20140922017309A

Accident · Substantial damage

FAA accident report · Schweizer 269C · Grand Forks, ND · September 22, 2014

Date
September 22, 2014 · 15:05 local
Place
Grand Forks, ND
Phase of flight
Landing: Touchdown
Operating rules
Pilot school (Part 141)
Operator
OG5S
Damage
Substantial damage
Aircraft
N1675U
NTSB investigation
NTSBCEN14CA513
Reported as
Schweizer 269C
Reported engine
Lycoming HIO-360 series
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Commercial pilot, flight instructor
Pilot’s flight hours
3,804 total1,175 in this make and model83 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.

Weather was VMC with light to moderate headwinds for the runway. The flight was an instruction flight to prepare a commercial pilot for an additional flight instructor rating. The pilot and flight instructor were coming to the end of the flight period was near conclusion and the student had conducted a successful touchdown 180 degree autorotation previously. They briefed for next 180 degree autorotation and preceded to enter the maneuver at approximately 1000 feet AGL. The instructor noted coming out of the turn the student was 5 knots slow. The student lowered the nose to accelerate and lined up with the intended touchdown runway. The maneuver was described as normal until the flare. Flight instructor stated that the student's flare was a little more nose high than normal but should have be within normal given the winds. Both pilots then noticed a high sink rate. Both pilots heard a bang and only the flight instructor felt the impact. The aircraft leveled and landed skids level. The flight instructor stated that impact on the landing was not much harder than a normal landing. Both pilots felt a high frequency vibration and both looked back to the tail section. Neither pilot observed and damage but could see the tailboom vibrating laterally. The flight instructor initiated an emergency shutdown. Damage to the vertical stab, horizontal stab, tail boom and drive shaft subsequently ensued.

As the FAA filed it

WEATHER WAS VMC WITH LIGHT TO MODERATE HEADWINDS FOR THE RUNWAY. THE FLIGHT WAS AN INSTRUCTION FLIGHT TO PREPARE A COMMERCIAL PILOT FOR AN ADDITIONAL FLIGHT INSTRUCTOR RATING. THE PILOT AND FLIGHT INSTRUCTOR WERE COMING TO THE END OF THE FLIGHT PERIOD WAS NEAR CONCLUSION AND THE STUDENT HAD CONDUCTED A SUCCESSFUL TOUCHDOWN 180 DEGREE AUTOROTATION PREVIOUSLY. THEY BRIEFED FOR NEXT 180 DEGREE AUTOROTATION AND PRECEDED TO ENTER THE MANEUVER AT APPROXIMATELY 1000 FEET AGL. THE INSTRUCTOR NOTED COMING OUT OF THE TURN THE STUDENT WAS 5 KNOTS SLOW. THE STUDENT LOWERED THE NOSE TO ACCELERATE AND LINED UP WITH THE INTENDED TOUCHDOWN RUNWAY. THE MANEUVER WAS DESCRIBED AS NORMAL UNTIL THE FLARE. FLIGHT INSTRUCTOR STATED THAT THE STUDENT'S FLARE WAS A LITTLE MORE NOSE HIGH THAN NORMAL BUT SHOULD HAVE BE WITHIN NORMAL GIVEN THE WINDS. BOTH PILOTS THEN NOTICED A HIGH SINK RATE. BOTH PILOTS HEARD A BANG AND ONLY THE FLIGHT INSTRUCTOR FELT THE IMPACT. THE AIRCRAFT LEVELED AND LANDED SKIDS LEVEL. THE FLIGHT INSTRUCTOR STATED THAT IMPACT ON THE LANDING WAS NOT MUCH HARDER THAN A NORMAL LANDING. BOTH PILOTS FELT A HIGH FREQUENCY VIBRATION AND BOTH LOOKED BACK TO THE TAIL SECTION. NEITHER PILOT OBSERVED AND DAMAGE BUT COULD SEE THE TAILBOOM VIBRATING LATERALLY. THE FLIGHT INSTRUCTOR INITIATED AN EMERGENCY SHUTDOWN. DAMAGE TO THE VERTICAL STAB, HORIZONTAL STAB, TAIL BOOM AND DRIVE SHAFT SUBSEQUENTLY ENSUED.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

Other reports on N1675U · 1

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