20030920026169A

Accident · Destroyed

FAA accident report · Braero HS125700A · Beaumont, TX · September 20, 2003

Date
September 20, 2003 · 18:54 local
Place
Beaumont, TX
Airport
Beaumont Municipal Airport
Phase of flight
Practice Training Manuevers
Operating rules
General operating rules (Part 91)
Operator
T8VA
Damage
Destroyed
Aircraft
N45BP
NTSB investigation
NTSBDEN03FA155
Reported as
Braero HS125700A
Reported engine
Garrett TFE731*
People aboard
3
Fatal injuries
3
Pilot’s flight hours
5,230 total1,300 in this make and model87 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) Aircraft destroyed and fatal injuries to all three pilots aboard. Several eyewitnesses described a flat spin of only several turns with rotation which stopped before impact. Evidence at the impact site is consistent with a near vertical impact on the belly of the aircraft. The main pieces of the cabin, aft fuselage, both engines, tail structure and cockpit roof were all found within 15 feet of the initial impact crater. All three landing gear legs were detached from the fuselage and were found buried in the mud in the initial impact crater. Evidence shows that the landing gear was extended and the flaps were in the "approach flap" position at the time of impact. Initial analysis of the ATC radar data shows that the Hawker had been on a northwest heading and level at approximately 5,000 feet MSL altitude for several minutes before radar contact was lost. The part 135 operator reported that the above listed two pilots and an additional pilot, (Mr. Ronald keith trahan - ATP 455390094) were onboard the Hawker and conducting pilot flight training in preparation for part 135 competency and proficiency tests scheduled to be conducted in this aircraft during the following week with part 135 proving tests to follow.

As the FAA filed it

(-23) AIRCRAFT DESTROYED AND FATAL INJURIES TO ALL THREE PILOTS ABOARD. SEVERAL EYEWITNESSES DESCRIBED A FLAT SPIN OF ONLY SEVERAL TURNS WITH ROTATION WHICH STOPPED BEFORE IMPACT. EVIDENCE AT THE IMPACT SITE IS CONSISTENT WITH A NEAR VERTICAL IMPACT ON THE BELLY OF THE AIRCRAFT. THE MAIN PIECES OF THE CABIN, AFT FUSELAGE, BOTH ENGINES, TAIL STRUCTURE AND COCKPIT ROOF WERE ALL FOUND WITHIN 15 FEET OF THE INITIAL IMPACT CRATER. ALL THREE LANDING GEAR LEGS WERE DETACHED FROM THE FUSELAGE AND WERE FOUND BURIED IN THE MUD IN THE INITIAL IMPACT CRATER. EVIDENCE SHOWS THAT THE LANDING GEAR WAS EXTENDED AND THE FLAPS WERE IN THE "APPROACH FLAP" POSITION AT THE TIME OF IMPACT. INITIAL ANALYSIS OF THE ATC RADAR DATA SHOWS THAT THE HAWKER HAD BEEN ON A NORTHWEST HEADING AND LEVEL AT APPROXIMATELY 5,000 FEET MSL ALTITUDE FOR SEVERAL MINUTES BEFORE RADAR CONTACT WAS LOST. THE PART 135 OPERATOR REPORTED THAT THE ABOVE LISTED TWO PILOTS AND AN ADDITIONAL PILOT, (MR. RONALD KEITH TRAHAN - ATP 455390094) WERE ONBOARD THE HAWKER AND CONDUCTING PILOT FLIGHT TRAINING IN PREPARATION FOR PART 135 COMPETENCY AND PROFICIENCY TESTS SCHEDULED TO BE CONDUCTED IN THIS AIRCRAFT DURING THE FOLLOWING WEEK WITH PART 135 PROVING TESTS TO FOLLOW.

NTSB investigation

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