# Accident 20000102011429A: Cessna 172A, Dos Palos, CA, January 2, 2000 - Type: FAA accident report (Accident/Incident Data System), as reported - Date: January 2, 2000, 14:30 local time - Place: Dos Palos, CA - Damage: Substantial damage - Phase of flight: Roll-Out (Fixed Wing) - Operating rules: General operating rules (Part 91) - Location: 37.0703° N, 120.6308° W: From the FAA, an estimate near the named town, within about 3 miles - Nearby events: https://openairdocs.org/map.md?lat=37.0703&lon=-120.6308&mi=10 - Aircraft: N7249T, a cancelled registration (https://openairdocs.org/deregistered/N7249T-2002-09-17) (OpenAirDocs) - Registry model: Cessna 172A (registry code 2072404, https://openairdocs.org/model/cessna-172a) (OpenAirDocs) - Registry engine: Continental 0-300 series (registry code 17022, https://openairdocs.org/engine/continental-0-300-series) (OpenAirDocs) - Reported make and model: CESSNA 172A - Reported engine: CONT O300* - Fatal injuries: 0 - Pilot certificates: Student - Pilot flight hours: 64 total - NTSB investigation: [NTSB LAX00LA062](https://openairdocs.org/ntsb/LAX00LA062) (OpenAirDocs) - FAA source: FAA Aviation Safety Information Portal (https://asip.faa.gov/) - Page: https://openairdocs.org/incident/20000102011429A ## Narrative As the FAA filed it, in capitals; the FAA replaces private details with ^PRIVACY DATA OMITTED^. (-23) ON 1/2/2000, THE STUDENT DEPARTED MCE RW 30, CLIMBED TO 1500 MSL AND AT 80 IAS AND 2200 RPM, MADE A LEFT TURN AND DEPARTED IN A SOUTHEASTERLY DIRECTION. AT CRUISE FOR APPROX. 15 MINUTES, THE PILOT NOTICED THE AIRSPEED WAS STILL AT 80 IAS AND THE ENGINE 1800 RPM. THE PILOT APPLIED FULL THROTTLE BUT THE RPM DID NOT INCREASE. CARBURETOR HEAT WAS APPLIED TWICE AT SHORT INTERVALS AND RETURNED TO THE COLD POSITION WITHOUT ANY RESPONSE IN RPM. THE PILOT COULD NOT MAINTAIN LEVEL FLIGHT AND HAD LOST APPROX. 200 FT. AND THE AIRSPEED WAS DECAYING TO AROUND 60 IAS. THE A/C SLOWLY IMPACT A SOFT DIRT PLOWED FIELD ON THE NOSE GEAR, SHEARING OFF THE FORK AND WHELL FROM THE STRUT AND OVERTURNED. (.4)ON JANUARY 2, 2000, AT 1415 HOURS PACIFIC STANDARD TIME, A CESSNA 172A, N7249T, EXPERIENCED A PARTIAL LOSS OF ENGINE POWER AND CAME TO REST INVERTED AFTER MAKING AN EMERGENCY LANDING IN AN OPEN DIRT FIELD NEAR DOS PALOS, CALIFORNIA. THE AIRPLANE, OWNED AND OPERATED BY THE PILOT UNDER 14 CFR PART 91, SUSTAINED SUBSTANTIAL DAMAGE. THE STUDENT PILOT RECEIVED MINOR INJURIES. VISUAL METEOROLOGICAL CONDITIONS EXISTED FOR THE INSTRUCTIONAL FLIGHT TH AT HAD DEPARTED THE MERCED, CALIFORNIA, AIRPORT AT 1400. NO FLIGHT PLAN WAS FILED. IN AN INTERVIEW WITH A FEDERAL AVIATION ADMINISTRATION (FAA) INSPECTOR, THE STUDENT PILOT REPORTED THAT SHE HAD REFUELED THE AIRPLANE SEVERAL WEEKS PRIOR