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 حالة الطقس في عنتبي ذلك اليوم المشؤم
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History for Entebbe, Uganda
on Saturday, July 30, 2005
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Airport Code:
Latest visited Airport Codes: HUEN | 63612
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Daily Summary
Actual Average Record
Temperature
Mean Temperature 73 °F / 22 °C -
Max Temperature 77 °F / 25 °C - - ()
Min Temperature 68 °F / 20 °C - - ()
Cooling Degree Days 8
Growing Degree Days 23 (Base 50)
Moisture
Dew Point 66 °F / 18 °C
Average Humidity 82
Maximum Humidity 94
Minimum Humidity 73
Precipitation
Precipitation 0.00 in / 0.00 cm - - ()
Sea Level Pressure
Sea Level Pressure 30.06 in / 1018 hPa
Wind
Wind Speed 10 mph / 16 km/h (NNE)
Max Wind Speed 12 mph / 19 km/h
Max Gust Speed -
Visibility 6 miles / 10 kilometers
Events
Key: T is trace of precipitation, MM is missing value
Source: NWS Daily Summary
Show full METARS (help) - Comma Delimited File
Time(EAT) Temperature Dew Point Humidity Sea Level Pressure Visibility Wind Direction Wind Speed Gust Speed Precipitation Events Conditions
9:00 AM 69.8 °F / 21.0 °C 64.4 °F / 18.0 °C 83% - / - 5.6 miles / 9.0 kilometers North 11.5 mph / 18.5 km/h - N/A Scattered Clouds
10:00 AM 73.4 °F / 23.0 °C 66.2 °F / 19.0 °C 78% - / - 5.6 miles / 9.0 kilometers North 11.5 mph / 18.5 km/h - N/A Scattered Clouds
12:00 PM 77.0 °F / 25.0 °C 68.0 °F / 20.0 °C 74% 30.12 in / 1020 hPa 7.0 miles / 10.0 kilometers NNW 9.2 mph / 14.8 km/h - N/A Scattered Clouds
2:00 PM 75.2 °F / 24.0 °C 68.0 °F / 20.0 °C 78% 30.06 in / 1018 hPa 5.6 miles / 9.0 kilometers NNW 6.9 mph / 11.1 km/h - N/A Scattered Clouds
4:00 PM 75.2 °F / 24.0 °C 66.2 °F / 19.0 °C 73% 30.04 in / 1017 hPa 7.0 miles / 10.0 kilometers SE 5.8 mph / 9.3 km/h - N/A Mostly Cloudy
6:00 PM 73.4 °F / 23.0 °C 66.2 °F / 19.0 °C 78% 30.04 in / 1017 hPa - East 10.4 mph / 16.7 km/h - N/A Overcast
8:00 PM 69.8 °F / 21.0 °C 66.2 °F / 19.0 °C 88% 30.06 in / 1018 hPa 7.0 miles / 10.0 kilometers East 5.8 mph / 9.3 km/h - N/A Mostly Cloudy
10:00 PM 69.8 °F / 21.0 °C 64.4 °F / 18.0 °C 83% 30.06 in / 1018 hPa 7.0 miles / 10.0 kilometers North 5.8 mph / 9.3 km/h - N/A Overcast
11:00 PM 68.0 °F / 20.0 °C 66.2 °F / 19.0 °C 94% 30.09 in / 1019 hPa 7.0 miles / 10.0 kilometers North 5.8 mph / 9.3 km/h - N/A Overcast
Astronomy
[Extended View] [Normal View]
July 30, 2005 Sun Rise Sun Set
Actual Time 6:53 AM EAT 7:00 PM EAT
Civil Twilight 6:31 AM EAT 7:21 PM EAT
Nautical Twilight 6:05 AM EAT 7:47 PM EAT
Astronomical Twilight 5:40 AM EAT 8:12 PM EAT
Moon (7/30) 2:01 AM EAT (7/30) 2:25 PM EAT
Length of Day: 12h 07m
Length Of Visible Light: 12h 51m
Moon Phase: Waning Crescent, 28% of moon illuminated
Star Chart
7 / 30 8 / 5 8 / 13 8 / 19 8 / 26
New First Quarter Full Last Quarter
- Definitions of Astronomy Terms -
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 Re: حالة الطقس في عنتبي ذلك اليوم المشؤم (Re: Ibrahim Adlan)
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2:00 PM 75.2 °F / 24.0 °C 68.0 °F / 20.0 °C 78% 30.06 in / 1018 hPa 5.6 miles / 9.0 kilometers NNW 6.9 mph / 11.1 km/h - N/A Scattered Clouds
عند قيام الطائرة
مدي الرؤيا تسعة كيلوميتر
الضغط الجوي 1018(يحدد ارتفاع الطائرة قياسا بمستوي سطح البحر)
السقف الجوي يوضح وجود سحب متفرقة
سرعة الرياح حوالي عشرة عقد
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Re: حالة الطقس في عنتبي ذلك اليوم المشؤم (Re: Ibrahim Adlan)
