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weight and performance calculations for the Ilyushin Il-62M
***** PRELIMINARY FILE ****
Ilyushin Il-62M CCCP-86509 c/n 2036829 at Schiphol airport
Ilyushin Il-62M
role : long-range jet airliner
importance : ****
first flight : 1971 operational : March 1974 (Aeroflot)
country : Russia
NATO reporting name : CLASSIC
design :
production : 193 aircraft
general information :
IL-62 version equipped with the more powerful Soloviev D-30KU turbofan, which allowed a higher MTOW. With an additional fuel tank in the tail, fuel capacity was increased with 5000 litre. This gave it an intercontinental range and allowed it to fly from Moscow to Havana no-stop. Probably because of the longer range, the number of passengers was reduced, so that they had more legroom. It was first publicly showed at the 1971 Paris air show.
CCCP-86673, the first IL-62M was on display at the Paris Air Show at Le Bourget in 1971 and in 1973.
Its dimensions are the same as those of the Il-62.
The Il-86MK is a high density version that can accommodate 198 passengers, first flight 1978. About 10 of this type were built.
Ilyushin Il-62MK RA-86468 c/n 4749857 Rossiya Airlines at night on the ramp
The Il-62 is the largest airliner with manual flight controls, using steel cables and rods, pulleys, aerodynamic and weight balances, and trim tabs. Another key Il-62 trademark is the "saw tooth" ("dog-tooth") on the wing leading edge. This prominent feature acts as an aerodynamic fence vortex generator (without which the wings would be almost vortex-free), and fixed leading edge droop/slat/flap. It ensures vice-free behaviour at high angles of attack and assists efficient long-range cruise.
The engines have clamshell thrust reversers.
It has an containerized baggage container system; 14 containers empty weight 45 kg, each with capacity of 1.6m3 / 600 kg luggage. Total available freight volume : 48m3
The Il-62M stayed in service for long time, in 2016 the average age of the aircraft still in service was more then 32 years !
primary users : Aeroflot, CSA, Cubana, Interflug, Air Koryo (former CAAK), LOT,
Luftwaffe
Accommodation:
flight crew : 5 cabin crew : 6
flight crew consist of captain, first officer, flight engineer and optionally a navigator and a radio officer
passengers : seating for 168 in all- coach class seats ( 34 -in pitch)
high density seating for 186 passengers
engine : 4 Soloviev D-30KU turbofan engines of 112.8 [KN] (25358.0 [lbf])
dimensions :
wingspan : 43.2 [m], length : 53.12 [m], height : 12.35 [m]
wing area : 279.55 [m^2] fuselage exterior width : 4.1 [m]
weights :
operating empty weight : 71600 [kg] max. structural payload : 23000 [kg]
Zero Fuel weight (ZFW) : 94600 [kg] max. landing weight (MLW) : 105000 [kg]
max.take-off weight : 165000 [kg] weight fuel : 84240 [kg] (105300 [liter])
performance :
Max. operating Mach number (Mmo) : 0.84 [Mach] (900 [km/hr]) at 10000 [m]
normal cruise speed : 850 [km/hr] (Mach 0.80 ) at 10500 [m] (32 [%] power)
economic cruise speed : 880 [km/hr] (Mach 0.82 ) at 10500 [m]
service ceiling : 12000 [m]
range with max fuel : 10000 [km] (ATA domestic fuel reserves - 820.0 [km] alternate)
description :
low-wing cantilever monoplane with retractable landing gear with nose wheel
tapered multi-cellular wing with flush-riveted stressed skin
with double slotted flaps with no leading edge flaps ,with spoilers airfoil : Ilyushin
sweep angle 3/4 chord: 35.0 [°]
engines attached to the tail, landing gear attached to the wings, fuel tanks in the wings and wing center section, and additional 5000 litre tank in the tail.
