20000830016929A

Accident · Substantial damage

FAA accident report · Bbavia 7BCM · Santa Fe, NM · August 30, 2000

Date
August 30, 2000 · 16:00 local
Place
Santa Fe, NM
Airport
Santa Fe County Municipal Airport
Phase of flight
Missed Approach IFR
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N66581
NTSB investigation
NTSBDEN00LA159
Reported as
Bbavia 7BCM
Reported engine
Continental C858F
People aboard
1
Fatal injuries
0
Pilot’s flight hours
6,500 total800 in this make and model85 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 August 30, 2000, at 1600 mountain daylight time, an Aeronca 7BCM, N66581, sustained substantial damage during a forced landing approximately 1/4 mile short of runway 20 at Santa Fe municipal airport, Santa Fe, new Mexico. The private pilot and sole occupant was not injured. The flight was a cross-country flight operating under title 14 CFR part 91 and no flight plan was filed. Visual meteorological conditions prevailed. The flight departed dumas, Texas, at 1200. According to the FAA inspector who responded to the accident, the flight was on final approach to land on runway 20 when the pilot applied carburetor heat about 1/4 mile from the runway and attempted to apply power. The engine did not respond and the aircraft sank below the runway height (runway 20 is on top of a hill). The pilot attempted to land on a dirt road that ran perpendicular to the runway, but ended up landing in a soft dirt field. According to the pilot, when the aircraft touched down in the soft terrain, the main landing gear was sheared off and the chrome-moly tube frame was twisted. In addition, the wing attach points on the fuselage were twisting the wings forward and down. Additionally, the windscre en was cracked and one propeller blade suffered tip damage. Examination of the engine by a mechanic provided evidence that the carburetor needle valve had stuck in the closed position. The reason for the valve sticking could not be determined. (-23)on final (approx 3 miles out) began descent to runway, applied carburetor heat, approaching runway (1/4 mile), attempted to apply power, no response from engine, a/c was sinking below runway height, (runway 20 on top of slight rise). Turned in an attempt to land on a dirt road running perpendicular to runway, landed instead in soft dirt field, hit dirt mound which removed landing gear and bent tip of one propeller blade. No injuries, no passengers. Pilot was positioning a/c to las vegas, NV for owner privacy data omittedflight origination was pensacola, FL.

As the FAA filed it

(.4)ON AUGUST 30, 2000, AT 1600 MOUNTAIN DAYLIGHT TIME, AN AERONCA 7BCM, N66581, SUSTAINED SUBSTANTIAL DAMAGE DURING A FORCED LANDING APPROXIMATELY 1/4 MILE SHORT OF RUNWAY 20 AT SANTA FE MUNICIPAL AIRPORT, SANTA FE, NEW MEXICO. THE PRIVATE PILOT AND SOLE OCCUPANT WAS NOT INJURED. THE FLIGHT WAS A CROSS-COUNTRY FLIGHT OPERATING UNDER TITLE 14 CFR PART 91 AND NO FLIGHT PLAN WAS FILED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED. THE FLIGHT DEPARTED DUMAS, TEXAS, AT 1200. ACCORDING TO THE FAA INSPECTOR WHO RESPONDED TO THE ACCIDENT, THE FLIGHT WAS ON FINAL APPROACH TO LAND ON RUNWAY 20 WHEN THE PILOT APPLIED CARBURETOR HEAT ABOUT 1/4 MILE FROM THE RUNWAY AND ATTEMPTED TO APPLY POWER. THE ENGINE DID NOT RESPOND AND THE AIRCRAFT SANK BELOW THE RUNWAY HEIGHT (RUNWAY 20 IS ON TOP OF A HILL). THE PILOT ATTEMPTED TO LAND ON A DIRT ROAD THAT RAN PERPENDICULAR TO THE RUNWAY, BUT ENDED UP LANDING IN A SOFT DIRT FIELD. ACCORDING TO THE PILOT, WHEN THE AIRCRAFT TOUCHED DOWN IN THE SOFT TERRAIN, THE MAIN LANDING GEAR WAS SHEARED OFF AND THE CHROME-MOLY TUBE FRAME WAS TWISTED. IN ADDITION, THE WING ATTACH POINTS ON THE FUSELAGE WERE TWISTING THE WINGS FORWARD AND DOWN. ADDITIONALLY, THE WINDSCRE EN WAS CRACKED AND ONE PROPELLER BLADE SUFFERED TIP DAMAGE. EXAMINATION OF THE ENGINE BY A MECHANIC PROVIDED EVIDENCE THAT THE CARBURETOR NEEDLE VALVE HAD STUCK IN THE CLOSED POSITION. THE REASON FOR THE VALVE STICKING COULD NOT BE DETERMINED. (-23)ON FINAL (APPROX 3 MILES OUT) BEGAN DESCENT TO RUNWAY, APPLIED CARBURETOR HEAT, APPROACHING RUNWAY (1/4 MILE), ATTEMPTED TO APPLY POWER, NO RESPONSE FROM ENGINE, A/C WAS SINKING BELOW RUNWAY HEIGHT, (RUNWAY 20 ON TOP OF SLIGHT RISE). TURNED IN AN ATTEMPT TO LAND ON A DIRT ROAD RUNNING PERPENDICULAR TO RUNWAY, LANDED INSTEAD IN SOFT DIRT FIELD, HIT DIRT MOUND WHICH REMOVED LANDING GEAR AND BENT TIP OF ONE PROPELLER BLADE. NO INJURIES, NO PASSENGERS. PILOT WAS POSITIONING A/C TO LAS VEGAS, NV FOR OWNER ^PRIVACY DATA O^FLIGHT ORIGINATION WAS PENSACOLA, FL.

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 N66581 · 1

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