19970517013929A

Accident · Substantial damage

FAA accident report · Piper PA-28R-201 · Las Vegas, NV · May 17, 1997

Date
May 17, 1997 · 15:40 local
Place
Las Vegas, NV
Airport
Henderson Sky Harbor Airport
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N38718
NTSB investigation
NTSBLAX97LA188
Reported as
Piper PA28R201
Reported engine
Lycoming IO360C1C6
People aboard
2
Fatal injuries
0
Pilot’s flight hours
111 total97 in this make and model3 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.

(.4)The pilot initiated an approach to runway 18 with the right wing low and landed on the right main gear. After the right tire touched down, the right wing came up and the aircraft veered to the left. The aircraft ran off the left side of the runway and struck a row of very large rocks that were alongside the runway. The main landing gear collapsed and the aircraft slid into a 8-foot rocky drop-off. The pilot stated that he did not have enough airspeed to attempt a go-around so he opted to allow the aircraft to run off the runway. The tower advised the pilot that surface winds were from 230 degrees at 15 knots, gusting to 25. The pilot operating handbook for the aircraft states the maximum demonstrated crosswind component is 17 knots. Considering that limitation, the maximum allowable component for a 50-degree crosswind was computed to be 19.15 knots.

As the FAA filed it

(.4)THE PILOT INITIATED AN APPROACH TO RUNWAY 18 WITH THE RIGHT WING LOW AND LANDED ON THE RIGHT MAIN GEAR. AFTER THE RIGHT TIRE TOUCHED DOWN, THE RIGHT WING CAME UP AND THE AIRCRAFT VEERED TO THE LEFT. THE AIRCRAFT RAN OFF THE LEFT SIDE OF THE RUNWAY AND STRUCK A ROW OF VERY LARGE ROCKS THAT WERE ALONGSIDE THE RUNWAY. THE MAIN LANDING GEAR COLLAPSED AND THE AIRCRAFT SLID INTO A 8-FOOT ROCKY DROP-OFF. THE PILOT STATED THAT HE DID NOT HAVE ENOUGH AIRSPEED TO ATTEMPT A GO-AROUND SO HE OPTED TO ALLOW THE AIRCRAFT TO RUN OFF THE RUNWAY. THE TOWER ADVISED THE PILOT THAT SURFACE WINDS WERE FROM 230 DEGREES AT 15 KNOTS, GUSTING TO 25. THE PILOT OPERATING HANDBOOK FOR THE AIRCRAFT STATES THE MAXIMUM DEMONSTRATED CROSSWIND COMPONENT IS 17 KNOTS. CONSIDERING THAT LIMITATION, THE MAXIMUM ALLOWABLE COMPONENT FOR A 50-DEGREE CROSSWIND WAS COMPUTED TO BE 19.15 KNOTS.

NTSB investigation

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