CU1216
1999-DEC-21 · La Aurora International Airport, Guatemala City, Guatemala

Cubana de Aviación — Flight CU1216

A Cubana de Aviacion DC-10, leased from AOM French Airlines, overran the runway while landing at La Aurora International Airport in heavy rain. The aircraft touched down too far down the wet runway and failed to decelerate sufficiently, eventually plunging down a steep slope at the end of the runway and crashing into ten houses in the La Libertad neighborhood. The accident resulted in 18 total fatalities: 16 people on board (8 passengers and 8 crew members) and 2 people on the ground.

Aircraft
McDonnell Douglas DC-10-30
Registration
F-GTDI
Phase
Cause
Souls on Board
314
Fatalities
18
Origin → Dest
José Martí International Airport, Havana, Cuba → La Aurora International Airport, Guatemala City, Guatemala
Report

Investigation Summary

Flight 1216 was a special charter flight repatriating Guatemalan students from universities in Cuba. The approach to Runway 19 was conducted visually with the assistance of PAPI (Precision Approach Path Indicator) and was described as stabilized. However, the aircraft touched down significantly further down the runway than intended. Despite the wet surface conditions, the crew did not initiate a go-around. Post-crash investigation revealed a significant discrepancy regarding the aircraft's spoilers: while the Flight Data Recorder (FDR) indicated they had deployed, the physical wreckage showed the spoilers in the down and locked position, and the cockpit spoiler handle was in an undefined state. The investigation could not definitively resolve this mechanical contradiction but concluded that the primary factors were the long touchdown and the crew's failure to abort the landing when it became clear the aircraft could not stop within the remaining distance.

Final Conclusions

The investigation, conducted by Guatemala's Directorate General of Civil Aeronautics (DGAC) with assistance from the French BEA, concluded that the accident was caused by the crew's failure to initiate a go-around after touching down too far along a wet runway. This resulted in insufficient deceleration and a subsequent runway excursion. The aircraft was destroyed by the impact with residential structures and subsequently written off.

Photographic Evidence (1)

GATWICK JULY 1998 AOM FRENCH AIRLINES DOUGLAS DC10 F-GTDI
© simon butler · Wikimedia Commons

Video Analysis

No video analysis linked for this case file yet.

Airframe & Maintenance

Airframe Hours
85,760
Cycles
27,331
Engines
General Electric CF6-50C

Crew Experience

Captain

Total hours
16,117
On type
4,872

Jorge Toledo, 54, employed by Cubana since 1972. Fatal.

First Officer

Total hours
8,115
On type
4,156

Cecelio Hernandez, 41, former Yak-42 captain. Fatal.

Flight Engineer

Total hours
22,819
On type
4,939

Moises Borges, 59, employed by Cubana since 1966. Fatal.

Systems & Failure Modes

i

Spoilers

Aerodynamic brakes used to reduce lift and increase drag upon landing. Investigators found a discrepancy between FDR data showing deployment and physical evidence showing them locked down.

i

PAPI

Precision Approach Path Indicator; a system of lights providing visual glideslope guidance to the pilots during the approach.

Interesting Facts

  • 01The aircraft was 27 years old and had previously been involved in a hijacking in 1987 while operated by Air Afrique under registration TU-TAL.
  • 02Among the fatalities was stewardess Johanna Toledo, the daughter of the flight's captain.
  • 03The runway was wet at the time of the accident with a reported cloud base of 2,200 feet.
  • 04The aircraft was leased from AOM French Airlines and carried French registration F-GTDI.

Safety Actions & Advisories

Runway Safety and Overrun Prevention

The investigation emphasized the importance of strict adherence to stabilized approach criteria and the necessity of initiating a go-around if a touchdown occurs beyond the designated landing zone, especially on wet or contaminated runways.

Spoiler System Maintenance and Verification

Following the discrepancy between FDR data and physical evidence, recommendations were made regarding the verification of spoiler deployment mechanisms and the reliability of cockpit indicators for ground spoilers.

Known Controversies & Unanswered Questions

Spoiler Deployment Discrepancy

Reference ↗

The investigation noted a conflict between the Flight Data Recorder, which recorded the spoilers as deployed, and the physical wreckage, where they were found retracted and locked. The cause of this discrepancy was never determined.

Location

La Aurora International Airport, Guatemala City, Guatemala · 14.5687, -90.5322

Case File History

  1. New evidenceUpdated findings.
  2. Status changeUpdated report status and safety actions.

Related Cases

Case ID · cubana-1216-1999Last updated · Filed

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