20080504833869I

Incident · No damage

FAA incident report · Doug MD-88 · Fort Collins/L, CO · May 4, 2008

Date
May 4, 2008 · 13:29 local
Place
Fort Collins/L, CO
Airport
Fort Collins-Loveland Municipal
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
Air carrier (Part 121)
Operator
WX0A
Damage
No damage
Aircraft
N402NV
Reported as
Doug MD88
Reported engine
Pratt & Whitney JT8D
People aboard
150
Fatal injuries
0
Pilot’s flight hours
6,046 total2,084 in this make and model132 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) Allegiant flight 464 landed on rw 15 at fnl 5-4-2008. The flight came to a stop with the nosewheel approximately 10' past the end of the runway. Landing weight was 138,000 lbs (1,500 lbs below max landing) approach was at F28 instead of F40, with vref of 140 KTS. Estimated ground speed was 160-165 KTS. Touchdown at 1500' mark. Difficulty getting #1 reverser deployed and thrust set. Crew became distracted with reverser and by the time they realized how close they were to the end, there was not enough runway to stop. Auto-brakes were not used and maximum reverse was not employed.

As the FAA filed it

(-23) ALLEGIANT FLIGHT 464 LANDED ON RW 15 AT FNL 5-4-2008. THE FLIGHT CAME TO A STOP WITH THE NOSEWHEEL APPROXIMATELY 10' PAST THE END OF THE RUNWAY. LANDING WEIGHT WAS 138,000 LBS (1,500 LBS BELOW MAX LANDING) APPROACH WAS AT F28 INSTEAD OF F40, WITH VREF OF 140 KTS. ESTIMATED GROUND SPEED WAS 160-165 KTS. TOUCHDOWN AT 1500' MARK. DIFFICULTY GETTING #1 REVERSER DEPLOYED AND THRUST SET. CREW BECAME DISTRACTED WITH REVERSER AND BY THE TIME THEY REALIZED HOW CLOSE THEY WERE TO THE END, THERE WAS NOT ENOUGH RUNWAY TO STOP. AUTO-BRAKES WERE NOT USED AND MAXIMUM REVERSE WAS NOT EMPLOYED.

Other reports on N402NV · 1

Matched to the same aircraft by N-number and date.