Il-62 DM-SEF c/n 31402, above it is indicated as an Il-62M, but looking at the engine cowlings and what is on internet, this drawing is of an Il-62.
construction : all-metal aluminium-alloy stressed-skin construction with pressurized fuselage
fuselage shape : 0
calculation : *1* (dimensions)
wing chord : 6.47 [m]
mean wing chord : 6.47 [m]
calculated average wing chord tapered wing with rounded tips: 6.43 [m]
wing aspect ratio : 6.68 []
seize (span*length*height) : 28341 [m^3]
calculation : *2* (fuel consumption)
oil consumption : 13.5 [kg/hr]
fuel consumption (econ. cruise speed) : 6851.3 [kg/hr] (8564.1 [litre/hr]) at 22 [%] power
distance flown for 1 kg fuel : 0.13 [km/kg] at 10500 [m] height, sfc : 69.0 [kg/KN/h]
total fuel capacity : 105300 [litre] (84240 [kg])
calculation : *3* (weight)
weight engine(s) dry : 9220.0 [kg] = 20.43 [kg/KN]
weight 232 litre oil tank : 19.72 [kg]
oil tank filled with 2.8 litre oil : 2.6 [kg]
oil in engine 5.5 litre oil : 5.0 [kg]
fuel in engine 24.6 litre fuel : 18.05 [kg]
weight fuel lines 314.0 [kg]
weight engine cowling 1173.1 [kg]
weight thrust reversers 180.5 [kg]
total weight propulsion system : 10933 [kg](6.6 [%])
Cubana CU-T1284 landing at Lisbon airport with its thrust reversers with clamshell doors deployed shortly for touching down acting as air-brake, this is normal landing procedure for the Il-62M.
***************************************************************
Accommodation cabin facilities:
Interflug cabin layout 28 rows x 6 abreast = 168 passengers. Il-62M DDR-SEM c/n 4140536
typical 1-class cabin layout for 168 passengers : economy : pitch : 86.4 [cm] ( 3+3 ) seating in 28.0 rows
weight seats : 895.0 [kg]
high density seating passengers : 186 [m2/pax] at 6 -abreast seating in 31.0 rows, pitch 86.4 [cm]
pax density, normal seating : 0.64 [m2/pax], high density seating : 0.58 [m2/pax]
weight 5 toilets : 78.9 [kg]
On board Air Koryo; the Il62M had closed overhead luggage compartments
weight 2 galleys : 128.5 [kg]
weight overhead stowage for hand luggage : 58.8 [kg]
weight 3 wardrobe closets : 33.6 [kg]
weight 58 windows : 52.2 [kg]
weight 2 1.83x0.86 [m] entrance/exit doors : 132.1 [kg]
Aeroflot Il-62M interior on a flight between Tokyo and Moscow, the IL-62M had closed overhead luggage storage.
