ANC98LA058

NTSB accident investigation · Luscombe 8A · Paxson, AK · May 27, 1998

Accident · No injuriesLimited investigationFinal report
Date
May 27, 1998, 14:10 local (22:10 UTC)
Place
Paxson, AK
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N1322BLuscombe 8A
Weather
Visual (VMC) · Day
Status
Completed · report November 17, 1999
Report
Approved by Office Director
NTSB office
Alaska Regional Office
FAA report
19980527011039A
Case key
3146

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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Probable cause

A loss of engine power due to a failure of the engine's number 3 intake valve. A factor in the accident was the unsuitable terrain for a forced landing.

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.

Loss of engine power(partial) - mech failure/malfCruise
Engine assembly,valve,intake - failureCause
Forced landingEmergency descent/landing
On ground/water collision with objectEmergency landing
Object - tree(s)
On ground/water encounter with terrain/waterLanding - roll
Terrain condition - drop-off/descending embankmentFactor

Analysis

The pilot made a forced landing on a highway following a partial loss of engine power. He stated that after the initial power loss, he attempted to divert to an alternate airport for landing. The airplane's engine continued to lose power, and the airplane was no longer able to maintain altitude. He selected a portion of the highway as an emergency landing area. During the landing roll, the right wing struck an overhanging tree, and the airplane turned to the right and struck an embankment. The airplane's wings and fuselage sustained substantial damage. A postaccident engine inspection revealed a broken intake valve on the number 3 cylinder.

Factual narrative

On May 27, 1998, about 1410 Alaska daylight time, a wheel equipped Luscombe 8A airplane, N1322B, sustained substantial damage during an emergency landing on a highway, about 5 miles south of Paxson, Alaska. The airplane was being operated as a visual flight rules (VFR) personal flight under Title 14 CFR Part 91 when the accident occurred. The certificated airline transport pilot, and the one passenger aboard, were not injured. Visual meteorological conditions prevailed, and no flight plan was filed. The flight originated at the Cantwell Airport, Cantwell, at 1230.

During a telephone conversation with the National Transportation Safety Board investigator-in-charge, on May 28, at 1015, the pilot reported that while in cruise flight, the engine began to run rough. The pilot said he attempted to divert to the Paxson Airport for landing, but the airplane's engine continued to lose power, and the airplane was no longer able to maintain altitude. The pilot selected a portion of the Richardson Highway as an emergency landing area. During the landing roll, the right wing struck an overhanging tree, and the airplane turned to the right and struck an embankment.

The airplane sustained substantial damage to the wings and fuselage.

The pilot noted in his written statement dated June 6, that a broken intake valve was discovered on the number 3 cylinder during a postaccident engine examination.

Aircraft

Registration
N1322B
Reported as
Luscombe 8A
Category
Airplane
Serial number
5949
Airframe hours
2,608
Engine
Continental A-65-8, 65 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
John U. Twiss
Airworthiness certificate
Standard, Normal
Last inspection
Annual · April 25, 1998 · 33 hours before
Departed
TTW · Cantwell, AK
Destination
GKN · Gulkana, AK

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
54
Certificates
Airline transport, Flight instructor
Airplane ratings
Multi-engine land, Single-engine sea, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Left
Flight hours
11,500 total · 100 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
180° at 10 knots
Visibility
25 statute miles
Lowest ceiling
6,000 ft broken
Temperature
61 °F

FAA reports on this event · 1

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