20190322001819I

Incident · Minor damage

FAA incident report · Piper PA-28-161 · El Cajon, CA · March 22, 2019

Date
March 22, 2019 · 15:00 local
Place
El Cajon, CA
Airport
Gillespie
Phase of flight
Maneuver
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N7938C
Reported as
Piper PA-28-161
Reported engine
Lycoming 0-320 series
People aboard
2
Fatal injuries
0
Other 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.

While practicing power on stalls, the crew experience an elevator failure. The CFI was the PIC. At apex of the power on stall, the crew heard a distinct "pop" and the pilot felt the pop, immediately suspected elevator failure and added nose down trim. The crew decided to return to the airport as soon as possible.

Maintenance discovered that the elevator control cable in the lower fuselage separated at the fwd end of the turnbucle where the cable swage end threads into the turnbucle cable swage end.

Contacted engineer regarding AD 2013-02-13 to inspect stabilator control system. Repetitive inspection not to exceed 2000 hours time in service or seven years, whichever occurs first, that AD was complied with. No other inspections required.

As the FAA filed it

WHILE PRACTICING POWER ON STALLS, THE CREW EXPERIENCE AN ELEVATOR FAILURE. THE CFI WAS THE PIC. AT APEX OF THE POWER ON STALL, THE CREW HEARD A DISTINCT "POP" AND THE PILOT FELT THE POP, IMMEDIATELY SUSPECTED ELEVATOR FAILURE AND ADDED NOSE DOWN TRIM. THE CREW DECIDED TO RETURN TO THE AIRPORT AS SOON AS POSSIBLE.

MAINTENANCE DISCOVERED THAT THE ELEVATOR CONTROL CABLE IN THE LOWER FUSELAGE SEPARATED AT THE FWD END OF THE TURNBUCLE WHERE THE CABLE SWAGE END THREADS INTO THE TURNBUCLE CABLE SWAGE END.

CONTACTED ENGINEER REGARDING AD 2013-02-13 TO INSPECT STABILATOR CONTROL SYSTEM. REPETITIVE INSPECTION NOT TO EXCEED 2000 HOURS TIME IN SERVICE OR SEVEN YEARS, WHICHEVER OCCURS FIRST, THAT AD WAS COMPLIED WITH. NO OTHER INSPECTIONS REQUIRED.