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LAX02FA214 · Cessna 310I

4 Jul 2002 · San Dimas, CA, United States

Cessna 310I · Accident: loss of engine power during initial climb

From Brackett Field (POC) to an unrecorded destination

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Event

NTSB case
LAX02FA214
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Completed
API-reported fatalities
4 · all aircraft and ground
Ground fatalities
2
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
General aviation
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

Cessna 310I

Aircraft type
Cessna 310
Category
Airplane
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N8145M
Operator
Unknown
Onboard fatalities
Unknown
Route
From Brackett Field (POC), La Verne, CATo not recorded
Aircraft age
Not recorded
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 91: General Aviation
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
Initial climb
First occurrenceThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Loss of engine power
Also codedOther events the NTSB coded in the sequence, such as a wire strike after a loss of power. Flight Findings uses them for its kinds of event. Glossary
Tree(s)
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Destroyed

Cause areas

  • Pilot in command › Aircraft control, not maintained
  • Reason for occurrence undetermined

Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.

NTSB narrative

The airplane impacted trees, terrain, and pedestrians after the pilot declared an emergency during takeoff from a nearby airport. Witnesses observed the airplane not climbing after takeoff and air traffic controllers heard the pilot declare mayday three times. The pilot did not elaborate on the emergency situation. Witnesses observed the airplane turn left over the shoreline of a reservoir where it impacted a tree with its left wing. One witness stated the left propeller was not turning as fast as the right propeller and he heard the engines backfiring. Post-accident examination of the aircraft revealed no flight control anomalies. The left engine's top spark plugs were covered with black soot and the piston and cylinders were dark in appearance, indicative of an overly rich fuel/air mixture. The reason for the excessively rich mixture was not determined. The left engine was successfully test run twice following the accident, once utilizing the systems and plumbing in the airframe, and the second time in an instrumented test cell. Examination of the wreckage did find irregularities in the wiring circuits for both boost pumps and their associated cockpit switches; however, the relationship of these irregularities to the loss of power is uncertain. Review of the airplane owner's manual revealed the emergency procedures for a loss of engine power after takeoff called for the retraction of the landing gear and the feathering of the propeller to obtain the maximum climb performance. The landing gear was not retracted and the left propeller was not feathered. Eighteen months prior to the accident, the pilot failed his first attempt to obtain his multiengine airplane rating due to improper emergency procedures during engine failure operations after liftoff. The pilot's total time in the same make and model as the accident airplane is unclear.

Probable cause

the pilot's failure to maintain control of the airplane following a loss of power in one engine during takeoff. The reason for the loss of power in the left engine could not be determined. Contributing factors to the accident were the pilot's failure to retract the landing gear and to feather the inoperative engine propeller.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record LAX02FA214
Event ID
20020710X01083
Case number
LAX02FA214
Dataset
historical-pre2008
Source SHA-256
89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
Source notes (4)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: investigation status, coordinates. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: 45d34b24c7746605501a2ec49aeee2b42456f97c71a2915a9556c1d13383698a; retrieved 2026-09-20T19:57:54.841Z.