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الأجهزة الملاحية الموجودة علي طائرة الرئاسة اليوغندية
THE OMEGA NAIVIGATIONAL SYSTEM
جهاز ملاحة جوية الكتروني يتم تغذيته بمعلومات نقطتي القيام و الوصول قبل قيام الطائرة يعمل بمساعدة نظام الGPS
THE ADF
OR THE AUTOMATIC DIRECTION FINDER
عبارة عن بوصلة ذات تذبذب عالي يلتقط الاشارات من محطة ارضية )محطة مطار لدوار الكيني) في حالة الطائرة المنكوبة وهو يبعد حوالي 45 كيلو من معسكر NEW SITE
ACAS - Aircraft Collision Avoidance System: Early relative of the now operational TCAS (Traffic Alert and Collision Avoidance
System) which warns pilots of potential conflicts with other aircraft
جهاز تحذير حالة اقتراب الطائرة من اي جسم في خط الطيران المتبع
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Re: حالة الطقس في عنتبي ذلك اليوم المشؤم (Re: Ibrahim Adlan)
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SIGMET - Significant Meteorological Advisory: Broadcast to pilots advising them of, for example, thunderstorms or heavy turbulence
هذه النشرة الجوية الخاصة بالطيران يتم بثها عند توقع حدوث زوابع رعدية او اي ظاهرة طقسية من شأنها التأثير علي سلامة الطائرة
(بحثت عن وجود هذه النشرة في ملفات مطاري عنتيبي و لودوار فلم اعثر علي ما يدل علي بثهما)
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Re: حالة الطقس في عنتبي ذلك اليوم المشؤم (Re: Ibrahim Adlan)
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يتم الطيران في حالات الطيران المنخفض8500 feet or below
اما عن طريق الـطيران المرئ VFR حيث يعتمد الطيار علي مدي الرؤيا وتتبع خط اساسه العلامات الأرضية مثل المدن و الجبال و الانهار و تتبعها حتي الوصول
او الإعتماد الكلي علي اجهزة الملاحة
يمكن معرفةكيف تم طيران الطائرة المنكوبة من تسجيلات برج المراقبة او ال FILED FLIGHT PLAN
او من الصندوق الاسود ان وجد
DFDR - Digital Flight Data Recorder: Records hundreds of performance parameters while an aircraft is in flight, too often used to determine what went wrong. Records 1/2 hour of data on a digital "loop" format.
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Re: حالة الطقس في عنتبي ذلك اليوم المشؤم (Re: Ibrahim Adlan)
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Lodwar, Kenya Page
World:Kenya:Rift Valley ProvinceLatitude 3.1167 Longitude 35.6000 Altitude (feet) 1568
Lat (DMS) 3° 7' 0N Long (DMS) 35° 36' 0E Altitude (meters) 477
Time zone (est) UTC+3
Approximate population for 7 km radius from this point: 942
نيو سايت يبعد حوالي 45 كيلو عن مطار لودوار و يعتبر مطار مناوب في حالة تعذر الهبوط في نيوسايت هيليبورت
Nearby Cities and Towns
West North East South
Kakuma (56.8 nm)
Lorugumu (25.2 nm) Lokwakangole (30.8 nm) Angorangora (31.4 nm)
Loichangamatak (29.2 nm)
Muriling (44.7 nm)
Nearby airports:Code IATA Name City Distance Bearing Airlines
HKLO LODWAR 0 nm E 58
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Re: حالة الطقس في عنتبي ذلك اليوم المشؤم (Re: Ibrahim Adlan)
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Mi-17 [Mi-8MT] HIP H
The MI-17 is a multirole helicopter used to resupply CLF guerrillas or insert PSOC detachments. It can also be very heavily armed with an extensive array or rockets, misslies and guns. It is often used to air assault infantry forces to attack the point of penetration, reinforce units in contact or disrupt counterattacks. Additional missions include; attack, direct air support, electronic warfare, airborne early warning, medevac, search and rescue, and minelaying.
