The U.S. aircraft register, updated daily
Accidents · NTSB WPR17FA152 · Final report

Amateur-built PAZMANY PL 2 accident near El Monte, California, July 14, 2017

On July 14, 2017 at about 4:32 pm local time, a 1979 amateur-built PAZMANY PL 2, registered N186EJ, was substantially damaged in an accident during initial climb near El Monte, California (San Gabriel Valley airport). It was a personal flight under general aviation rules (Part 91). 1 person was killed. The weather was visual conditions (good weather).

The NTSB's probable cause their words, unchanged

A total loss of engine power due to fuel starvation for reasons that could not be determined based on the available evidence. Also causal was the pilot's decision to return to the runway following the loss of engine power, and his failure to maintain airspeed during the turn, which resulted in the airplane exceeding its critical angle of attack and experiencing an aerodynamic stall/spin.

Source: NTSB aviation accident database, copy made October 5, 2026. Docket and reports at the NTSB.

What the record shows

Date
July 14, 2017 · about 4:32 pm local time
Place
El Monte, California · San Gabriel Valley · map
Type
Accident
Injuries
1 person was killed.
Weather
visual conditions (good weather)
Aircraft
Amateur-built PAZMANY PL 2, built 1979
Registration
N186EJ · no longer on the register · serial 186
Damage
Substantial damage
Flight
Personal flight · general aviation rules (Part 91)

The NTSB's narrative final · quoted from the NTSB record

About 15 minutes after arriving at the airport, the private pilot departed on a local flight. A witness reported that, shortly after takeoff, the engine "sputtered and quit." The airplane appeared to continue climbing straight ahead to an altitude about 200 ft above ground level, then initiated a left turn as if attempting to return to the runway. The airplane reached an approximate 90° angle of bank and the nose dropped before the airplane descended almost vertically to ground contact, consistent with an aerodynamic stall/spin. Examination of the airframe and engine revealed no anomalies that would have precluded normal operation. The propeller did not exhibit indications of rotation at the time of impact. The fuel selector was set to the left tank position. Both left and right fuel tanks were breached and devoid of fuel; however, the asphalt surrounding the wreckage was discolored consistent with fuel spillage. The gascolator bowl contained some fuel; however, the carburetor bowl and accelerator pump well were devoid of fuel. Examination of the fuel system revealed no evidence of blockage that would have prevented fuel flow to the engine. The quantity and distribution of fuel on board the airplane at the time of the accident could not be determined; however, the lack of fuel in the carburetor bowl and accelerator pump is consistent with a fuel starvation event. The reason for the fuel starvation could not be determined based on the available information.  Following the loss of engine power, the pilot attempted to return to the runway; however, the airplane did not have sufficient altitude to complete the 180° turn. During the turn, the pilot failed to maintain sufficient airspeed, which resulted in the airplane exceeding its critical angle of attack and entering an aerodynamic stall and spin.

The complete narrative as the NTSB published it. The NTSB's docket holds the report as a PDF and any photographs, statements and other documents from the investigation.

The factual record from the NTSB's investigation tables, in plain English

What happened, in order

  1. Fuel starvation during initial climb defining event
  2. Loss of engine power (total) during initial climb
  3. Loss of control in flight during initial climb

The NTSB's findings

  • cause Aircraft › Fluids/misc hardware › Fluids › Fuel › Not specified
  • cause Personnel issues › Task performance › Use of equip/info › Aircraft control › Pilot
  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Airspeed › Not attained/maintained
  • cause Aircraft › Aircraft oper/perf/capability › Performance/control parameters › Angle of attack › Capability exceeded
  • cause Personnel issues › Action/decision › Info processing/decision › Decision making/judgment › Pilot

Pilot

  • Certificate: private
  • Ratings: multi-engine land; single-engine land; instrument: airplane; rotorcraft: helicopter
  • Flight time: 4,200 hours in all
  • Medical certificate: Class 2 (with waivers/limitations)
  • Seat: left
  • Injury: fatal

The aircraft

  • Last inspection: condition inspection, August 8, 2016; 451 hours since
  • Seats: 2
  • Landing gear: fixed
  • Engine: Lycoming O-320 SERIES (piston); 450 hours total

The flight

  • Departed from: EMT El Monte CA at 4:31 pm
  • Destination: EMT El Monte CA
  • Flight plan: none
  • Runway 19, 3,995 ft by 75 ft

Weather at the time

  • Light: daylight
  • Wind: from 230° at 5 knots
  • Visibility: 10 statute miles
  • Sky: clear
  • Temperature: 77°F (25°C), dew point 61°F (16°C)
  • Altimeter: 30.03 inHg
  • Observation at 4:45 pm from KEMT

Injuries

FatalSeriousMinorNone
Flight crew1

Documents from the investigation the NTSB's docket: the evidence folder behind the report

8 documents, released by the NTSB on February 27, 2018. View them here, or download them; the NTSB redacts some personal details before release, and this site shows the NTSB's own titles rather than its file names.

The same docket at the NTSB · documents without a copy here are fetched from the NTSB when you open them.

Everything on this page comes from the NTSB's public records. The narrative, probable cause and findings are the NTSB's own words; the coded tables behind the report are written out in plain English, with pilots' ages, home towns and medical details left out. The documents and photographs are the NTSB's docket, shown as the NTSB released them. This site's own text never names anyone involved. A preliminary report can change; the final report usually follows one to two years later, and the page is refreshed when it does.