19990228014099A

Accident · Substantial damage

FAA accident report · Piper PA-23-250 · Stuart, FL · February 28, 1999

Date
February 28, 1999 · 18:45 local
Place
Stuart, FL
Airport
Witham Field Airport
Phase of flight
Level Off Touchdown
Operating rules
Air taxi and commuter (Part 135)
Operator
VSAA
Damage
Substantial damage
Aircraft
N2313Z
NTSB investigation
NTSBMIA99LA096
Reported as
Piper PA23250
Reported engine
Lycoming IO540*
People aboard
4
Fatal injuries
0
Pilot’s flight hours
2,625 total62 in this make and model76 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.

(.19) On February 28, 1999, about 1845 eastern standard time, a Piper PA-23-250, N2313Z, registered to Stuart jet center, inc., experienced a hard landing at the Witham Field Airport, Stuart, Florida. Visual meteorological conditions prevailed at the time and an IFR flight plan was filed for the 14 CFR part 135, nonscheduled, domestic, passenger flight. The airplane was substantially damaged and the commercial-rated pilot and three passengers were not injured. The flight originated about 10 minutes earlier from the st. lucie county international airport, fort pierce, Florida. According to FAA personnel, the airplane bounced after touchdown and the pilot performed a go-around. He then returned and landed hard. Damage to the airplane consisted of buckling to the fuselage near the pilot's window, the copilot's seat back stop failed, and the entrance door was damaged. (-23) during landing at sua, the pilot encountered a wind gust immediately prior to touchdown, causing the aircraft to climb slightly. The pilot corrected by pushing the nose of the aircraft over which caused the nosewheel to contact the runway first. The main gear then contacted the runway asymmetrically which resulte d in the right gear and propeller striking the ground first. Followed by the left side. The pilot then made a go-around and subsequently landed the aircraft after flying by the tower to have the gear checked visually. Inspection of the aircraft revealed the right propeller had struck the runway, the entry door was buckled and both wing roots showed evidence of deformation. (.4) the pilot was advised that the wind at an airport near his destination airport was 250 degrees at 15 knots. The first leg of the flight was turbulent but that flight and the next 2 flights were uneventful. During the final leg, the pilot contacted the air traffic control tower and was advised that the wind was from 250 degrees at 18 knots with gusts to 25 knots. The pilot reported that during the flare to land, the nose pitched up then the airplane landed first on the nose landing gear. The airplane then bounced and the pilot performed a go-around. The flight returned for landing, and the airplane was landed in a three point attitude. During the landing roll, the pilot heard a sound from the nose landing gear and noted that the nose landing gear tire was flat. The airplane was secured on the runwa y. examination of the airplane by an FAA airworthiness inspector revealed that the left main wing spar was damaged, the top skin of the nose section was wrinkled, the balance weight for the nose landing gear tire was separated, and fuselage damage near the pilot's window was noted.

As the FAA filed it

(.19) ON FEBRUARY 28, 1999, ABOUT 1845 EASTERN STANDARD TIME, A PIPER PA-23-250, N2313Z, REGISTERED TO STUART JET CENTER, INC., EXPERIENCED A HARD LANDING AT THE WITHAM FIELD AIRPORT, STUART, FLORIDA. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME AND AN IFR FLIGHT PLAN WAS FILED FOR THE 14 CFR PART 135, NONSCHEDULED, DOMESTIC, PASSENGER FLIGHT. THE AIRPLANE WAS SUBSTANTIALLY DAMAGED AND THE COMMERCIAL-RATED PILOT AND THREE PASSENGERS WERE NOT INJURED. THE FLIGHT ORIGINATED ABOUT 10 MINUTES EARLIER FROM THE ST. LUCIE COUNTY INTERNATIONAL AIRPORT, FORT PIERCE, FLORIDA. ACCORDING TO FAA PERSONNEL, THE AIRPLANE BOUNCED AFTER TOUCHDOWN AND THE PILOT PERFORMED A GO-AROUND. HE THEN RETURNED AND LANDED HARD. DAMAGE TO THE AIRPLANE CONSISTED OF BUCKLING TO THE FUSELAGE NEAR THE PILOT'S WINDOW, THE COPILOT'S SEAT BACK STOP FAILED, AND THE ENTRANCE DOOR WAS DAMAGED. (-23) DURING LANDING AT SUA, THE PILOT ENCOUNTERED A WIND GUST IMMEDIATELY PRIOR TO TOUCHDOWN, CAUSING THE AIRCRAFT TO CLIMB SLIGHTLY. THE PILOT CORRECTED BY PUSHING THE NOSE OF THE AIRCRAFT OVER WHICH CAUSED THE NOSEWHEEL TO CONTACT THE RUNWAY FIRST. THE MAIN GEAR THEN CONTACTED THE RUNWAY ASYMMETRICALLY WHICH RESULTE D IN THE RIGHT GEAR AND PROPELLER STRIKING THE GROUND FIRST. FOLLOWED BY THE LEFT SIDE. THE PILOT THEN MADE A GO-AROUND AND SUBSEQUENTLY LANDED THE AIRCRAFT AFTER FLYING BY THE TOWER TO HAVE THE GEAR CHECKED VISUALLY. INSPECTION OF THE AIRCRAFT REVEALED THE RIGHT PROPELLER HAD STRUCK THE RUNWAY, THE ENTRY DOOR WAS BUCKLED AND BOTH WING ROOTS SHOWED EVIDENCE OF DEFORMATION. (.4) THE PILOT WAS ADVISED THAT THE WIND AT AN AIRPORT NEAR HIS DESTINATION AIRPORT WAS 250 DEGREES AT 15 KNOTS. THE FIRST LEG OF THE FLIGHT WAS TURBULENT BUT THAT FLIGHT AND THE NEXT 2 FLIGHTS WERE UNEVENTFUL. DURING THE FINAL LEG, THE PILOT CONTACTED THE AIR TRAFFIC CONTROL TOWER AND WAS ADVISED THAT THE WIND WAS FROM 250 DEGREES AT 18 KNOTS WITH GUSTS TO 25 KNOTS. THE PILOT REPORTED THAT DURING THE FLARE TO LAND, THE NOSE PITCHED UP THEN THE AIRPLANE LANDED FIRST ON THE NOSE LANDING GEAR. THE AIRPLANE THEN BOUNCED AND THE PILOT PERFORMED A GO-AROUND. THE FLIGHT RETURNED FOR LANDING, AND THE AIRPLANE WAS LANDED IN A THREE POINT ATTITUDE. DURING THE LANDING ROLL, THE PILOT HEARD A SOUND FROM THE NOSE LANDING GEAR AND NOTED THAT THE NOSE LANDING GEAR TIRE WAS FLAT. THE AIRPLANE WAS SECURED ON THE RUNWA Y. EXAMINATION OF THE AIRPLANE BY AN FAA AIRWORTHINESS INSPECTOR REVEALED THAT THE LEFT MAIN WING SPAR WAS DAMAGED, THE TOP SKIN OF THE NOSE SECTION WAS WRINKLED, THE BALANCE WEIGHT FOR THE NOSE LANDING GEAR TIRE WAS SEPARATED, AND FUSELAGE DAMAGE NEAR THE PILOT'S WINDOW WAS NOTED.

NTSB investigation

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