20030705013739A

Accident · Substantial damage

FAA accident report · Snias AS350B · Temple Bay, AZ · July 5, 2003

Date
July 5, 2003 · 16:30 local
Place
Temple Bay, AZ
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
Air taxi and commuter (Part 135)
Operator
KBMA
Damage
Substantial damage
Aircraft
N2273A
NTSB investigation
NTSBLAX03LA225
Reported as
Snias AS350B
Fatal injuries
0
Pilot’s flight hours
1,209 total125 in this make and model76 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 July 5, 2003, at approximately 1630 hrs. While enroute to the grand canyon the pilot noticed a hot battery indication and elected to land as soon as possible. During the landing phase and after calling his company to alert them of the situation and his intentions, total electric failure occurred. At 100FT AGL the pilot noted engine noise reduced in pitch and tone, he immediately initiated autorotation. During the "flair" the tail rotor made contact with the ground, and after leveling the helicopter it bounced on touch down and rolled over on it's right side. (Pilot statement).

As the FAA filed it

(-23) ON JULY 5, 2003, AT APPROXIMATELY 1630 HRS. WHILE ENROUTE TO THE GRAND CANYON THE PILOT NOTICED A HOT BATTERY INDICATION AND ELECTED TO LAND AS SOON AS POSSIBLE. DURING THE LANDING PHASE AND AFTER CALLING HIS COMPANY TO ALERT THEM OF THE SITUATION AND HIS INTENTIONS, TOTAL ELECTRIC FAILURE OCCURRED. AT 100FT AGL THE PILOT NOTED ENGINE NOISE REDUCED IN PITCH AND TONE, HE IMMEDIATELY INITIATED AUTOROTATION. DURING THE "FLAIR" THE TAIL ROTOR MADE CONTACT WITH THE GROUND, AND AFTER LEVELING THE HELICOPTER IT BOUNCED ON TOUCH DOWN AND ROLLED OVER ON IT'S RIGHT SIDE. (PILOT STATEMENT).

NTSB investigation

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