Aviation Crash Map

Fairchild SA227-AC N343AE

29 September 2002 · Hawthorne, California, United States · Serious injuries

Summary

On 29 September 2002 at about 16:13 local time, a Fairchild SA227-AC registered N343AE, operated by C.A.T.S. Tours, Inc., was involved in an accident near Hawthorne, California, United States. 21 people were on board and one was seriously injured. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 16:13
Classification
Accident
Location
Hawthorne, California, United States
Nearest airport
Hawthorne (HAW)
Coordinates
33.9225, -118.3314
Aircraft
Fairchild SA227-AC
Registration
N343AE
Category
Airplane
Engines
2
Operator
C.A.T.S. Tours, Inc.
Operating rule
Part 135: Air Taxi & Commuter
Phase of flight
Not recorded
Route
Hawthorne → Grand Canyon
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
LAX02FA300

People

1 person was seriously injured.

On board Died Serious Minor Uninjured
21 0 1 0 20

Probable cause

The pilot-in-command's failure to maintain directional control during the rejected takeoff. The loss of directional control was caused by the crew's failure to follow prescribed pretakeoff and takeoff checklist procedures to ensure the both propellers were out of the start locks. Contributing factors were the failure of the crew to follow normal company procedures during takeoff, the failure of the flightcrew to recognize an abnormal propeller condition during takeoff, and a lack of crew coordination in performing a rejected takeoff.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

The airplane veered off the runway during a rejected takeoff, overran an airport sign, and impacted a hangar. The captain stated that during the after start checklist he moved the power levers to disengage the start locks on the propellers. Post accident examination found that the left propeller was still in the start lock position, while the right propeller was in the normal operating range. The captain was the pilot flying (PF) and the second-in-command (SIC) was the nonflying pilot (NFP). After receiving their clearance, the PF taxied onto the runway and initiated the takeoff sequence. The SIC did not set and monitor the engine power during takeoff, as required by the company procedures. During the takeoff acceleration when the speed was between 40 and 60 knots, the captain released the nose gear steering control switch as the rudder became aerodynamically effective. When the switch was released, the airplane began immediately veering left due to the asymmetrical thrust between the left and right engine propellers. The PIC did not advise the SIC that he had lost directional control and was aborting the takeoff, as required by company procedures. The distance between where the PIC reported that he began the takeoff roll and where the first tire marks became apparent was about 630 feet, and the distance between where the marks first became apparent and where the airplane's left main landing gear tire marks exited the left side of the runway was about 220 feet. Thereafter, marks (depressions in the dirt) were noted for a 108-foot-long distance in the field located adjacent to the runway. Medium intensity tire tread marks were apparent on the parallel taxiway and the adjacent vehicle service road. These tread marks, over a 332-foot-long distance, led directly to progressively more pronounced marks and rubber transfer, and to the accident airplane's landing gear tires. Based on an examination of tire tracks and skid marks, the PIC did not reject the takeoff until the airplane approached the runway's edge, and was continuing its divergent track away from the runway's centerline. The airplane rolled on the runway through the dirt median and across a taxiway for 850 feet prior to the PIC applying moderate brakes, and evidence of heavier brake application was apparent only a few hundred feet from the impacted hangar. No evidence of preimpact mechanical failures or malfunctions was found with the propeller assemblies, nose wheel steering mechanism, or brakes.

Quoted verbatim from the NTSB record.

Other Fairchild SA227 accidents

Date Aircraft Location Operator Outcome Died
28 Nov 2000 Fairchild SA227-AC
N3107P
Trujillo, Peru
no coordinates
Aero Condor No injuries -
12 Oct 1999 Fairchild SA227-AC
N438MA
Opa Locka, Florida, United States Merlin Express, Inc. No injuries -
12 Mar 1998 Fairchild SA227-AC
N730C
Tyler, Texas, United States Austin Express No injuries -
17 Aug 2006 Fairchild SA227-AC
N620PA
Grain Valley, Missouri, United States PAC West Airlines Inc Minor injuries -
5 Jan 1997 Fairchild SA227-AC
N165SW
Bullhead City, Arizona, United States
no coordinates
FNG Aviation Inc Minor injuries -
22 Aug 1997 Fairchild SA227-AC
N27188
Anchorage, Alaska, United States Merlin Express No injuries -

All 37 records for this type

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15 Mar 2002 Trenti RV-4
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23 Feb 2002 Thunder and Colt COLT 120 A
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no coordinates
- Serious injuries -
21 Sep 2002 Pzl-Bielsko SZD-42-2 JANTAR
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All 170,864 records in United States