N384MQ

Unknown
None

Short Brothers SD3-60-200 S/N: SH3711

Accident Details

Date
Tuesday, July 9, 1996
NTSB Number
MIA96IA179
Location
SAN JUAN, PR
Event ID
20001208X06307
Aircraft Damage
Unknown
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
12
Total Aboard
12

Probable Cause and Findings

Fatigue failure of a segment of the elevator trim control cable. Contributing to the accident was the failure of the airplane manufacturer to require a replacement interval of the cables.

Aircraft Information

Registration
N384MQ
Make
SHORT BROTHERS
Serial Number
SH3711
Model / ICAO
SD3-60-200

Registered Owner (Historical)

Name
SKY WAY ENTERPRISES INC
Address
PO BOX 205
Status
Deregistered
City
WASHINGTON
State / Zip Code
DC 20044-0205
Country
United States

Analysis

On July 9, 1996, about 1605 Atlantic Standard Time, a Short Brothers SD3-60-200, N384MQ, operated by Executive Airlines, Inc., dba American Eagle as flight No. 5514, experienced failure of a segment of the elevator trim cable system during the initial climb after takeoff at the Luis Munoz Marin International Airport, San Juan, Puerto Rico. Visual meteorological conditions prevailed at the time and an IFR flight plan was filed for the scheduled, domestic, passenger flight operated in accordance with 14 CFR Part 121. The airplane was not damaged and the airline transport-rated pilot and first officer, 1 flight attendant, and 9 passengers were not injured. The flight originated about 5 minutes earlier.

The first officer who was flying the airplane stated that after flap retraction while retrimming the airplane to a nose-up attitude, he felt no resistance from the manual elevator trim wheel. The flight then returned and landed uneventfully.

Examination of the elevator trim control system revealed a failed cable segment between fuselage station 74 in the cockpit and fuselage station 310 in the cabin area. The cable failed about midpoint between a 45-degree change in direction and was for nose-up trim. The failed cable was removed for further examination.

Metallurgical examination of the failed cable revealed that 36 of the 49 individual wire strands failed due to fatigue. Additionally, wear was noted adjacent to the fatigue failed strands. The remaining strands failed due to overload.

The airplane manufacturer requires the elevator trim control system to be inspected every 4,800 hours of 4 years, but replacement is on condition. The airplane operator introduced an engineering change order to the fleet which required inspection every 2,400 hours. Review of the airplane maintenance records revealed that the trim control system was last inspected 2,247.5 hours and 3,969 cycles earlier at the time of the failure.

The airplane was released to Mr. Ramon Ruiz, Director of Quality Assurance on July 11, 1996. The retained cable was released to Mr. Luiz Ruiz, Stores Regional Manager, on May 12, 1997.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# MIA96IA179