20110924020849I

Incident · Minor damage

FAA incident report · Piper PA-28R-200 · Stuart, FL · September 24, 2011

Date
September 24, 2011 · 12:52 local
Place
Stuart, FL
Airport
Witham Field
Phase of flight
Landing: Touchdown
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N55660
Reported as
Piper PA-28R-200
Reported engine
Lycoming I0-360 series
People aboard
1
Fatal injuries
0
Other injuries
0
Pilot’s certificate
Private pilot
Pilot’s flight hours
1,928 total450 in this make and model30 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 stated he became distracted on entering the sua tfc pattern by a new GPS receiver he recently had installed, and forgot to lower the gear prior to landing. Had auto-deploy system overridden because of some previous stall/spin accidents attributed to inadvertent actuation of the gear and subsequent reduction in airspeed. Asked if he heard the gear horn or saw the flashing amber gear advisory light, and stated he had a noise-cancelling headset on, and only heard the horn while in the flare just prior to touchdown. Did not see the warning light. §61.56 current. Pilot further stated he had just modified his pattern procedures to not drop the gear at 120 KTS, but to delay so as to not put a high aerodynamic load on the gear, per his CFI. Gear speed is 150 KTS. Intend to counsel CFI. Counseled airman during the interview, no further action intended.

As the FAA filed it

PILOT STATED HE BECAME DISTRACTED ON ENTERING THE SUA TFC PATTERN BY A NEW GPS RECEIVER HE RECENTLY HAD INSTALLED, AND FORGOT TO LOWER THE GEAR PRIOR TO LANDING. HAD AUTO-DEPLOY SYSTEM OVERRIDDEN BECAUSE OF SOME PREVIOUS STALL/SPIN ACCIDENTS ATTRIBUTED TO INADVERTENT ACTUATION OF THE GEAR AND SUBSEQUENT REDUCTION IN AIRSPEED. ASKED IF HE HEARD THE GEAR HORN OR SAW THE FLASHING AMBER GEAR ADVISORY LIGHT, AND STATED HE HAD A NOISE-CANCELLING HEADSET ON, AND ONLY HEARD THE HORN WHILE IN THE FLARE JUST PRIOR TO TOUCHDOWN. DID NOT SEE THE WARNING LIGHT. §61.56 CURRENT. PILOT FURTHER STATED HE HAD JUST MODIFIED HIS PATTERN PROCEDURES TO NOT DROP THE GEAR AT 120 KTS, BUT TO DELAY SO AS TO NOT PUT A HIGH AERODYNAMIC LOAD ON THE GEAR, PER HIS CFI. GEAR SPEED IS 150 KTS. INTEND TO COUNSEL CFI. COUNSELED AIRMAN DURING THE INTERVIEW, NO FURTHER ACTION INTENDED.

Other reports on N55660 · 3

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