20180725024999I

Incident · Minor damage

FAA incident report · Cessna 172S · Cincinnati, OH · July 25, 2018

Date
July 25, 2018 · 18:30 local
Place
Cincinnati, OH
Phase of flight
Maneuver
Operating rules
Pilot school (Part 141)
Operator
K20S
Damage
Minor damage
Aircraft
N132RM
Reported as
Cessna 172S
Reported engine
Lycoming I0360 SER A&C
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.

An incident occurred with N132RM a CE-172 on Wednesday 7/25/2018. An instructor and his student were practicing forward slips in the practice area when they heard a loud bang. They found the rudder was stuck hard to the left. They were unable to correct the problem in the air and cross-controlled the airplane in order to get it back to luk. They did not declare an emergency and were able to land without incident. After landing it was found that the lead counterweight at the top of the rudder had come loose and slid forward when the rudder was full left. The counterweight was jammed between the rudder and the vertical stabilizer.

Reviewed by dws 09/07/2018

As the FAA filed it

AN INCIDENT OCCURRED WITH N132RM A CE-172 ON WEDNESDAY 7/25/2018. AN INSTRUCTOR AND HIS STUDENT WERE PRACTICING FORWARD SLIPS IN THE PRACTICE AREA WHEN THEY HEARD A LOUD BANG. THEY FOUND THE RUDDER WAS STUCK HARD TO THE LEFT. THEY WERE UNABLE TO CORRECT THE PROBLEM IN THE AIR AND CROSS-CONTROLLED THE AIRPLANE IN ORDER TO GET IT BACK TO LUK. THEY DID NOT DECLARE AN EMERGENCY AND WERE ABLE TO LAND WITHOUT INCIDENT. AFTER LANDING IT WAS FOUND THAT THE LEAD COUNTERWEIGHT AT THE TOP OF THE RUDDER HAD COME LOOSE AND SLID FORWARD WHEN THE RUDDER WAS FULL LEFT. THE COUNTERWEIGHT WAS JAMMED BETWEEN THE RUDDER AND THE VERTICAL STABILIZER.

REVIEWED BY DWS 09/07/2018