ASN logo
Last updated: 18 January 2019
Status:Definitief
Datum:maandag 21 december 1992
Tijd:08:33
Type:Silhouette image of generic DC10 model; specific model in this crash may look slightly different
McDonnell Douglas DC-10-30CF
Luchtvaartmaatschappij:Martinair Holland
Registratie: PH-MBN
Constructienummer: 46924/218
Bouwjaar: 1975
Aantal vlieguren:61543
Aantal vluchten:14615
Motoren: 3 General Electric CF6-50C
Bemanning:slachtoffers: 2 / inzittenden: 13
Passagiers:slachtoffers: 54 / inzittenden: 327
Totaal:slachtoffers: 56 / inzittenden: 340
Schade: Afgeschreven
Gevolgen: Written off (damaged beyond repair)
Plaats:Faro Airport (FAO) (   Portugal)
Fase: Landing (LDG)
Soort vlucht:Internationale charter
Vliegveld van vertrek:Amsterdam-Schiphol International Airport (AMS/EHAM), Nederland
Vliegveld van aankomst:Faro Airport (FAO/LPFR), Portugal
Vluchtnummer: 495
Beschrijving:
At 05:52 LT Flight 495 took off from Amsterdam for a flight to Faro. The flight had been delayed for 40 minutes due to no. 2 engine reverser problems. After a flight of 2 and 17 minutes a the flight was cleared to descend to FL70. Shortly afterwards Faro Approach Control provided the crew with the following weather: wind 15deg./18 kts; 2500 m visibility; thunderstorms with 3/8 clouds at 500 feet, 7/8 clouds at 2300 feet and 1/8 cumulonimbus at 2500 feet, temp. 16deg. C.
Clearance to descend to 1220 m was given at 08:20, followed by a clearance to 915 m and 650 m 4, resp. 6 minutes later. At 08:29 the crew were informed that the runway was flooded. At an altitude of 303 m and 140 knots speed the approach became unstable and at 177 m the first officer switched the autopilot from CMD (command mode) to CWS (control-wheel steering). One minute later it was switched from CWS to manual and the airspeed began falling below approach reference speed. About 3-4 seconds short of touchdown elevator was pulled to pitch up and engine power was increased. When the no. 3 and 5 spoilers extended, the aircraft had a 25deg. bank, left wing up. The right main gear contacted the runway with a 900 feet/min descent rate at 126 knots, +8.79deg. pitch up, +5.62deg roll and 1,9533G. The right wing separated while the aircraft slid down the runway. The aircraft came to rest 1100 m from the runway 11 threshold and 100 m to the right of the centreline and caught fire.

Probable Cause:

PROBABLE CAUSES: "The high rate of descent in the final phase of the approach and the landing made on the right landing gear, which exceeded the structural limitations of the aircraft.; The crosswind, which exceeded the aircrafts limits and which occurred in the final phase of the approach and during landing. The combination of both factors determined stresses which exceeded the structural limitations of the aircraft.
Contributing factors were: The instability of the approach; the premature power reduction, and the sustaining of this condition, probably due to crew action; the incorrect wind information delivered by Approach Control; the absence of an approach light system; the incorrect evaluation by the crew of the runway conditions; CWS mode being switched off at approx. 80ft RA, causing the aircraft to be in manual control in a critical phase of the landing; the delayed action of the crew in increasing power; the degradation of the lift coefficient due to heavy showers." (DGAC Portugal)

The Netherlands Aviation Safety Board commented that the probable cause should read: "a sudden and unexpected wind variation in direction and speed (windshear) in the final stage of the approach. Subsequently a high rate of descent and an extreme lateral displacement developed, causing a hard landing on the right-hand main gear, which in combination with a considerable crab angle exceeded the aircraft structural limitations.
Contributing factors: From the forecast and the prevailing weather the crew of MP495 did not expect the existence of windshear phenomena.; The premature large power reduction and sustained flight idle thrust, most probable due to crew action.; CWS mode being disengaged at approx. 80ft RA, causing the aircraft to be in manual control at a critical stage in the landing phase."

Accident investigation:
cover
Investigating agency: GPIA Portugal
Status: Investigation completed
Accident number: 22/ACCID/GPI/92
Download report: Final report

Bronnen:
» Flight Crew of DC-10 Encounters Microburst During Unstabilized Approach, Ending in Runway Accident (Flight Safety Foundation - Accident Prevention August 1996)
» Air Safety Week 4 January 1993 (p. 1, 2)


Foto's

photo of McDonnell Douglas DC-10-30CF PH-MBN
photo of McDonnell Douglas DC-10-30CF PH-MBN
photo of McDonnell Douglas DC-10-30CF PH-MBN
photo of McDonnell Douglas DC-10-30CF PH-MBN
Add your photo of this accident or aircraft
 

Kaart
Deze kaart geeft het vliegveld van vetrek weer en de geplande bestemming van de vlucht. De lijn tussen de vliegvelden geeft niet de exacte vliegroute weer.
De afstand tussen Amsterdam-Schiphol International Airport en Faro Airport bedraagt 1955 km (1222 miles).
Accident location: Exact; as reported in the official accident report.

This information is not presented as the Flight Safety Foundation or the Aviation Safety Network’s opinion as to the cause of the accident. It is preliminary and is based on the facts as they are known at this time.
languages: languages

Share

DC-10

  • 446 built
  • 20e ongeval
  • 12e dodelijk ongeval
  • 8e zwaarste ongeval
» safety profile

 Portugal
  • 5e zwaarste ongeval
» safety profile