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Aeroflot Flight 1969

31 Mar 1971 · 13 km southwest of Voroshilovgrad Airport

Antonov An-10 · Structural failure of the right wing for reasons unknown, loss of control

From Kurumoch International Airport (KUF) to an unrecorded destination

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Event

Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
Event fatalities
65 · all aircraft and ground
Ground fatalities
Unknown
Occupants
65
Survivors
0
InjuriesFatal: death within 30 days. Serious: over 48 hours in hospital within a week, most broken bones, severe bleeding, nerve or organ damage, or serious burns. Minor: anything less. Glossary
Unknown
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
Airline

Antonov An-10

Aircraft type
Antonov AN-10
Category
Airplane · from aircraft type
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
CCCP-11145
Operator
Aeroflot
Onboard fatalities
65
Route
From Kurumoch International Airport (KUF)To not recorded

Cause areas

  • Aircraft › Aircraft structures
  • Not determined › Not determined

From the investigation findings the Wikipedia article reports, sorted into the NTSB's cause areas with AI assistance.

Not plotted · Not plotted: the Wikipedia article gives no coordinates, and its site names no town or airport that matches exactly.

From the Wikipedia article

Aeroflot Flight 1969 was a passenger flight operated by an Antonov An-10 that crashed during the approach to Voroshilovgrad (now Luhansk) on 31 March 1971, resulting in the death of all 65 people on board. An investigation revealed that the Antonov's right wing failed structurally during the approach.

Accident

Flight 1969 was a scheduled domestic flight from Kurumoch to Luhansk. At 11:13 local time the An-10 departed Kurumoch International Airport and climbed to a cruising altitude of 7,800 m. After passing a waypoint at Rostov the crew was instructed by air traffic control (ATC) to descend to an altitude of 5,700 m. Shortly afterwards the crew received a report of weather conditions at the destination airport: solid clouds with a base of 600 m, visibility 10 km, wind 50 degrees at 8 m/s with gusts up to 12 m/s.

At 12:58:46 the crew reported an altitude of 1,200 m and were given permission to continue their descent to 600 m. The crew's last transmission was at 12:58:50 when they reported they were continuing to descend. Before the An-10 reached 600 metres, approximately 13 m2 of the right wing including an aileron, separated from the rest of the aircraft severing hydraulic lines during the process. Part of the detached wing section struck the right horizontal stabilizer, damaging its structure while tearing off part of it and its elevator. The aircraft immediately yawed right and entered a steep bank also to the right. As the Antonov plummeted towards the ground both right engines lost oil pressure, causing their propellers to go into fine pitch, inducing both of them to rotate at very high rpm. At 12:59:30 the aircraft struck the ground in a 60 degree pitch down, 50 degree bank right attitude, killing all 69 people on board.

Investigation and cause

Investigation

Investigators discovered that a riveted seam of the right wing nine ribs wide had separated in flight due to excessive shear loads. The investigators focused on two scenarios that could have led to the accident. The first was that the wing fractured due to over pressurization. It was theorized that if the vent outlet of the air bleed anti ice system were blocked by ice build up, too much pressure could cause a riveted seam to split open. Static testing with partially and completely blocked outlets showed that the pressure build up was negligible, due mostly to the systems design having numerous other paths for the bleed air to escape. The second synopsis was based on weakness of the joint due to a defect and/or fatigue cracks near the riveted seam. Testing of similar structures under laboratory conditions were performed but no weakening of the wing panel was found. Investigators failed to find the root cause of the wing panel failure and an official cause of the accident was never established.

Text from the Wikipedia article “Aeroflot Flight 1969” (revision 1346571410, retrieved 2026-09-18) by its authors, under CC BY-SA 4.0. Extracted as plain text: references, tables, images and some sections are left out. Read the article

Sources

Wikipedia article: Aeroflot Flight 1969
Article
Aeroflot Flight 1969
Revision
1346571410 · 2026-04-01 · retrieved 2026-09-18
Wikidata
Q16662327
Licence
Text CC BY-SA 4.0, by the article's authors; Wikidata CC0; town positions GeoNames (CC BY 4.0)
Where each value comes from
Record
Wikipedia article "Aeroflot Flight 1969" (page 57826684, revision 1346571410)
Date
Wikipedia infobox: date
Place and country
Wikipedia infobox: site
Map position
none
Aircraft, operator and route
Wikipedia infobox: aircraft type, registration, operator, origin and destination; route airports from the linked airport articles' Wikidata codes (OurAirports)
Operation
flight number in the article title
Fatalities
Wikipedia infobox: aircraft fatalities
Ground fatalities
not stated in the Wikipedia infobox
Summary
Wikipedia infobox: summary
Source notes (1)
  • Wikipedia · Facts from the Wikipedia article's infobox and coordinates, not checked against an investigation report. Independent review pending.