Jet Commander Aircraft - The IAI Westwind is a commercial aircraft originally manufactured by Aero Commander as the 1121 Jet Commander. Powered by twin GE CJ610 turbojets, it first flew on January 27, 1963, and received its certification on November 4, 1964, before its first delivery. This program was purchased by Israel Aircraft Industries (IAI) in 1968, which was slightly expanded into the 1123 Westwind, and retrofitted with Garrett TFE731 turbofans into the 1124 Westwind. The 16,800–23,500 lb (7.6–10.7 t) MTOW aircraft could carry up to 8 or 10 passengers, and 442 were produced until 1987.
The first 1121 Jet Commanders were powered by separate CJ610 turbojets, and they had five starboards and three or four ports.
Jet Commander Aircraft
After 1123 Westwinds were stretched by 22 in (56 cm), they have heads, with six stars and five windows.
Jet Commander Aircraft Sunscreens
The 1124 Westwind is powered by two large Garrett TFE731 turbofans, maritime patrol aircraft Sea Scan from the Israeli Air Force has a nose radome and additional aerials.
The Westwind was first built in the United States by Aero Commander as a derivative of its twin-wing aircraft, first flown on January 27, 1963, as the Aero Commander 1121 Jet Commander.
After successful trials, the aircraft was produced and deliveries to customers began in 1965.
After initial testing of the model, it was changed to a design with an additional 2.5 ft to the lgth of the fuselage and increased payload and maximum weight. The second prototype first flew on April 14, 1964, which was followed by the first production aircraft in November 1964. Type approval was awarded by the FAA in November, it could deliver the first customer on January 11, 1965.
History Space: Mystery Of The Missing Jet
Shortly thereafter, Aero Commander was acquired by North American Rockwell. Aircraft Leader created a problem, because Rockwell already had a pilot plane of its own design, the Sabreliner, and could not keep both in production due to antitrust laws. . Therefore, the company decided to sell out the rights of Jet Commander, which was bought by IAI in 1968.
Jet Commander production consisted of 150 aircraft in the United States and Israel before IAI made several modifications to create the 1123 Westwind. This included lengthening the fuselage and increasing maximum takeoff, maximum landing, and maximum zero fuel weight, with the wings modified to incorporate double-slotted flaps and drooped edges and tip tanks. The trimmable horizontal stabilizer has also been modified for increased lift and more travel.
Shortly after the aircraft went into production, the original Geral Electric CJ610 turbojet engines were replaced with more fuel-efficient Garrett TFE731 turbofans.
Some airframe modifications were also made, such as the edges of the wings, the dorsal fin, modified gine pylons and nacelles, and increased maximum climb, maximum landing height, and maximum height of heavy fuel. Along with improvements to many onboard systems including, well, these changes have been made to the 1124 Westwind.
Aero Commander 1121b Jet Commander
In 1976, after the terrorist takeover of the Savoy Hotel in Tel Aviv, the Israeli Air Force decided to use Westwind as a base for maritime patrol aircraft, which became known as the IAI Sea Scan. It was originally designed to meet the requirements of the United States Coast Guard to replace the Grumman HU-16 Albatross, but they chose the Dassault Ukay instead.
In 1980, deliveries of the Model 1124A began; Modifications include new wing sections and added winglets to the tips. The improved aircraft was named Westwind II, replacing the original model in production. IAI built its last Westwind in 1987, after a total of 442 Jet Commanders and Westwinds had been built, replacing production for the Astra.
Commander / Westwind aircraft is a general convtional business aircraft design, with two gins installed in the nacelles carried on the rear fuselage, but the wings are installed half of the fuselage instead of one less - the arrangement of the wings of the aircraft in this class.
At FL310 and Mach 0.74 (436 kn; 808 km/h), the 1124 burned 1,600 lb (730 kg) per hour, and 1,200 lb (540 kg) at Mach 0.7 (413 kn; 764 km/h).
Israeli Jet Aircraft Administrative Aero Commander / Jet Command Editorial Photography
1124N Sea Scan is a sea surveillance aircraft, and 1124 was rammed Westwind I after the introduction of 1124A Westwind II.
1121C is the unofficial designation for the 1121 aircraft which was converted to a Supplemental Certificate with full weight available from 1971.
