19980203007289A

Accident · Substantial damage

FAA accident report · Cessna 172M · Bulverde, TX · February 3, 1998

Date
February 3, 1998 · 19:45 local
Place
Bulverde, TX
Airport
Bulverde Airpark Airport
Phase of flight
Final Approach
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N13711
NTSB investigation
NTSBFTW98LA118
Reported as
Cessna 172M
Reported engine
Lycoming O320E2D
People aboard
1
Fatal injuries
0
Pilot’s flight hours
118 total75 in this make and model20 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.

Total electric failure. Struck trees on night landing. Came to rest 100 ft short of runway in 100 ft tall trees. (.4)on ferurary 3, 1998, at 1945 central standard time, a Cessna 172M, airplane, N13711, struck trees during the landing approach near Bulverde, Texas, after experiencing a total electrical system failure. The airplane was operated by one of the co-owners under title 14 CFR part 91. The private pilot, sole occupant, was not injured, and the airplane sustained substantial damage. Visual meteorological conditions prevailed for the cross country flight and a flight plan was not filed. The flight departed boerne, Texas, approximately 15 minutes prior to the accident. During a personal telephone interview, conducted by the investigator-in-charge (iic), and on the pilot/operator aircraft accident report (NTSB form 6120.1/2), the pilot reported that the flight departed the boeme stage field airport for the return flight to Bulverde airpork airport. En route, the pilot obtained weather information by listening to the ATIS for san antonio, Texas. At Bulverde, the pilot executed a downwind entry for runway 16 and activated the pilot controlled runway lights. During the completion of the landing checklist, the pilot selected the flaps; however, the flaps did not extend. Subsequently, the pilot checked the electrical system by trying the landing lights; however, the landing lights did not operate. During the base to final turn, the cockpit panel lights began to dim, and the radio stopped operateing. The pilot bounced back into the air. The pilot initiated a go-around and entered the pattern for a landing on runway 34. The pilot used a flashlight for monitoring the cockpit instruments. When the airplane was on short final for runway 34, the pilot "put one hand on the throttle. I was on a flatter approach that I otherwise would have been if I had flaps, and was descending to touch down just beyond the threshold lights to allow as much runway possible for a faster than normal landing. Approximately 75-100 yards short of the end of the runway, the shadow of a tree came into view just above the glare shield immediately in front of the airplane." The airplane struck the tree and descended to the ground. The pilot and the FAA inspectors who examined the site reported that the trees along the wreckage distribution path were 70 to 100 teet tall. The airplane came to rest approximately 100 yards short of the runway. Structural damage ocurred to the propeller, engine mounts, firewall, wings, and empennage. The alternator circuit breaker was found "popped." On februrary 13, 1998, at alamo accessories, san antonio, Texas, the alternator, alternator circuit breaker, and the voltage regulator were examined under the surveillance of the FAA inspector. The FAA inspector reported that the alternator "worked fine", but the voltage regulator did not work. The "voltage regulator finally came on line, but after running for a while the voltage and amperage would drop off gradually to 'o' settings." Maintenance history for the electrical system components is unknown. The pilot's flight records were reviewed by the iic. The pilot had logged 4.4 hours of night flight time. (-23) see narrative #FTW98LA118.

