20140503010969I

Incident · Minor damage

FAA incident report · Glazier Patrick R SONEX · Greenville, SC · May 3, 2014

Date
May 3, 2014 · 19:33 local
Place
Greenville, SC
Airport
Greenville Downtown
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N390SG
Reported as
Glazier Patrick R Sonex
Reported engine
Revmaster R2200
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
4,574 total30 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.

After takeoff from runway 19 at gmu the engine started indicating a hot cylinder. The power was reduced and left turn was started toward runway 28 at gmu. Due to the low power setting the approach was lower than normal in the abbreviated pattern they were flying. The pilot (flying) at the time (privacy data omitted) was getting a biennial flight review, and was unfamiliar with the airport. The aircraft was in too close and the pilot (flying) could not find the runway while looking into the setting sun. At this time the instructor privacy data omitted took control of the aircraft and turned left to get back to the runway. privacy data omitted Then made an immediate right turn to line up with the runway. They were low enough coming out of the right turn that they had already started to flare. They landed hard with significant drift to the left but were successful at gaining directional control on roll out. Began braking and the aircraft started a gentle left turn. Full rudder would not stop the turn and it got sharper. The aircraft existed the runway to the left but skid sliding to to the right. The only damage is to the right main gear gear lower strut to axle attach point.

The Sonex only has a single brake handle that applies pressure to both brakes, so you could not use differential braking.

As the FAA filed it

AFTER TAKEOFF FROM RUNWAY 19 AT GMU THE ENGINE STARTED INDICATING A HOT CYLINDER. THE POWER WAS REDUCED AND LEFT TURN WAS STARTED TOWARD RUNWAY 28 AT GMU. DUE TO THE LOW POWER SETTING THE APPROACH WAS LOWER THAN NORMAL IN THE ABBREVIATED PATTERN THEY WERE FLYING. THE PILOT (FLYING) AT THE TIME (^PRIVACY DATA OMITTED^) WAS GETTING A BIENNIAL FLIGHT REVIEW, AND WAS UNFAMILIAR WITH THE AIRPORT. THE AIRCRAFT WAS IN TOO CLOSE AND THE PILOT (FLYING) COULD NOT FIND THE RUNWAY WHILE LOOKING INTO THE SETTING SUN. AT THIS TIME THE INSTRUCTOR ^PRIVACY DATA OMITTED^ TOOK CONTROL OF THE AIRCRAFT AND TURNED LEFT TO GET BACK TO THE RUNWAY. ^PRIVACY DATA OMITTED^ THEN MADE AN IMMEDIATE RIGHT TURN TO LINE UP WITH THE RUNWAY. THEY WERE LOW ENOUGH COMING OUT OF THE RIGHT TURN THAT THEY HAD ALREADY STARTED TO FLARE. THEY LANDED HARD WITH SIGNIFICANT DRIFT TO THE LEFT BUT WERE SUCCESSFUL AT GAINING DIRECTIONAL CONTROL ON ROLL OUT. BEGAN BRAKING AND THE AIRCRAFT STARTED A GENTLE LEFT TURN. FULL RUDDER WOULD NOT STOP THE TURN AND IT GOT SHARPER. THE AIRCRAFT EXISTED THE RUNWAY TO THE LEFT BUT SKID SLIDING TO TO THE RIGHT. THE ONLY DAMAGE IS TO THE RIGHT MAIN GEAR GEAR LOWER STRUT TO AXLE ATTACH POINT.

THE SONEX ONLY HAS A SINGLE BRAKE HANDLE THAT APPLIES PRESSURE TO BOTH BRAKES, SO YOU COULD NOT USE DIFFERENTIAL BRAKING.

Other reports on N390SG · 1

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