20140515007179A

Accident · Substantial damage

FAA accident report · Kalman George LANCAIR 360 · Grand Canyon, AZ · May 15, 2014

Date
May 15, 2014 · 17:50 local
Place
Grand Canyon, AZ
Airport
Grand Canyon National Park Air
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N521SH
NTSB investigation
NTSBWPR14CA193
Reported as
Kalman George Lancair 360
Reported engine
Lycoming I0360 SER A&C
People aboard
2
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
550 total40 in this make and model20 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.

Initial report stated that N521SH skidded 1800FT down rwy 3 at gcn after a blown tire and came to rest off the right side of rwy in the median.

Inspector recieved a written statement from PIC airman privacy data omitted stating the following:

"I was cleared for runway 03 by the kgcn tower and flew a right-hand pattern as instructed. There was little wind and visibility was good. I moved the flaps to 10 degrees, lowered the landing gear, and then moved the flaps to 40 degrees on downwind according to standard practice for this plane. On final, I established 80 KTS and carried that speed over the runway numbers. Since I was over the runway at the proper speed, I cut engine power to idle and flared above the runway. I think I flared higher than normal, and I held a steady pitch attitude. As the airspeed decreased, the airplane made a sharper than expected drop to the runway resulting in a hard landing. I believe part of the landing gear broke at that point because I lost directional control, and the plane skidded off the right side of the runway into a grassy area."

Inspector statement:

The weather conditoin at the time of the accident were; wind was 31008KTS and clr. Speaking with PIC privacy data omitted he also stated that weather was not a factor.

Reviewing photos from the accident of the damage to the landing gear; there is buckling of the main struts and a damage actuator. This damage concurrs with the PIC statement of having a hard landing.

There does not appear to be any other factors that contributed to the accident.

As the FAA filed it

INITIAL REPORT STATED THAT N521SH SKIDDED 1800FT DOWN RWY 3 AT GCN AFTER A BLOWN TIRE AND CAME TO REST OFF THE RIGHT SIDE OF RWY IN THE MEDIAN.

INSPECTOR RECIEVED A WRITTEN STATEMENT FROM PIC AIRMAN ^PRIVACY DATA OMITTED^ STATING THE FOLLOWING:

"I WAS CLEARED FOR RUNWAY 03 BY THE KGCN TOWER AND FLEW A RIGHT-HAND PATTERN AS INSTRUCTED. THERE WAS LITTLE WIND AND VISIBILITY WAS GOOD. I MOVED THE FLAPS TO 10 DEGREES, LOWERED THE LANDING GEAR, AND THEN MOVED THE FLAPS TO 40 DEGREES ON DOWNWIND ACCORDING TO STANDARD PRACTICE FOR THIS PLANE. ON FINAL, I ESTABLISHED 80 KTS AND CARRIED THAT SPEED OVER THE RUNWAY NUMBERS. SINCE I WAS OVER THE RUNWAY AT THE PROPER SPEED, I CUT ENGINE POWER TO IDLE AND FLARED ABOVE THE RUNWAY. I THINK I FLARED HIGHER THAN NORMAL, AND I HELD A STEADY PITCH ATTITUDE. AS THE AIRSPEED DECREASED, THE AIRPLANE MADE A SHARPER THAN EXPECTED DROP TO THE RUNWAY RESULTING IN A HARD LANDING. I BELIEVE PART OF THE LANDING GEAR BROKE AT THAT POINT BECAUSE I LOST DIRECTIONAL CONTROL, AND THE PLANE SKIDDED OFF THE RIGHT SIDE OF THE RUNWAY INTO A GRASSY AREA."

INSPECTOR STATEMENT:

THE WEATHER CONDITOIN AT THE TIME OF THE ACCIDENT WERE; WIND WAS 31008KTS AND CLR. SPEAKING WITH PIC ^PRIVACY DATA OMITTED^ HE ALSO STATED THAT WEATHER WAS NOT A FACTOR.

REVIEWING PHOTOS FROM THE ACCIDENT OF THE DAMAGE TO THE LANDING GEAR; THERE IS BUCKLING OF THE MAIN STRUTS AND A DAMAGE ACTUATOR. THIS DAMAGE CONCURRS WITH THE PIC STATEMENT OF HAVING A HARD LANDING.

THERE DOES NOT APPEAR TO BE ANY OTHER FACTORS THAT CONTRIBUTED TO THE ACCIDENT.

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 N521SH · 1

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