20050511008309A

Accident · Substantial damage

FAA accident report · Robsin R44 · Gustine, CA · May 11, 2005

Date
May 11, 2005 · 09:45 local
Place
Gustine, CA
Airport
Gustine Airport
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N144SM
NTSB investigation
NTSBLAX05LA164
Reported as
Robsin R44
People aboard
2
Fatal injuries
0
Pilot’s flight hours
780 total197 in this make and model247 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) Maintenance had been performed on the helicopter as follows: 1. Annual inspection on 05/09/2005 at los banos, CA. Tt 1601.8 hrs. 2. Installed new bulkhead p/n C261-5 at top of mast fairing on 05/09/2005 at los banos, CA. Tt 1601.8 hrs. The installation of the mast fairing bulkhead required that the (2) two cyclic control rods (robinson-sleeve p/n A143-I) be removed. At the accident site the left sleeve was found to not be connected to the stationary swashplate. The rod end, p/n D173-1 was missing (broken) from the sleeve. The sleeve rod end to swashplane attaching bolt (NA6605-19) & nut (MS21042L5) were found on the runway near the helicopters last departure point prior to the accident.

As the FAA filed it

(-23) MAINTENANCE HAD BEEN PERFORMED ON THE HELICOPTER AS FOLLOWS: 1. ANNUAL INSPECTION ON 05/09/2005 AT LOS BANOS, CA. TT 1601.8 HRS. 2. INSTALLED NEW BULKHEAD P/N C261-5 AT TOP OF MAST FAIRING ON 05/09/2005 AT LOS BANOS, CA. TT 1601.8 HRS. THE INSTALLATION OF THE MAST FAIRING BULKHEAD REQUIRED THAT THE (2) TWO CYCLIC CONTROL RODS (ROBINSON-SLEEVE P/N A143-I) BE REMOVED. AT THE ACCIDENT SITE THE LEFT SLEEVE WAS FOUND TO NOT BE CONNECTED TO THE STATIONARY SWASHPLATE. THE ROD END, P/N D173-1 WAS MISSING (BROKEN) FROM THE SLEEVE. THE SLEEVE ROD END TO SWASHPLANE ATTACHING BOLT (NA6605-19) & NUT (MS21042L5) WERE FOUND ON THE RUNWAY NEAR THE HELICOPTERS LAST DEPARTURE POINT PRIOR TO THE ACCIDENT.

NTSB investigation

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