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Aviation safety reports, made easier to study

NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.

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NTSB Report

August 28, 1992 · Cessna 150M · N211AF

Temecula, CA

Overview

Report Status
Probable Cause
Event Type
Accident
Date
August 28, 1992
Injury Outcomes
2 injuries (2 minor injuries)
Location
Temecula, CA
Aircraft
Cessna 150M
Tail Number
N211AF
Operator
Armed Forces Flying Club
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
LAX92LA368

The instructor pilot said that during climb to cruise the engine suddenly quit completely with a loud noise. The instructor landed the aircraft in a field and the aircraft nosed over after colliding with a berm. Examination of the aircraft revealed that the rear dome of the left muffler had blown out. Scorching and exhaust stains were evident on the firewall to the rear of the muffler and wire bundles routed in this area were found burned with melted insulation noted. The 'P' leads for the magnetos were found routed in this wire bundle. Visual examination and electrical continuity checks of the 'P' leads revealed that the internal insulation had melted allowing the conductors to short within the wires. Examination of the muffler revealed severe internal erosion, with holes through the cabin heat shroud. The failed end of the muffler was found to be severely eroded around the failure point on the end piece, with small holes and external discoloration noted.

NTSB Probable Cause

THE SHUTDOWN OF THE ENGINE DUE TO THE FAILURE OF THE MUFFLER AND THE RESULTING HEAT INDUCED SHORTING OF THE MAGNETO GROUND WIRES, AND THE INADEQUATE MAINTENANCE INSPECTION OF THE MUFFLER AND THE ENGINE EXHAUST SYSTEM.

Full Narrative

THE INSTRUCTOR PILOT SAID THAT DURING CLIMB TO CRUISE THE ENGINE SUDDENLY QUIT COMPLETELY WITH A LOUD NOISE. THE INSTRUCTOR LANDED THE AIRCRAFT IN A FIELD AND THE AIRCRAFT NOSED OVER AFTER COLLIDING WITH A BERM. EXAMINATION OF THE AIRCRAFT REVEALED THAT THE REAR DOME OF THE LEFT MUFFLER HAD BLOWN OUT. SCORCHING AND EXHAUST STAINS WERE EVIDENT ON THE FIREWALL TO THE REAR OF THE MUFFLER AND WIRE BUNDLES ROUTED IN THIS AREA WERE FOUND BURNED WITH MELTED INSULATION NOTED. THE 'P' LEADS FOR THE MAGNETOS WERE FOUND ROUTED IN THIS WIRE BUNDLE. VISUAL EXAMINATION AND ELECTRICAL CONTINUITY CHECKS OF THE 'P' LEADS REVEALED THAT THE INTERNAL INSULATION HAD MELTED ALLOWING THE CONDUCTORS TO SHORT WITHIN THE WIRES. EXAMINATION OF THE MUFFLER REVEALED SEVERE INTERNAL EROSION, WITH HOLES THROUGH THE CABIN HEAT SHROUD. THE FAILED END OF THE MUFFLER WAS FOUND TO BE SEVERELY ERODED AROUND THE FAILURE POINT ON THE END PIECE, WITH SMALL HOLES AND EXTERNAL DISCOLORATION NOTED.

Flight

Event TypeAccident
Event Time15:20 PDT
Nearest Airport0nm N
Runway0
Flight Plan FiledVFR
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCessna 150M
Tail NumberN211AF
Aircraft CategoryAir
DamageSubstantial
OperatorArmed Forces Flying Club
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsContinental · O-200-A48B · Reciprocating · 100
Seats2

People & Injuries

Injury Summary2 injuries (2 minor injuries)
Fatal0
Serious0
Minor2
Uninjured0
Total2
Crew 1Age 33 · First Class

Conditions

ConditionsVMC
LightDaylight
Wind180° @ 15 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point55
Altimeter30.00 inHg
Weather SourcePILO

Appendix: Source Data