The Mi-17 helicopter, developed at the Mil Design Bureau from the Mi-8 helicopter, is in serial manufactured at the Kazan Helicopter Production Association. The designation Mi-17 is for export; the Russian armed forces called it Mi-8MT. The Mi-17 can be recognized because it has the tail rotor at the starboard side, instead of the port side. The Mi-17 added a number of improvements to its predecessor, including a vibration damper to increase comfort for crew members and passengers. The helicopter features a high thrust-to-weight ratio pair of TVZ-117MT or TVZ-117VM shaft-turbine engines with a takeoff power of 1,900 hp. The Mi-17 is capable of single-engine flight in the event of loss of power by one engine (depending on aircraft mission weight) because of an engine load sharing system. If one engine fails, the other engine’s output is automatically increased to allow continued flight.
The Mi-17 is capable of carrying cargoes in the cabin (including long cargo) with half-open or removed doors, external loads, or passengers (24 people). The Mi-17 can carry up to 30 troops and up to 20 wounded; it can also be used for in-flight unloading of special cargoes. The transport version of the MI-17 helicopter is intended to carry cargoes (loads) in the cargo compartment, including long-size cargo with partially- opened or removed cargo doors, external loads, or executives (up to 24 persons). Interior seats are removable for cargo carrying. The rear clamshell doors open, an internal winch facilitates loading of heavy freight. Floor has tiedown rings throughout. The aircraft carries a rescue hoist capable to 150 kg.
External stores are mounted on weapons racks on each side of the fuselage. The Mi-17 has six external hardpoints. The Mi-17 is provided with missiles, bombs, small arms and cannons. It carries four missile launchers of the B8V20 type, with missiles launched with the aid of an on-board PUS-31-71 electrical fire control system. The BDZ-57KRVM bomb carrier is used for the attachment of bombs up to 500kg. Not all vailable munitions are employed at one time, mission dictates weapon configuration. The helicopter carries four UPK-23-250 gun containers with GSh-23L 23mm guns and pivoted mounts (eight units). The forward and aft hemispheres are protected by PKT machine-guns with independent power supply and remote control circuits.
The helicopter may be provided with longrange communication equipment and a radar, and it can carry equipment with phased-array antennas for suppression of enemy electronic attack and air defence facilities, such as airborne radars, air defence (artillery) weapons control radars, surveillance and target detection radars and missile radar homing #########. The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode.
VARIANTS
Mi-17: A mid-life upgrade of the widely proliferated Mi-8 HIP H medium assault/ transport helicopter. Initially, only the export version was known as the Mi-17. The only visible differences between this variant and the older Mi-8s is that the tail rotor is on the portside rather than the starboard side, and crew armor plating.
Mi-17P: A descendent of the HIP K airborne jamming platform characterized by large rectangular antennas along the aft fuselage. The Mi-17P (Mi-8MTPB `Hip-K derivative') is provided with long-range communication equipment and a radar, and it can carry equipment with phased-array antennas for suppression of enemy electronic attack and air defence facilities, such as airborne radars, air defence (artillery) weapons control radars, surveillance and target detection radars and missile radar homing #########. The ECM equipment can work both in the reconnaissance and ECM modes or in the reconnaissance mode.
Mi-171/-17M/-17V: Also known as Mi-8MTV, and a descendent of the HIP H. The engines are upgraded to 2x 2,070-shp Klimov TV3-117VMAs to allow greater rates of climb and hover ceilings, yet performance characteristics remain virtually unchanged from the baseline Mi-17.
Specifications
Country of Origin Russia
Builder Mil
Date of Introduction 1981 (as Mi-17)
Role
Similar Aircraft
Length Length (rotors turning): 25.4 meters
Length (fuselage): 18.4 meters
Height 5.7 meters
Width 2.5 meters
Main Rotor Diameter 21.3 meters
Tail Rotor Diameter 3.9 meters
Cargo Compartment Dimensions Floor Length: 5.3 meters
Width: 2.3 meters
Height: 1.8 meters
Weight Maximum Gross: 13,000 kg
Normal Takeoff: 11,100 kg
Empty: 7,100-7,370 kg (variant dependant)
Blades Main rotor: 5
Tail rotor: 3
Engine 2x 1,950-shp Isotov TV3-117MT turboshaft
Fuel Internal: 445 liters
Internal Aux Tank: 915 liters ea.
