N655AW

Substantial
None

Airbus Industrie A320-232 S/N: 1075

Accident Details

Date
Monday, June 12, 2000
NTSB Number
LAX00LA223
Location
LAS VEGAS, NV
Event ID
20001212X21264
Coordinates
36.250885, -115.040824
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
152
Total Aboard
152

Probable Cause and Findings

The failure of the mechanic to refasten the cowling door prior to returning the aircraft to service.

Aircraft Information

Registration
Make
AIRBUS INDUSTRIE
Serial Number
1075
Engine Type
Turbo-fan
Year Built
1999
Model / ICAO
A320-232
Aircraft Type
Fixed Wing Multi Engine
No. of Engines
2
Seats
200
FAA Model
A320-232

Registered Owner (Current)

Name
US BANK NA TRUSTEE
Address
CORPORATE TRUST SERVICES
ONE FEDERAL ST
City
BOSTON
State / Zip Code
MA 02110
Country
United States

Analysis

On June 12, 2000, at 1314 hours Pacific daylight time, an Airbus A320-232, N655AW, was substantially damaged when the engine cowling separated and struck the horizontal stabilizer during takeoff at McCarran International Airport, Las Vegas, Nevada. The airline transport certificated pilot, the second pilot, 3 flight attendants and 147 passengers were not injured. The aircraft was operated by America West Airlines, Inc., under 14 CFR Part 121 as flight 2747, a regularly scheduled domestic passenger flight, destined for Columbus, Ohio. Visual meteorological conditions prevailed and the flight was operating on an instrument flight plan.

According to the operator, the pilot reported there had been an abnormal vibration as the aircraft accelerated through takeoff rotation speed (Vr). Several passengers pressed their flight attendant call buttons and alerted the flight attendants who, in turn, reported the cowling separation to the cockpit crew. The return for landing at the departure airport at 1331 was unremarkable. The aircraft was taxied to the terminal gate and the passengers deplaned normally.

Postflight inspection revealed that the outboard, forward cowl door on the left (number 1) engine had separated from the engine nacelle. There was a 10-inch cut through the landing gear (strut) door and there were 3 holes in the lower surface of the left horizontal stabilizer, each approximately 2 inches wide and 8 inches long. The cowling door hold-open rod penetrated the lower skin and aft spar web of the horizontal stabilizer. No damage was observed on the wing or wing flap. The opposite (inboard) cowl door and the "bull nose," where the two doors hinge at the 12 o'clock position, were damaged but remained attached to the nacelle. The cowl door over-center type latches on the inboard door were found latched, however, the hooks were intact and undamaged. Similarly, the latch receptacles on the outboard door were visibly undamaged. The latches were painted red.

The operator reported that the aircraft remained overnight in Las Vegas and an "RON-check" (Remain Over Night) had been performed during hours of darkness. The RON-check required that the cowling doors be opened; however, the mechanic performing the work reported that the cowl doors were closed and re-latched about 0530 - 0600 during hours of daylight. In the morning, the aircraft was handed over from the maintenance graveyard shift to the day shift. Maintenance items remained to be completed in areas of the aircraft other than the number 1 engine. The takeoff where the cowling separated was the first flight following return to service.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX00LA223