Accident Piper PA-28R-200 N33SM,
ASN logo
ASN Wikibase Occurrence # 362924
 
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:Tuesday 15 September 1992
Time:13:00 LT
Type:Silhouette image of generic P28R model; specific model in this crash may look slightly different    
Piper PA-28R-200
Owner/operator:Air Desert Pacific Corporation
Registration: N33SM
MSN: 28R-35234
Year of manufacture:1969
Total airframe hrs:4697 hours
Engine model:LYCOMING IO-360-C1C
Fatalities:Fatalities: 0 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:Avalon, CA -   United States of America
Phase: Manoeuvring (airshow, firefighting, ag.ops.)
Nature:Private
Departure airport:La Verne, CA (KPOC)
Destination airport:
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
DAMAGE TO THE AIRCRAFT FIREWALL, PROPELLER AND OTHER EXTERNAL STRUCTURES WAS REPORTED BY THE CATALINA AIRPORT ASST MANAGER SUBSEQUENT TO THE AIRCRAFT LANDING AT THE ISLAND. THE PILOT TOLD THE AIRPORT MANAGER THAT WHILE ENROUTE BETWEEN THE MAINLAND AND THE ISLAND HIS ENGINE QUIT, AND, JUST BEFORE IMPACT WITH THE OCEAN, HE WAS ABLE TO GET THE ENGINE RESTARTED. THE PILOT REPORTEDLY SAID THAT THE NOSE GEAR HIT THE WATER DURING THE EVENT. THE PILOT, AN ITALIAN NATIONAL, DID NOT REPORT THE ACCIDENT TO THE FAA, THE SAFETY BOARD OR THE FBO WHERE THE AIRCRAFT WAS RENTED AND IMMEDIATELY RETURNED TO ITALY. AFTER THE AIRPLANE LANDED, AIRPORT EMPLOYEES OBSERVED THE PILOT POUR A HANDFUL OF DIRT INTO THE OIL FILLER TUBE. AN FAA AIRWORTHINESS INSPECTOR EXAMINED THE AIRCRAFT. HE REPORTED THAT THE TIPS OF BOTH PROPELLER BLADES WERE BENT SYMMETRICALLY BACK AT 45 DEGREE ANGLES WITHOUT LEADING EDGE DAMAGE OR CORDWISE SCRATCHES. THE BOTTOM PART OF THE FIREWALL WAS BENT AFT AND UPWARD CRUSH DAMAGE WAS OBSERVED ON THE BOTTOM OF THE ENGINE COWL. THE ENTRY STEP WAS RIPPED FROM THE AIRCRAFT AND THE LOWER ROTATING BEACON WAS FOUND PUSHED UP THROUGH THE FUSELAGE SKIN PANEL. OTHER EXTERNAL AND INTERNAL WATER DAMAGE WAS ALSO NOTED.

Probable Cause: THE PILOT'S INTENTIONAL FLIGHT AT AN ALTITUDE WHICH PROVIDED INSUFFICIENT CLEARANCE FROM THE WATER.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: LAX92LA398
Status: Investigation completed
Duration: 12 months
Download report: Final report

Sources:

NTSB LAX92LA398

Location

Revision history:

Date/timeContributorUpdates
18-Mar-2024 11:39 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