No fatalities

Engine Power Loss Leads to Forced Landing and Nose-Over After Induction System Separation (N507SD)

Independence, MO, US

On May 20, 1998, a Cessna 182 (registration N507SD) operated by Charlotte Leach was involved in an aviation accident near Independence, MO. No fatalities were reported. Investigators recorded the probable cause as: A loss of engine power due to the separation of the induction system balance tube coupling from the intake manifold tube assembly. A related factor was the soft field. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive; 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 2026-07-04Data APIEditorial standards

A pilot experienced engine power loss at 4,000 feet, then a backfire and engine stoppage. She performed a forced landing in a field, hitting a fence post and nosing over. Examination revealed a separated induction system balance tube.

Pilot Report

The pilot reported that while descending through 4,000 feet mean sea level, the engine began losing power. She leveled off, engaged carburetor heat, and switched fuel tanks. According to her account, upon attempting to restart, the engine backfired and quit. She trimmed the airplane for best glide at 80 mph and headed directly for an airport located 2.5 miles away. When she was half a mile from the airport, she determined that she would not reach the runway and decided to land short. She set 10 degrees of flaps and touched down in a field. During the landing roll, the airplane struck a wooden fence post in the muddy terrain and nosed over.

Engine Examination

An examination of the engine disclosed that the induction system balance tube had separated from the intake manifold tube assembly. It was noted that the coupling of the induction system balance tube did not align properly with the intake manifold.

Test Run

A test run of the engine was conducted. During the initial test, the induction system balance tube coupling was left disconnected. The engine started but would only run when the throttle was continuously pumped. After connecting the balance tube coupling and restarting, the engine operated without requiring continuous throttle pumping. The engine was run up to 1,700 RPM and ran smoothly with no missing or backfiring. No other pre-impact mechanical anomalies were identified on the engine.

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Frequently asked questions

What happened in the 20 May 1998 Cessna 182 accident near Independence, MO?

A pilot experienced engine power loss at 4,000 feet, then a backfire and engine stoppage. She performed a forced landing in a field, hitting a fence post and nosing over. Examination revealed a separated induction system balance tube.

Were there any fatalities in the 20 May 1998 Cessna 182 accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 20 May 1998 involved a Cessna 182, registration N507SD, operated by Charlotte Leach, at Independence, MO.

What was the probable cause of the accident?

A loss of engine power due to the separation of the induction system balance tube coupling from the intake manifold tube assembly. A related factor was the soft field.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20001211X10015. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.