weight 2 freight doors (belly) : 104.9 [kg]
cabin volume (usable), excluding flight deck : 228.55 [m3]
passenger cabin max.width : 3.49 [m] cabin length : 34.22 [m] cabin height : 2.12 [m]
floor area : 107.6 [m2]
weight cabin facilities : 1484.0 [kg]
safety facilities:
weight 4 over wing emergency exits : 63.0 [kg]
weight 8 hand fire extinguisher : 25 [kg]
weight lifejackets : 75.6 [kg]
weight cockpit voice recorder (CVR) and flight data recorder (FDR): 20.0 [kg]
weight oxygen masks & oxygen generators : 109.2 [kg]
weight emergency flare installation : 10 [kg]
weight 4 emergency evacuation slides : 86.1 [kg]
weight safety equipment & facilities : 389 [kg]
fuselage construction:
fuselage aluminium frame : 18607 [kg]
floor loading (payload/m2): 214 [kg/m2]
weight rear pressure bulkhead : 202.8 [kg]
fuselage covering ( 443.3 [m2] duraluminium 3.56 [mm]) : 4173.9 [kg]
weight floor beams : 617.6 [kg]
weight cabin furbishing : 903.6 [kg]
weight cabin floor : 1633.7 [kg]
fuselage (sound proof) isolation : 322.1 [kg]
weight 13735 [litre] main central fuel tanks empty : 769.2 [kg]
weight engine mounts : 226 [kg]
weight fuselage structure : 27455.3 [kg]
Domodedovo airlines RA-86519 Il-62M cockpit, March 2019, Khabarovsk, Russia
Avionics:
weight HF and UHF radio : 7.0 [kg]
weight dual cloud-collision radar : 25.0 [kg]
weight VOR/ILS,RMI,Doppler,radio altimeter : 12.0 [kg]
weight automatic flight control System / auto-pilot : 23.0 [kg]
weight artificial horizons, compass, alti-meters : 7 [kg]
weight engine monitoring gauches & control switches : 12 [kg]
weight avionics : 86.0 [kg]
Systems:
Air-conditioning and pressurisation system maintains sea level conditions up to 7100 [m]
and gives equivalent of 2100 [m] at 12500 [m]. pressure differential : 0.62 [bars] (kg/cm2)
weight air-conditioning and pressurisation system : 251 [kg]
weight APU / engine starter: 56.4 [kg]
weight lighting : 55.4 [kg]
weight engine-driven 40kVA electricity generators : 42.0 [kg]
weight controls : 21.6 [kg]
weight systems : 426.3 [kg]
total weight fuselage : 29840 [kg](18.1 [%])
***************************************************************
total weight aluminium ribs (1302 ribs) : 5884 [kg]
weight 6 fuel tanks empty for total 91565 [litre] fuel : 5128 [kg]
weight wing covering (painted aluminium 2.30 [mm]) : 3473 [kg]
total weight aluminium spars (multi-cellular wing structure) : 4405 [kg]
weight wings : 13762 [kg]
weight wing/square meter : 49.23 [kg]
weight thermal leading-edge anti-icing : 47.5 [kg]
weight fin & rudder (21.7 [m2]) : 1069.6 [kg]
On May 27, 1977, the Il-62M CCCP-86614 of the Aeroflot crashed 1km short off the runway at Havana international airport. It had left Lisbon with 61 passengers and 9 crew members for the 7079km long flight to Havana. During the approach of RW05, it flew into power lines in foggy weather and crashed 1270 [m] short of the runway. 121m to the right of the extended centerline. There were 69 deaths. 1st flight : 1975 c/n 51903 (location 22°58'17.61"N 82°26'00.08"W +-100m)
weight stabilizer & elevator (31.4 [m2]): 1550.3 [kg]
weight flight control hydraulic servo actuators: 71.3 [kg]
weight double slotted flaps (43.7 [m2]) : 920.3 [kg]
weight spoilers (9.5 [m2]) : 40.9 [kg]
total weight wing surfaces & bracing : 22590 [kg] (13.7 [%])
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Can only operate from paved runways
wheel pressure : 18150.0 [kg]
weight 8 main wheels (1450 [mm] by 450 [mm]) : 1272.6 [kg]
tyre pressure main wheels :9.31 [Bar] (nitrogen)
weight 2 nose wheels : 159.1 [kg]
weight mult-disc wheel-brakes : 94.6 [kg]
weight flywheel detector type anti-skid units : 9.0 [kg]
