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Let L-410 crash in Poti

29 Mar 1983 · near Poti (Georgian SSR, USSR)

Aeroflot (Georgian Civil Aviation Directorate, Sukhumi Joint Aviation Detachment) Let L-410 Turbolet · Engine failure, design deficiencies of the aircraft

From Poti to Babushara, Sukhumi

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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
6 · all aircraft and ground
Ground fatalities
Unknown
Occupants
Unknown
Survivors
12
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

Let L-410 Turbolet

Aircraft type
Let L-410
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-67190
Onboard fatalities
6
Route
From PotiTo Babushara, Sukhumi

Cause areas

  • Personnel issues › Action/decision
  • Aircraft › Aircraft oper/perf/capability

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

Approximate · Estimated position: Poti, near the place the Wikipedia article names. Not the accident site.

From the Wikipedia article

The Let L-410 crash in Poti was an aviation accident involving a Let L-410M (Let L-410M) passenger aircraft of the company Aeroflot, which occurred on Tuesday 29 March 1983 in the Poti area; 6 people were killed.

Crash

The aircraft was operating domestic passenger flight G-70 from Poti to Sukhumi, and 15 passengers boarded it, including one who was not registered — E. P. Chitava, an instructor pilot of the Sukhumi aviation detachment. The airliner's take-off weight was 5685 kg with a centre of gravity of 28 % MAC, which was within permissible limits. At that time there was broken middle-level cloud in the sky, wind 210° 2 m/s, visibility up to 20 kilometres. At 15:16 local time (14:16 MSK), with 18 people on board, flight 70 took off from runway 10 of Poti Airport.

The pilots retracted the landing gear, and the flaps were extended to 15°, when 14 seconds after lift-off, at an altitude of 60 metres, with the aircraft flying at an indicated airspeed of 195 km/h, the rpm of both engines suddenly dropped. In the left engine the rpm dropped to 60 %, that is, to flight idle, but then began to increase again and by the 25th second after take-off had returned to the original 94.5 %. However, in the right engine the rpm continued to decrease after the drop and soon fell practically to zero. Since L-410 aircraft are not equipped with an automatic propeller feathering system, the right propeller continued to rotate in autorotation (windmilling) mode, thereby creating considerable aerodynamic drag. This imbalance led to a vertical load factor of 1.35 units appearing, and the elevator began to vibrate at high frequency, which continued right up to the crash.

The crew began to make a right turn, while altitude and speed were simultaneously decreasing. 1 minute 20 seconds after the start of the take-off run and 44 seconds after the start of the drop in engine rpm, the speed had already fallen to 130 km/h, so the aircraft entered a stall, and three seconds later, having entered a steep right bank, struck the treetops with its right wing. The pilots corrected the bank, but 38 metres after the first impact the airflow separated on the wing because of the low speed. The aircraft again entered a steep right bank and began to crash into the trees. Having ploughed through them for 50 metres, 88 metres from the point of first impact with the trees and 2240 metres south-east (azimuth 125°) of the Poti aerodrome reference point, the airliner, on a heading of 325°, crashed into marshy ground, after which it swung round and came to a stop. There was no fire, but the forward part of the fuselage was destroyed, killing both pilots and another four passengers, including the instructor pilot, that is, 6 people in total. The remaining 12 people (the check pilot and 11 passengers) were injured but survived.

Investigation and cause

Investigation

As the commission established, the pilots carried out the take-off using the normal engine control system from the engine control levers. The shut-off cocks of the emergency circuit were not used, and judging by how the engine rpm changed, the crew could not have accidentally activated these shut-off cocks. Moreover, the reduction in engine rpm occurred because the pilots deliberately moved both engines simultaneously to idle, after which, 4 seconds later, they moved the left engine back to take-off power, while the right one, on the contrary, was shut down. The latter was deliberately shut down probably because the torque meter (IKM) pressure and propeller rpm were above the maximum permissible values, which in turn could have been caused by a temporary failure of the propeller speed governor, as the spool valve of the centrifugal mechanism momentarily stuck. Such failures had already occurred before on L-410M aircraft.

The crew shut down the right engine and moved the left one to idle, after which they set the elevator to dive, that is, lowered the nose of the aircraft and it began to descend, while the indicated airspeed decreased from 195 to 70 km/h. It is possible that the pilots intended to make a forced landing straight ahead, acting in accordance with the flight operations manual. However, when the altitude decreased to 50 metres, the pilots saw beneath them a forested plain, a landing on which could have led to the destruction of the aircraft, so they decided to stop the descent and head for the forced-landing site for local air lines aircraft. To do this, the crew moved the left engine to take-off power, after which they turned right towards the site, trying as far as possible to maintain direction and altitude. But since the airliner's weight was close to the maximum take-off weight and the flaps were extended to 15°, the thrust of one engine under such conditions was insufficient, so the aircraft began to lose altitude and speed until the latter fell to 130 km/h. Having entered a stall, the "Let" crashed into the trees.

The right propeller did not …

Translated into English with AI assistance from the Russian Wikipedia article “Катастрофа Let L-410 в Поти” (revision 154269100, retrieved 2026-09-19) by its authors, under CC BY-SA 4.0. Extracted as plain text: references, tables, images and some sections are left out; the translation may contain errors, and long articles were cut to their first 700 words. Read the article

Sources

Russian Wikipedia article: Катастрофа Let L-410 в Поти
Article
Катастрофа Let L-410 в Поти
Translation
Into English with AI assistance; names of linked operators and aircraft types from Wikidata. It may contain errors.
Revision
154269100 · 2026-08-06 · retrieved 2026-09-19
Wikidata
Q19910773
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
ru Wikipedia article "Катастрофа Let L-410 в Поти" (page 5398233, revision 154269100), translated into English with AI assistance
Date
Wikipedia infobox: date
Place and country
Wikipedia infobox: site
Map position
place the Wikipedia infobox site links (Wikidata coordinates)
Aircraft, operator and route
Wikipedia infobox: aircraft type, registration, operator, origin and destination; route airports from the linked airport articles' Wikidata codes (OurAirports)
Operation
operator is an airline according to Wikidata
Fatalities
Wikipedia infobox: aircraft fatalities
Ground fatalities
not stated in the Wikipedia infobox
Summary
Wikipedia infobox: summary
Source notes (1)
  • Wikipedia · Facts from the Russian Wikipedia article's infobox, translated into English with AI assistance, not checked against an investigation report. Independent review pending.