperature in respect to ISA. The air is conditionally unstable if the temperature drops more than 2° per 1,000 feet on ascent. So if the OAT at 6000ft is -13°C, at 7000ft it will be -15°C, or minus 16 from the International Standard Atmosphere (ISA) which should be +1°C (15 - 2*7 = 1). This results in an increase of 38.5°F. 1,000 m = 8 degrees: 100 m = 14 degrees: 14-8=6 degrees colder. If there's no snow/rain falling from the sky, then the temperature decreases by about 5.4°F for every 1,000 feet up you go in elevation & decrease the same for every 1,000 feet you go down. A runway upslope increases takeoff distance by 7% per degree. If there's no snow (or rain) falling from the sky and you’re not in a cloud, then the temperature decreases by about 5.4°F for every 1,000 feet up you go in elevation. 5 The temperature will drop around 2° Celsius (-1.98 to be more precise) for each 1000 feet you climb. Convert an altitude in feet or metres of height above sea level to a pressure reading in millibar (mbar, mb or mbr) , pounds per square inch ( psi ), millimetres of mercury at zero degrees celsius ( mmHg @ 0 deg C) or inches of mercury at zero degrees celsius ( … Originally Answered: How much does the temperature drop per 1000 feet? The temperature will drop around 2° Celsius ( -1.98 to be more precise) for each 1000 feet you climb. So if the OAT at 6000ft is -13°C, at 7000ft it will be -15°C, or minus 16 from the International Standard Atmosphere (ISA) which should be +1°C (15 - 2*7 = 1). Length In Miles: Mi. The Troposphere is closest to the surface of the earth, and as you climb into it, on average, the temperature decreases by roughly Here is more information of Celsius, Fahrenheit, Kelvin, Réaumur, and Rankine Temperature Conversion. As moist, unstable air rises, clouds often form at the altitude where temperature and dewpoint reach the same value. You can also use about 1.2 degrees Celsius per ever 1000 feet, or about 1 degree Celsius per 100 meters (source, NFW who showed me my typo on the metric conversion in the comments). Takeoff Distance. In sunny weather, subtract about 5.4 degrees Fahrenheit for every 1,000 feet you go up in elevation. If radiation were the only way to transfer energy from the ground to space, the greenhouse effect of gases in the atmosphere would keep the ground at roughly 333 K (60 °C; 140 °F). Temperature decreases at a rate of 3.5°F (2°C) per thousand feet. For every 1,000 feet you climb, the air temperature will decrease by 35°F. *. However, most commercial aircraft fly in the bottom two layers — the Troposphere and the Stratosphere. Standard lapse rate = -1" hg. 5. than dry air since the moist air must rise higher before its temperature cools to that of the surrounding air. (1 Foot = 12 Inches, 1 Mile = 5280 Feet) (Concept: Elemental Geosystems, P. 20) Length In Feet: Ft. Rising parcels that are unsaturated cool at a rate of 10° C per 1000 meters they are lifted. It is this simple misconception that often disguises the hazards associated with high density altitudes. At A Scale Of 1:24,000, How Long (in Miles) Is An Object On Earth That Is 6 Inches Long On A Map? When it reaches the 5,000-foot level, the parcel has descended 7,000 feet at a rate of 5 1/2°F per 1,000 feet. by Robert Fogt on 03/04/03 at 19:48:15. What does that mean? Add an additional 20 percent for each additional 1,000-feet density altitude above 8,000 feet. The calculated data is based on the assumption from standard conditions that the air temperature drops 9.84 degrees C per 1000 m of altitude and the dewpoint drops 1.82 degrees C per 1000 meters altitude. Lapse rates are usually expressed as the amount of temperature change associated with a specified amount of altitude change, such as 9.8 K per kilometre, 0.0098 K per metre or the equivalent 5.4 °F per 1000 feet. Since the dew point temperature is a measure of the amount of water vapor in the parcel, it does not change unless there is a phase change of water happening in the parcel. Air temperature in the ISA is +15 o C at Mean Sea Level and decreases at approximately 2oC per 1000 feet … Consider experimenting to see how far your aircraft can glide. for each 1000' increase in altitude Sea level standard temperature = 15°C / 