19980613013409A

Accident · Substantial damage

FAA accident report · Piper J3C-65 · Midland, TX · June 13, 1998

Date
June 13, 1998 · 14:50 local
Place
Midland, TX
Airport
Skywest Inc Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N42559
NTSB investigation
NTSBFTW98LA265
Reported as
Piper J3C65
Reported engine
Continental C8512F
Fatal injuries
0
Pilot’s flight hours
7,211 total104 in this make and model36 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.

Acft crashed into a telephone pole on landing after encountering a strong crosswind. Midland, TX. (-23) pilot initiated go-around due to loss of directional control during landing as a result of a wind shift. As a/c became airborne, wind caused a/c to turn perpendicular to runway. A/c struck power pole, causing left wing to separated from fuselage. A/c came to rest upright 488 ft from runway. (.4)the commercial pilot lost control of the tailwheel equipped airplane when the wind shifted to a gusty tailwind during the landing roll. Witness observed the airplane execute a 'nice wheel landing on the centerline' of runway 16. After all 3 wheels were on the ground, the airplane started drifting to the left of the centerline. The left main wheel went off the pavement and as the right wing started to come up, the pilot advanced the engine to full power. The witness stated that he looked back at the windsock, he noticed that the winds had suddenly shifted from a quartering headwind, to a gusting quartering tailwind. The airplane cleared the airport's perimeter fence; however, the left wing of the airplane impacted a power line pole. The winds at the Midland international airport, located 9 nautical miles to the northwest were reported from 230 degrees at 11 knots. In the enclosed NTSB form 6120.1/2, the pilot reported that the winds were from the southwest at 15 knots, gusting to 20 knots.

As the FAA filed it

ACFT CRASHED INTO A TELEPHONE POLE ON LANDING AFTER ENCOUNTERING A STRONG CROSSWIND. MIDLAND, TX. (-23) PILOT INITIATED GO-AROUND DUE TO LOSS OF DIRECTIONAL CONTROL DURING LANDING AS A RESULT OF A WIND SHIFT. AS A/C BECAME AIRBORNE, WIND CAUSED A/C TO TURN PERPENDICULAR TO RUNWAY. A/C STRUCK POWER POLE, CAUSING LEFT WING TO SEPARATED FROM FUSELAGE. A/C CAME TO REST UPRIGHT 488 FT FROM RUNWAY. (.4)THE COMMERCIAL PILOT LOST CONTROL OF THE TAILWHEEL EQUIPPED AIRPLANE WHEN THE WIND SHIFTED TO A GUSTY TAILWIND DURING THE LANDING ROLL. WITNESS OBSERVED THE AIRPLANE EXECUTE A 'NICE WHEEL LANDING ON THE CENTERLINE' OF RUNWAY 16. AFTER ALL 3 WHEELS WERE ON THE GROUND, THE AIRPLANE STARTED DRIFTING TO THE LEFT OF THE CENTERLINE. THE LEFT MAIN WHEEL WENT OFF THE PAVEMENT AND AS THE RIGHT WING STARTED TO COME UP, THE PILOT ADVANCED THE ENGINE TO FULL POWER. THE WITNESS STATED THAT HE LOOKED BACK AT THE WINDSOCK, HE NOTICED THAT THE WINDS HAD SUDDENLY SHIFTED FROM A QUARTERING HEADWIND, TO A GUSTING QUARTERING TAILWIND. THE AIRPLANE CLEARED THE AIRPORT'S PERIMETER FENCE; HOWEVER, THE LEFT WING OF THE AIRPLANE IMPACTED A POWER LINE POLE. THE WINDS AT THE MIDLAND INTERNATIONAL AIRPORT, LOCATED 9 NAUTICAL MILES TO THE NORTHWEST WERE REPORTED FROM 230 DEGREES AT 11 KNOTS. IN THE ENCLOSED NTSB FORM 6120.1/2, THE PILOT REPORTED THAT THE WINDS WERE FROM THE SOUTHWEST AT 15 KNOTS, GUSTING TO 20 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.