CHI08LA160

NTSB accident investigation · Piper PA-44-180 · Battle Creek, MI · June 8, 2008

Accident · No injuriesLimited investigationFinal report
Date
June 8, 2008, 13:15 local (17:15 UTC)
Place
Battle Creek, MI
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Enroute
Aircraft
N159WMPiper PA-44-180
Defining event
Enroute-cruise: Powerplant sys/comp malf/fail
Weather
Visual (VMC) · Day
Status
Completed · report December 24, 2008
Report
Approved by Office Director
Parties
Federal Aviation Administration, Hartzell Propeller, Piper
FAA report
20080608838749A
Case key
68220

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

On this page

Probable cause

The in-flight separation of the tip of a propeller blade due to metal fatigue that resulted from an inadequate inspection and repair.

Findings · 4

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Propeller system: propeller blade sectionAircraft › Aircraft propeller/rotor · Fatigue/wear/corrosionPiper PA-44-180: 1 caseAll aircraft: 51 casesProbable cause
Propeller system: propeller blade sectionAircraft › Aircraft propeller/rotor · FailurePiper PA-44-180: 1 caseAll aircraft: 51 casesProbable cause
Maintenance: repairPersonnel issues › Task performance · Maintenance personnelPiper PA-44-180: 1 caseAll aircraft: 99 casesProbable cause
Action: forgotten action/omissionPersonnel issues › Action/decision · Maintenance personnelPiper PA-44-180: 8 casesAll aircraft: 440 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The twin-engine airplane sustained substantial damage due to a separated propeller blade tip impacting the airplane's nose during cruise. The tip separation exhibited signs of fatigue failure. Witness marks consistent with tool file marks made during a leading edge repair were found at the area of the origin of fatigue. According to maintenance information published by the propeller manufacturer, a 10x magnifying glass should be used to examine repairs to ensure damage, file marks, and any course surface finish are removed prior to returning the propeller back to service.. The airplane accumulated a total time of 1,997 hours.

Factual narrative

On June 8, 2008, at 1315 eastern daylight time, a Piper PA-44-180, N159WM, sustained substantial damage due to a separated propeller blade tip impacting the airplane's nose during cruise near Battle Creek, Michigan. The airplane landed without further incident at the W K Kellogg Airport (BTL), near Battle Creek, Michigan. Visual meteorological conditions prevailed at the time of the accident. The 14 CFR Part 91 instructional flight was not operating on a flight plan. The certified flight instructor (CFI) and the commercial pilot receiving dual instruction were uninjured. The local flight originated from BTL about 1230.

The flight was returning to BTL at the time of the accident. CFI's report, in part, stated:

A large BANG was heard and felt 8 to 10 miles south east of the

airport. At that point we scanned the gauges and saw no sign of

problems. When we looked out the windscreen; however we saw

a large depression in the nose section of the aircraft. Initially we

thought we had ... a bird strike.

N159WM was a 2002, Piper PA-44-180, which was a twin engine, four seat airplane with serial number 4496159. The airplane was powered by two Lycoming engines. Each engine drove its own Hartzell propeller. The propeller blade was a model FJC7666A-2R that was installed in a model HC-C2YR-2CLEUF hub assembly. The serial number of the blade with the tip separation was J73543.

The airplane accumulated a total time of 1,997 hours.

The outboard section of the remaining propeller blade was cut away and sent to the National Transportation Safety Board's Materials Laboratory. A Senior Materials Engineer examined the propeller section and produced Materials Laboratory Factual Report number 08-097. The report referred to repair data from the propeller manufacturer's website indicating that a 10x magnifying glass should be used to examine repairs to ensure damage, file marks, and any course surface finish are removed prior to returning the propeller back to service. The laboratory report, in part, stated:

Fatigue features emanated from a fatigue origin area located at the

leading edge near the flat side of the blade ... . ... Angled file marks

consistent with a leading edge repair were observed between the

leading edge and the flat side of the blade ... .

Aircraft

Registration
N159WM
Reported as
Piper PA-44-180
Category
Airplane
Serial number
4496159
Airframe hours
1,997
Engines
Lycoming LO-360-A1H6, 180 horsepower, reciprocatingLycoming O-360-A1H6, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Registered owner
Western Michigan University
Airworthiness certificate
Standard, Normal
Last inspection
AAIP · May 1, 2008 · 47 hours before
Departed
BTL · Battle Creek, MI
Airport
BTL · W K Kellogg

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 · 2

As NTSB recorded them. NTSB leaves out names.

Role
Flight instructor
Age
26
Injuries
None
Certificates
Flight instructor, Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 1, Without waivers/limitations
Last flight review
February 1, 2007
Seat
Right
Flight hours
650 total · 200 in this make and model · 580 as pilot in command · 114 in the last 90 days · 24 in the last 30 days · 1 in the last 24 hours
Role
Student pilot
Age
26
Injuries
None
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 1, With waivers/limitations
Last flight review
February 1, 2007
Seat
Left

Weather

Conditions
Visual (VMC) · Day
Wind
220° at 15 knots, gusting 22
Visibility
10 statute miles
Lowest ceiling
None
Temperature
84 °F, dew point 72 °F
Altimeter
29.88 inHg
Observed at
BTL, 10 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.