External Fuel Tank:
Port Tank: 745 liters
Starboard Tank: 680 liters
Maximum speed 250 km/h
Cruising speed 240 km/h
Range Normal Load: 495 km
With Aux Fuel: 1,065 km
Ceiling Service: 5,000-5,700 meters (variant dependant)
Hover (out of ground effect): 1,760 meters
Hover (in ground effect): 1,900-3,980 meters (variant dependant)
Vertical Climb Rate 9 m/s
Armament 2x 7.62-mm or 1x 12.7-mm MG
4-6 - AT-2C or AT-3 ATGMs
4-6 - 57-mm rocket pods (16 each)
2 - 80-mm rocket pods (20 each)
4 - 250-kg bombs
2 - 500-kg bombs
1 - 12.7-mm MG pod
2 - Twin 23-mm gun pods
1,830 - Additional fuel tanks (liters)
Most Probable Armament: fitted with 2x 7.62-mm machineguns or possibly 2x 23-mm GSh-23 gun packs in cabin, 57-mm rockets, and AT3/SAGGER ATGMs.
Loaded combat troops can fire personal weapons through cabin windows from inside cabin.
Standard Payload Internal load: 4,000 kg
External on sling only: 3,000 kg
Transports 24 troops and cargo, or
armaments on 6x external hardpoints.
Survivability/Countermeasures Main and tail rotor blades electrically deiced. Infrared jammer, chaff and flares.
AVIONICS The Mi-17 is equipped with instruments, avionics, Doppler radar, and a fully functioning autopilot for operation in day, night, and instrument meteorological conditions.
Crew 3 (2x pilots, 1x flight engineer)
Cost
User Countries At least 22 countries
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Re: حالة الطقس في عنتبي ذلك اليوم المشؤم (Re: Ibrahim Adlan)
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Reports reaching The New Times Investigative Desk indicate that the Russian built Mi-17 Ugandan Presidential chopper, in which the Sudanese first Vice President Lt. Gen. Dr John Garang met his death, was involved in six 'crash incidents' eight months earlier and was not airworthy.
Garang was returning to his base in New Site, southern Sudan, after holding talks with Ugandan President Yoweri Museveni.
According to a source close to Uganda's Presidential Guard Brigade who spoke to this reporter on condition of anonymity, the latest crash was in a potato garden in Wakiso district and involved the Ugandan President, Yoweri Museveni.
Yesterday The Monitor also reported that the parliamentary committee on Presidential and Foreign Affairs had recommended the purchase of a new chopper instead of overhauling the one that took Garang's life. The Paper quoted an MP and member of the Presidential and Foreign Affairs' committee, Mr. Aggrey Awori, saying "This helicopter had structural problems. It was unfit to fly at night. I told the State House Comptroller [Richard Muhinda] that we should buy a new helicopter at $5 million but he insisted that they could repair it for $2.5 million", adding, "I told him [Muhinda] that they were taking a chance with the President's life. I even argued with the Presidential Guard Brigade [PGB] recently over the same issue."
However, in a telephone interview Ugandan Defense and Army Spokesman, Lt. Col. Shaban Bantariza said that the allegations of six crash incidences involving the fateful chopper were a hoax. "Dismiss the rumours. That is not true. Not true at all," Bantariza emphasised.
Bantariza further dismissed allegations that the chopper's flying hours had expired. "The helicopter had been overhauled about a month ago. Now it has a flight time of eight years," he said.
"I don't have the figures of the helicopters flight time before it was taken for re-servicing. But normally the pilots and other flight technical teams notify the Army Commander about the need for overhauling the helicopter and the latter endorses it. This is what happened to the helicopter in which Garang crashed," Bantariza added.
However, a source close to the Ugandan Ministry of Defense told this reporter that after its involvement in the six crash incidents, the chopper was put on hold for the last eight months until it was cleared to airlift Gen. Garang to New Site in the Sudan.
