20000204020379I

Incident

FAA incident report · Piper PA-28-161 · Orlando, FL · February 4, 2000

Date
February 4, 2000 · 11:45 local
Place
Orlando, FL
Airport
Orlando Executive Airport
Phase of flight
Normal Cruise
Operating rules
General operating rules (Part 91)
Aircraft
N5680V
Reported as
Piper PA28161
People aboard
2
Fatal injuries
0
Pilot’s flight hours
12,000 total450 in this make and model10 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)During course of private pilot check ride, while demonstraing steep turns, pilot examiner ^priva^ heard a pop and felt stabilator control lose effectiveness. After determining that he had no primary elevator control. privacy data omitted Declared an emergency, then, using power and the elevator trim control, flew the aircraft to an uneventful alnding at Orlando Executive Airport (orl). An examination of the aircraft by an investigatior from the Orlando FSDO revealed the up elevator cable had broken at the swedged turnbuckle fitting on the forward cable, it broke on the unthreaded portion of the fitting, just out to the turnbuckle barrell.

As the FAA filed it

(-23)DURING COURSE OF PRIVATE PILOT CHECK RIDE, WHILE DEMONSTRAING STEEP TURNS, PILOT EXAMINER ^PRIVA^ HEARD A POP AND FELT STABILATOR CONTROL LOSE EFFECTIVENESS. AFTER DETERMINING THAT HE HAD NO PRIMARY ELEVATOR CONTROL. ^PRIVACY D^ DECLARED AN EMERGENCY, THEN, USING POWER AND THE ELEVATOR TRIM CONTROL, FLEW THE AIRCRAFT TO AN UNEVENTFUL ALNDING AT ORLANDO EXECUTIVE AIRPORT (ORL). AN EXAMINATION OF THE AIRCRAFT BY AN INVESTIGATIOR FROM THE ORLANDO FSDO REVEALED THE UP ELEVATOR CABLE HAD BROKEN AT THE SWEDGED TURNBUCKLE FITTING ON THE FORWARD CABLE, IT BROKE ON THE UNTHREADED PORTION OF THE FITTING, JUST OUT TO THE TURNBUCKLE BARRELL.

Other reports on N5680V · 1

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