[1] Under license from Fouga. [2] Joint venture with RUAG. [3] Alliance with Rafael. [4] Joint venture with DRDO. [5] Merged with Boeing. While flying at an altitude of 37,000 feet on a flight from El Paso to Toluca, it was cleared to climb to 41,000 feet to avoid a storm. Shortly after, the plane entered the uncontrolled area and crashed near the village of Las Carboneras. The plane was completely destroyed and all four occupants were killed.
Uncontrollable during the cruise after the plane encountered severe turbulence while flying in the area of thunderstorms and cumulonimbus and severe turbulences.
Twin Commander Aircraft
On December 14, 1995, at about 0014 local time N503U, Aero Commander 1121, operated by American Air Network crashed about 10 miles north of Guatemala City, Guatemala, while in 14 CFR Part 135 in-will, worldwide, cargo. Weather instruments were defeated at that time and an IFR flight plan was filed. The plane was destroyed and the pilot and co-pilot were seriously injured. The flight started from Miami, Florida about 2200 days ago. The crew had completed three tests to the Guatemala City airport, and announced to mission management that they had no fuel and could not go to their airport.
After the plane took off from Córdoba-Pajas Blancas Airport on runway 36, the crew started turning around and the plane took off. It collided with trees past the end of the runway, stopped and hit a forest area 2 km from the end of the runway, burst into flames. One pilot was seriously injured while eight others were killed.
It was determined that the crew failed to plan the flight according to published procedures and failed to comply with the pre-departure checklist. After the wrong installation, the body began to rotate too late, retracted the flaps too quickly after rotation, causing the plane to crash and stall. The distance separating the plane from the ground is not enough for the crew to expect to return. At the time of the accident, the total weight of the aircraft was higher than MTOW, which is considered critical.
The plane was completing a charter flight from Kingston, Jamaica, to Houston, Texas, with an intermediate stop in Cozumel, Quintana Roo, carrying six passengers and a crew of six. The route to Cozumel Airport began at night and was in VFR mode when, at the short end, the aircraft crashed near a light and fell 503 meters short of the runway 29 starting point. One pilot was killed while the second was seriously injured. All six passengers escaped with minor injuries.
Iai Eleven 23 Westwind
Ground disturbances during sunset (afternoon) and wrong altimeter settings in the second officer's equipment, when the operation was completed in VFR mode.
The aircraft entered an area where moderate icing was predicted. The ice detection system works continuously. The plane got stuck in the ice while checking the flight inspection equipment. The evidence shows that the workers recorded the ice to make ice, opened the ice hole, the ice broke and entered the machine. Both engines are on. In an emergency, the crew starts again, but no engine can sustain the power. The crew asked for a vector to a more distant airport. Both pilots were seen drinking last night. The copilot recently lost his driver's license for dui. The captain decided to retire that day. Copilots work on flight ops 3 days in 8 weeks and have limited training in flight reviews. Both pilots have personal issues that may affect performance. The captain's thoracic duct blood showed 0.057% alcohol. Putrefaction will be accentuated in the alcohol section. The copilot only had alcohol in his urine. Both machines see the same fod compressor and ice. No other aircraft systems or engine malfunctions were observed.
The failure of the pilot on command to detect the speed of ice on the aircraft because his attention was diverted.
The pilot, following an ILS approach, saw the first drop in hydraulic pressure and announced that the target would land without using flaps, speed brakes, reverse or nose wheel. The plane ran off the end of the runway during landing, traveled about 1,300 feet and came to rest on a golf course after hitting two cars and a chain link fence. After the accident investigation found 0.8 quarts of hydraulic fluid (skydrol) in the reservoir. The reservoir capacity is 1.28 U.S. gallon The pilot said he pulled the brakes on the approach to generate power in an emergency. The pilot reported that he did not brake after touchdown. The 1121 Commander's Aircraft operator's manual cautions against this practice. The functional inspection of the thrust reverser by the inspector at work has completed two work cycles. Two people in the ground vehicle were injured during the overrun landing.
Aero Commander U 4b > National Museum Of The United States Air Force™ > Display
On the final approach to Loba-Hart Memorial Airport, the crew is
Military aircraft jobs, military aircraft, military aircraft museum, military aircraft cargo, modern japanese military aircraft, military aircraft tug, japanese military aircraft ww2, military aircraft companies, japanese aircraft, military aircraft maintenance, military aircraft hangar, military aircraft toys
0 Comments