Accident Rans S-6ES-503 Coyote II EC-CK9,
ASN logo
ASN Wikibase Occurrence # 279423
 
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. If you feel this information is incomplete or incorrect, you can submit corrected information.

Date:Saturday 11 June 2022
Time:07:50
Type:Silhouette image of generic COY2 model; specific model in this crash may look slightly different    
Rans S-6ES-503 Coyote II
Owner/operator:Private
Registration: EC-CK9
MSN: S-6A-125
Year of manufacture:1996
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:Albacete -   Spain
Phase: Take off
Nature:Private
Departure airport:La Gineta Airfield
Destination airport:La Gineta Airfield
Investigating agency: CIAIAC
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The aircraft made an emergency landing attempt on a disused road, which was aborted after touchdown. In the subsequent initial climb, the aircraft pilot was unable to avoid contact of the right wing with a tree; the aircraft then plunged into the ground in a level attitude, both horizontally and longitudinally.
The aircraft had taken off 20 minutes earlier from the La Gineta (Albacete) aerodrome for a local private flight with the pilot as the sole occupant. After 15 minutes of flight, the pilot began to notice loud noises and vibrations coming from the engine compartment and decided to make an emergency landing.
The accident resulted in damage to the landing gear, wings and propeller. The pilot was unharmed.

The abnormal noises and vibrations coming from the engine compartment were due to the in-flight breakage of a rubber damper in the engine exhaust system.
The rubber damper that broke in flight had not been replaced according to the instructions contained in the ROTAX engine maintenance manual.
The emergency landing and the aborted landing maneuver were performed with flap 2 instead of flap 0, as recommended in the aircraft's Flight Manual. Although the engine never stopped providing power, the aircraft was not able to gain sufficient altitude or speed to continue the flight safely.

Accident investigation:
cover
  
Investigating agency: CIAIAC
Report number: ULM A-015/2022
Status: Investigation completed
Duration: 7 months
Download report: Final report

Sources:

https://www.mitma.gob.es/organos-colegiados/ciaiac/ultraligeros-motorizados-ulm/2022/a-15_2022

Revision history:

Date/timeContributorUpdates
20-Jun-2022 07:09 harro Added
20-Jun-2022 17:42 RobertMB Updated [Aircraft type, Cn]

Corrections or additions? ... Edit this accident description

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2024 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314
www.FlightSafety.org