59°F Standard Lapse Rate = -2°C / -3.5°F for each 1000’ increase in altitude Adding the 38.5°F increase to the original 12,000 feet temperature of 23°F, the parcel has a new temperature of 61.5°F. The temperature drops approximately 5.4 degrees Fahrenheit per 1000 feet. Aviation Weather Center Homepage provides comprehensive user-friendly aviation weather Text products and graphics. Forced Landing Tips A good way to prepare for a forced landing is Sunlight hits the condensed matter surface of the earth, land and sea, and heats them. If there's no rain or snow falling from the sky and you're not in a cloud, the temperature decreases by about 5.4°F for every 1,000 feet (9.8°C per 1,000 meters) up you go in elevation. WARNING! The temperature profile of the atmosphere is a result of an interaction between thermal conduction, thermal radiation, and natural convection. Due to the unequal heating of the earth's surface by the sun, however, the real atmosphere is far from 'standard', and if an altimeter were not adjustable, its reading would At 2000 feet elevation, the temperature is 42 degrees F. What. True Airspeed. 2)You have calculated the recurrence level of a stram with a discharge of 250 cms to be 25 years. The standard temperature at 7,000 feet msl, therefore, is only 1 degree C (or 34 degrees F). It decreases about 2 degrees C (or 3.5 degrees F) per 1,000 feet of altitude above sea level. What is the approximate base of the cumulus clouds if the surface air temperature at 1,000 feet MSL is 70°F and the dewpoint is 48°F? Re: temperature drop with altitude gained. 6. They then heat the air above the surface. The dry adiabatic lapse rate (unsaturated air) is 3 °C (5.4 °F) per 1,000 feet. 1)Normal lapse rate is 3.5 degrees per 1000 feet. 1000 ft elevation and decreases in temperature at a rate of about 2 C per 1000 ft elevation. Temperature Lapse Rate. Unsaturated air moving upward and downward cools and warms at about 3C (5.4F) per 1000 ft. dry adiabatic lapse rate. When the surface wind shifts to the north or northeast after passage of a cold front, that front may well be back as a warm front in a day or so. If you are IN a cloud, or if it is snowing or raining, subtract about 3.3 degrees Fahrenheit for every 1,000 feet you go up in elevation. Though as a hiker, you wont have to worry about that. A rule of thumb for Cessna 152s and 172s is 1.5 nautical miles per 1,000 feet of altitude above ground level. Above this point, the temperature is considered constant up to 80,000 feet. True airspeed increases by 2% for every 1,000′ of altitude. In mathematical speak that is 9.8°C per 1,000 meters. If you’re in a cloud or if it's raining/snowing, the temperature decreases by about 3.3°F for every 1,000 feet (6°C per 1,000 meters) up you go in elevation. On a dry, sunny day, the temperature typically drops 3 1/2 degrees per 1000 feet of altitude increase in dry air. 2. ... Meso: 30+ mi, sharp temp drop Thermo: 30+, sharp increase in temperature. *. 3)You have a topographic map at a scale of 1:24,000. For safe wiring practices, consult the National Electrical Code®, your local building inspector, or a qualified electrician. Takeoff distance increases by 10% for every 1,000′ of density altitude above sea level. **Based on 60°C per NEC 110.14(c)(1)(a). You don’t need any fancy equipment to estimate how temperature might change with altitude. 5. There are variables, though. glide per 1,000 feet of altitude is another very useful thing to know. The moist adiabatic lapse rate varies from 1.1 °C to 2.8 °C (2 °F to 5 °F) per 1,000 feet. This continues up for around 36,000 feet, where you run into the Tropopause, which is the boundary layer before reaching the Stratosphere. Be aware of max ISA temperatures that cannot be exceeded ***Based on 75°C per NEC 110.14(c)(1)(b). Atmospheric pressure, also known as barometric pressure (after the barometer), is the pressure within the atmosphere of Earth.The standard atmosphere (symbol: atm) is a unit of pressure defined as 101,325 Pa (1,013.25 hPa; 1,013.25 mbar), which is equivalent to 760 mm Hg, 29.9212 inches Hg, or 14.696 psi. At 9,000 feet density altitude (8 * .12 = .96 plus .20 = 1.16). You will lose an average 3.5 degrees Fahrenheit for every 1000 feet of elevation you gain. If you start out at 1000 feet, and climb to 6000 feet, that’s a 5000 foot difference (6000 – 1000 = 5000). So, since you’re gaining 5,000 feet in elevation, you’ll use a 5 in your calculation. 