Grumman G-73 Mallard

Recent plane crashes

1960 USAF Serial Numbers
Those systems and components used for collating and computing data from unrelated systems and transmitting same automatically. You may use this page for your own, non-commercial reference purposes only. The Brazilian Air Force used Trackers. Lecture empreintes sous l'écran. Ford chose to land on a nearby golf course, clipping the top of a tree before landing. That portion of the system which is used to dump injection water and to purge the system. The aircraft in cruise at about 33, feet when it experienced a catastrophic in flight breakup.

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All four crew members and 35 people on the ground were killed were killed. The aircraft was on an unscheduled international flight from Sochi, Russia to Latakia, Syria. The aircraft, which was transporting members of the Alexandrov Ensemble, the official choir of the Russian Armed forces, crashed into the Black Sea shortly after takeoff.

Wreckage was found about one mile 1. All eight crew members and 84 passengers were killed. Just after takeoff, the aircraft crossed a road that was about meters beyond the end of the runway, apparently hitting at least one fence and dragging the rear part of the aircraft on the ground.

The aircraft became airborne, but did not gain a significant amount of altitude. The aircraft was videotaped making a descending right turn just before it crashed and caught fire. The crash site was about 10 miles 16 km from the airport.

Five of the six crew members were killed. While en route, the crew reported that there was an engine problem, and that the aircraft was descending. Shortly afterwards, the crew declared an emergency. The aircraft crashed into a hillside and caught fire. All five crew members and 42 passengers were killed.

Shortly before landing, the crew declared an emergency, reportedly due to an electrical problem, and the plane crashed into mountainous terrain near Medellín. Seven of the nine crew members and 64 of the 68 passengers were killed in the crash. Apparently, the owner of the airline, who was also a member of the flight crew, was killed in the crash. At some point during the landing, the left main landing gear collapsed, and the aircraft came to rest near the landing runway.

A fire broke out, seriously damaging the left side of the aircraft. The two crew members were not injured. During the takeoff, the right engine experienced an uncontained failure, and the flight crew aborted the takeoff. The aircraft caught fire in the area of the right engine, and the aircaft occupants evacuated the aircraft. There were eight minor injuries among the passengers and nine crew members. After landing, the crew was unable to come to a stop on the runway.

The aircraft was slowed by an arrestor bed of low-density concrete that was in place beyond the end of the runway. None of the 40 passengers or crew were injured. The crew was attempting to execute a go-around shortly after the main landing gear touched down on the runway, but the aircraft was unable to gain altitude. The crew apparently did not advance the thrust beyond idle until after the aircraft had lifted off the runway. The crew had also commanded the landing gear to retract before commanding an increase in engine thrust.

The aircraft settled down onto the runway at a rate of descent of feet per minute and skidded to a stop on the runway. The aircraft was seriously damaged, with the right engine separated from the wing. There was a subsequent fire and explosion that destroyed most of the fuselage. None of the 18 crew members or passengers were killed or seriously injured, though one responding firefighter was killed. The ballon crashed burned after striking power lines about eight miles The pilot and all 15 passengers were killed.

While the victims and the ballon's gondola an open basket were near the point where the ballon struck power lines, the envelope was located roughly three-quarters of a mile 1. These prior events involved at most six fatalities More on this event. The aircraft was on a scheduled international flight from Paris, France to Cairo, Egypt when radar contact was lost. The aircraft was cruising at 37, feet and over the eastern Mediterranean Sea north of the Egyptian coast and crashed into the sea.

There were no survivors among the 56 passengers and 10 crew members on board. Three of the crew members were reportedly security personnel. The aircraft aborted its first landing approach, and entered a holding pattern for roughly an hour before its second attempt. During the second landing attempt, the crew indicated that they planed to execute a go-around procedure, the aircraft then entered a steep descent, and then crashed on the edge of the runway. All seven crew members and 55 passengers were killed.

The aircraft was on a domestic scheduled flight from Pokhara to Jomsom Airport and crashed while en route to its destination. All three crew members and 20 passengers were killed. Tara Air is a subsidiary of Yeti Airlines. This airline is also banned from operating within the European Union. Tara Airlines had a previous fatal crash in December , killing all three crew members and 19 passengers.

