20190320001699A

Accident · Substantial damage

FAA accident report · Piper PA-28-140 · Savannah, GA · March 20, 2019

Date
March 20, 2019 · 15:06 local
Place
Savannah, GA
Airport
Savannah/Hilton Head International
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N2667Q
NTSB investigation
NTSBGAA19CA176
Reported as
Piper PA-28-140
Reported engine
Lycoming 0-320 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
80 total78 in this make and model34 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.

On March 20, 2019 about 1506 eastern daylight time, a Piper cherokee, P-28-140, N2667Q, was substantially damaged after losing control on runway 01 during landing roll out and catching fire after the pilot attempted to restart the engine at the Savannah/Hilton Head International Airport (sav) Savannah, Georgia.

The flight departed summerville airport (dyb); summerville, south carolina at 1415, destined for sav after the pilot received his temporary airman certificate for private pilot earlier that afternoon. Day visual meteorological conditions prevailed, and no flight plan was filed for the personal flight, which was conducted under the provisions of 14 code of federal regulations part 91.

The PIC was landing on runway 01 with a 10 knot crosswind with 17 knot gusts. The aircraft POH states the maximum crosswind component in which the aeroplane has been demonstrated to be safe for take-off and landing is 17 knots at a tower height of 33 feet.

The private pilot was not injured.

Aircraft substained damage to the right hand wing tip and lower right hand outboard wing skin during landing and the propeller had damage to the blade tips from a pro strike.

PA-28-140 POH states engine fires during start are usually the result of overpriming, PIC attempted to start the engine when hot. Engine caught fire and the aircraft was substantially damaged as a result. Engine fire damage was observed to the left hand side of the engine compartment, nose wheel fairing, left seat cockpit floor, fuselage skin, and firewall.

As the FAA filed it

ON MARCH 20, 2019 ABOUT 1506 EASTERN DAYLIGHT TIME, A PIPER CHEROKEE, P-28-140, N2667Q, WAS SUBSTANTIALLY DAMAGED AFTER LOSING CONTROL ON RUNWAY 01 DURING LANDING ROLL OUT AND CATCHING FIRE AFTER THE PILOT ATTEMPTED TO RESTART THE ENGINE AT THE SAVANNAH/HILTON HEAD INTERNATIONAL AIRPORT (SAV) SAVANNAH, GEORGIA.

THE FLIGHT DEPARTED SUMMERVILLE AIRPORT (DYB); SUMMERVILLE, SOUTH CAROLINA AT 1415, DESTINED FOR SAV AFTER THE PILOT RECEIVED HIS TEMPORARY AIRMAN CERTIFICATE FOR PRIVATE PILOT EARLIER THAT AFTERNOON. DAY VISUAL METEOROLOGICAL CONDITIONS PREVAILED, AND NO FLIGHT PLAN WAS FILED FOR THE PERSONAL FLIGHT, WHICH WAS CONDUCTED UNDER THE PROVISIONS OF 14 CODE OF FEDERAL REGULATIONS PART 91.

THE PIC WAS LANDING ON RUNWAY 01 WITH A 10 KNOT CROSSWIND WITH 17 KNOT GUSTS. THE AIRCRAFT POH STATES THE MAXIMUM CROSSWIND COMPONENT IN WHICH THE AEROPLANE HAS BEEN DEMONSTRATED TO BE SAFE FOR TAKE-OFF AND LANDING IS 17 KNOTS AT A TOWER HEIGHT OF 33 FEET.

THE PRIVATE PILOT WAS NOT INJURED.

AIRCRAFT SUBSTAINED DAMAGE TO THE RIGHT HAND WING TIP AND LOWER RIGHT HAND OUTBOARD WING SKIN DURING LANDING AND THE PROPELLER HAD DAMAGE TO THE BLADE TIPS FROM A PRO STRIKE.

PA-28-140 POH STATES ENGINE FIRES DURING START ARE USUALLY THE RESULT OF OVERPRIMING, PIC ATTEMPTED TO START THE ENGINE WHEN HOT. ENGINE CAUGHT FIRE AND THE AIRCRAFT WAS SUBSTANTIALLY DAMAGED AS A RESULT. ENGINE FIRE DAMAGE WAS OBSERVED TO THE LEFT HAND SIDE OF THE ENGINE COMPARTMENT, NOSE WHEEL FAIRING, LEFT SEAT COCKPIT FLOOR, FUSELAGE SKIN, AND FIREWALL.

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 N2667Q · 2

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