20000819029279I

Incident · Minor damage

FAA incident report · Doug DC1010F · Mobile, AL · August 19, 2000

Date
August 19, 2000 · 12:42 local
Place
Mobile, AL
Airport
Brookley
Phase of flight
Level Off Touchdown
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N364FE
Reported as
Doug DC1010F
People aboard
9
Fatal injuries
0
Pilot’s flight hours
6,500 total2,000 in this make and model26 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)All (4) tires on right main landing gear truck blew during take-off and landing. Aircraft damages due to rubber debris are: 1)the #3 engine fan section inlet (2 each blades), 2)the right wing lower inboard flap, 3)the lower trapezoidal panel, 4)all four brakes, 5)the landing gear anti-skid wire harness, 6)all four wheels. Boeing engineers theorize the brakes appeared to be dragging during taxi for takeoff as indicated by the tire tracks on taxiway. After lift-off the #7 blew, after gear retraction the #3 fuse plugs melted and the tire deflated while in the gear well. Upon landing the #4 & 8 tire blew from the exetensive load and possible dragging brakes. One of the dual brake control valve(s) is suspect, valves shipped by Boeing for bench test. Both calves were overhauled in 1999, by curtiss wright services, certificate #TR2R197, (44973-2/12/99, installed 3/16/99), (313-1/28/99, installed 2/27/99), time in sevice 31.25 hours. The bench test was not accomplished prior to teardown. Awaiting teardown report.

As the FAA filed it

(-23)ALL (4) TIRES ON RIGHT MAIN LANDING GEAR TRUCK BLEW DURING TAKE-OFF AND LANDING. AIRCRAFT DAMAGES DUE TO RUBBER DEBRIS ARE: 1)THE #3 ENGINE FAN SECTION INLET (2 EACH BLADES), 2)THE RIGHT WING LOWER INBOARD FLAP, 3)THE LOWER TRAPEZOIDAL PANEL, 4)ALL FOUR BRAKES, 5)THE LANDING GEAR ANTI-SKID WIRE HARNESS, 6)ALL FOUR WHEELS. BOEING ENGINEERS THEORIZE THE BRAKES APPEARED TO BE DRAGGING DURING TAXI FOR TAKEOFF AS INDICATED BY THE TIRE TRACKS ON TAXIWAY. AFTER LIFT-OFF THE #7 BLEW, AFTER GEAR RETRACTION THE #3 FUSE PLUGS MELTED AND THE TIRE DEFLATED WHILE IN THE GEAR WELL. UPON LANDING THE #4 & 8 TIRE BLEW FROM THE EXETENSIVE LOAD AND POSSIBLE DRAGGING BRAKES. ONE OF THE DUAL BRAKE CONTROL VALVE(S) IS SUSPECT, VALVES SHIPPED BY BOEING FOR BENCH TEST. BOTH CALVES WERE OVERHAULED IN 1999, BY CURTISS WRIGHT SERVICES, CERTIFICATE #TR2R197, (44973-2/12/99, INSTALLED 3/16/99), (313-1/28/99, INSTALLED 2/27/99), TIME IN SEVICE 31.25 HOURS. THE BENCH TEST WAS NOT ACCOMPLISHED PRIOR TO TEARDOWN. AWAITING TEARDOWN REPORT.

Other reports on N364FE · 1

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