The aircraft was on a scheduled international flight from Mogadishu, Somalia to Djibouti. Shortly after takeoff, when the aircraft was at about 11, feet, there was an explosion caused by a bomber that caused a fuselage rupture in the forward portion of the passenger cabin. There was also evidence of fire in the area of the fuselage damage. The crew was able to return to the departure airport at Mogadishu. The only person killed was the bomber, who was ejected out of the aircraft.

None of the other 73 passeners were killed, though two were injured. All seven crew members survived. The aircraft was on a scheduled domestic flight from Houston, TX to Nashville, TN After arrival, the aircraft slid off the taxiway, collapsing its nose landing gear and coming to rest in a ditch. None of the five crew members or passengers were killed. Several passengers sustained minor injuries. The executive jet was on a nonscheduled domestic passegner flight from Dayton, OH, to Akron, OH, and crashed about two miles 3.

Shortly before the crash, the jet was seen to be banking to the left before hitting power lines and crashing into a pair of residential structures. Both pilots and all seven passengers were killed. No one on the ground was injured. The aircraft was on a nonscheduled domestic cargo flight from Juba to Paloich, South Sudan, and crashed shortly after takeoff. While the aircraft was operating as a cargo flight and was not authorized to carry passengers, there were roughly a dozen passengers on board All six crew members all but two of the passengers were killed.

One of the survivors was a month-old girl, Nyalou Thong. The total number of passengers, and the number killed on the ground, is unclear, but there were a total of 37 reported fatalities. The aircraft was on a nonscheduled international flight from Sharm el Sheikh, Egypt to St.

Air traffic control lost contact with the flight about 23 minutes after departure, after the aircraft reached a cruising altitude of about 31, feet. The aircraft crashed in a remote area of the Sinai Peninsula shortly thereafter. All seven crew members and passengers were killed. This is the second fatal crash for this airline. In January , three passengers were killed after a Kolavia Tu caught fire shortly before takeoff. Metrojet operated as Kogalymavia or Kolavia until The aircraft was on a scheduled international flight from Fort Lauderdale, FL to Caracas, Venezuela when a fire broke out in the area of the left engine prior to takeoff.

There were over a dozen injuries among 90 passengers and 11 crew members. The first officer continued the flight and the aircraft diverted to Syracuse, NY. None of the other crew members or passengers were injured. ANA or other standard specification number and grade if applicable of fuel, oil, fluid, and other material used shall be given.

Specifications and grades should be shown grouped on one page to facilitate revisions. For fuel, give expansion volume, total fuel capacity, sump capacity, net fuel capacity as applicable for each tank. For oil, give allowance for expansion. Includes instructions such as those for periodic lubrication of components, radioactivity decontamination, aircraft external and internal cleaning, disinfection of aircraft, sanitation of drinking water, etc.

Shall not include lubrication procedures required for the accomplishment of maintenance practices. Includes instructions such as those for ice and snow removal from parked aircraft, etc.

Includes cabin supercharger, equipment cooling, heater, heater fuel system, expansion turbine, valves, scoops, ducts, etc. Includes items such as controls and indicating systems related to the compressors, wiring, etc.

Does not include the pressure control and indicating system for the cabin pressurization. Includes equipment rack cooling systems and items such as blowers, scoops, ducting, inlets, check valves, wiring, etc. Does not include valves which are part of pressurization and temperature control.

Includes items such as control valves, relief valves, indicators, switches, amplifiers, wiring, etc. Includes items such as heater panels and other units, fuel system and control, ignition, indicating systems related to heater operation, wiring, etc. Does not include temperature control and indicating systems.

Includes items such as the cooling unit, indicating systems related to the cooler operation, wiring, etc. Includes items such as control valves, thermal sensing devices, switches, indicators, amplifiers, wiring, etc. Includes those units and components which control direction, heading, attitude, altitude and speed. This includes power source devices, interlocking devices and amplifying, computing, integrating, controlling, actuating, indicating and warning devices such as computers, servos, control panels, indicators, warning lights, etc.

This includes sensing, computing, actuating, indicating, internal monitoring, and warning devices, etc. This includes engaging, sensing, computing, amplifying, controlling, actuating and warning devices such as amplifiers, computers, servos, limit switches, clutches, gear boxes, warning lights, etc.

This includes sensing, computing, indicating and warning devices, control panels, etc. This includes sensing, computing, actuating, indicating internal monitoring, warning devices, etc. Includes items such as amplifiers, speakers, handsets, reproducers, control panels, control -units, etc. Also includes items of audio, video, and film equipment. Includes items such as amplifier, handset, etc.

