20091118051319I

Incident · Minor damage

FAA incident report · Mcdonnell D DC-9-87 · Wichita, KS · November 18, 2009

Date
November 18, 2009 · 19:20 local
Place
Wichita, KS
Airport
Mid-Continent
Phase of flight
Takeoff: Climb Out
Operating rules
Air carrier (Part 121)
Operator
WX0A
Damage
Minor damage
Aircraft
N952MA
Reported as
Mcdonnell D DC-9-87
Reported engine
Pratt And Whitney JT8D
People aboard
133
Fatal injuries
0
Other injuries
2
Pilot’s certificates
Airline transport, commercial pilot
Pilot’s flight hours
6,500 total1,500 in this make and model226 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

On November 18, 2009 flight 5813 departed runway 19R and at approximately 2000 feet AGL the flight crew heard a loud bang and the aircraft momentarily "lurched with very little yaw". The crew did not get a fire warning indication and by the time they were able to observe the engine instruments, they found the left engine RPM was winding down, but the exhaust gas temperature was approaching 800 degrees. The crew secured the left engine and contacted ict control tower to initiate a return to the airport. The crew accomplished the emergency check list and shut the fuel off to the engine. The aircraft landed on runway 19R at approximately 7:20 pm. After landing, the crew elected to come to a full stop on the runway. The tower then notified the crew that it appeared they had an engine exhaust duct fire. The crew used both fire extinguisher bottles on the left engine. And notified the cabin crew to emergency evacuate the passengers. After approximately 20 passengers were evacuated, the crew was notified the fire was extinguished, and the remaining passengers exited through the main cabin door, using portable stairs. Preliminary investigation revealed major damage to the left engine (no.1) third stage turbine wheel and support struts the failure was entirely contained inside the engine. No intake fan damage was found. It is speculated that the damage and fire were caused by internal engine failure.

As the FAA filed it

ON NOVEMBER 18, 2009 FLIGHT 5813 DEPARTED RUNWAY 19R AND AT APPROXIMATELY 2000 FEET AGL THE FLIGHT CREW HEARD A LOUD BANG AND THE AIRCRAFT MOMENTARILY "LURCHED WITH VERY LITTLE YAW". THE CREW DID NOT GET A FIRE WARNING INDICATION AND BY THE TIME THEY WERE ABLE TO OBSERVE THE ENGINE INSTRUMENTS, THEY FOUND THE LEFT ENGINE RPM WAS WINDING DOWN, BUT THE EXHAUST GAS TEMPERATURE WAS APPROACHING 800 DEGREES. THE CREW SECURED THE LEFT ENGINE AND CONTACTED ICT CONTROL TOWER TO INITIATE A RETURN TO THE AIRPORT. THE CREW ACCOMPLISHED THE EMERGENCY CHECK LIST AND SHUT THE FUEL OFF TO THE ENGINE. THE AIRCRAFT LANDED ON RUNWAY 19R AT APPROXIMATELY 7:20 PM. AFTER LANDING, THE CREW ELECTED TO COME TO A FULL STOP ON THE RUNWAY. THE TOWER THEN NOTIFIED THE CREW THAT IT APPEARED THEY HAD AN ENGINE EXHAUST DUCT FIRE. THE CREW USED BOTH FIRE EXTINGUISHER BOTTLES ON THE LEFT ENGINE. AND NOTIFIED THE CABIN CREW TO EMERGENCY EVACUATE THE PASSENGERS. AFTER APPROXIMATELY 20 PASSENGERS WERE EVACUATED, THE CREW WAS NOTIFIED THE FIRE WAS EXTINGUISHED, AND THE REMAINING PASSENGERS EXITED THROUGH THE MAIN CABIN DOOR, USING PORTABLE STAIRS.PRELIMINARY INVESTIGATION REVEALED MAJOR DAMAGE TO THE LEFT ENGINE (NO.1) THIRD STAGE TURBINE WHEEL AND SUPPORT STRUTS THE FAILURE WAS ENTIRELY CONTAINED INSIDE THE ENGINE. NO INTAKE FAN DAMAGE WAS FOUND. IT IS SPECULATED THAT THE DAMAGE AND FIRE WERE CAUSED BY INTERNAL ENGINE FAILURE.

Other reports on N952MA · 1

Matched to the same aircraft by N-number and date.