FLIGHT FINDINGSAVIATION OCCURRENCE MAP
Back to map

ERA23LA120 · Mooney M20C

28 Jan 2023 · Calhoun, GA, United States

Mooney M20C · Accident: loss of engine power (partial) during initial climb

From Tom B. David Field (CZL) to an unrecorded destination

Report a problem

Event

NTSB case
ERA23LA120
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
0 · all aircraft and ground
Ground fatalities
Unknown
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

Mooney M20C

Aircraft type
Mooney M20
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
N5587Q
Operator
Unknown
Onboard fatalities
Unknown
Route
From Tom B. David Field (CZL), Calhoun, GATo not recorded
Aircraft age
About 58 years (built 1965)
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
Defining eventThe 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 (partial)
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

  • Aircraft › Aircraft power plant
  • Personnel issues › Task performance

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

NTSB narrative

The pilot reported that the right magneto dropped 150 rpm when he and the flight instructor performed the engine runup. They leaned the fuel mixture and ran the engine up to about 1,700 rpm a couple of times until both magnetos dropped 125 rpm during the magneto checks. Once the magneto checks were normal, they initiated the takeoff. The pilot retracted the landing gear and a few moments later, while they were about 70 ft above the runway, there was a popping noise, the engine rpm went to nearly zero, and they began to lose altitude. They lowered the landing gear and touched down near the end of the runway. The airplane skidded off the end of the runway into the grass and slid into an earth embankment. The airplane then became airborne, rotated 90º to the left, and came to rest after a few hundred feet. The flight instructor then advised the pilot of flames near the pilot’s feet and they both exited the airplane. The airplane was destroyed by the postimpact fire. Examination of the engine revealed that the No. 3 bottom spark plug was not in the spark plug hole and was hanging from the ignition cable. The spark plug hole thread insert (Helicoil) was partially pulled from the spark plug hole. Examination of the spark plug revealed the lower three threads of the spark plug displayed absence of rust, but the threads located above them were rusty, and the bottom portion of the Helicoil was still intact. No other anomalies were discovered with the engine that would have precluded normal operation. Review of maintenance records indicated the engine had last been overhauled about 30 years ago, but this most probably did not contribute to the accident. The most recent annual inspection was completed about 2 months before the accident. Review of the logbook entry for the annual inspection indicated that during the annual, the spark plugs had been “removed, cleaned, inspected and installed.” The engine time in service between the last annual inspection and the last recorded entry in the engine logbook, which stated that the No. 2 cylinder spark plug was replaced was 1 hour. The investigation was not able to determine if the No. 3 cylinder spark plug was removed and reinstalled at that time. The accident occurred 14 days later. Therefore, it is likely that the No. 3 bottom spark plug was either not inserted all the way or it wasn’t properly torqued when it was installed during the annual inspection or most recent maintenance work.

Probable cause

A partial loss of engine power during the initial climb due to an improperly installed spark plug.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record ERA23LA120
Event ID
20230130106649
Case number
ERA23LA120
Dataset
full-current
Source SHA-256
5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
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, cause areas. 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: 6f97e42a6f3f3e816f9bbdd5e1c5f7b22bba7bad8304fd2a2de2925ef9148459; retrieved 2026-09-16T17:17:17.886Z.