Plane Crash List

Piper PA 32R-301T C-GKLY

8 September 2002 · Byram Township, New Jersey, United States · Fatal

Summary

On 8 September 2002 at about 22:21 local time, a Piper PA 32R-301T registered C-GKLY was involved in an accident near Byram Township, New Jersey, United States. 4 people were on board and 2 died, 2 were seriously injured. The aircraft was destroyed. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 22:21
Classification
Accident
Location
Byram Township, New Jersey, United States
Nearest airport
Andover-Aeroflex (12N)
Coordinates
40.9967, -74.6753
Aircraft
Piper PA 32R-301T
Registration
C-GKLY
Category
Airplane
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Teterboro → London, Ontario
Aircraft damage
Destroyed
Weather
VMC
Light
Day
NTSB number
IAD02FA091

People

2 people died.

On board Died Serious Minor Uninjured
4 2 2 0 0

Probable cause

the improper manufacturing of the crankshaft gear bolt, which resulted in the failure of the bolt due to hydrogen embrittlement, and the subsequent loss of engine power. Also causal was the engine manufacturer's failure to remove the affected bolts from fixed wing engines during the 4-year period that transpired between the initial failures and removal of the bolts from stock for installation, until the accident flight. A factor in the accident was inadequate oversight (lack of action) by the FAA during the 4-year period in which the bolts remained in serviceable engines.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The airplane was in cruise flight at 3,500 feet mean sea level when the engine lost power. The pilot then performed a forced landing to trees. Examination of the Lycoming IO-540 series engine revealed that the zinc-plated crankshaft gear attachment bolt was fractured, and that the crankshaft no longer drove the gear. Fracture surface analysis revealed intergranular separation due to hydrogen-assisted cracking. Engines had previously been built with cadmium-plated bolts, but zinc-plated bolts were being used because they were readily available, and had a "positive impact" on production. Lycoming received 8,500 zinc-plated bolts between November 1996 and July 1998. Lycoming manufactured or re-built/overhauled 1,088 engines with zinc-plated bolts, and shipped 2,667 zinc-plated bolts as spares. Two zinc-plated gear bolt failures were documented in helicopter engines in 1998, due to hydrogen embrittlement. One bolt failed at 30 hours of operation, and the other at 19 hours. Lycoming and FAA personnel believed the failures occurred due to the higher loads generated by helicopters. Based upon the two failures, Lycoming removed the bolts from its stock as a "precautionary measure" in July 1998. Bolt recalls were issued by the helicopter manufacturer and Lycoming in July 1998. The FAA issued an Airworthiness Directive (AD) in February 1999 to replace the crankshaft bolts in affected helicopter engines worldwide. In July 1999, a Piper PA-32R-301 bolt failed due to hydrogen embrittlement at 327 hours. Between March 2000 and January 2001, two bolts failed on Royal Jordanian Falcon trainer airplanes, at 292 and 179 hours. As a "precautionary measure," Lycoming replaced the crankshaft gear bolts in the five-airplane Jordanian Falcon fleet about February 2001. Lycoming and FAA personnel believed the failures did not extend beyond helicopter and aerobatic applications, although the PA-32R-301 failure occurred in 1999. In June 2002, another bolt failed on a Piper PA-32R-301, at 448 hours. The engine was examined by Lycoming and FAA personnel, and a Lycoming laboratory report stated the failure was due to hydrogen embrittlement. In September 2002, this accident occurred, and as a result of the investigation, about 2 weeks after the accident, Lycoming issued a Service Bulletin (SB) to replace bolts on certain 540-series engines. In October 2002, the FAA issued an Emergency AD to also replace the bolts. The common cause for hydrogen embrittlement is a missed or under baked condition.

Quoted verbatim from the NTSB record.

Other Piper PA-32R accidents

Date Aircraft Location Operator Outcome Died
13 Jun 2002 Piper PA-32R-300
N38709
Beaumont, Kansas, United States - No injuries -
24 Sep 2002 Piper PA-32R-301T
N106JG
Yeehaw Junction, Florida, United States - Fatal 2
28 Mar 2002 Piper PA-32R-301T
D-ENEC
Ramstein, Germany
no coordinates
Dr. Manfred Ziegler Fatal 1
24 May 2002 Piper PA-32R-300
N9243K
Noorvik, Alaska, United States - No injuries -
24 Feb 2002 Piper PA-32R-300
N47465
Ferron, Utah, United States - Minor injuries -
4 Sep 2002 Piper PA-32R
N40449
Manley Hot Spgs, Alaska, United States Bidzy TA HOT Aana Corp. No injuries -

All 525 records for this type

Other accidents in this area

Date Aircraft Location Operator Outcome Died
5 May 2002 D'apuzzo D-260
N112JF
Andover, New Jersey, United States - No injuries -
23 Feb 2002 Piper PA-24-260
N9055P
Atlantic City, New Jersey, United States - No injuries -
16 Nov 2002 Mooney M10
N9502V
Fairfield, New Jersey, United States - Fatal 2
12 Nov 2002 Cessna 182P
N1835M
Lincoln Park, New Jersey, United States - No injuries -
24 Mar 2002 Cessna 172P
N9847L
Ocean City, New Jersey, United States - No injuries -
20 Jul 2002 Wehrlen GLASSAIR II RG
N79CW
Jackson, New Jersey, United States - Fatal 1

All 170,864 records in United States