Accident Piper PA-28-140 N4487X,
ASN logo
ASN Wikibase Occurrence # 34662
 
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:Monday 18 July 1994
Time:11:06 LT
Type:Silhouette image of generic P28A model; specific model in this crash may look slightly different    
Piper PA-28-140
Owner/operator:Maurice E. Zeigler
Registration: N4487X
MSN: 28-7625043
Year of manufacture:1975
Total airframe hrs:2828 hours
Engine model:Lycoming O-320-E3D
Fatalities:Fatalities: 1 / Occupants: 3
Aircraft damage: Destroyed
Category:Accident
Location:Banning, CA -   United States of America
Phase: Initial climb
Nature:Private
Departure airport:(KBNG)
Destination airport:Van Nuys, CA (KVNY)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
THE AIRCRAFT WAS FLYING FROM PHOENIX TO VAN NUYS, CALIFORNIA, AND STOPPED AT BANNING FOR FUEL. AFTER ARRIVAL, 45.1 GALLONS OF 100 LL AVIATION FUEL WERE LOADED INTO THE AIRCRAFT'S FUEL TANKS. THE AIRCRAFT THEN TAXIED OUT AND DEPARTED ON THE 5,200-FOOT-LONG RUNWAY 26, WHICH HAS AN UPHILL GRADIENT OF 2.4 PERCENT. ACCORDING TO WITNESSES ON THE AIRPORT, THE AIRCRAFT USED APPROXIMATELY 4,200 FEET OF THE RUNWAY LENGTH DURING THE GROUND RUN AND NEVER ACHIEVED MORE THAN 200 FEET ABOVE GROUND LEVEL IN THE CLIMB. THE AIRCRAFT THEN SLOWLY DESCENDED IN A NOSE-HIGH ATTITUDE AS THE WINGS OSCILLATED SLIGHTLY. A PILOT WITNESS DRIVING ON A HIGHWAY PARALLEL TO THE AIRCRAFT'S FLIGHT PATH REPORTED THAT THE AIRCRAFT'S GROUND SPEED GRADUALLY DECAYED BELOW 55 MPH AS THE NOSE ROSE HIGHER AND HIGHER. THE AIRCRAFT BEGAN A SLIGHT LEFT TURN, THEN IT COLLIDED WITH THE TOP OF A 40-FOOT-TALL POWER POLE AND CAME TO REST ON THE DRIVEWAY OF A COMMERCIAL BUILDING. THE AIRCRAFT WAS LOADED 223 POUNDS OVER MAX ALLOWABLE GROSS WEIGHT. THE DENSITY ALTITUDE WAS 4,240 FEET. NO MECHANICAL DISCREPANCIES WERE FOUND WITH THE AIRFRAME OR ENGINE.

Probable Cause: the pilot's failure to obtain and maintain an appropriate climb airspeed after lift-off which resulted in an inadvertent stall mush condition. Factors in the accident were the high-density altitude condition, the pilot's selection of a runway with an uphill gradient, and the pilot's loading of the aircraft 223 pounds in excess of the maximum allowable gross takeoff weight.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: LAX94LA290
Status: Investigation completed
Duration: 11 months
Download report: Final report

Sources:

NTSB LAX94LA290

Location

Revision history:

Date/timeContributorUpdates
24-Oct-2008 10:30 ASN archive Added
10-Apr-2024 05:57 ASN Update Bot Updated [Time, Operator, Other fatalities, Phase, Departure airport, Destination airport, Source, Narrative, Category, Accident report]

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