20140301001289A

Accident · Substantial damage

FAA accident report · Piper PA-11S · Marlboro, MA · March 1, 2014

Date
March 1, 2014 · 13:00 local
Place
Marlboro, MA
Airport
Marlboro Airport
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N5556H
NTSB investigation
NTSBERA14CA139
Reported as
Piper PA-11S
Reported engine
Continetal C90
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificates
Airline transport, flight instructor
Pilot’s flight hours
6,630 total23 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.

Pilot landed on runway 32 with winds gusting 15 KTS and steady 8 - 10 KTS. Upon touchdown the aircraft veered off to the left side of runway with propeller contacting pavement and aircraft hitting snow/ice bank approximately three feet high. Left main landing gear was sheared off and contacted left wing struts, which bent midway between fuselage and wing. The propeller tips were bent back approximately 3 -4 inches and lower left engine mount to firewall area is bent. Left wing strut to fuselage area bent at attach point and to the rear approximately 15 inches.

As the FAA filed it

PILOT LANDED ON RUNWAY 32 WITH WINDS GUSTING 15 KTS AND STEADY 8 - 10 KTS. UPON TOUCHDOWN THE AIRCRAFT VEERED OFF TO THE LEFT SIDE OF RUNWAY WITH PROPELLER CONTACTING PAVEMENT AND AIRCRAFT HITTING SNOW/ICE BANK APPROXIMATELY THREE FEET HIGH. LEFT MAIN LANDING GEAR WAS SHEARED OFF AND CONTACTED LEFT WING STRUTS, WHICH BENT MIDWAY BETWEEN FUSELAGE AND WING. THE PROPELLER TIPS WERE BENT BACK APPROXIMATELY 3 -4 INCHES AND LOWER LEFT ENGINE MOUNT TO FIREWALL AREA IS BENT. LEFT WING STRUT TO FUSELAGE AREA BENT AT ATTACH POINT AND TO THE REAR APPROXIMATELY 15 INCHES.

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 N5556H · 1

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