Does not include the interphone system within the flight compartment which is part of the integrating system. Includes items such as audio selector control panel, micro-phones, headphones, cockpit loudspeakers, etc.

Includes voice recorders, television, monitors, externally mounted camera, etc. Includes such items as integrated frequency selector panels, digital frequency control computers, integrated frequency display panels, etc.

Also includes common electrical items such as wiring, switches, connectors, etc. Includes items such as oil system, connecting devices, indicating and warning systems for the drive, etc.

Includes items such as receptacles, relays, switches, wiring, warning lights, etc. Includes items such as AC main and secondary busses, main system circuit breakers, power system devices, etc. Includes items such as DC main and secondary busses, main system circuit breakers, power system devices, etc. Includes emergency, buffet, and lavatory equipment. Does not include structures of equipment assigned specifically to other chapters.

Includes items such as flight crew seats, tables, pilot check lists and food containers, wardrobes, curtains, manuals, electronic equipment rack, spare bulbs, fuses, etc. Does not include cargo compartments. Includes lounges but not dressing rooms. Includes items such as seats, berths, overhead storage compartments, curtains, wall coverings, carpets, magazine racks, wardrobes, movable partitions, wall type thermometers, spare bulbs, fuses, etc.

Includes items such as removable and fixed cabinets, ovens, refrigerators, garbage containers, dish racks, coffee maker and dispensers, containers, electrical outlets, wiring, etc. Includes items such as mirrors, seats, cabinets, dispensing equipment, electrical outlets, wiring, etc.

Wash basins and water closets are included in Chapter Includes drive systems, rollers, latches, restraint nets, etc. Includes items such as evacuation equipment, life rafts, jackets, emergency locator transmitters, underwater locator devices, first aid kit, incubators, oxygen tents, medical stretchers, landing and signal flares, drag parachutes, evacuation signaling systems, etc.

Does not include fire extinguishers, oxygen equipment or masks. Includes flight compartments, passenger compartment, cargo and accessory compartment insulation, etc.

Also includes the functioning and maintenance aspects of the flaps, spoilers, and other control surfaces, but does not include the structure which is covered in the Structures Chapters. Does not include rotorcraft rotor controls which are covered in the Rotor Chapter Includes items such as the control wheels, cables, boosters, linkages, control surfaces, indicators, etc.

Includes items such as the rudder pedals, tab control wheel, cables, boosters, linkages, control surfaces, position indicators, etc. Includes items such as the control column, stickshaker units, automatic stall recovery devices, tab control wheels, cables, boosters, linkages, control surfaces, position indicators, stall warning systems, etc. Includes items such as control handle, cables, jackscrews, motors, warning systems, linkages, control surfaces, position indicators, etc.

Includes items such as control handles, cables, actuators, warning systems, linkages, control surfaces, position indicators, etc. Includes items such as control handles, cables, warning systems, linkages, spoilers, drag devices, position indicators, etc. Does not include locking the control by means of flight control boost system. Includes items such as control handles, cables, actuators, linkages, warning systems, control surfaces, position indicators, etc.

Does not include trailing edge flaps. Includes engine driven fuel pumps for reciprocating engines, includes tanks bladder , valves, boost pumps, etc. Includes integral and tip fuel tank leak detection and sealing.

Includes tank sealing, bladder type cells, ventilating system, cell and tank inter -connectors, over wing filler necks and caps, etc. Also includes reservoir feed pumping systems and reservoirs within the tanks which are not part of the distribution system.

Includes items such as plumbing, pumps, valves, controls, etc. Includes items such as plumbing, valves, controls, chutes, etc. Includes pressure warning systems for pumping systems within the tank, etc. Does not include engine fuel flow or pressure. Includes items such as tanks, accumulators, valves, pumps, levers, switches, cables, plumbing, wiring, external connectors, etc. Does not include the supply valves to the using systems. Includes items such as tanks and accumulators which are separate from the main system, hand pumps, auxiliary pumps, valves, plumbing, wiring, etc.

Includes items such as transmitters, indicators, wiring, warning systems, etc. Does not include the basic windshield panel. For turbine type power plants using air as the anti-icing medium, engine anti-icing is contained under Air System. Includes wings, airfoil sections of the empennage, and pylons. Includes power plant cowling anti-icing. Includes all components up to but not including rotating assembly. Procedural coverage of those systems which give visual or aural warning of conditions in unrelated systems.

