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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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November 20, 1986 · Cessna U206F · N7311Q

Moose Creek, ID

Overview

Report Status
Preliminary report
Event Type
Accident
Date
November 20, 1986
Injury Outcomes
2 injuries (1 fatality, 1 serious injury)
Location
Moose Creek, ID
Aircraft
Cessna U206F
Tail Number
N7311Q
Injuries
Fatal
Aircraft Damage
Destroyed
NTSB Number
SEA87FA027

AFTER DEPARTURE AND DURING THE INITIAL CRUISE CLIMB THE PLT AND PAX HEARD A METALLIC CLICKING DESCRIBED AS SOUNDING LIKE A 'VALVE TAP' IN AN AUTOMOBILE AND COMING FROM THE ENG AREA. THE PLT EXECUTED AN IMMEDIATE COURSE REVERSAL BACK TO THE AIRSTRIP WHILE STILL WITHIN THE NARROW GORGE OF THE SELWAY RIVER. THE IMMEDIACY OF THE REVERSE TURN WAS BROUGHT ABOUT BY THE PLT'S EXPECTATION OF IMPENDING MECH PROBLEM WITH THE ACFT AS WELL AS ANXIETY OF THE SITUATION AT SUCH A CRITICAL TIME DURING THE FLT. THE TURN AT A RELATIVELY LOW ALT WITHIN THE GORGE NECESSITATED A TIGHT TURN RADIUS AND THUS REDUCED THE RATE OF CLIMB IN AN ALREADY HEAVILY LOADED ACFT. THIS EVENT PLACED THE ACFT IN A POSITION WHEREBY CLEARANCE WITH THE HEAVILY WOODED UPSLOPING SIDES OF THE GORGE WAS NOT POSSIBLE. DISASSEMBLY, INSPECTION AND TESTING (WHERE POSSIBLE) OF THE ENG, PROP AND ASSOCIATED COMPONENTS REVEALED NO EVIDENCE OF ANY PREIMPACT MALFUNCTION WHICH WOULD HAVE RESULTED IN A POWER LOSS, NOR ANY EXPLANATION FOR THE CLICKING NOISE.

Full Narrative

AFTER DEPARTURE AND DURING THE INITIAL CRUISE CLIMB THE PLT AND PAX HEARD A METALLIC CLICKING DESCRIBED AS SOUNDING LIKE A 'VALVE TAP' IN AN AUTOMOBILE AND COMING FROM THE ENG AREA. THE PLT EXECUTED AN IMMEDIATE COURSE REVERSAL BACK TO THE AIRSTRIP WHILE STILL WITHIN THE NARROW GORGE OF THE SELWAY RIVER. THE IMMEDIACY OF THE REVERSE TURN WAS BROUGHT ABOUT BY THE PLT'S EXPECTATION OF IMPENDING MECH PROBLEM WITH THE ACFT AS WELL AS ANXIETY OF THE SITUATION AT SUCH A CRITICAL TIME DURING THE FLT. THE TURN AT A RELATIVELY LOW ALT WITHIN THE GORGE NECESSITATED A TIGHT TURN RADIUS AND THUS REDUCED THE RATE OF CLIMB IN AN ALREADY HEAVILY LOADED ACFT. THIS EVENT PLACED THE ACFT IN A POSITION WHEREBY CLEARANCE WITH THE HEAVILY WOODED UPSLOPING SIDES OF THE GORGE WAS NOT POSSIBLE. DISASSEMBLY, INSPECTION AND TESTING (WHERE POSSIBLE) OF THE ENG, PROP AND ASSOCIATED COMPONENTS REVEALED NO EVIDENCE OF ANY PREIMPACT MALFUNCTION WHICH WOULD HAVE RESULTED IN A POWER LOSS, NOR ANY EXPLANATION FOR THE CLICKING NOISE.

Flight

Event TypeAccident
Event Time11:12 PST
Nearest Airport0nm N
Runway0
Runway Length0
Runway Width0
Flight Plan FiledNone
Aircraft FireGrd
Aircraft ExplosionGrd

Aircraft

AircraftCessna U206F
Tail NumberN7311Q
Aircraft CategoryAir
DamageDestroyed
Operating RulePart 135
Engines1
Engine TypeReciprocating
Engine DetailsContinental · IO-520-F · Reciprocating · 300
Seats2

People & Injuries

Injury Summary2 injuries (1 fatality, 1 serious injury)
Fatal1
Serious1
Minor0
Uninjured0
Total2
Crew 1Age 33 · Second Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility25 sm
CeilingNone
Temperature / Dew Point0 C / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data