# Accident 20000901008379A: Piper PA46310P, South Lake Taho, CA, September 1, 2000 - Type: FAA accident report (Accident/Incident Data System), as reported - Date: September 1, 2000, 15:48 local time - Place: South Lake Taho, CA - Airport: Lake Tahoe - Damage: Destroyed - Phase of flight: Climb - Operating rules: General operating rules (Part 91) - Location: 38.8939° N, 119.9953° W: From the FAA - Nearby events: https://openairdocs.org/map.md?lat=38.8939&lon=-119.9953&mi=10 - Aircraft: N88AM, a cancelled registration (https://openairdocs.org/deregistered/N88AM-2001-04-12) (OpenAirDocs) - Registry model: Piper PA-46-310P (registry code 7104605, https://openairdocs.org/model/piper-pa-46-310p) (OpenAirDocs) - Reported make and model: PIPER PA46310P - Reported engine: CONT TSIO550C - People aboard: 4 - Fatal injuries: 4 - Pilot flight hours: 2,400 total, 130 in this make and model, 50 in the last 90 days - NTSB investigation: [NTSB LAX00FA322](https://openairdocs.org/ntsb/LAX00FA322) (OpenAirDocs) - FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/) - Page: https://openairdocs.org/incident/20000901008379A ## Narrative As the FAA filed it, in capitals; the FAA replaces private details with ^PRIVACY DATA OMITTED^. (-23) NOTE: ALL A/C AND PILOT TOTAL TIMES USED ON THIS FORM ARE APPROX. AT 1541 LOCAL TIME, N88AM REQUESTED TAXI CLEARANCE AND A/C DEPARTED TVL (SOUTH LANKE TAHOE) AIRPORT AT 1548 LOCAL TIME ON RUNWAY 180. A/C CLIMBED AND COMPLETED LEFT CROSSWIND DEPARTURE AND THEN TURNED ONTO LEFT DOWNWIND. A/C DIDN'T APPEAR TO BE GAINING ANY ALTITUDE. EYEWITNESSES SAID THAT A/C WAS APPROX. 100 FEET ABOVE GROUND WHEN NOSE OF A/C PITCHED UP 20 TO 30 DEGREES AND THEN PITCHED-DOWN AND A/C WENT INTO A SHARP LEFT NOSE DIVE, LEFT WING LOOKED TO BE 90 DEGREES STRAIGHT UP, AS IT PLUNGED INTO GROUND. (.4) HISTORY OF FLIGHT: ON SEPTEMBER 1, 2000, AT 1550 PACIFIC DAYLIGHT TIME, A PIPER PA-46-310P, N88AM, CRASHED INTO TREES AND TERRAIN WHILE TURNING DOWNWIND AFTER TAKEOFF FROM THE LAKE TAHOE AIRPORT, SOUTH LAKE TAHOE, CALIFORNIA. THE PILOT HAD REQUESTED AND BEEN APPROVED FOR A LEFT DOWNWIND DEPARTURE FROM RUNWAY 18 BY THE AIRPORT CONTROL TOWER OPERATOR. THE AIRPLANE WAS DESTROYED BY THE COLLISION SEQUENCE AND POST IMPACT FIRE. THE CERTIFICATED PRIVATE PILOT AND THREE PASSENGERS RECEIVED FATAL INJURIES. THE AIRPLANE WAS OWNED AND OPERATED BY THE PILOT AS A PERSONAL FLIGHT UNDER 14 CFR PART 91. THE FLIGHT ORIGINATED FROM SOUTH LAKE TAHOE AIRPORT AT 1549. MARGINAL VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME AND AN IFR FLIGHT PLAN HAD BEEN FILED BUT NOT ACTIVATED. THE ACCIDENT SITE WAS ABOUT 0.5 MILES FROM THE AIRPORT. THE AIRPORT ELEVATION WAS 6,264 FEET MSL. ACCORDING TO THE LAKE TAHOE CONTROL TOWER OPERATOR, AT 1542, A CLEARANCE TO TAXI TO RUNWAY 18 WAS ISSUED AFTER A TRANSMITTED REQUEST FROM THE PILOT. ADDITIONAL WIND AND ALTIMETER INFORMATION WAS GIVEN. AT 1548, THE PILOT REQUESTED TAKEOFF CLEARANCE AND A LEFT DOWNWIND DEPARTURE. THE CONTROLLER GAVE THE CLEARANCE TO TAKEOFF, APPROVED A LEFT DOWNWIND DEPARTURE, AND ISSUED WINDS AT 140 DEGREES AND 12 KNOTS. THE CONTROLLER THEN REPORTED HEARING AN ELT (EMERGENCY LOCATOR