Units which record, store or compute data from unrelated systems. Also includes general coverage of instrument panel vibrators and other panel accessories.

Includes items such as inclinometers, clocks, etc. Includes items such as flight recorders, performance or maintenance recorders, VG recorders, etc. Includes items such as master warning or flight warning systems, central instrument warning, or caution and warning systems, tone generators, annunciators, etc. Includes tail skid assembly, brakes, wheels, floats, skids, skis, doors, shock struts, tires, linkages, position indicating and warning systems.

Also includes the functioning and maintenance aspects of the landing gear doors but does not include the structure which is covered in Chapter 52 DOORS. Includes items such as shock struts, bogie axles, drag struts, linkages, attach bolts, etc. Includes items such as shock struts, drag struts, linkages, attach bolts, etc. Includes items such as actuating mechanisms, bogie trim, bungees, up and down latches, operating controls, valves and motors, cables, wiring, plumbing, etc.

Includes items such as bearings, tires, valves, de -boosters, swivel glands, anti-skid devices, pressure indicators, plumbing, etc. Includes items such as actuating cylinders, controls, bogie swivel unlock, etc. Includes items such as switches, relays, lights, indicators, horns, wiring, etc. Includes items such as shock strut, skid block, wheels, etc. Includes light fixtures, switches and wiring.

Does not include warning lights for individual systems or self -illuminating signs see Chapter Does not include cargo compartment. Includes direct and indirect illumination of work areas, panels, and instruments. Includes master warning light and warning light dimming systems, where not integrated with a central audio or visual system under Includes items such as direct and indirect illumination, passenger call system, lighted signs, etc.

Includes lights such as landing, navigation, position indicating, wing illumination, rotating, courtesy, taxi, etc. Includes items such as inertia flashlights, lanterns, etc. This includes sensing, computing, indicating and warning devices such as magnetic compasses, vertical and directional references, magnetic heading systems, attitude director systems, symbol generators, turn and bank, rate of turn, amplifiers, indicators, etc.

Includes Flight Director when it is not integral with the auto pilot computation. Includes items such as localizer, glide slope, ILS, markers, paravisual director ground guidance systems, etc. Includes items such as inertial guidance systems, weather radar, Doppler, proximity warning, collision avoidance, star tracker, etc. Includes items such as course computers, flight management computers, performance data computers, and associated control display units, warning annunciators, etc.

Includes items such as ducts, valves, actuators, heat exchangers, controls, etc. Includes temperature and pressure warning systems. Includes pressure warning system.

Includes wash basins, toilet assemblies, tanks, valves, etc. Includes wash water system if the potable water is also used for washing. Includes items such as wash basins, water closets, flushing systems, etc. Does not include units or components covered in Chapter Includes removable tanks bladder cells , interconnecting balance pipes, filler valves, etc.

Includes computers, storage devices, control and display devices. For example, 45 XX would identify all air conditioning monitoring and testing provided by the Central Maintenance System, and would provide directions for using the Central Maintenance System to execute those maintenance functions.

Detailed testing not capable of coverage in Chapter 45 would be appropriately cross referenced and would be provided in Chapter Similarly, 45 XX would identify landing gear monitoring and testing provided by the Central Maintenance System.

Includes units that are dedicated to the information storage and retrieval function such as the Electronic Library mass storage and controller. Does not include units or components installed for other uses and shared with other systems, such as flight deck printer or general use display. Includes power and drive section, fuel, ignition and control systems; also wiring, indicators, plumbing, valves, and ducts up to the power unit.

Does not include generators, alternators, hydraulic pumps, etc. Primary and secondary structure diagram. Principal area and dimensional data. Access door and panel identification. Cleanup of dents, cracks, scratches, corrosion, etc. Aerodynamic smoothness requirements for the airplane, and permissible contour variations, gaps, and mismatch data. Will not include general engineering practices unless specific deviations are required. Unique processes such as welding specifications, etc.

Where possible, permissible substitutes and sources of supply will be given. Procedures for fastener installation and removal including hole preparation. Fastener strength values and substitution data. Includes locations for supports and contour dimensions for required ground equipment. Where applicable, individual repairs will contain their own balancing instructions.

Includes passenger and crew doors, cargo doors, emergency exits, etc. Electrical and hydraulic systems associated with door control are included as appropriate. Does not include doors installed in movable partitions which are covered in Chapter Stairs whose primary structure is a door shall be covered under the appropriate topic.

