19980426007599A

Accident · Substantial damage

FAA accident report · Piper PA-32-300 · New Bedford, MA · April 26, 1998

Date
April 26, 1998 · 22:30 local
Place
New Bedford, MA
Airport
New Bedford Municipal
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
General operating rules (Part 91)
Damage
Substantial damage
Aircraft
N15326
NTSB investigation
NTSBNYC98LA102
Reported as
Piper PA32300
Reported engine
Lycoming TIO540*
People aboard
1
Fatal injuries
1
Pilot’s flight hours
958 total5 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Departed with control locks engaged. Lost control. (.4)a witness observed the airplane depart runway 5 and climb at a steep angle. The aircraft then turned to the northwest, then to the northeast, and descended steeply to the ground. Examination of the wreckage by a federal aviation administration inspector revealed a control lock device, with a locked pad lock, installed on the right hand flight control column. Toxicological testing revealed 155 mg/dl (0.155%) ethanol detected in the pilot's blood, 187 mg/dl ethanol detected in the vitreous, and 205 mg/dl ethanol detected in the urine. A review of 14 CFR part 91.17, stated, '(a) no person may act or attempt to act as a crewmember of a civil aircraft...(4) while having a .04 percent by weight or more alcohol in the blood.'

As the FAA filed it

DEPARTED WITH CONTROL LOCKS ENGAGED. LOST CONTROL. (.4)A WITNESS OBSERVED THE AIRPLANE DEPART RUNWAY 5 AND CLIMB AT A STEEP ANGLE. THE AIRCRAFT THEN TURNED TO THE NORTHWEST, THEN TO THE NORTHEAST, AND DESCENDED STEEPLY TO THE GROUND. EXAMINATION OF THE WRECKAGE BY A FEDERAL AVIATION ADMINISTRATION INSPECTOR REVEALED A CONTROL LOCK DEVICE, WITH A LOCKED PAD LOCK, INSTALLED ON THE RIGHT HAND FLIGHT CONTROL COLUMN. TOXICOLOGICAL TESTING REVEALED 155 MG/DL (0.155%) ETHANOL DETECTED IN THE PILOT'S BLOOD, 187 MG/DL ETHANOL DETECTED IN THE VITREOUS, AND 205 MG/DL ETHANOL DETECTED IN THE URINE. A REVIEW OF 14 CFR PART 91.17, STATED, '(A) NO PERSON MAY ACT OR ATTEMPT TO ACT AS A CREWMEMBER OF A CIVIL AIRCRAFT...(4) WHILE HAVING A .04 PERCENT BY WEIGHT OR MORE ALCOHOL IN THE BLOOD.'

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

Other reports on N15326 · 2

Matched to the same aircraft by N-number and date.