weight oleo-pneumatic shock absorbers : 126.1 [kg]
weight wheel hydraulic operated retraction system : 1326.3 [kg]
weight undercarriage struts (four-wheel bogies) with axle 3577.5 [kg]
total weight landing gear : 6565.3 [kg] (4.0 [%]
*******************************************************************
********************************************************************
calculated empty weight : 69928 [kg](42.4 [%])
Shortly after the start of Moscow–Sheremetyevo airport (SVO) on July 6, 1982, fire alarm lights began flashing aboard Aeroflot's IL-62M CCCP-86513. The lights indicated that 2 engines were on fire. The captain turns off both engines and tries to return to Sheremetyevo. However, he loses control and crashes 10km North West of Sherenetjevo airport, Moscow, 1.5 [km] east of village of Medeleevo. It had taken off as flight 411 with 82 passengers and 8 crew members with Dakar as its destination. All 90 passengers were killed. 1st flight : 1980 c/n 4037536. Probably the fire alarm was false... (location +-100 [m] 56°01’37"N 37°15'37"E ) c/n 4037536 cycles : 1139 flying hours : 4818
weight oil for 14.1 hours flying : 199.7 [kg]
weight catering : 321.2 [kg]
weight water : 128.5 [kg]
weight crew : 891 [kg]
weight crew lugage,nav.chards,flight doc.,miscell.items : 131 [kg]
operational weight empty : 71600 [kg] (43.4 [%])
********************************************************************
weight 168 passengers : 12936 [kg]
weight luggage : 2688 [kg]
weight cargo : 7376 [kg]
zero fuel weight (ZFW): 94600 [kg](57.3 [%])
weight fuel for landing (1.5 hours flying) : 10400 [kg]
max. landing weight (MLW): 105000 [kg](63.6 [%])
max. fuel weight : 155840 [kg] (94.4 [%])
payload with max fuel : 98 passengers+luggage 9160 [kg]
published maximum take-off weight : 165000 [kg] (100.0 [%])
calculation : * 4 * (engine power)
power loading (Take-off) : 366 [kg/KN]
power loading (Take-off) 1 PUF: 488 [kg/KN]
max. total take-off power : 451.2 [KN]
calculation : *5* (loads)
manoeuvre load : 5.3 [g] at 1000 [m]
limit load : 3.0 [g] ultimate load : 4.5 [g] load factor : 0.7 [g]
design flight time : 3.82 [hours]
design cycles : 8124 sorties, design hours : 31065 [hours]
max. wing loading (MTOW & flaps retracted) : 590 [kg/m2]
wing stress (2 g) during operation : 192 [N/kg] at 2g emergency manoeuvre
calculation : *6* (angles of attack)
angle of attack zero lift : -1.83 ["]
max. angle of attack (stalling angle, clean) : 12.14 ["]
max. angle of attack (full flaps) : 11.34 ["]
angle of attack at max. speed : 2.66 ["]
On September 29, 1982, Aeroflot Il-62M CCCP-86470 shoots to the right of the runway upon landing at RW06 of Luxembourg-Findel Airport and ends in a ravine. Operated Flight 343 from Moscow(MOW) to Luxembourg(LUX) with 66 passengers and 11 crew members. There are 14 deaths. 1st flight : 1977 c/n 1725234. Cause : non-working thrust reverser. (location +-75m 49°37'31.90"N 6°12'54.21"E )
calculation : *7* (lift & drag ratios
lift coefficient at angle of attack 0° : 0.15 [ ]
lift coefficient at max. speed : 0.37 [ ]
lift coefficient at max. angle of attack : 1.14 [ ]
max. lift coefficient full flaps : 1.69 [ ]
drag coefficient at max. speed : 0.0304 [ ]
drag coefficient at econ. cruise speed : 0.0307 [ ]
induced drag coefficient at econ. cruise speed : 0.0088 [ ]
drag coefficient (zero lift) : 0.0219 [ ]
lift/drag ratio at max. speed : 12.07 [ ]
calculation : *8* (speeds
stalling speed clean at sea-level (OW loaded : 158149 [kg]): 320 [km/u]
stalling speed at sea-level with full flaps (normal landing weight): 200 [km/u]
landing speed at sea-level (normal landing weight : 104775 [kg]): 229 [km/hr]
