Accident Piper PA-34-200 N1392T,
ASN logo
ASN Wikibase Occurrence # 131909
 
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:Wednesday 7 July 1993
Time:20:37 LT
Type:Silhouette image of generic PA34 model; specific model in this crash may look slightly different    
Piper PA-34-200
Owner/operator:Air Desert Pacific
Registration: N1392T
MSN: 34-7250306
Total airframe hrs:3573 hours
Engine model:Lycoming IO-360-C1E6
Fatalities:Fatalities: 0 / Occupants: 3
Aircraft damage: Destroyed
Category:Accident
Location:La Verne, CA -   United States of America
Phase: Initial climb
Nature:Training
Departure airport:
Destination airport:
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
THE FLIGHT INSTRUCTOR (CFI) SAID THAT DURING THE INITIAL CLIMB AND AFTER GEAR RETRACTION THE LEFT ENGINE LOST POWER. HE TOOK CONTROL AND FEATHERED THE LEFT PROP, BUT WAS UNABLE TO ESTABLISH A SINGLE-ENGINE RATE-OF-CLIMB. HE ATTEMPTED TO FLY THROUGH A LOW POINT IN HILLY TERRAIN, BUT THE AIRPLANE COLLIDED WITH A POWER LINE AND CRASHED INTO A RAVINE. THE LANDING GEAR WAS FOUND IN THE EXTENDED AND LOCKED POSITION, AND A GROUND WITNESS SAW THE GEAR EXTENDED DURING THE FLIGHT. THE LEFT ENGINE FUEL FLOW DIVIDER WAS FOUND TO BE PARTIALLY PLUGGED WITH A GREY/WHITE MATERIAL (CONTAMINATION). LABORATORY ANALYSIS IDENTIFIED THE MATERIAL AS POLYETHYLENE TEREPHTHALATE (PET), A THERMOPLASTIC MATERIAL. ORIGIN OF THE CONTAMINATE WAS UNKNOWN. ACCORDING TO THE AIRCRAFT SINGLE ENGINE PERFORMANCE CHART, THE AIRPLANE SHOULD HAVE BEEN ABLE TO CLIMB AT ABOUT 150 FEET PER MINUTE. A PILOT-RATED PASSENGER IN THE REAR HEARD THE STALL HORN SOUNDING AFTER THE CFI TOOK CONTROL AND ATTEMPTED TO ESTABLISH A SINGLE-ENGINE CLIMB. VYSE IS 103 MPH AND VSO IS 73 MPH.

Probable Cause: THE FLIGHT INSTRUCTOR'S FAILURE TO OBTAIN/MAINTAIN BEST THE SINGLE-ENGINE RATE-OF-CLIMB AIRSPEED, AND HIS FAILURE TO ENSURE THAT THE LANDING GEAR WAS RETRACTED. A FACTOR RELATED TO THE ACCIDENT WAS CONTAMINATION IN THE FUEL SYSTEM, WHICH BLOCKED FUEL FLOW THROUGH THE FLOW DIVIDER AND RESULTED IN FUEL STARVATION TO ONE ENGINE.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: LAX93FA282
Status: Investigation completed
Duration: 2 years and 4 months
Download report: Final report

Sources:

NTSB LAX93FA282

Location

Revision history:

Date/timeContributorUpdates
21-Dec-2016 19:25 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
10-Apr-2024 12:43 ASN Update Bot Updated [Time, Other fatalities, Phase, 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