Incident Canadair CL-600-2C10 Regional Jet CRJ-702ER 7O-FAB,
ASN logo
ASN Wikibase Occurrence # 180096
 
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 13 September 2014
Time:06:38 UTC
Type:Silhouette image of generic CRJ7 model; specific model in this crash may look slightly different    
Canadair CL-600-2C10 Regional Jet CRJ-702ER
Owner/operator:Felix Airways
Registration: 7O-FAB
MSN: 10268
Fatalities:Fatalities: 0 / Occupants:
Aircraft damage: Minor
Location:Hodeida International Airport (HOD) -   Yemen
Phase: Initial climb
Nature:Passenger - Scheduled
Departure airport:Hodeida International Airport (HOD)
Destination airport:Sana'a International Airport (SAH)
Confidence Rating: Information verified through data from accident investigation authorities
Narrative:
A Felix Airways CRJ702ER, registration number 7O-FAB, powered by two General Electric (GE) CF34-8C5B1 turbofan engines, experienced a No. 1 (left) engine failure just after takeoff from the Hodeida International Airport (HOD), Yemen. The flight crew received a No. 1 engine fire warning indication along with high N2 vibrations and performed an inflight shutdown (IFSD) of the engine and made an uneventful air turn back (ATB) and landing at HOD. The operator reported that after landing, damage was observed to the turbine blades, holes were found in the low pressure turbine (LPT) case and the aft cowl, and that the No. 1 engine needed to be replaced. The event flight, flight No.171, was a regularly scheduled flight from Hodeida to Sana'a International Airport (SAH), Yemen.

PROBABLE CAUSE: "The probable cause of the undercowl engine fire was the burn-through of the combustion chamber inner liner from the accumulation of dust that became molten during operating and infiltrated the combustion chamber thermal barrier coating causing it to spall off and accelerate normal thermal distress. The burn-though of the combustion chamber caused downstream hardware to experience higher than designed temperatures that resulted in mechanical and thermal distress to the point that the low pressure turbine case began to melt. Contributing to the combustion chamber failure was the operators' failure to do recommended borescope inspections that would have detected the combustion chamber distress and hence the removal of the engine before it was allowed to progress to the point that the
combustion and turbine sections of the engine failed."

Sources:

NTSB

History of this aircraft

Other occurrences involving this aircraft
1 January 1970 7O-FAB Felix Airways 0 San'a International Airport (SAH) min
Security issues

Revision history:

Date/timeContributorUpdates
02-Oct-2015 17:09 harro Added
16-Mar-2016 13:01 harro Updated [Narrative]

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