max. rate of climb speed : 680 [km/hr] at sea-level
max. endurance speed : 656 [km/u] min. fuel/hr : 6189 [kg/hr] at height : 9449 [m]
max. range speed : 899 [km/u] min. fuel consumption : 7.448 [kg/km] at cruise height : 11278 [m]
cruising speed : 850 [km/hr] at 10500 [m] (power:21 [%])
max. operational speed (Mmo) : 900.00 [km/hr] (Mach 0.84 ) at 10000 [m] (power:23.1 [%])
airflow at cruise speed per engine : 152.2 [kg/s]
speed of thrust jet : 1421 [km/hr]
climbing speed at sea-level (loaded) : 1982 [m/min]
climbing speed at 1000 [m] with 1 engine out (PUF / MTOW) : 1258 [m/min]
climbing speed at 1000 [m] with 2 engines out (2xPUF / MTOW) : 499 [m/min]
On 01 July 1983, the IL-62M P-889 c/n 2139.1 of the North Korean CAAK (now Air Koryo) crashed in the Fouta Djallon highlands near Labe, Guinea-Bissau. There are 23 deaths. Flight from Pyongyang (FNJ), via Kabul and Cairo to Conakry (CKY), 1st flight : 1981 (location is +-25 km 11°19'11.98"N 12°17'59.99"W )
calculation : *9* (regarding various performances)
take-off speed : 381.9 [km/u]
high wheel pressure, can only take off from paved runways
take-off distance at sea-level concrete runway : 3157 [m]
take-off distance at sea-level over 15 [m] height : 3243 [m]
landing run : 812 [m]
landing run (C.A.R.) from 15 [m] : 1131 [m]
lift/drag ratio : 13.44 [ ]
climb to 5000 [m] with max payload : 2.74 [min]
climb to 10000 [m] with max payload : 4.59 [min]
theoretical ceiling fully loaded (mtow- 60 min. fuel:158149 [kg] ) : 14800 [m]
calculation *10* (action radius & endurance)
range with max. payload: 8753 [km] with 23000.0 [kg] max. useful load (83.6 [%] fuel)
range with high density pax: 9590 [km] with 186 passengers (90.3 [%] fuel)
range with typical two-class pax: 9840 [km] with 168 passengers (92.3 [%] fuel)
range with max.fuel : 10820 [km] with 11 crew and 98 [kg] passengers and 100.0 [%] fuel
ferry range : 11330 [km] with 5 crew and zero payload (100.0 [%] fuel)
max range theoretically with additional fuel tanks total 117919.6 [litre] fuel : 12402 [km]
Available Seat Kilometres (ASK) : 1653126 [paskm]
useful load with range 1000km : 23000 [kg]
useful load with range 1000km : 186 passengers
production (theor.max load): 19550 [tonkm/hour]
production (useful load): 19550 [tonkm/hour]
production (passengers): 142800 [paskm/hour]
oil and fuel consumption per tonkm : 0.351 [kg]
fuel cost per paskm : 0.048 [eur]
crew cost per paskm : 0.011 [eur]
On May 9, 1987, at 10:18 a.m., flight 5055 departed Warsaw for New York. A distance of 7257km. There were 172 passengers and 11 crew members aboard the Il-62M SP-LBG "Kosciuszko" c/n 3344942 of the LOT. 23 minutes after the start at 8200ft altitude, the low-pressure turbine shaft broke loose from the Soloviev D-30KU turbofan, causing the turbine rotor to fail. Shooting engine parts pierced the hull after which a fire broke out in the rear cargo hold. The steering of the elevators was also damaged. The crew switched off engines 1 and 2 and thought that this had also extinguished the fire. However, this was not the case. They made a rapid descent and first wanted to land at Modlin airport, but, ignorant of the fire in the tail, changed this to Warsaw-Okecie int'l airport (WAW) because there was better rescue equipment available there. At 11.09 am they made a turn at 1450m for the approach of RW33. During the turn, the crew lost control after which the plane crashes at 465 km/h in a forest 6 km in front of the runway, SE of the airport. A piece of forest of 400m long is cleared. All 183 on-board are killed. 1st flight : 1983 6972 flight hours 1752 cycles.