TO THE ACCIDENT FLIGHT. THE AIRPLANE WAS REFUELED WITH APPROXIMATELY 30 GALLONS, AND SHE HAD NOT FLOWN IT SINCE IT HAD BEEN REFUELED. THE PILOT STATED THAT DURING THE PREFLIGHT SHE VERIFIED THAT SHE HAD "IN EXCESS OF 15 GALLONS" OF FUEL IN EACH WING BY UTILIZING A GRADUATED FUEL GAGE. SHE THEN CHECKED FOR FUEL CONTAMINATION BY TAKING A SAMPLE FROM THE PORT OF EACH WING WITH NO DISCREPANCIES NOTED. SHE REPORTED THAT THERE WERE NO PROBLEMS ENCOUNTERED DURING THE RUN-UP TO THE DEPARTURE FOR MERCED. WHILE ENROUTE TO THE PRACTICE AREA, SHE PERFORMED SEVERAL PRACTICE TURNS. ABOUT 30 MINUTES INTO THE FLIGHT, SHE NOTED A LOSS OF ALTITUDE AND ADDED THROTTLE TO REGAIN ALTITUDE, BUT DID NOT RECEIVE A CORRESPONDING POWER INDICATION. SHE NOTED THE FUEL SELECTOR WAS IN THE BOTH POSITION AND ATTEMPTED TO TROUBLESHOOT THE PROBLEM BY SWITCHING TO THE LEFT AND THEN RIGHT FUEL TANK POSITIONS, AND APPLYING CARBURETOR HEAT. SHE STATED THAT THERE WAS NO CHANGE AN D THE RPM'S CONTINUED TO DROP. THE ENGINE INSTRUMENTS WERE CROSSCHECKED AND SHE REAPPLIED CARBURETOR HEAT WITH NO CHANGE. THE PILOT REPORTED THAT THE ENGINE WAS NOT RUNNING ROUGH OR SPUTTERING, IT WAS JUST NOT PRODUCING ENGOUGH POWER TO SUSTAIN FLIGHT. DURING THE LANDING ROLLOUT, THE NOSE GEAR DUG INTO THE PLOWED DIRT FIELD, COLLAPSED, AND THE AIRPLANE NOSED OVER AND CAME TO REST INVERTED. THE STUDENT PILOT INDICATED THAT SHE HAD PURCHASED THE ARIPLANE IN JUNE 1999, WITHOUT THE LOGBOOKS. THE AIRFRAME AND POWERPLANT (A&P) MECHANIC WHO PERFORMED THE ANNUAL INSPECTION OF THE AIRPLANE SENT A LETTER TO THE FORMER OWNER REQUESTING THE LOGBOOKS. THE FORMER OWNER RESPONDED BY INDICATING THAT THE LOGBOOKS HAD BEEN ACCIDENTALLY BURNED WITH THE TRASH. IN THE LAST ENTRY FOR THE ANNUAL PERFORMED ON JUNE 6, 1999, THE A&P MECHANIC INDICATES THAT THE CARBURTOR WAS REPLACED TO COMPLY WITH AIRWORTHINESS DIRECTIVES 72-06-05, 93-19-04, AND 98-01-06. AN ENGINE INSPECTION WAS CONDUCTED AT PLAIN PARTS IN PLEASANT GROVE, CALIFORNIA, ON FEBRUARY 9, 2000. IT WAS NOTED THAT THE RETAINING NUT THAT HOLDS IN PLACE THE SERRATED THROTTLE LEVER TO THE SERRATED STOP OF THE THROTTLE SHAFT OF THE CARBURETOR DID NOT HAVE A COTTER PIN. THE RETAINING NUT WAS FOUND LOOSE ON THE SHAFT, ALLOWING THE SERRATED PORTION OF THE THROTTLE LEVER TO NOT ENGAGE PROPERLY WITH THE SERRATED STOP OF THE THROTTLE SHAFT. ## 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 LAX00LA062](https://openairdocs.org/ntsb/LAX00LA062), Jan 2, 2000: Cessna 172A (N7249T), Dos Palos, CA, substantial damage. Probable cause: A partial loss of engine power due to the failure of maintenance personnel to properly install and safety the throttle arm to the carburetor throttle shaft. 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.