5,000 feet, times 3.5 degrees. Just drop the (thousand). So, ( 5 x 3.5 = 17.5 degrees). So roughly, you’ll expect to lose at least 17.5 degrees. Although the actual atmospheric lapse rate varies, under normal atmospheric conditions the average atmospheric lapse rate results in a temperature decrease of 3.5°F/1,000 ft (6.4°C/km) of altitude. Answer has 2 votes. The temperature of the atmosphere actually heats up when you get above the dense gas altitudes. is the temperature at 0 feet elevation? The temperature of the atmosphere actually heats up when you get above the dense gas altitudes. Altitude to Pressure Conversion Table. The standard temperature at 7,000 feet msl, therefore, is only 1 degree C (or 34 degrees F). For example, the density altitude at an airport 7000 feet above sea level, with a temperature of 18 degrees Celsius and a pressure altitude of 7000 (assuming standard pressure) would be calculated as follows. 18 – 1 = 17. If the atmospheric air cools with increasing altitude, the lapse rate may be expressed as a negative number. Here, the temperature stops falling with increased height and becomes a constant value. 7 / 1000 = .007 = seven thousandth of a degree per meter. The voltage drop V in volts (V) is equal to the wire current I in amps (A) times 2 times one way wire length L in feet (ft) times the wire resistance per 1000 feet R in ohms (Ω/kft) divided by 1000: Vdrop (V) = Iwire (A) × Rwire(Ω) = Iwire (A) × (2 × L(ft) × Rwire(Ω/kft) / 1000 (ft/kft)) The voltage drop … Let’s say you typically ride at 1,000 feet elevation but are headed to 6,000 feet-plus for a snowmobiling trip. Using the formula below, you can make a quick determination as to the approximate loss in horsepower that you will experience at the higher elevation: … A standard temperature lapse rate is when the temperature decreases at the rate of approximately 3.5°F or 2°C per thousand feet up to 36,000 feet, which is approximately –65 °F or –55 °C. Inversions A standard pressure lapse rate is The change in temperature from 0 to 1,000 meters is 7 degrees Celsius, what is the change in temperature per meter of altitude? Air pressure in the ISA is 1013 hectoPascals at Mean Sea Level and the pressure decreases with altitude, at about 1 hPa per 30 feet gain in height in the lower levels of the atmosphere. The earth’s atmosphere is around 300 miles thick and is divided into five main layers. This results in a convergence of temperature and dewpoint at a rate of 4.4°F. So in Denver (at 6,000 feet amsl), if the local pressure is 24″, the radio will report the barometric pressure to be 30″. Using ISA standards, the defaults for pressure and temperature at sea level are 101,325 Pa and 288 K. Due to the fact that weather conditions affect pressure and altitude calculations, the pressure and temperature at sea level must be known. However, if it is snowing/raining, the temperature decreases/increases by about 3.3°F for every 1,000 feet up/down you go in elevation. As aircraft climb, the air gets colder. Some people use 9.8 degrees Celsius per 1000 meters). The "sweet spot" of flying is regarded as Installation of electrical wire can be hazardous if done improperly, and can result in personal injury or property damage. When lifted, unsaturated air cools at a rate of 5.4°F per 1,000 feet and the dewpoint temperature decreases at a rate of 1°F per 1,000 feet. If you do high altitude shooting at long range, bring along a Kestral, or remember to mentally correct the radio station’s pressure, by 1″ per 1,000 feet.” Add 116 percent to sea-level takeoff distance. This is only true in the troposphere, which is 36,000 feet and below.
temperature drop per 1,000 feet aviation
