Engine Shutdown Likely Cause Of 2005 NWA Ground Collision | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Most Recent Daily Episodes

Episode Date

Airborne-Monday

Airborne-Tuesday

Airborne-Wednesday Airborne-Thursday

Airborne-Friday

Airborne On YouTube

Airborne-Unlimited-04.22.24

Airborne-Unlimited-04.16.24

Airborne-FlightTraining-04.17.24 Airborne-AffordableFlyers-04.18.24

Airborne-Unlimited-04.19.24

Join Us At 0900ET, Friday, 4/10, for the LIVE Morning Brief.
Watch It LIVE at
www.airborne-live.net

Thu, May 03, 2007

Engine Shutdown Likely Cause Of 2005 NWA Ground Collision

Loss Of Hydraulics Led To Domino Effect

The National Transportation Safety Board has released a probable cause report, stating a Northwest Airlines captain's decision to shut down the left engine on a DC-9 was responsible for the jet's May 2005 ground collision with a Northwest Airbus A319 at Minneapolis-St. Paul International Airport.

As ANN reported, the DC-9 -- having lost its steering or braking capability as it taxied to the terminal building -- impacted the right wing of a much bigger A319 after running under the tail.

Four crewmembers on the DC-9 were injured, including the captain and first officer. Two ground workers were also injured in the incident. A section of the DC-9 roof peeled back and the A319 wing was damaged, spilling a puddle of jet fuel a few hundred feet wide. The 94 passengers on the DC-9 and 39 passengers on the A319 were evacuated.

The 16 mph impact occurred shortly after the DC-9's pilots became aware they had a problem with their right hydraulic system, according to Minnesota's Star-Tribune. 

According to the NTSB report, the left hydraulic system was operating properly and when the captain shut off the left engine after the plane landed in the Twin Cities, the "airplane experienced a loss of steering and a loss of brakes."

Northwest spokesman Bill Mellon said Tuesday that Northwest has developed an inspection procedure for its fleet relating to the rudder shutoff valve but declined to comment to the newspaper on other aspects of the NTSB report.

The NTSB probable cause reads: "the Captain's decision to shutdown the left engine during taxi with no hydraulic pressure on the right side hydraulic system to effectively operate the brakes, steering, or thrust reversers. A factor was the fatigue fracture of the rudder shutoff valve which resulted in the loss of right side hydraulic pressure."

FMI: www.ntsb.gov, www.nwa.com

Advertisement

More News

ANN's Daily Aero-Term (04.24.24): Runway Lead-in Light System

Runway Lead-in Light System Runway Lead-in Light System Consists of one or more series of flashing lights installed at or near ground level that provides positive visual guidance a>[...]

ANN's Daily Aero-Linx (04.24.24)

Aero Linx: Aviation Without Borders Aviation Without Borders uses its aviation expertise, contacts and partnerships to enable support for children and their families – at hom>[...]

Aero-FAQ: Dave Juwel's Aviation Marketing Stories -- ITBOA BNITBOB

Dave Juwel's Aviation Marketing Stories ITBOA BNITBOB ... what does that mean? It's not gibberish, it's a lengthy acronym for "In The Business Of Aviation ... But Not In The Busine>[...]

Classic Aero-TV: Best Seat in The House -- 'Inside' The AeroShell Aerobatic Team

From 2010 (YouTube Version): Yeah.... This IS A Really Cool Job When ANN's Nathan Cremisino took over the lead of our Aero-TV teams, he knew he was in for some extra work and a lot>[...]

Airborne Affordable Flyers 04.18.24: CarbonCub UL, Fisher, Affordable Flyer Expo

Also: Junkers A50 Heritage, Montaer Grows, Dynon-Advance Flight Systems, Vans' Latest Officially, the Carbon Cub UL and Rotax 916 iS is now in its 'market survey development phase'>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2024 Web Development & Design by Pauli Systems, LC