| Date: | Wednesday 14 October 2020 |
| Time: | 13:21 |
| Type: | Antonov An-32A |
| Owner/operator: | AerCaribe Peru |
| Registration: | OB-2120-P |
| MSN: | 1805 |
| Year of manufacture: | 1989 |
| Total airframe hrs: | 9830 hours |
| Cycles: | 10893 flights |
| Engine model: | Ivchenko AI-20D-5 |
| Fatalities: | Fatalities: 0 / Occupants: 4 |
| Other fatalities: | 0 |
| Aircraft damage: | Destroyed, written off |
| Category: | Accident |
| Location: | Iquitos-Coronel Francisco Secada Vignetta International Airport (IQT) -
Peru
|
| Phase: | Landing |
| Nature: | Cargo |
| Departure airport: | Lima-Jorge Chávez International Airport (LIM/SPJC) |
| Destination airport: | Iquitos-Coronel FAP Francisco Secada Vignetta International Airport (IQT/SPQT) |
| Investigating agency: | CIAA |
| Confidence Rating: | Accident investigation report completed and information captured |
Narrative:An Aer Caribe Antonov An-32 cargo plane suffered a runway excursion after landing on runway 06 at Iquitos Airport, Peru.
Upon touchdown, the crew proceeded to disconnect the propeller stops to use reverse power as a braking measure. However, the aircraft veered sharply to the left, off the side of the runway.
The aircraft crossed an area of vegetation and a drainage channel, suffering severe structural damage including breakage and separation of the right wing, the main landing gear and the right engine; in addition, there was a fuel spill which caused a fire on the wing.
The airport emergency services managed to control the fire and evacuate the crew and passenger on board.
PROBABLE CAUSE
Runway Excursion due to loss of directional control of the aircraft after landing by disengaging the propeller stops for aerodynamic braking at a higher than established speed, which generated an uncontrollable leftward turning moment of the trajectory, due to asymmetric thrust of the propellers.
CONTRIBUTING FACTORS
1. Performing a landing on an Unstabilised Approach, not executing the established Go-Around procedure.
2. Performing a failed landing due to asymmetric thrust of the propellers, not applying the procedure established in the Operator's QRH to shut down the failed engine.
3. Probable failure of the KTA Fuel Regulator of the Automatic Engine Rotation Frequency and Power Regulation System, which blocked the reduction of the power of the N°2 engine to established operating regimes for the approach and landing.
METAR:
17:00 UTC / 12:00 local time:
SPQT 141700Z 35004KT 310V090 9999 SCT020 32/23 Q1011 NOSIG RMK BIRD HAZARD RWY 06/24 PP000
18:00 UTC / 13:00 local time:
SPQT 141800Z VRB04KT 9999 VCSH BKN020 33/24 Q1009 NOSIG RMK BIRD HAZARD RWY 06/24 PP000
18:33 UTC / 13:33 local time:
SPQT 141833Z 34008KT 300V360 8000 2000N TSRA BKN020 FEW025CB 28/22 Q1008
19:00 UTC / 14:00 local time:
SPQT 141900Z 36008KT 4000 TSRA BKN020 FEW025CB BKN100 25/23 Q1008 TEMPO 5000 SHRA RMK PP024
Accident investigation:
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| | |
| Investigating agency: | CIAA |
| Report number: | CIAA-ACCID-003-2020 |
| Status: | Investigation completed |
| Duration: | 3 years and 11 months |
| Download report: | Final report
|
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Sources:
rpp.pe AerCaribe
NBAAI
History of this aircraft
Other occurrences involving this aircraft Location
Revision history:
| Date/time | Contributor | Updates |
| 16-Sep-2024 09:25 |
ASN |
Updated [Narrative, Accident report, ] |
| 16-Sep-2024 09:26 |
ASN |
Updated |