19991002038259A

Accident · Substantial damage

FAA accident report · Piper PA-12 · Las Cruces, NM · October 2, 1999

Date
October 2, 1999 · 07:50 local
Place
Las Cruces, NM
Airport
Las Cruces International Airport
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N2493M
NTSB investigation
NTSBDEN00LA003
Reported as
Piper PA12
Reported engine
Lycoming O235C
People aboard
2
Fatal injuries
0
Pilot’s flight hours
348 total348 in this make and model1 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.

(.4) On October 2, 1999, approximately 0750 mountain daylight time, a Piper PA-12, n 2493M, registered to and operated by the pilot, was substantially damaged when it veered off the side of the runway while landing at Las Cruces International Airport, Las Cruces, new Mexico. The private pilot and his private pilot certificated passenger were not injured. Visual meteorological conditions prevailed, and no flight plan had been filed for the personal flight being conducted under title 14 CFR part 91. The flight originated at el paso, Texas, approximately 0730. The pilot said that while on final approach to runway 26, he noticed that engine power remained too high even though the throttle had been retarded completely. He made a go around. On the second approach to the same runway, he noticed engine power was still too high with the throttle closed. He initiated a second go around and when the airplane was 50 feet above the ground, he slowly moved the mixture control towards idle cutoff "to decrease power." The airplane touched down at high speed and, according to the pilot, directional control was lost when he became distracted, and the airplane ground looped to the right. The left wing buckled when it struck the runway, and the side loads tore off the left main landing gear and damaged the right main landing gear. The pilot later reported the clamp that secures the throttle sleeve to the throttle housing had come loose, allowing the sleeve (not the cable) to move when the throttle control was operated.

As the FAA filed it

(.4) ON OCTOBER 2, 1999, APPROXIMATELY 0750 MOUNTAIN DAYLIGHT TIME, A PIPER PA-12, N 2493M, REGISTERED TO AND OPERATED BY THE PILOT, WAS SUBSTANTIALLY DAMAGED WHEN IT VEERED OFF THE SIDE OF THE RUNWAY WHILE LANDING AT LAS CRUCES INTERNATIONAL AIRPORT, LAS CRUCES, NEW MEXICO. THE PRIVATE PILOT AND HIS PRIVATE PILOT CERTIFICATED PASSENGER WERE NOT INJURED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED, AND NO FLIGHT PLAN HAD BEEN FILED FOR THE PERSONAL FLIGHT BEING CONDUCTED UNDER TITLE 14 CFR PART 91. THE FLIGHT ORIGINATED AT EL PASO, TEXAS, APPROXIMATELY 0730. THE PILOT SAID THAT WHILE ON FINAL APPROACH TO RUNWAY 26, HE NOTICED THAT ENGINE POWER REMAINED TOO HIGH EVEN THOUGH THE THROTTLE HAD BEEN RETARDED COMPLETELY. HE MADE A GO AROUND. ON THE SECOND APPROACH TO THE SAME RUNWAY, HE NOTICED ENGINE POWER WAS STILL TOO HIGH WITH THE THROTTLE CLOSED. HE INITIATED A SECOND GO AROUND AND WHEN THE AIRPLANE WAS 50 FEET ABOVE THE GROUND, HE SLOWLY MOVED THE MIXTURE CONTROL TOWARDS IDLE CUTOFF "TO DECREASE POWER." THE AIRPLANE TOUCHED DOWN AT HIGH SPEED AND, ACCORDING TO THE PILOT, DIRECTIONAL CONTROL WAS LOST WHEN HE BECAME DISTRACTED, AND THE AIRPLANE GROUND LOOPED TO THE RIGHT. THE LEFT WING BUCKLED WHEN IT STRUCK THE RUNWAY, AND THE SIDE LOADS TORE OFF THE LEFT MAIN LANDING GEAR AND DAMAGED THE RIGHT MAIN LANDING GEAR. THE PILOT LATER REPORTED THE CLAMP THAT SECURES THE THROTTLE SLEEVE TO THE THROTTLE HOUSING HAD COME LOOSE, ALLOWING THE SLEEVE (NOT THE CABLE) TO MOVE WHEN THE THROTTLE CONTROL WAS OPERATED.

NTSB investigation

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