Aviation Crash Map

Aero Vodochody L39C N111XN

9 July 2011 · West Milford, New Jersey, United States · Serious injuries

Summary

On 9 July 2011 at about 16:39 local time, a Aero Vodochody L39C registered N111XN, operated by Air Vatche Inc., was involved in an accident near West Milford, New Jersey, United States. One person was 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 16:39
Classification
Accident
Location
West Milford, New Jersey, United States
Nearest airport
Greenwood Lake Airport (4N1)
Coordinates
41.1283, -74.3464
Aircraft
Aero Vodochody L39C
Registration
N111XN
Category
Airplane
Engines
1
Operator
Air Vatche Inc.
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Montgomery → West Milford
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
ERA11LA390

People

1 person was seriously injured.

On board Died Serious Minor Uninjured
1 0 1 0 0

Probable cause

The pilot's excessive airspeed and failure to attain the proper landing point, which resulted in the airplane touching down too fast and too far down the short runway. Contributing to the accident was the pilot's failure to retract the flaps after landing, which resulted in delayed brake activation, the pilot’s decision to land on a runway with an insufficient safety margin for the landing conditions, and the pilot’s failure to use the emergency brake lever.

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

Read the full NTSB narrative

While landing on runway 24 at an airport that had obstructions on both ends of the runway, had only 3,471 feet of usable runway available, and which required a 3.50 degree glideslope for landing, the pilot of the ex-military jet trainer landed the airplane and overran the runway. According to the pilot's written statement, during the landing he touched down 5 to 6 feet prior to the painted "24" on the runway. He then lowered the nose of the airplane and "retracted" the wing flaps. He then pushed the control stick forward and applied the brakes by squeezing the control-stick-mounted brake handle, but braking did not occur. He then applied the brakes a second time, extended the speed brakes, wiggled the control stick, and pushed the control stick forward and applied the brakes a third time without result before applying them a fourth time. He then felt the anti-skid engage. The airplane then struck a chain link fence and went over an embankment before impacting the ground, nosing over, and coming to rest inverted. The pilot was seriously injured during the impact sequence and the airplane incurred substantial damage to the forward fuselage. Review of the pilot's statement also revealed that he had not touched down at 96 knots indicated airspeed, as specified by the landing speeds chart, but had touched down at 106 knots, which would have extended his landing distance by about 20 percent. Further, witnesses observed the airplane actually touch down about 300 to 400 feet past the painted "24" on the runway, not the 5 to 6 feet prior to the painted "24" as stated by the pilot. Skid marks that matched the width of the airplane's main landing gear geometry were also present on the runway surface. The marks started about 1,270 feet past the painted "24" on the runway and continued until they left the pavement. Review of performance planning charts also revealed that the safety margin for operating at the airport was insufficient: even if the airplane had touched down just prior to the painted "24" on the runway, the pilot would already have 205 feet of the usable runway behind him, and with moderate braking the landing roll would have been about 2,500 feet, and the landing distance, when landing over a 50 foot obstacle, would have been about 3,370 feet. With intensive braking, the landing roll would have been about 2,000 feet, and the landing distance, when landing over a 50 foot obstacle, would have been about 2,900 feet. The pilot also would not have met the accelerate/stop criteria for takeoff or a balked landing, as the airplane required 3,600 feet to accelerate to takeoff speed and then stop after an aborted takeoff. Examination of the airplane did not reveal any evidence of a preimpact mechanical failure or malfunction that would have resulted in failure of the normal braking system. The flaps were also in the 44 degree (landing) position and had not been retracted, as was required for a minimum run landing to reduce lift, increase weight on the wheels, and reduce tire skidding. Examination of the flight manual also revealed that, in the event of a brake failure, activation of the main wheel brake units still would have been possible if the pilot had operated the emergency brake lever. According to the flight manual, he should have used the emergency brake lever if he believed that he had lost normal braking.

Quoted verbatim from the NTSB record.

Other Aero Vodochody L39C accidents

Date Aircraft Location Operator Outcome Died
1 Sep 2012 Aero Vodochody L39C
N139GS
Davenport, Iowa, United States - Fatal 1
21 Jan 2012 Aero Vodochody L39C
N16RZ
Rainbow City, Alabama, United States Thomas L. Coble Fatal 1
14 Jun 2013 Aero Vodochody L39C
N8124N
Reno, Nevada, United States Larry Lee No injuries -
8 Oct 2017 Aero Vodochody L39C
N580LL
Vernon, Texas, United States - Fatal 1

All 5 records for this type

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All 170,864 records in United States