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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

August 26, 1995 · Piper PA-28-181 · N2937X

Juneau, AK

Overview

Report Status
Final with probable cause
Event Type
Incident
Date
August 26, 1995
Injury Outcomes
No injuries (3 uninjured)
Location
Juneau, AK
Aircraft
Piper PA-28-181
Tail Number
N2937X
Injuries
None
Aircraft Damage
Minor
NTSB Number
ANC95IA151

Just after takeoff the airplane began to vibrate. The pilot reduced the power and returned for an immediate landing. Examination showed that 6 inches of one blade had separated from the propeller. The separated piece was recovered, and metallurgical examination showed that the blade separated due to a fatigue crack emanating from a gouge associated with foreign object damage. The propeller blade material met the material and hardness specifications as prescribed by the manufacturer.

NTSB Probable Cause

failure and separation of the propeller blade due to foreign object damage and fatigue.

Full Narrative

On August 26, 1995, at 0945 Alaska daylight time, a wheel equipped Piper PA-28-181 airplane, N2937X, registered to and operated by Skagway Air Service of Skagway, Alaska, experienced a severe vibration during climbout from the Juneau Airport, Juneau, Alaska. The airplane returned to the Juneau airport. The air taxi flight, operating under 14 CFR Part 135, departed Juneau and the destination was Gustavus, Alaska. A company visual flight rules flight plan was in effect and visual meteorological conditions prevailed. The airline transport certificated pilot and the two passengers were not injured and the airplane received minor damage. According to the operator, approximately 6 inches of one propeller blade separated from the propeller. As a result of the vibration, the alternator broke away from the engine case resulting in a small engine compartment fire. The separated propeller tip was recovered. The propeller tip and propeller were sent the NTSB's Materials Laboratory Division for examination. The examination revealed that the area of the fatigue origin was a wedge shaped cavity on the leading edge of the blade. The cavity was oriented approximately 35 degrees to the leading edge of the blade and extended below the surface about 0.03 inch. The total length of the cavity (on both separated pieces) was approximately 0.25 inch. The composition and hardness of the material from which the propeller was manufactured was checked and found to meet the manufacturer's specifications. According to a McCauley Service Letter 1995-4, dated February 10, 1995, it states that stress riser damage caused by stones or other small objects striking the propeller blade as it is rotating is the only damage that needs to be repaired in the field. During a telephone conversation with the pilot, she said she did not see any nicks or gouges in the leading edges of the blades during preflight.

Flight

Event TypeIncident
Event Time09:45 AKDT
Nearest Airport0nm
Runway0
Flight Plan FiledCvfr
Aircraft FireGrd
Aircraft ExplosionNo

Aircraft

AircraftPiper PA-28-181
Tail NumberN2937X
Aircraft CategoryAir
DamageMinor
Operating RulePart 135
Engines1
Engine TypeReciprocating
Engine DetailsLycoming · O-360 · Reciprocating · 180
Seats4

People & Injuries

Injury SummaryNo injuries (3 uninjured)
Fatal0
Serious0
Minor0
Uninjured3
Total3
Crew 1Age 25 · First Class

Conditions

ConditionsVMC
LightDaylight
WindCalm
Visibility99 sm
CeilingNone
Temperature / Dew Point63 F / 0 C
Altimeter0
Weather SourcePILO

Appendix: Source Data