Crash-site SP-LBG (locatie +- 15 [m] 52°06’46.07’’N 21°02’46.17’’O)
source : google earth
economic hours : 22300 [hours] is less then design hours
time between engine failure : 481 [hr]
can continue fly on 3 engines, low risk for emergency landing for PUF
writing off per paskm : 0.018 [eur]
insurance per paskm : 0.0009 [eur]
maintenance cost per paskm : 0.018 [eur]
direct operating cost per paskm : 0.095 [eur]
direct operating cost per tonkm (max. load): 0.697 [eur]
direct operating cost per tonkm (normal useful load): 0.697 [eur]
The aircraft involved in the hijack pictured at Dar es Salaam airport, registration unknown CCCP-86478 ?? or 86474 ??)
On 18 May 1989 an A South African armed with a grenade, hijacked an Aeroflot IL-62 airliner carrying members of the African National Congress after take-off from Luanda, Angola. The hijacker was shot by a security guard as he attempted to enter the cockpit of the aircraft. The airplane continued to the planned stop at Dar Es Salaam, Tanzania.
The hijacker was sentenced to fifteen years in prison. (source : aviation safety net)
SOUTH AFRICA ACCUSED IN ATTEMPTED AIR HIJACKING
By William Claiborne
June 3, 1989
JOHANNESBURG, JUNE 2 -- The exiled African National Congress today accused South African police of sending white undercover agents to try to hijack a Soviet airliner flying from Angola to Tanzania last month with 174 black nationalist guerrillas aboard and force it to fly to Johannesburg. Two white South African men were said by Tanzanian officials to have been overpowered and disarmed by Soviet guards on the plane on May 18. A crew member was reported injured and one hijacker wounded by gunfire in the struggle. If the alleged attempted hijacking had been successful, it would have resulted in the largest mass arrest of ANC guerrillas ever, and would likely have provoked an international uproar and accusations of state-sponsored air piracy. Details of the incident remain sketchy and clouded in secrecy. The South African government denied complicity and suggested that ANC "dissidents" may have tried to hijack the plane because they wanted to return home. Soviet Embassy officials in Dar es Salaam have refused to comment, and the ANC headquarters in Lusaka, Zambia, had few details when contacted by telephone today. However, Tom Sebina, spokesman for the guerrilla movement, said South African police were responsible and that there was "a lot to suspect about" the men who were arrested aboard the plane. A 30-year-old South African, identified as Bradley Richard Stacey, was sentenced Thursday to 15 years' imprisonment in a court in the Tanzanian capital of Dar es Salaam after pleading guilty to charges that he took explosives, detonators and hand grenades aboard an Aeroflot Iluyshin airliner traveling from Luanda, Angola, to Dar es Salaam. According to news agency reports in Dar es Salaam, court officials said another, as yet unidentified, South African in a Tanzanian military hospital faces similar charges and will appear in court on June 13. The Soviet airliner reportedly was ferrying ANC guerrillas from training bases in Angola that were shut down as part of the Dec. 22 regional peace agreement between South Africa, Angola and Cuba. An estimated 7,000 ANC guerrillas in Angola are supposed to be moved to bases in Tanzania, Nigeria and Uganda as a result of the peace accord. A spokesman in the South African police command in Pretoria, Capt. R.A. Crewe, said he would not respond to "vaguely put allegations" but denied that there was any official involvement in the incident. Crewe referred to anonymous letters sent to several South African journalists last month, purporting to have been written by "dissident" ANC guerrillas, and said, "They correspond with our information that hundreds of ANC members are dissatisfied and don't want to go to those countries, but want to return home." ANC sources suggested that the letters, which claimed that many ANC guerrillas were resisting being transported from Angola to camps elsewhere in Africa, were forgeries mailed by the South African security police. On several occasions in recent years, the ANC's exile training bases have been infiltrated by white South African police agents posing as anti-apartheid activists. Some of them have been sent to the Soviet Union and to East Bloc countries for guerrilla training and have resurfaced in South Africa as senior security police officers.
