20060904022589A

Accident · Substantial damage

FAA accident report · Bbavia 7GCAA · Belmar/Farmingd, NJ · September 4, 2006

Date
September 4, 2006 · 11:00 local
Place
Belmar/Farmingd, NJ
Airport
Allaire Airport
Phase of flight
Climb
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N5501A
NTSB investigation
NTSBNYC06CA218
Reported as
Bbavia 7GCAA
Reported engine
Lycoming O320*
People aboard
1
Fatal injuries
0

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) The pilot stated that he took off from runway 32R and flew a right traffic pattern to pick up a banner. After capturing the banner he applied aft pressure on the stick to initiate a climb. He heard something snapped and the elevator control pressure was lost. He reached for the aft control stick located behind the forward seat, and there was no control pressure there either. He reduced the engine power and crashed landed the aircraft. The aircraft sustained significant damage to the propeller, engine cowling, fuselage, and tail wheel assembly. The investigation revealed that the elevator control cable had failed due to extensive corrosion.

As the FAA filed it

(-23) THE PILOT STATED THAT HE TOOK OFF FROM RUNWAY 32R AND FLEW A RIGHT TRAFFIC PATTERN TO PICK UP A BANNER. AFTER CAPTURING THE BANNER HE APPLIED AFT PRESSURE ON THE STICK TO INITIATE A CLIMB. HE HEARD SOMETHING SNAPPED AND THE ELEVATOR CONTROL PRESSURE WAS LOST. HE REACHED FOR THE AFT CONTROL STICK LOCATED BEHIND THE FORWARD SEAT, AND THERE WAS NO CONTROL PRESSURE THERE EITHER. HE REDUCED THE ENGINE POWER AND CRASHED LANDED THE AIRCRAFT. THE AIRCRAFT SUSTAINED SIGNIFICANT DAMAGE TO THE PROPELLER, ENGINE COWLING, FUSELAGE, AND TAIL WHEEL ASSEMBLY. THE INVESTIGATION REVEALED THAT THE ELEVATOR CONTROL CABLE HAD FAILED DUE TO EXTENSIVE CORROSION.

NTSB investigation

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

Other reports on N5501A · 1

Matched to the same aircraft by N-number and date.