Accident Aérospatiale AS332L Super Puma N25AN,
ASN logo
ASN Wikibase Occurrence # 357110
 
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. If you feel this information is incomplete or incorrect, you can submit corrected information.

Date:Friday 5 July 1996
Time:17:30 LT
Type:Silhouette image of generic AS32 model; specific model in this crash may look slightly different    
Aérospatiale AS332L Super Puma
Owner/operator:Trump Plaza Management
Registration: N25AN
MSN: 2087
Total airframe hrs:1459 hours
Engine model:Turbomeca MAKILA 1A
Fatalities:Fatalities: 0 / Occupants: 3
Aircraft damage: Substantial
Category:Accident
Location:Lakewood, NJ -   United States of America
Phase: Standing
Nature:Executive
Departure airport:(N12)
Destination airport:Morristown, NJ
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
After three flights, the helicopter was landed and the engines were shut down. When a passenger was boarded, the engines were restarted, and the pilot taxied the helicopter for takeoff. While waiting to takeoff, about 5 to 10 minutes after the engines were started, the pilot noticed a stiffness in the flight controls. This was followed immediately by illumination of electrical warning lights, loss of power from both alternators, and an odor of smoke in the cabin. Both engines were shut down, fire bottles were discharged, and the crew and passenger exited the helicopter. Examination of the fuselage revealed a fire had been centered around the right lateral hydraulic servo. The number two hydraulic lower cylinder distribution module of the right lateral servo had melted, and the high pressure lines were found 'free' of the module. The helicopter's alternators, located aft of the main transmission, contained internal cooling fans that drew air through the alternators. The alternators and their respective wiring bundles were extensively damaged by fire. The ignition source of the fire was not determined. The fire detection system (with visual and aural signals) did not activate prior to the electrical warning lights.

Probable Cause: a number two system module hydraulic oil leak, which was ignited by an undetermined source and resulted in a hydraulic fluid fire.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: NYC96LA143
Status: Investigation completed
Duration: 10 months
Download report: Final report

Sources:

NTSB NYC96LA143

Revision history:

Date/timeContributorUpdates
13-Mar-2024 14:18 ASN Update Bot Added

Corrections or additions? ... Edit this accident description

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2024 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314
www.FlightSafety.org