As the FAA filed it

TOTAL ELECTRIC FAILURE. STRUCK TREES ON NIGHT LANDING. CAME TO REST 100 FT SHORT OF RUNWAY IN 100 FT TALL TREES. (.4)ON FERURARY 3, 1998, AT 1945 CENTRAL STANDARD TIME, A CESSNA 172M, AIRPLANE, N13711, STRUCK TREES DURING THE LANDING APPROACH NEAR BULVERDE, TEXAS, AFTER EXPERIENCING A TOTAL ELECTRICAL SYSTEM FAILURE. THE AIRPLANE WAS OPERATED BY ONE OF THE CO-OWNERS UNDER TITLE 14 CFR PART 91. THE PRIVATE PILOT, SOLE OCCUPANT, WAS NOT INJURED, AND THE AIRPLANE SUSTAINED SUBSTANTIAL DAMAGE. VISUAL METEOROLOGICAL CONDITIONS PREVAILED FOR THE CROSS COUNTRY FLIGHT AND A FLIGHT PLAN WAS NOT FILED. THE FLIGHT DEPARTED BOERNE, TEXAS, APPROXIMATELY 15 MINUTES PRIOR TO THE ACCIDENT. DURING A PERSONAL TELEPHONE INTERVIEW, CONDUCTED BY THE INVESTIGATOR-IN-CHARGE (IIC), AND ON THE PILOT/OPERATOR AIRCRAFT ACCIDENT REPORT (NTSB FORM 6120.1/2), THE PILOT REPORTED THAT THE FLIGHT DEPARTED THE BOEME STAGE FIELD AIRPORT FOR THE RETURN FLIGHT TO BULVERDE AIRPORK AIRPORT. EN ROUTE, THE PILOT OBTAINED WEATHER INFORMATION BY LISTENING TO THE ATIS FOR SAN ANTONIO, TEXAS. AT BULVERDE, THE PILOT EXECUTED A DOWNWIND ENTRY FOR RUNWAY 16 AND ACTIVATED THE PILOT CONTROLLED RUNWAY LIGHTS. DURING THE COMPLETION OF THE LANDING CHECKLIST, THE PILOT SELECTED THE FLAPS; HOWEVER, THE FLAPS DID NOT EXTEND. SUBSEQUENTLY, THE PILOT CHECKED THE ELECTRICAL SYSTEM BY TRYING THE LANDING LIGHTS; HOWEVER, THE LANDING LIGHTS DID NOT OPERATE. DURING THE BASE TO FINAL TURN, THE COCKPIT PANEL LIGHTS BEGAN TO DIM, AND THE RADIO STOPPED OPERATEING. THE PILOT BOUNCED BACK INTO THE AIR. THE PILOT INITIATED A GO-AROUND AND ENTERED THE PATTERN FOR A LANDING ON RUNWAY 34. THE PILOT USED A FLASHLIGHT FOR MONITORING THE COCKPIT INSTRUMENTS. WHEN THE AIRPLANE WAS ON SHORT FINAL FOR RUNWAY 34, THE PILOT "PUT ONE HAND ON THE THROTTLE. I WAS ON A FLATTER APPROACH THAT I OTHERWISE WOULD HAVE BEEN IF I HAD FLAPS, AND WAS DESCENDING TO TOUCH DOWN JUST BEYOND THE THRESHOLD LIGHTS TO ALLOW AS MUCH RUNWAY POSSIBLE FOR A FASTER THAN NORMAL LANDING. APPROXIMATELY 75-100 YARDS SHORT OF THE END OF THE RUNWAY, THE SHADOW OF A TREE CAME INTO VIEW JUST ABOVE THE GLARE SHIELD IMMEDIATELY IN FRONT OF THE AIRPLANE." THE AIRPLANE STRUCK THE TREE AND DESCENDED TO THE GROUND. THE PILOT AND THE FAA INSPECTORS WHO EXAMINED THE SITE REPORTED THAT THE TREES ALONG THE WRECKAGE DISTRIBUTION PATH WERE 70 TO 100 TEET TALL. THE AIRPLANE CAME TO REST APPROXIMATELY 100 YARDS SHORT OF THE RUNWAY. STRUCTURAL DAMAGE OCURRED TO THE PROPELLER, ENGINE MOUNTS, FIREWALL, WINGS, AND EMPENNAGE. THE ALTERNATOR CIRCUIT BREAKER WAS FOUND "POPPED." ON FEBRURARY 13, 1998, AT ALAMO ACCESSORIES, SAN ANTONIO, TEXAS, THE ALTERNATOR, ALTERNATOR CIRCUIT BREAKER, AND THE VOLTAGE REGULATOR WERE EXAMINED UNDER THE SURVEILLANCE OF THE FAA INSPECTOR. THE FAA INSPECTOR REPORTED THAT THE ALTERNATOR "WORKED FINE", BUT THE VOLTAGE REGULATOR DID NOT WORK. THE "VOLTAGE REGULATOR FINALLY CAME ON LINE, BUT AFTER RUNNING FOR A WHILE THE VOLTAGE AND AMPERAGE WOULD DROP OFF GRADUALLY TO 'O' SETTINGS." MAINTENANCE HISTORY FOR THE ELECTRICAL SYSTEM COMPONENTS IS UNKNOWN. THE PILOT'S FLIGHT RECORDS WERE REVIEWED BY THE IIC. THE PILOT HAD LOGGED 4.4 HOURS OF NIGHT FLIGHT TIME. (-23) SEE NARRATIVE #FTW98LA118.

NTSB investigation

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