Includes items such as switches, lights, bells, horns, etc. Does not include landing gear door warning which is covered in Chapter The section locations shall be defined by manufacturing joints or other suitable demarcations in sequence from front to rear. Does not include movable partitions covered in Chapter 25 nor the functional and maintenance aspects of variable aerodynamic fairings covered in Chapter Also includes the structure of power plant cowling inclusive of the structural portion of the inlet whether or not integral with the aircraft.

Structural portions of the exhaust system are excluded where they are not integral with the airframe. The section locations shall be defined by manufacturing joints or other suitable demarcations in a logical sequence.

Includes items such as the transparent material and its frame of sliding and fixed windows and windshields, handles, latching mechanisms, etc. Includes items such as transparent material, its frame, frost shield, etc.

Includes items such as transparent material, its frame, etc. Does not include emergency exit windows. Includes spars, skin, ribs, stringers, clamshells, scuppers, etc. Includes propeller spinner synchronizers. Also includes propulsor duct assemblies, including aerodynamic fairing of mechanical components, stators, vectoring systems, etc. Includes items such as blades, dome, hub, spinner, slip ring, deicer boot, distributor valve, etc.

Includes items such as governor synchronizers, switches, wiring, cables, levers, etc. Does not include any parts which rotate with the propeller assembly. Also includes all those units and components provided for the propulsor vector drive system. Includes flight deck control, drive motors, gearboxes, drive shafts, synchronizing shafts, etc. Includes brake mechanisms, levers, pulleys, cables, switches, wiring, plumbing, etc.

Includes items such as light, switches, wiring etc. Does not include the rotor anti-icing system which is dealt with in chapter 30 "Ice and Rain Protection". Includes sleeves, spindles, dampers, rotor head fairing s as well as rotor shaft s and swashplate s if the rotor head and shaft constitute a non-dissociable assembly. Includes items such as lights, gauges, switches, wiring, etc.

Includes the mechanical power take -off s and accessory drives but does not include the accessories themselves alternators, hydraulic pumps, etc. Includes the rotor blades and rotor head. Does not include the rotor anti-icing system which is dealt with in chapter For an integral unit, only one section will be used. Includes the control units, caption lights, indicators, wiring, etc. Includes items such as control linkage and control cables for collective pitch, cyclic pitch, directional control, servo-controls and corresponding system.

The trim system and the indicating and monitoring system. Includes items such as collective pitch lever, cyclic pitch stick and corresponding linkage and cable controls, coupling, and mixing units, and artificial feel unit system.

Also includes the control position indicating system. Includes items such as tail rotor control pedals, relevant linkage and cable controls, bellcranks constituting the yaw control channel and the control position indicating system.

In the maintenance manual this section shall cover subjects such as engine changes, run-up, externally mounted spare power plants, etc. In the overhaul manual, this section shall cover subjects such as power plant build-up, teardown, etc. Includes the functioning and maintenance aspects of items such as accessory section cowls, cowl flaps, cowling supports, and attach and locking mechanisms, etc.

Does not include the structure integral with the airframe which shall be covered in the applicable Structures chapter. Includes items such as engine mounts, vibration dampeners, support links, mounting bolts, etc. Does not include those fire-walls which are included in Chapter Does not include the wiring which is specifically covered under another system.

Includes items such as nose ring cowls, scoops, compressor fan cowls, buried engine ducts, vortex generators, actuators, control handles, cables, wiring, plumbing, linkages, doors, warning systems, position indicators, etc. Does not include integral structure with the airframe, which shall be included in the applicable Structures chapter. Includes drainlines, manifolds, tanks, flame arrestors, vents, and their supporting brackets, etc.

Also includes components that are an integral part of, or fitted to the power plant cowling. Includes, for the turbine engine, air inlet, compessor, diffuser, combustion chambers, turbine and exhaust; and for the reciprocating engine, blower and clutch, clutch control valve, cylinder, cylinder baffles, intake pipes, crankshaft assembly, etc.

Used to transmit power to the propeller shaft, if any, and accessory drives. Includes reduction gearing, gear trains, extension shaft and torque meter. Within the profile of the basic engine, used to supplement the functioning of other defined systems external to the engine.

Includes items such as accessory drive, mechanical portion of the spark advance mechanism, oil transfer tubes from the propeller governor pad to the propeller shaft, BMEP section, etc. Used to control and direct the flow of lubrication through the engine from the inlet fitting to the outlet fitting.

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