SEA85FA110

NTSB accident investigation · Cessna 402 · Pocatello, ID · May 16, 1985

Accident · FatalField investigationFinal report
Date
May 15, 1985, 18:26 local (May 16, 1985, 00:26 UTC)
Place
Pocatello, ID
Injuries
1 fatal
Damage
Destroyed
Phase of flight
Unknown
Aircraft
N402CSCessna 402
Weather
Visual (VMC) · Day
Status
Completed
Report
Approved by Office Director
FAA report
19850515022699A
Case key
40042

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Airframe/component/system failure/malfunctionUnknown
Exhaust system,manifold/pipe - corrodedCause
Maintenance,inspection - inadequateCompany maintenance personnelCause
Procedure inadequateManufacturerFactor
Inadequate surveillance of operationFaa(organization)Factor
Exhaust system,manifold/pipe - failure,totalCause
Exhaust system,manifold/pipe - leakCause
Loss of engine power(partial) - mech failure/malfCruise - normal
InitiatedPilot in command
FireDescent
Miscellaneous - fireCause
Wing,spar - burned
Airframe/component/system failure/malfunctionDescent
Wing - failure,totalCause
Wing - separation
In flight collision with terrain/waterDescent - uncontrolled

Analysis

Shortly after departure & level off, the plt reported an eng malfunction & initiated a return to the arpt. About 2 min later, he reported an eng fire & declared an emergency. Aprx 1 min thereafter, the rgt wing separated from the acft & the plane crashed. An exam of the wreckage revealed extensive inflt fire damage in the area of separation. A 2.5 by 3 inch hole was found in the rgt inboard exhaust tube, pn 0850712-6. It was oriented toward the accessory compartment withnumerous fuel & oil lines which were fire damaged & charred. Also, much of the eng support structure & wing spar were melted in that area. An exam of the exhaust tube revealed its walls were thin, brittle & discolored in the area of the rupture & several areas of cracks & small holes were found. The exhaust tube had 5862 hrs of total service & 1762 hours since it was overhauled. Records showed that AD 75-23-08 had been complied with during the last inspection, 25 flt hrs prior to the accident.

Aircraft

Registration
N402CS
Reported as
Cessna 402
Category
Airplane
Serial number
402-0108
Airframe hours
5,862
Engine
Continental TSIO-520-E, 300 horsepower, reciprocating
Damage
Destroyed
Fire
In-Flight
Flight
Part 135
Operator
Regional Express Company
Registered owner
Fbn Leasing Corp
Airworthiness certificate
Standard, Normal
Last inspection
Unknown · February 11, 1985 · 12 hours before
Departed
PIH · Pocatello, ID
Destination
SLC · Salt Lake City, UT
Flight plan
IFR

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
37
Certificates
Airline transport, Military, Flight instructor
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane
Medical
Class 1, Valid Medical--no waivers/lim.
Seat
Left
Toxicology
Performed
Flight hours
4,500 total · 350 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
360° at 15 knots
Visibility
40 statute miles
Lowest ceiling
None
Temperature
63 °F, dew point 46 °F
Altimeter
30.00 inHg
Observed at
PIH, 12 nm away

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.