After the death of Dr. Garang the Ugandan president Mr. Yoweri Museveni issued a statement saying, "It has now been confirmed that our dear brother, Dr John Garang, 1st Vice President of the Sudan and President of Southern Sudan, with others, died in a helicopter crashâ-oeHe was aboard our Presidential helicopter M1-172 (VIP version) piloted by Colonel Nyakairu and Capt. Kiyimba. Major Kigundu was the flight Engineer. The helicopter was a recently overhauled executive helicopter that has served us well for the last 8 yearsâ-oeI have decided to create a panel of three (3) experts to look into this crash. The Minister of Transport will name the team. We have also approached a certain foreign government to rule out any form of sabotage or terrorism", the statement seen by The New Times reads in part.
Media reports indicate that the presidential chopper that killed the founder and leader of the twenty three-year SPLM/A rebel organization crashed in southern Sudan due to poor weather conditions. The Nation and The East African Standard had reported that after realizing that the weather was bad and the helicopter couldn't land, the pilots wanted to fly back to Entebbe but the chopper lacked sufficient fuel.
In the interview Bantariza also dispelled assertions that the chopper could have been brought down by the Lord's Resistance Army (LRA), a rebel outfit that has been fighting the government of President Yoweri Museveni for the last eighteen years.
"LRA rebels have no technology to shoot down the ultra-modern presidential chopper. The crash wasn't in their area of operation. The crash was in the far east of Imatong hills. Far away from the rebels," Bantariza said. During his meeting with President Museveni Gen. Garang gave an ultimatum to Joseph Kony's LRA to leave southern Sudan.
"Kony doesn't have the capacity to shoot the helicopter at night. He wasn't even in the area of the crash," said Bantariza.
Asked whether the helicopter was junk, Bantariza replied: "The helicopter had been functional and in better condition and had just been overhauled about a month ago." He added that president Museveni had been using the chopper while touring parts of northern Uganda, recently.
When contacted over the matter the Ugandan Presidential Guard Brigade (PGB) Spokesman Lt. Edison Kwesiga, told this reporter that the presidential chopper had never been involved in any crash incidents as alleged. "Not true. Not true. Learn from me the helicopter has never crashed," Kwesiga said.
The presidential chopper belonging to the Ugandan military crashed into the mountainous terrain of Imatong hills, killing all 14 people on board that included seven crew members and six companions.
According to the Uganda Defense Ministry Website, "Gen.Garang had been in Uganda for a two-day official visit. On Saturday he left President Yoweri Museveni's country home in Rwakitura, Mbarara where Museveni introduced him to envoys who included the US Ambassador Mr. Jimmy Kolker, Mr. Tore Gjos of Norway, Mrs. Yoke Brandt of the Netherlands and British High Commissioner, Mr. Francois Gordon.
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'Thereafter Garang left Rwakitura in the afternoon headed for Southern Sudan, where he expected to meet former commanders of Sudan Peoples' Liberation Army (SPLA),' read the report in part.
In the past, the Ugandan military has been accused of and implicated in the purchase of junk military equipment, including choppers.
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Re: حالة الطقس في عنتبي ذلك اليوم المشؤم (Re: Ibrahim Adlan)
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إبراهيم عدلان ، خريج المعهد القومي للطيران المدني وعمل ضابط برج وإقتراب في برج المراقبة بمطار الخرطوم ثم ضابط مراقبة جوية في بمركز المراقبة الجوية { FIC } في مطار الخرطوم / الطيران المدني ويعتبر من أميز المراقبين الجويين السودانيين خصة وهو قد تلقى تدريبه العملي على يد الرعيل الأول من المراقبين الجويين أمثال الراحل محمد الحسن عبدالخير وزامل فطاحلة في المجال مثل فيصل محمد أحمد ومحمد البهرة الطيب والتيجاني حسن أبوزيد ، وهو يكتب بمهنية عالية لتوضيح الأمر فيما يتعلق بظروف رحلة الطائرة المنكوبة
وياريت يا إبراهيم توضح لينا إمكانيات الطائرات العمودية { الهليوكوبتر } وقدرتها على تفادي المخاطر الجوية ومرونتها في الهبوط الإضطراري
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خدر
أبو ساندرا
saif massad ali
فيس بوك
تويتر
انستقرام
يوتيوب
بنتيريست