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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

July 22, 1983 · Cessna T188C · N2834J

Bozeman, MT

Overview

Report Status
Preliminary report
Event Type
Accident
Date
July 22, 1983
Injury Outcomes
No injuries (1 uninjured)
Location
Bozeman, MT
Aircraft
Cessna T188C
Tail Number
N2834J
Injuries
None
Aircraft Damage
Substantial
NTSB Number
DEN83LA172

THE ACFT SETTLED INTO TREES AFTER THE ENGINE LOST POWER DURING A SWATH RUN. THE FLT HAD BEEN IN PROGRESS FOR ABOUT 15 MINUTES. THE PLT STARTED THE 4TH RUN AND THE ACFT STARTED TO SETTLE. THE PLT DUMPED THE LOAD BUT DID NOT TOUCH THE THROTTLE OR MIXTURE. HE HAD SET THE THROTTLE AND MIXTURE FOR THE OPERATION AND TIGHTENED THE FRICTION ADJUSTMENT. THE MIXTURE HAD BEEN LEANED TO PEAK TEMPERATURE AND THEN ENRICHED SO THE CYL HEAD TEMP WAS PEAK TEMP MINUS 125 DEGREES. THE MANIFOLD PRESSURE WAS 32 INCHES AND THE PROP SET AT 2400 RPM THE PILOT WAS ASKED ABOUT HIS USE OR POWER AND MIXTURE AND HE SAID HE DID NOT MOVE OR ADJUST THEM FROM THE TIME HE SET THEM AFTER INITIAL LEVELOFF UNTIL GROUND IMPACT. HE SAIDTHAT AFTER THE ACCIDENT THESE CONTROLS WERE IN A NORMAL FLT POSITION. THE PILOT WAS WEARING A HELMET AND SAID IT WOULD BE POSSIBLE FOR THE ENGINE TO STOP AND HIM NOT BE ABLE TO HEAR IT. FROM THE CONDITION OF THE PROPELLER IT WAS DETERMINEDTHAT THE ENGINE WAS NOT PRODUCING POWER AT IMPACT. DURING INSPECTION, NOTHING WAS FOUND WRONG WITH THE POWERPLANT.

Full Narrative

THE ACFT SETTLED INTO TREES AFTER THE ENGINE LOST POWER DURING A SWATH RUN. THE FLT HAD BEEN IN PROGRESS FOR ABOUT 15 MINUTES. THE PLT STARTED THE 4TH RUN AND THE ACFT STARTED TO SETTLE. THE PLT DUMPED THE LOAD BUT DID NOT TOUCH THE THROTTLE OR MIXTURE. HE HAD SET THE THROTTLE AND MIXTURE FOR THE OPERATION AND TIGHTENED THE FRICTION ADJUSTMENT. THE MIXTURE HAD BEEN LEANED TO PEAK TEMPERATURE AND THEN ENRICHED SO THE CYL HEAD TEMP WAS PEAK TEMP MINUS 125 DEGREES. THE MANIFOLD PRESSURE WAS 32 INCHES AND THE PROP SET AT 2400 RPM THE PILOT WAS ASKED ABOUT HIS USE OR POWER AND MIXTURE AND HE SAID HE DID NOT MOVE OR ADJUST THEM FROM THE TIME HE SET THEM AFTER INITIAL LEVELOFF UNTIL GROUND IMPACT. HE SAIDTHAT AFTER THE ACCIDENT THESE CONTROLS WERE IN A NORMAL FLT POSITION. THE PILOT WAS WEARING A HELMET AND SAID IT WOULD BE POSSIBLE FOR THE ENGINE TO STOP AND HIM NOT BE ABLE TO HEAR IT. FROM THE CONDITION OF THE PROPELLER IT WAS DETERMINEDTHAT THE ENGINE WAS NOT PRODUCING POWER AT IMPACT. DURING INSPECTION, NOTHING WAS FOUND WRONG WITH THE POWERPLANT.

Flight

Event TypeAccident
Event Time10:30 MDT
Nearest Airport0nm
Runway0
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftCessna T188C
Tail NumberN2834J
Aircraft CategoryAir
DamageSubstantial
Operating RulePart 137
Engines1
Engine TypeReciprocating
Engine DetailsContinental · TS10-520-T · Reciprocating · 310
Seats1

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 38 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind310° @ 5 kt
Visibility20 sm
CeilingBroken clouds 20000 ft
Temperature / Dew Point70 F / 48
Altimeter30.00 inHg
Observation Time16:50
Weather SourceWFAC

Appendix: Source Data