20020810020829I

Incident · Minor damage

FAA incident report · Doug DC1010 · Tampa, FL · August 10, 2002

Date
August 10, 2002 · 07:17 local
Place
Tampa, FL
Airport
Tampa International
Phase of flight
Initial Approach-IFR
Operating rules
Air carrier (Part 121)
Operator
FDEA
Damage
Minor damage
Aircraft
N388FE
NTSB investigation
NTSBATL02IA155
Reported as
Doug DC1010
People aboard
3
Fatal injuries
0
Pilot’s flight hours
3,109 total62 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) On August 10, 2002, during the approach to landing at Tampa International Airport a federal express aircraft N388FE experienced a left main landing gear problem when the gear was extended. The upper support frame assembly (pn: ARB0642-1) which is the top attachment point for the retract cylinder broke which let the left main gear slam down to the extended position. The gear down and lock switch was broken during this failure which indicated that the left main gear was unsafe. The #3 hydraulic system decreased to zero due to lines sheared. After the pilot landed the DC10 aircraft it is company procedure to shut down all three engines for a gear failure which in turn disabled the anti-skid system due to loss of electrical power. All eight brakes locked up on landing which blew all main tires and damaged wheel rims.

As the FAA filed it

(-23) ON AUGUST 10, 2002, DURING THE APPROACH TO LANDING AT TAMPA INTERNATIONAL AIRPORT A FEDERAL EXPRESS AIRCRAFT N388FE EXPERIENCED A LEFT MAIN LANDING GEAR PROBLEM WHEN THE GEAR WAS EXTENDED. THE UPPER SUPPORT FRAME ASSEMBLY (PN: ARB0642-1) WHICH IS THE TOP ATTACHMENT POINT FOR THE RETRACT CYLINDER BROKE WHICH LET THE LEFT MAIN GEAR SLAM DOWN TO THE EXTENDED POSITION. THE GEAR DOWN AND LOCK SWITCH WAS BROKEN DURING THIS FAILURE WHICH INDICATED THAT THE LEFT MAIN GEAR WAS UNSAFE. THE #3 HYDRAULIC SYSTEM DECREASED TO ZERO DUE TO LINES SHEARED. AFTER THE PILOT LANDED THE DC10 AIRCRAFT IT IS COMPANY PROCEDURE TO SHUT DOWN ALL THREE ENGINES FOR A GEAR FAILURE WHICH IN TURN DISABLED THE ANTI-SKID SYSTEM DUE TO LOSS OF ELECTRICAL POWER. ALL EIGHT BRAKES LOCKED UP ON LANDING WHICH BLEW ALL MAIN TIRES AND DAMAGED WHEEL RIMS.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.

Other reports on N388FE · 1

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