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July 6, 2011 · Cessna R182 · N7392X

Hesperia, CA

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
July 6, 2011
Injury Outcomes
2 injuries (2 minor injuries)
Location
Hesperia, CA
Aircraft
Cessna R182
Tail Number
N7392X
Operator
Chris E Waggener
Injuries
Minor
Aircraft Damage
Substantial
NTSB Number
WPR11LA311

The airplane's engine stopped making sufficient power to maintain a climb, so the pilot decided to turn back toward the airport. However, after he flew into a valley, he realized that the airplane would not make it back to the airport. After seeing power lines along the airplane's flightpath, he turned the airplane toward an open field. The airplane subsequently hit the ground hard and then hit a tree, which separated the right wing from the airframe. During the postaccident engine examination, the muffler was disassembled. One internal baffle cone was found separated from the end plate and was blocking the opening of the muffler. Upon shaking the muffler, the baffle cone was free to move around within the muffler assembly. The other baffle cone had a hole eroded in its center. Internal engine failures can cause partial or complete engine power loss by restricting the flow of the exhaust gases. If pieces of the internal baffling break loose and partially or totally block the flow of exhaust gases, an engine failure can occur. It is likely the exhaust gas was partially or totally blocked by the separated baffle cone during the flight, which resulted in a loss of engine power.

NTSB Probable Cause

The separation of the end baffle cone inside the muffler, which blocked airflow through the engine after takeoff and resulted in a loss of engine power and an off-airport landing into obstacles.

Full Narrative

HISTORY OF FLIGHTOn July 5, 2011, about 1900 Pacific daylight time, a Cessna R182, N7392X, collided with a tree during an off airport forced landing following a loss of engine power during climb to cruise altitude after takeoff from Hesperia, California. The pilot/owner was operating the airplane under the provisions of 14 Code of Federal Regulations (CFR) Part 91. The private pilot and one passenger sustained minor injuries; the airplane sustained substantial damage from impact forces. The personal cross-country flight departed Hesperia about 1855 with a planned destination of Adelanto, California. Visual meteorological conditions prevailed, and no flight plan had been filed. The pilot stated that he had flown to Hesperia from Adelanto earlier that evening, and purchased about 29 gallons of fuel. During the climb to cruise, the airplane was unable to climb, and the pilot turned back toward the airport. He flew into a valley, and realized that the airplane would not make it back to the airport. He saw power lines in his flight path, and turned toward an open field. The airplane hit the ground hard, and then a tree, which separated the right wing from the airframe. Fuel spray from the wing set a car on fire. The airplane spun around, and came to rest with the nose on the ground, and the left wing and tail resting against a house. ADDITIONAL INFORMATIONThe FAA Publication Aviation Maintenance Technician Handbook – Powerplant, Volume 1, Chapter 3, describes induction and exhaust systems. One section of that chapter discusses internal muffler failures. It states that internal failures (baffles, diffusers, etc.) can cause partial or complete engine power loss by restricting the flow of the exhaust gases. If pieces of the internal baffling break loose and partially or totally block the flow of exhaust gases, engine failure can occur. TESTS AND RESEARCHInvestigators examined the wreckage at Aircraft Recovery Service, Littlerock, California, on July 14, 2011. A detailed report is part of the public docket for this accident. Examination of the airframe and engine revealed no anomalies that would have precluded normal operation. Investigators disassembled the muffler, and noted that one cone-shaped baffle had separated from the end plate, and was blocking the end opening of the muffler. Upon shaking the muffler, the cone was free to move around within the muffler assembly. The other cone had a hole eroded in its center.

Flight

Event TypeAccident
Event Time19:00 PDT
Nearest AirportHESPERIA (3nm WSW)
Runway21
Runway Length3900 ft
Runway Width50 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCessna R182
Tail NumberN7392X
Aircraft CategoryAir
DamageSubstantial
OperatorChris E Waggener
Operating RulePart 91
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-540-J3C5D · Reciprocating · 250
Seats4

People & Injuries

Injury Summary2 injuries (2 minor injuries)
Fatal0
Serious0
Minor2
Uninjured0
Total2
Crew 1Age 54 · Third Class · Minor

Conditions

ConditionsVMC
LightDaylight
Wind300° @ 6 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point63 F
Altimeter30.00 inHg
Observation Time02:55
Weather SourceWFAC

Appendix: Source Data