20010718018579I

Incident · Minor damage

FAA incident report · Boeing 747-283B · Anchorage, AK · July 18, 2001

Date
July 18, 2001 · 06:37 local
Place
Anchorage, AK
Airport
Anchorage International
Phase of flight
Level Off Touchdown
Operating rules
Air carrier (Part 121)
Operator
IPXA
Damage
Minor damage
Aircraft
N523UP
Reported as
Boeing 747283B
Pilot’s flight hours
10,000 total

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) Tail strike was a result of a possible flawed cockpit procedure in determining and setting approach and landing speeds. Second officer properly determined the aircraft weight for landing and passed the information to the first officer who is the one to determine the landing speed from a flip chart. He flipped to the wrong weight and was off by more than 80,000 lbs which gave a speed fourteen knots slower than the proper speed and a higher deck angle which cause the tail strike. The poi reported that the information provided by the flight crew was up front and very helpful to determine if there needs to be a change in the procedures for determining the approach and landing speeds. The incident was classified as a minor damage incident.

As the FAA filed it

(-23) TAIL STRIKE WAS A RESULT OF A POSSIBLE FLAWED COCKPIT PROCEDURE IN DETERMINING AND SETTING APPROACH AND LANDING SPEEDS. SECOND OFFICER PROPERLY DETERMINED THE AIRCRAFT WEIGHT FOR LANDING AND PASSED THE INFORMATION TO THE FIRST OFFICER WHO IS THE ONE TO DETERMINE THE LANDING SPEED FROM A FLIP CHART. HE FLIPPED TO THE WRONG WEIGHT AND WAS OFF BY MORE THAN 80,000 LBS WHICH GAVE A SPEED FOURTEEN KNOTS SLOWER THAN THE PROPER SPEED AND A HIGHER DECK ANGLE WHICH CAUSE THE TAIL STRIKE. THE POI REPORTED THAT THE INFORMATION PROVIDED BY THE FLIGHT CREW WAS UP FRONT AND VERY HELPFUL TO DETERMINE IF THERE NEEDS TO BE A CHANGE IN THE PROCEDURES FOR DETERMINING THE APPROACH AND LANDING SPEEDS. THE INCIDENT WAS CLASSIFIED AS A MINOR DAMAGE INCIDENT.

Other reports on N523UP · 1

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