TRANSMITTER) TRANSMISSION AT 1550. A VERBAL TRANSMISSION FROM AN UNKNOWN SOURCE WAS ALSO RECEIVED AT 1550, AND IT COMMUNICATED THAT THERE WAS AN AIRCRAFT DOWN. SMOKE WAS OBSERVED 0.5 MILES SOUTHEAST OF THE AIRPORT. NO EMERGENCY TRANSMISSIONS FROM THE PILOT WERE REPORTED. WITNESSES ON THE GROUND REPORTED THE AIRPLANE LIFTED OFF ON THE 8,544-FOOT-LONG RUNWAY 18 ABEAM THE TERMINAL BUILDING AT MIDFIELD, THEN ALMOST IMMEDIATELY BEGIN A CROSSWIND TURN. THE TURN HAD CONTINUED NEARLY 180 DEGREES WHEN THE AIRPLANE DESCENDED SUDDENLY STRIKING SEVERAL PINE TREES BEFORE CRASHING BETWEEN TWO HOUSES. SEVERAL WITNESSES DESCRIBED THE AIRPLANE'S BANK ANGLE AT NEARLY 90 DEGREES. ADDITIONAL WITNESSES REPORTED SEEING THE AIRPLANE IN FLIGHT MOMENTS BEFORE IT CRASHED. AN EMPLOYEE OF ALLEGIANT AIR WHO WAS ON THE OBSERVATION DECK AT THE TERMINAL SAW THE AIRPLANE BANK HARD TO THE LEFT AND STATED THAT SHE THOUGHT IT WAS IN TROUBLE AND GOING TO STALL. "THE TURN WAS TOO STEEP [FOR HAVING JUST LIFTED OFF] AND THE AIRPLANE HAD BANKED BETTER THAN 45 DEGREES AS IT FLEW OVER THE WINDSOCK," SHE CONTINUED. A MECHANIC WHO WORKED ON THE AIRPLANE EARLIER THAT DAY WATCHED THE AIRPLANE TAKEOFF. HE REPORTED THE ENGINE SOUNDING LIKE IT WAS UNDER FULL POWER. TWO OTHER WITNESSES ALSO GAVE AN ACCOUNT OF THE ENGINE SOUND. ONE LIVED JUST OUTSIDE THE AIRPORT AND REPORTED HEARING THE LOUD ROAR OF THE ENGINE AS IT APPROACHED AND CRASHED THROUGH THE TREES. THE OTHER REPORTED HEARING THE ENGINE REVVED UP VERY LOUD AND HEARING AN INCONSISTENCY IN THE SOUND JUST BEFORE THE CRASH. ACCORDING TO THE WITNESS, THE ENGINE SPUTTERED AND THEN THE POWER RETURNED. THE STATEMENT ALSO INDICATED THAT THE WING ATTITUDE WAS VERTICAL INSTEAD OF HORIZONTAL BEFORE THE CRASH. ## The NTSB's investigation of this event (1) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB LAX00FA322](https://openairdocs.org/ntsb/LAX00FA322), Sep 1, 2000: Piper PA-46-310P (N88AM), So. Lake Tahoe, CA, destroyed, 4 fatal. Probable cause: The pilot's in-flight loss of control in the takeoff initial climb for undetermined reasons. ## Other reports on N88AM (3) Matched to the same aircraft by N-number and date. - [Incident 19950306007009I](https://openairdocs.org/incident/19950306007009I), Mar 6, 1995: Piper PA46310P (N88AM), Orlando, FL. Narrative: on March 6, 1995, a Piper PA-46-310P aircraft experienced an engine failure at 4000 feet MSL shortly after departing (mco) Orlando, Florida. The… - [Incident 19890128021329I](https://openairdocs.org/incident/19890128021329I), Jan 28, 1989: Piper PA46310P (N88AM), Cincinnati, OH, Minor damage. Nose gear collapsed after engine pre takeoff check. - [Incident 19870723065349I](https://openairdocs.org/incident/19870723065349I), Jul 23, 1987: Piper PA46310P (N88AM), Blue Ash, OH, Minor damage. The nosewheel collapsed as brakes were applied on rollout. Gear selector valve caused failure of actuator cable. From the FAA Accident/Incident Data System. Reports are matched to registry aircraft 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. For accidents, the NTSB's own investigation is the fuller record. --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.