Air temperature drops an average of 6.5 degrees Celsius per every 1000 feet. One of the central reasons behind aircraft altitude is that, as the air gets thinner with every foot climbed, planes can travel more easily and therefore move faster and burn less fuel, saving money. Note that the dew point temperature remains constant until saturation is reached. 6.5°C per 1,000 m – or about 3.5°F (2°C) per 1,000 ft. – from sea level to 11,000 meters (approximately 36,000 ft.) From 11,000 meters (approximately 36,000 ft.) up to 20,000 meters (approximately 65,600 ft.), constant temperature is -56.5°C (-69.7°F), and this is also the lowest assumed temperature in respect to ISA. The air is conditionally unstable if the temperature drops more than 2° per 1,000 feet on ascent. So if the OAT at 6000ft is -13°C, at 7000ft it will be -15°C, or minus 16 from the International Standard Atmosphere (ISA) which should be +1°C (15 - 2*7 = 1). This results in an increase of 38.5°F. 1,000 m = 8 degrees: 100 m = 14 degrees: 14-8=6 degrees colder. If there's no snow/rain falling from the sky, then the temperature decreases by about 5.4°F for every 1,000 feet up you go in elevation & decrease the same for every 1,000 feet you go down. A runway upslope increases takeoff distance by 7% per degree. If there's no snow (or rain) falling from the sky and you’re not in a cloud, then the temperature decreases by about 5.4°F for every 1,000 feet up you go in elevation. 5 The temperature will drop around 2° Celsius (-1.98 to be more precise) for each 1000 feet you climb. Convert an altitude in feet or metres of height above sea level to a pressure reading in millibar (mbar, mb or mbr) , pounds per square inch ( psi ), millimetres of mercury at zero degrees celsius ( mmHg @ 0 deg C) or inches of mercury at zero degrees celsius ( … Originally Answered: How much does the temperature drop per 1000 feet? The temperature will drop around 2° Celsius ( -1.98 to be more precise) for each 1000 feet you climb. So if the OAT at 6000ft is -13°C, at 7000ft it will be -15°C, or minus 16 from the International Standard Atmosphere (ISA) which should be +1°C (15 - 2*7 = 1). Length In Miles: Mi. The Troposphere is closest to the surface of the earth, and as you climb into it, on average, the temperature decreases by roughly Here is more information of Celsius, Fahrenheit, Kelvin, Réaumur, and Rankine Temperature Conversion. As moist, unstable air rises, clouds often form at the altitude where temperature and dewpoint reach the same value. You can also use about 1.2 degrees Celsius per ever 1000 feet, or about 1 degree Celsius per 100 meters (source, NFW who showed me my typo on the metric conversion in the comments). Takeoff Distance. In sunny weather, subtract about 5.4 degrees Fahrenheit for every 1,000 feet you go up in elevation. If radiation were the only way to transfer energy from the ground to space, the greenhouse effect of gases in the atmosphere would keep the ground at roughly 333 K (60 °C; 140 °F). Temperature decreases at a rate of 3.5°F (2°C) per thousand feet. For every 1,000 feet you climb, the air temperature will decrease by 35°F. *. However, most commercial aircraft fly in the bottom two layers — the Troposphere and the Stratosphere. Standard lapse rate = -1" hg. 5. than dry air since the moist air must rise higher before its temperature cools to that of the surrounding air. (1 Foot = 12 Inches, 1 Mile = 5280 Feet) (Concept: Elemental Geosystems, P. 20) Length In Feet: Ft. Rising parcels that are unsaturated cool at a rate of 10° C per 1000 meters they are lifted. It is this simple misconception that often disguises the hazards associated with high density altitudes. At A Scale Of 1:24,000, How Long (in Miles) Is An Object On Earth That Is 6 Inches Long On A Map? When it reaches the 5,000-foot level, the parcel has descended 7,000 feet at a rate of 5 1/2°F per 1,000 feet. by Robert Fogt on 03/04/03 at 19:48:15. What does that mean? Add an additional 20 percent for each additional 1,000-feet density altitude above 8,000 feet. The calculated data is based on the assumption from standard conditions that the air temperature drops 9.84 degrees C per 1000 m of altitude and the dewpoint drops 1.82 degrees C per 1000 meters altitude. Lapse rates are usually expressed as the amount of temperature change associated with a specified amount of altitude change, such as 9.8 K per kilometre, 0.0098 K per metre or the equivalent 5.4 °F per 1000 feet. Since the dew point temperature is a measure of the amount of water vapor in the parcel, it does not