20000818038639A

Accident · Substantial damage

FAA accident report · Cessna 172N · Flagstaff, AZ · August 18, 2000

Date
August 18, 2000 · 09:13 local
Place
Flagstaff, AZ
Airport
Flagstaff Pulliam Airport
Phase of flight
Go Round (Aborted VFR)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N2078E
NTSB investigation
NTSBLAX00LA305
Reported as
Cessna 172N
Reported engine
Lycoming O360*
People aboard
1
Fatal injuries
0
Pilot’s flight hours
80 total35 in this make and model2 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.

(-23)Pilot stated that he made a normal approach and after touch-down, ballooned slightly and added a small amount of power to correct. The a/c ballooned even more, so full power was added to initiate a balked landing (go-around), flaps were reduced one notch(to 20 degrees). A high sink rate developed, flaps were put back in, a hard landing resulted, the aircraft bounced again, control was lost and a distance remaining sign was stuck, resulting in substantial damage to the right wing spar and nosewheel. (.4)on August 18, 2000, about 0913 hours mountain standard time, a Cessna 172, N2078E, was substantially damaged during landing at Flagstaff, Arizona. The private pilot was not injured. The airplane was operated under the provisions of 14 CFR part 91 by glendale aviation, glendale, Arizona, and rented by the pilot for a local area personal flight. Visual meteorological conditions prevailed and no flight plan was filed. The flight originated at glendale on the morning of the accident about 0700. According to the Flagstaff control tower, the pilot was landing on runway 21 when directional control was lost and the airplane veered off the left side of the runway collidin g with a 5,000-foot remaining marker sign. The winds were reported as 220 degrees at 6 knots and the density altitude was 9,083 feet. The 80-hour private pilot reported that during the landing touchdown on runway 21, the airplane bounced and ballooned. He added power to soften the landing, but the airplane ballooned further. At that point, the pilot decided to perform a go-around. He applied full power and started climbing. The stall warning was going off, so he reduced the angle of attack. He removed the first notch of flaps, as directed by the balked landing procedure, and the airplane started settling back down quickly. He put the flaps back down, but the descent was not stopped. About the same time, the airplane was hit by a wind gust from the right, pushing the plane left. The pilot attempted to correct but was blown off the runway, colliding with a runway length remaining sign and subsequently, a ditch. He reported that he was number three to land on a long final with full flaps. He stated that there were no mechanical issues with the airplane.

As the FAA filed it

(-23)PILOT STATED THAT HE MADE A NORMAL APPROACH AND AFTER TOUCH-DOWN, BALLOONED SLIGHTLY AND ADDED A SMALL AMOUNT OF POWER TO CORRECT. THE A/C BALLOONED EVEN MORE, SO FULL POWER WAS ADDED TO INITIATE A BALKED LANDING (GO-AROUND), FLAPS WERE REDUCED ONE NOTCH(TO 20 DEGREES). A HIGH SINK RATE DEVELOPED, FLAPS WERE PUT BACK IN, A HARD LANDING RESULTED, THE AIRCRAFT BOUNCED AGAIN, CONTROL WAS LOST AND A DISTANCE REMAINING SIGN WAS STUCK, RESULTING IN SUBSTANTIAL DAMAGE TO THE RIGHT WING SPAR AND NOSEWHEEL. (.4)ON AUGUST 18, 2000, ABOUT 0913 HOURS MOUNTAIN STANDARD TIME, A CESSNA 172, N2078E, WAS SUBSTANTIALLY DAMAGED DURING LANDING AT FLAGSTAFF, ARIZONA. THE PRIVATE PILOT WAS NOT INJURED. THE AIRPLANE WAS OPERATED UNDER THE PROVISIONS OF 14 CFR PART 91 BY GLENDALE AVIATION, GLENDALE, ARIZONA, AND RENTED BY THE PILOT FOR A LOCAL AREA PERSONAL FLIGHT. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AND NO FLIGHT PLAN WAS FILED. THE FLIGHT ORIGINATED AT GLENDALE ON THE MORNING OF THE ACCIDENT ABOUT 0700. ACCORDING TO THE FLAGSTAFF CONTROL TOWER, THE PILOT WAS LANDING ON RUNWAY 21 WHEN DIRECTIONAL CONTROL WAS LOST AND THE AIRPLANE VEERED OFF THE LEFT SIDE OF THE RUNWAY COLLIDIN G WITH A 5,000-FOOT REMAINING MARKER SIGN. THE WINDS WERE REPORTED AS 220 DEGREES AT 6 KNOTS AND THE DENSITY ALTITUDE WAS 9,083 FEET. THE 80-HOUR PRIVATE PILOT REPORTED THAT DURING THE LANDING TOUCHDOWN ON RUNWAY 21, THE AIRPLANE BOUNCED AND BALLOONED. HE ADDED POWER TO SOFTEN THE LANDING, BUT THE AIRPLANE BALLOONED FURTHER. AT THAT POINT, THE PILOT DECIDED TO PERFORM A GO-AROUND. HE APPLIED FULL POWER AND STARTED CLIMBING. THE STALL WARNING WAS GOING OFF, SO HE REDUCED THE ANGLE OF ATTACK. HE REMOVED THE FIRST NOTCH OF FLAPS, AS DIRECTED BY THE BALKED LANDING PROCEDURE, AND THE AIRPLANE STARTED SETTLING BACK DOWN QUICKLY. HE PUT THE FLAPS BACK DOWN, BUT THE DESCENT WAS NOT STOPPED. ABOUT THE SAME TIME, THE AIRPLANE WAS HIT BY A WIND GUST FROM THE RIGHT, PUSHING THE PLANE LEFT. THE PILOT ATTEMPTED TO CORRECT BUT WAS BLOWN OFF THE RUNWAY, COLLIDING WITH A RUNWAY LENGTH REMAINING SIGN AND SUBSEQUENTLY, A DITCH. HE REPORTED THAT HE WAS NUMBER THREE TO LAND ON A LONG FINAL WITH FULL FLAPS. HE STATED THAT THERE WERE NO MECHANICAL ISSUES WITH THE AIRPLANE.

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 N2078E · 1

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