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|
Attributes | |
ACN | 446204 |
Time | |
Date | 199908 |
Day | Mon |
Local Time Of Day | 0601 To 1200 |
Place | |
Locale Reference | airport : msp.airport |
State Reference | MN |
Altitude | agl single value : 0 |
Environment | |
Flight Conditions | Mixed |
Weather Elements | Rain |
Light | Daylight |
Aircraft 1 | |
Controlling Facilities | tower : msp.tower |
Operator | common carrier : air carrier |
Make Model Name | DC-10 40 |
Operating Under FAR Part | Part 121 |
Navigation In Use | ils localizer & glide slope : 30r |
Flight Phase | landing : roll |
Route In Use | approach : instrument precision |
Flight Plan | IFR |
Person 1 | |
Affiliation | company : air carrier |
Function | flight crew : captain oversight : pic |
Qualification | pilot : atp |
Experience | flight time total : 10000 |
ASRS Report | 446204 |
Person 2 | |
Affiliation | company : air carrier |
Function | flight crew : first officer |
Qualification | pilot : multi engine pilot : instrument pilot : commercial pilot : atp |
Experience | flight time last 90 days : 120 flight time total : 8000 flight time type : 300 |
ASRS Report | 446846 |
Events | |
Anomaly | aircraft equipment problem : critical non adherence : far other anomaly other |
Independent Detector | other flight crewa other flight crewb other other : 3 |
Resolutory Action | none taken : insufficient time |
Consequence | faa : investigated faa : reviewed incident with flight crew other other |
Supplementary | |
Problem Areas | Aircraft Environmental Factor Weather Flight Crew Human Performance |
Primary Problem | Ambiguous |
Air Traffic Incident | Pilot Deviation |
Narrative:
Flew an uneventful 35 degree flap ILS approach to runway 30R. All normal checklists were completed in accordance with sopa. Touched down well within the normal landing zone in a light rain on a wet runway. Vref was 152 KTS, approach was flown at 157 KTS. Landing gross weight was 402000 pounds. Immediately applied reverse thrust on engines #2 and #3 (engine #1 thrust reverser was on MEL). Full anti-skid braking was applied and the anti-skid could be felt cycling. On rollout, the so announced #3 engine did not spool up in reverse and the #2 engine was at 90% N1. Throttles were in the full aft position. As we approached the end of the runway we offset slightly right of centerline to avoid as many REIL's as possible. We were unable to stop the aircraft until approximately 200 ft into the overrun. We communicated with tower and crash fire rescue equipment, informing them of our status. The captain shut down #2 engine and turned the nose gear full travel so brakes did not have to be set. Several PA calls were made to the passenger informing them of the situation and to remain seated. All normal checklists were completed and after a hot brake inspection by crash crews, maintenance towed the aircraft to the gate. Passenger were deplaned normally. Aircraft on postflt inspection had no apparent damage.
Original NASA ASRS Text
Title: DC10 STOPS 200 FT INTO RWY OVERRUN AT MSP.
Narrative: FLEW AN UNEVENTFUL 35 DEG FLAP ILS APCH TO RWY 30R. ALL NORMAL CHKLISTS WERE COMPLETED IN ACCORDANCE WITH SOPA. TOUCHED DOWN WELL WITHIN THE NORMAL LNDG ZONE IN A LIGHT RAIN ON A WET RWY. VREF WAS 152 KTS, APCH WAS FLOWN AT 157 KTS. LNDG GROSS WT WAS 402000 LBS. IMMEDIATELY APPLIED REVERSE THRUST ON ENGS #2 AND #3 (ENG #1 THRUST REVERSER WAS ON MEL). FULL ANTI-SKID BRAKING WAS APPLIED AND THE ANTI-SKID COULD BE FELT CYCLING. ON ROLLOUT, THE SO ANNOUNCED #3 ENG DID NOT SPOOL UP IN REVERSE AND THE #2 ENG WAS AT 90% N1. THROTTLES WERE IN THE FULL AFT POS. AS WE APCHED THE END OF THE RWY WE OFFSET SLIGHTLY R OF CTRLINE TO AVOID AS MANY REIL'S AS POSSIBLE. WE WERE UNABLE TO STOP THE ACFT UNTIL APPROX 200 FT INTO THE OVERRUN. WE COMMUNICATED WITH TWR AND CFR, INFORMING THEM OF OUR STATUS. THE CAPT SHUT DOWN #2 ENG AND TURNED THE NOSE GEAR FULL TRAVEL SO BRAKES DID NOT HAVE TO BE SET. SEVERAL PA CALLS WERE MADE TO THE PAX INFORMING THEM OF THE SIT AND TO REMAIN SEATED. ALL NORMAL CHKLISTS WERE COMPLETED AND AFTER A HOT BRAKE INSPECTION BY CRASH CREWS, MAINT TOWED THE ACFT TO THE GATE. PAX WERE DEPLANED NORMALLY. ACFT ON POSTFLT INSPECTION HAD NO APPARENT DAMAGE.
Data retrieved from NASA's ASRS site as of July 2007 and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.