Washington post article, 3 June 1989
DDR-SEW at Schiphol airport, Amsterdam, October 1988.
On June 17, 1989, the Il-62M DDR-SEW of Interflug breaks off the start because the elevators were stuck. Wanted to take off with 103 passengers and 10 crew members from East Berlin-Schonefeld (SXF) for a flight to Moscow (SVO). Does not stop in time and shoots past the end of RW25L, it hits an obstacle and catches fire. (location 52°21'58.09"N 13°28'40.57"E) 20 passengers are killed and 1 person on the ground and there are 54 injured. 1st Flight 1988. c/n 2850324
DDR-SEW crash site
On September 3, 1989, Cubana's Il-62M CU-T1281 takes off from Havana-Jose Marti international airport (HAV) in heavy rain with 115 mostly German and Italian tourists and 11 crew members sailing 8150km away from Cologne (CGN). Immediately after take-off, the aircraft enters a strong downward airflow that blows the aircraft to the ground in a residential area 1km past the runway. All on-board are killed as well as 45 people on the ground. There are also another 63 people wounded on the ground. 1st flight : 1988 c/n 3850453 flight 9046. (location +-100m 23°00'08"N 82°23'13"W
The pilot should not have taken off in the rapidly deteriorating weather situation. This was the last fatal accident involving an Il-62M.
On 24 July 2009 Aria Air IL-62M UP-16208 c/n 1951525 overran Mashhad’s RW13L on landing and came to rest outside the airport perimeter. It approached the runway with 325 [km/hr], 50 [km/hr] above its assigned approach speed with a weight of 93 ton and touched down with 275 [km/hr]. Rate of descent 10 [m/s]. The crew did not communicate properly, high landing speed and wrong use of thrust reversers caused the overrun. Flight 1525 had taken off from Tehran (THR) with destination Mashad (MHD) in Iran with 156 passengers and 17 crew. First flight : 1989 total airframe hours : 13573 cycles : 3987 engines : Soloviev D-30KU-2 Ex-reg : UN-86509, UK-86578, CCCP-86578, D-AOAM, DDR-SEY. 11 crew and 5 passengers died in the crash.
Location : +- 30m 36°13’05.60”N 59°39’57.42”E
Aeroflot Ilyushin Il-62m CCCP-66700 at Frankfurt am Main airport, March 1976
Uzbekistan government Ilyushin Il-62M UK 86579 c/n 2951636 at Schiphol airport, Amsterdam
The Luftwaffe also used the Il-62M, pictured above is reg. 11-20
Landing Cubana Il-62M CU-T1217 c/n 3933232
Literature :
Bekende vliegt. Italie en Rusland page 86,87
Verkeersvliegtuigen (vd Klauw) page 55
Jane’s commercial transport aircraft page 167
Ilyushin IL-62M, Zvezda 1:144 von Bernhard Pethe (modellversium.de)
Jane’s All the world aircraft 1979-1980 page 186,187
The flier’s handbook page 113
Aviation disasters (Gero) page 208
Observers Airliners page 119
DISCLAIMER Above calculations are based on published data, they must be
regarded as indication not as facts.
Calculated performance and weight may not correspond with actual weights
and performances and are assumptions for which no responsibility can be taken.
Calculations are as accurate as possible, they can be fine-tuned when more data
is available, you are welcome to give suggestions and additional information
so we can improve our program. For copyright on drawings/photographs/
content please mail to below mail address
(c) B van der Zalm 22 October 2022 contact : info.aircraftinvestigation@gmail.com python 3.7.4