change unless there is a phase change of water happening in the parcel. Air temperature in the ISA is +15 o C at Mean Sea Level and decreases at approximately 2oC per 1000 feet … Consider experimenting to see how far your aircraft can glide. for each 1000' increase in altitude Sea level standard temperature = 15°C / 59°F Standard Lapse Rate = -2°C / -3.5°F for each 1000’ increase in altitude Adding the 38.5°F increase to the original 12,000 feet temperature of 23°F, the parcel has a new temperature of 61.5°F. The temperature drops approximately 5.4 degrees Fahrenheit per 1000 feet. Aviation Weather Center Homepage provides comprehensive user-friendly aviation weather Text products and graphics. Forced Landing Tips A good way to prepare for a forced landing is Sunlight hits the condensed matter surface of the earth, land and sea, and heats them. If there's no rain or snow falling from the sky and you're not in a cloud, the temperature decreases by about 5.4°F for every 1,000 feet (9.8°C per 1,000 meters) up you go in elevation. WARNING! The temperature profile of the atmosphere is a result of an interaction between thermal conduction, thermal radiation, and natural convection. Due to the unequal heating of the earth's surface by the sun, however, the real atmosphere is far from 'standard', and if an altimeter were not adjustable, its reading would At 2000 feet elevation, the temperature is 42 degrees F. What. True Airspeed. 2)You have calculated the recurrence level of a stram with a discharge of 250 cms to be 25 years. The standard temperature at 7,000 feet msl, therefore, is only 1 degree C (or 34 degrees F). It decreases about 2 degrees C (or 3.5 degrees F) per 1,000 feet of altitude above sea level. What is the approximate base of the cumulus clouds if the surface air temperature at 1,000 feet MSL is 70°F and the dewpoint is 48°F? Re: temperature drop with altitude gained. 6. They then heat the air above the surface. The dry adiabatic lapse rate (unsaturated air) is 3 °C (5.4 °F) per 1,000 feet. 1)Normal lapse rate is 3.5 degrees per 1000 feet. 1000 ft elevation and decreases in temperature at a rate of about 2 C per 1000 ft elevation. Temperature Lapse Rate. Unsaturated air moving upward and downward cools and warms at about 3C (5.4F) per 1000 ft. dry adiabatic lapse rate. When the surface wind shifts to the north or northeast after passage of a cold front, that front may well be back as a warm front in a day or so. If you are IN a cloud, or if it is snowing or raining, subtract about 3.3 degrees Fahrenheit for every 1,000 feet you go up in elevation. Though as a hiker, you wont have to worry about that. A rule of thumb for Cessna 152s and 172s is 1.5 nautical miles per 1,000 feet of altitude above ground level. Above this point, the temperature is considered constant up to 80,000 feet. True airspeed increases by 2% for every 1,000′ of altitude. In mathematical speak that is 9.8°C per 1,000 meters. If you’re in a cloud or if it's raining/snowing, the temperature decreases by about 3.3°F for every 1,000 feet (6°C per 1,000 meters) up you go in elevation. On a dry, sunny day, the temperature typically drops 3 1/2 degrees per 1000 feet of altitude increase in dry air. 2. ... Meso: 30+ mi, sharp temp drop Thermo: 30+, sharp increase in temperature. *. 3)You have a topographic map at a scale of 1:24,000. For safe wiring practices, consult the National Electrical Code®, your local building inspector, or a qualified electrician. Takeoff distance increases by 10% for every 1,000′ of density altitude above sea level. **Based on 60°C per NEC 110.14(c)(1)(a). You don’t need any fancy equipment to estimate how temperature might change with altitude. 5. There are variables, though. glide per 1,000 feet of altitude is another very useful thing to know. The moist adiabatic lapse rate varies from 1.1 °C to 2.8 °C (2 °F to 5 °F) per 1,000 feet. This continues up for around 36,000 feet, where you run into the Tropopause, which is the boundary layer before reaching the Stratosphere. Be aware of max ISA temperatures that cannot be exceeded ***Based on 75°C per NEC 110.14(c)(1)(b). Atmospheric pressure, also known as barometric pressure (after the barometer), is the pressure within the atmosphere of Earth.The standard atmosphere (symbol: atm) is a unit of pressure defined as 101,325 Pa (1,013.25 hPa; 1,013.25 mbar), which is equivalent to 760 mm Hg, 29.9212 inches Hg, or 14.696 psi. At 9,000 feet density altitude (8 * .12 = .96 plus .20 = 1.16). You will lose an average 3.5 degrees Fahrenheit for every 1000 feet of elevation you gain. If you start out at 1000 feet, and climb to 6000 feet, that’s a 5000 foot difference (6000 – 1000 = 5000). So, since you’re gaining 5,000 feet in elevation, you’ll use a 5 in your calculation. 