20200908014049I

Incident · No damage

FAA incident report · Rockwell International 690A · Pocatello, ID · September 8, 2020

Date
September 8, 2020 · 15:40 local
Place
Pocatello, ID
Phase of flight
Takeoff: Climb Out
Operating rules
General operating rules (Part 91)
Operator
V8ZA
Damage
No damage
Aircraft
N112EE
Reported as
Rockwell International 690A
Reported engine
AiResearch TPE331-10T
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Airline transport
Pilot’s flight hours
19,908 total

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.

The PIC of the incident aircraft stated the aircraft was blown out of its chocks and the rudder gust lock was dislodged after a night of severe winds at Pocatello regional airport. The PIC had maintenance personell inspect the aircraft for wind damage and, finding no apparent damage, the aircraft was released for flight. On the date of the incident, the aircraft was dispatched on a 14 CFR § 91 fire fighting mission with the PIC and air attack mission controller on board. Once airborne and climbing through approximately 700' AGL, the PIC noted a complete loss of rudder control, declared an emergency and, using differential engine power for yaw control, returned to land uneventfully. After inspection and tear-down, maintenance personnel determined all of the rivets securing the rudder control torque tube to the mounting collar had been sheared in the previous night's wind storm.

As the FAA filed it

THE PIC OF THE INCIDENT AIRCRAFT STATED THE AIRCRAFT WAS BLOWN OUT OF ITS CHOCKS AND THE RUDDER GUST LOCK WAS DISLODGED AFTER A NIGHT OF SEVERE WINDS AT POCATELLO REGIONAL AIRPORT. THE PIC HAD MAINTENANCE PERSONELL INSPECT THE AIRCRAFT FOR WIND DAMAGE AND, FINDING NO APPARENT DAMAGE, THE AIRCRAFT WAS RELEASED FOR FLIGHT. ON THE DATE OF THE INCIDENT, THE AIRCRAFT WAS DISPATCHED ON A 14 CFR § 91 FIRE FIGHTING MISSION WITH THE PIC AND AIR ATTACK MISSION CONTROLLER ON BOARD. ONCE AIRBORNE AND CLIMBING THROUGH APPROXIMATELY 700' AGL, THE PIC NOTED A COMPLETE LOSS OF RUDDER CONTROL, DECLARED AN EMERGENCY AND, USING DIFFERENTIAL ENGINE POWER FOR YAW CONTROL, RETURNED TO LAND UNEVENTFULLY. AFTER INSPECTION AND TEAR-DOWN, MAINTENANCE PERSONNEL DETERMINED ALL OF THE RIVETS SECURING THE RUDDER CONTROL TORQUE TUBE TO THE MOUNTING COLLAR HAD BEEN SHEARED IN THE PREVIOUS NIGHT'S WIND STORM.