20000911011229A

Accident · Substantial damage

FAA accident report · Amtr HORNET · Camp Verde, AZ · September 11, 2000

Date
September 11, 2000 · 08:30 local
Place
Camp Verde, AZ
Airport
Montezuma Heights Airport
Phase of flight
Forced/Precautionary Landing
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N707BD
NTSB investigation
NTSBLAX00LA350
Reported as
Amtr Hornet
Reported engine
HIRTH 2706*
People aboard
1
Fatal injuries
0
Pilot’s flight hours
12,000 total164 in this make and model65 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) See attached pilot statement (.4) on September 11, 2000, at 0830 hours mountain standard time, an experimental worgull Hornet, N707BD, experienced a loss of engine power and made a forced landing on interstate 17 after takeoff from the Montezuma airport, Camp Verde, Arizona. During the attempted landing, the airplane landed hard as the pilot was maneuvering to avoid obstacles. The airplane, owned and operated by the pilot under the provisions of 14 CFR part 91, sustained substantial damage. The airline transport pilot, the sole occupant, was not injured. Visual meteorological conditions prevailed for the personal flight. A flight plan had not been filed. The flight was originating at the time of the accident. In an interview with a safety board investigator, the pilot stated that a spark plug was found detached from the forward cylinder. He reported that the spark plug threads in the cylinder heads are made out of aluminum and the threaded portions of the spark plug barrels are made of steel. In the pilot's written statement to the safety board, he indicated that new spark plugs had been installed prior to the last flight, and that they were torqued to the manufacturer's recommendation of 110-inch pounds. He further indicated that there was deterioration of the threads inside of the cylinder head. He recommended a visual inspection of the spark plug threads and cylinder head threads during periodic spark plug removal. A federal aviation administration inspector examined the airplane at the owner's facilities on September 22, 2000. He noted that the threads on both cylinders showed evidence of wear and appeared flattened.

As the FAA filed it

(-23) SEE ATTACHED PILOT STATEMENT (.4) ON SEPTEMBER 11, 2000, AT 0830 HOURS MOUNTAIN STANDARD TIME, AN EXPERIMENTAL WORGULL HORNET, N707BD, EXPERIENCED A LOSS OF ENGINE POWER AND MADE A FORCED LANDING ON INTERSTATE 17 AFTER TAKEOFF FROM THE MONTEZUMA AIRPORT, CAMP VERDE, ARIZONA. DURING THE ATTEMPTED LANDING, THE AIRPLANE LANDED HARD AS THE PILOT WAS MANEUVERING TO AVOID OBSTACLES. THE AIRPLANE, OWNED AND OPERATED BY THE PILOT UNDER THE PROVISIONS OF 14 CFR PART 91, SUSTAINED SUBSTANTIAL DAMAGE. THE AIRLINE TRANSPORT PILOT, THE SOLE OCCUPANT, WAS NOT INJURED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED FOR THE PERSONAL FLIGHT. A FLIGHT PLAN HAD NOT BEEN FILED. THE FLIGHT WAS ORIGINATING AT THE TIME OF THE ACCIDENT. IN AN INTERVIEW WITH A SAFETY BOARD INVESTIGATOR, THE PILOT STATED THAT A SPARK PLUG WAS FOUND DETACHED FROM THE FORWARD CYLINDER. HE REPORTED THAT THE SPARK PLUG THREADS IN THE CYLINDER HEADS ARE MADE OUT OF ALUMINUM AND THE THREADED PORTIONS OF THE SPARK PLUG BARRELS ARE MADE OF STEEL. IN THE PILOT'S WRITTEN STATEMENT TO THE SAFETY BOARD, HE INDICATED THAT NEW SPARK PLUGS HAD BEEN INSTALLED PRIOR TO THE LAST FLIGHT, AND THAT THEY WERE TORQUED TO THE MANUFACTURER'S RECOMMENDATION OF 110-INCH POUNDS. HE FURTHER INDICATED THAT THERE WAS DETERIORATION OF THE THREADS INSIDE OF THE CYLINDER HEAD. HE RECOMMENDED A VISUAL INSPECTION OF THE SPARK PLUG THREADS AND CYLINDER HEAD THREADS DURING PERIODIC SPARK PLUG REMOVAL. A FEDERAL AVIATION ADMINISTRATION INSPECTOR EXAMINED THE AIRPLANE AT THE OWNER'S FACILITIES ON SEPTEMBER 22, 2000. HE NOTED THAT THE THREADS ON BOTH CYLINDERS SHOWED EVIDENCE OF WEAR AND APPEARED FLATTENED.

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 N707BD · 1

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