19940721031609I

Incident · Minor damage

FAA incident report · Bell 206B · El Cajon, CA · July 21, 1994

Date
July 21, 1994 · 16:00 local
Place
El Cajon, CA
Airport
Gillespie Field Airport
Phase of flight
Pwr Off Run Land (Autorotation
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N2750F
Reported as
Bell 206B
People aboard
2
Fatal injuries
0
Pilot’s flight hours
2,750 total350 in this make and model15 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.

Narrative: on July 21, 1994, Bell helicopter, model 206, N2750F, prepared to depart Gillespie airport (see), El Cajon, California on a local maintenance test flight. Immediately following take-off, while in transitioning to forward flight, all cyclic lateral control input was lost, resulting in a hard landing incident. Damage to the aircraft was minor and the pilot and passenger were not injured.. Post incident investigation revealed that prior to the incident flight, the cyclic lateral control rod had been removed from the swash plate assembly to access and repair an oil leak. Following repair, the lateral control rod attachment bolt was not re-installed, and this was not discovered during pre-flight inspection. This incident is under investigation privacy data omitted this incident did not involve a NMAC or pilot deviation.

As the FAA filed it

NARRATIVE: ON JULY 21, 1994, BELL HELICOPTER, MODEL 206, N2750F, PREPARED TO DEPART GILLESPIE AIRPORT (SEE), EL CAJON, CALIFORNIA ON A LOCAL MAINTENANCE TEST FLIGHT. IMMEDIATELY FOLLOWING TAKE-OFF, WHILE IN TRANSITIONING TO FORWARD FLIGHT, ALL CYCLIC LATERAL CONTROL INPUT WAS LOST, RESULTING IN A HARD LANDING INCIDENT. DAMAGE TO THE AIRCRAFT WAS MINOR AND THE PILOT AND PASSENGER WERE NOT INJURED.. POST INCIDENT INVESTIGATION REVEALED THAT PRIOR TO THE INCIDENT FLIGHT, THE CYCLIC LATERAL CONTROL ROD HAD BEEN REMOVED FROM THE SWASH PLATE ASSEMBLY TO ACCESS AND REPAIR AN OIL LEAK. FOLLOWING REPAIR, THE LATERAL CONTROL ROD ATTACHMENT BOLT WAS NOT RE-INSTALLED, AND THIS WAS NOT DISCOVERED DURING PRE-FLIGHT INSPECTION. THIS INCIDENT IS UNDER INVESTIGATION ^PRIVACY DATA OMITTED^ THIS INCIDENT DID NOT INVOLVE A NMAC OR PILOT DEVIATION.