5,000 feet, times 3.5 degrees. Just drop the (thousand). So, ( 5 x 3.5 = 17.5 degrees). So roughly, you’ll expect to lose at least 17.5 degrees. Although the actual atmospheric lapse rate varies, under normal atmospheric conditions the average atmospheric lapse rate results in a temperature decrease of 3.5°F/1,000 ft (6.4°C/km) of altitude. Answer has 2 votes. The temperature of the atmosphere actually heats up when you get above the dense gas altitudes. is the temperature at 0 feet elevation? The temperature of the atmosphere actually heats up when you get above the dense gas altitudes. Altitude to Pressure Conversion Table. The standard temperature at 7,000 feet msl, therefore, is only 1 degree C (or 34 degrees F). For example, the density altitude at an airport 7000 feet above sea level, with a temperature of 18 degrees Celsius and a pressure altitude of 7000 (assuming standard pressure) would be calculated as follows. 18 – 1 = 17. If the atmospheric air cools with increasing altitude, the lapse rate may be expressed as a negative number. Here, the temperature stops falling with increased height and becomes a constant value. 7 / 1000 = .007 = seven thousandth of a degree per meter. The voltage drop V in volts (V) is equal to the wire current I in amps (A) times 2 times one way wire length L in feet (ft) times the wire resistance per 1000 feet R in ohms (Ω/kft) divided by 1000: Vdrop (V) = Iwire (A) × Rwire(Ω) = Iwire (A) × (2 × L(ft) × Rwire(Ω/kft) / 1000 (ft/kft)) The voltage drop … Let’s say you typically ride at 1,000 feet elevation but are headed to 6,000 feet-plus for a snowmobiling trip. Using the formula below, you can make a quick determination as to the approximate loss in horsepower that you will experience at the higher elevation: … A standard temperature lapse rate is when the temperature decreases at the rate of approximately 3.5°F or 2°C per thousand feet up to 36,000 feet, which is approximately –65 °F or –55 °C. Inversions A standard pressure lapse rate is The change in temperature from 0 to 1,000 meters is 7 degrees Celsius, what is the change in temperature per meter of altitude? Air pressure in the ISA is 1013 hectoPascals at Mean Sea Level and the pressure decreases with altitude, at about 1 hPa per 30 feet gain in height in the lower levels of the atmosphere. The earth’s atmosphere is around 300 miles thick and is divided into five main layers. This results in a convergence of temperature and dewpoint at a rate of 4.4°F. So in Denver (at 6,000 feet amsl), if the local pressure is 24″, the radio will report the barometric pressure to be 30″. Using ISA standards, the defaults for pressure and temperature at sea level are 101,325 Pa and 288 K. Due to the fact that weather conditions affect pressure and altitude calculations, the pressure and temperature at sea level must be known. However, if it is snowing/raining, the temperature decreases/increases by about 3.3°F for every 1,000 feet up/down you go in elevation. As aircraft climb, the air gets colder. Some people use 9.8 degrees Celsius per 1000 meters). The "sweet spot" of flying is regarded as Installation of electrical wire can be hazardous if done improperly, and can result in personal injury or property damage. When lifted, unsaturated air cools at a rate of 5.4°F per 1,000 feet and the dewpoint temperature decreases at a rate of 1°F per 1,000 feet. If you do high altitude shooting at long range, bring along a Kestral, or remember to mentally correct the radio station’s pressure, by 1″ per 1,000 feet.” Add 116 percent to sea-level takeoff distance. This is only true in the troposphere, which is 36,000 feet and below.
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