20080516838849A

Accident · Destroyed

FAA accident report · Hiller FH-1100 · Comstock, MI · May 16, 2008

Date
May 16, 2008 · 11:53 local
Place
Comstock, MI
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N5049F
NTSB investigation
NTSBCHI08FA132
Reported as
Hiller FH1100
Reported engine
Allison 250C18
People aboard
1
Fatal injuries
1
Pilot’s flight hours
2,006 total0 in this make and model6 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) At approximately 11:33 am local time, a fairchild Hiller helicopter FH-1100 crashed in a remote area called chipman preserve, near Comstock, Michigan. The sole occupant of the aircraft was the new owner and suffered fatal injuries. There was no post-crash fire. Subsequent investigation found no obvious possible reason for the crash and focused on the airworthiness of parts installed on the aircraft. During the on-scene investigation, FAA inspectors determined that there appeared to be fuel running through the fuel lines to the engine and the pilot had received in-flight instruction from a flight instructor in the previous few days. The possible cause of the accident continues to be under investigation with no possible reason immediately clear, though airworthiness of the helicopter is a focal point. The deceased pilot had just retired and had purchased the helicopter a day or two before but the bill of sale had not been processed by the FAA. He recently received dual instruction from a flight instructor who judged the airman's performance as satisfacotry. He had a third-class medical issued on may 9, 2008, which was under review by cami on the day of the fatal accident. However, results of the autopsy indicated death was caused by blunt force trauma and not physiology relating to any preexisting medical condition. The engine was crated and prepared for shipment for tear-down, per instructions from the NTSB. Though NTSB investigators were not on-scene, they assumed control of the investigation on may 17, 2008. FAA inspectors learned almost immediately that the aircraft had been involved in an on-going criminal investigation relating to the installation of possible unapproved parts. During a teleconference on may 18, 2008, an agreement was reached between the FAA, NTSB, and a law enforcement agencies involved that the NTSB accident investigation would proceed first.

As the FAA filed it

(-23) AT APPROXIMATELY 11:33 AM LOCAL TIME, A FAIRCHILD HILLER HELICOPTER FH-1100 CRASHED IN A REMOTE AREA CALLED CHIPMAN PRESERVE, NEAR COMSTOCK, MICHIGAN. THE SOLE OCCUPANT OF THE AIRCRAFT WAS THE NEW OWNER AND SUFFERED FATAL INJURIES. THERE WAS NO POST-CRASH FIRE. SUBSEQUENT INVESTIGATION FOUND NO OBVIOUS POSSIBLE REASON FOR THE CRASH AND FOCUSED ON THE AIRWORTHINESS OF PARTS INSTALLED ON THE AIRCRAFT. DURING THE ON-SCENE INVESTIGATION, FAA INSPECTORS DETERMINED THAT THERE APPEARED TO BE FUEL RUNNING THROUGH THE FUEL LINES TO THE ENGINE AND THE PILOT HAD RECEIVED IN-FLIGHT INSTRUCTION FROM A FLIGHT INSTRUCTOR IN THE PREVIOUS FEW DAYS. THE POSSIBLE CAUSE OF THE ACCIDENT CONTINUES TO BE UNDER INVESTIGATION WITH NO POSSIBLE REASON IMMEDIATELY CLEAR, THOUGH AIRWORTHINESS OF THE HELICOPTER IS A FOCAL POINT. THE DECEASED PILOT HAD JUST RETIRED AND HAD PURCHASED THE HELICOPTER A DAY OR TWO BEFORE BUT THE BILL OF SALE HAD NOT BEEN PROCESSED BY THE FAA. HE RECENTLY RECEIVED DUAL INSTRUCTION FROM A FLIGHT INSTRUCTOR WHO JUDGED THE AIRMAN'S PERFORMANCE AS SATISFACOTRY. HE HAD A THIRD-CLASS MEDICAL ISSUED ON MAY 9, 2008, WHICH WAS UNDER REVIEW BY CAMI ON THE DAY OF THE FATAL ACCIDENT. HOWEVER, RESULTS OF THE AUTOPSY INDICATED DEATH WAS CAUSED BY BLUNT FORCE TRAUMA AND NOT PHYSIOLOGY RELATING TO ANY PREEXISTING MEDICAL CONDITION. THE ENGINE WAS CRATED AND PREPARED FOR SHIPMENT FOR TEAR-DOWN, PER INSTRUCTIONS FROM THE NTSB. THOUGH NTSB INVESTIGATORS WERE NOT ON-SCENE, THEY ASSUMED CONTROL OF THE INVESTIGATION ON MAY 17, 2008. FAA INSPECTORS LEARNED ALMOST IMMEDIATELY THAT THE AIRCRAFT HAD BEEN INVOLVED IN AN ON-GOING CRIMINAL INVESTIGATION RELATING TO THE INSTALLATION OF POSSIBLE UNAPPROVED PARTS. DURING A TELECONFERENCE ON MAY 18, 2008, AN AGREEMENT WAS REACHED BETWEEN THE FAA, NTSB, AND A LAW ENFORCEMENT AGENCIES INVOLVED THAT THE NTSB ACCIDENT INVESTIGATION WOULD PROCEED FIRST.

NTSB investigation

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