20020826026219I

Incident · Minor damage

FAA incident report · Bolkms BK117A4 · Bradenton, FL · August 26, 2002

Date
August 26, 2002 · 20:35 local
Place
Bradenton, FL
Phase of flight
Normal Cruise
Operating rules
Air taxi and commuter (Part 135)
Operator
R7MA
Damage
Minor damage
Aircraft
N528SF
NTSB investigation
NTSBMIA02IA160
Reported as
Bolkms BK117A4
Reported engine
Lycoming LTS101*
People aboard
5
Fatal injuries
0
Pilot’s flight hours
6,800 total1,200 in this make and model50 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.

(-23) On August 26, 2002, at 2035 EDT, a Eurocopter MBB-BK117, N528SF, registered to rocky mountain holdings LLC, experienced an in-flight engine fire and emergency landing on a road near Bradenton, Florida. The aircraft was on a part 135 air ambulance flight. Visual meteorological conditions prevailed at the time and no flight plan was filed. The aircraft sustained minor damage and the commercial rated pilot, flight nurse, and three passengers were not injured. The flight originated at naples, Florida on August 26, 2002 at 1950 hours. The pilot reported he had a loud explosion from the right side of the aircraft while in cruise flight and a simultaneous #2 engine fire light. He reported an indication of power loss in the #1 engine and the aircraft yawing several times from left to right. Engine fire procedures were executed. An autorotation landing was made at the intersection of I-275 and US41. The aircraft was shutdown and evacuated. The pilot extinguished the remaining fire prior to arrival of the fire department. The investigation disclosed failure of the #2 engine power turbine rotor blades. Half of one of the blades and a portion of another separated from the rotor assembly and exited through the tailpipe. The subsequent imbalance resulted in a fire that exited through the compressor inlet and through the turbine exhaust causing damage to the cowlings and engine compartment components. The fire was ingested by the #1 engine causing a power loss. The engine compartment design does not include a firewall between the engine compressor inlets to block the passage of flame from one inlet to the other.

As the FAA filed it

(-23) ON AUGUST 26, 2002, AT 2035 EDT, A EUROCOPTER MBB-BK117, N528SF, REGISTERED TO ROCKY MOUNTAIN HOLDINGS LLC, EXPERIENCED AN IN-FLIGHT ENGINE FIRE AND EMERGENCY LANDING ON A ROAD NEAR BRADENTON, FLORIDA. THE AIRCRAFT WAS ON A PART 135 AIR AMBULANCE FLIGHT. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME AND NO FLIGHT PLAN WAS FILED. THE AIRCRAFT SUSTAINED MINOR DAMAGE AND THE COMMERCIAL RATED PILOT, FLIGHT NURSE, AND THREE PASSENGERS WERE NOT INJURED. THE FLIGHT ORIGINATED AT NAPLES, FLORIDA ON AUGUST 26, 2002 AT 1950 HOURS. THE PILOT REPORTED HE HAD A LOUD EXPLOSION FROM THE RIGHT SIDE OF THE AIRCRAFT WHILE IN CRUISE FLIGHT AND A SIMULTANEOUS #2 ENGINE FIRE LIGHT. HE REPORTED AN INDICATION OF POWER LOSS IN THE #1 ENGINE AND THE AIRCRAFT YAWING SEVERAL TIMES FROM LEFT TO RIGHT. ENGINE FIRE PROCEDURES WERE EXECUTED. AN AUTOROTATION LANDING WAS MADE AT THE INTERSECTION OF I-275 AND US41. THE AIRCRAFT WAS SHUTDOWN AND EVACUATED. THE PILOT EXTINGUISHED THE REMAINING FIRE PRIOR TO ARRIVAL OF THE FIRE DEPARTMENT. THE INVESTIGATION DISCLOSED FAILURE OF THE #2 ENGINE POWER TURBINE ROTOR BLADES. HALF OF ONE OF THE BLADES AND A PORTION OF ANOTHER SEPARATED FROM THE ROTOR ASSEMBLY AND EXITED THROUGH THE TAILPIPE. THE SUBSEQUENT IMBALANCE RESULTED IN A FIRE THAT EXITED THROUGH THE COMPRESSOR INLET AND THROUGH THE TURBINE EXHAUST CAUSING DAMAGE TO THE COWLINGS AND ENGINE COMPARTMENT COMPONENTS. THE FIRE WAS INGESTED BY THE #1 ENGINE CAUSING A POWER LOSS. THE ENGINE COMPARTMENT DESIGN DOES NOT INCLUDE A FIREWALL BETWEEN THE ENGINE COMPRESSOR INLETS TO BLOCK THE PASSAGE OF FLAME FROM ONE INLET TO THE OTHER.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.