20030401003799I

Incident · Minor damage

FAA incident report · Braero BAE125800A · Seattle, WA · April 1, 2003

Date
April 1, 2003 · 15:30 local
Place
Seattle, WA
Airport
Boeing Field-King County International
Phase of flight
Other Ground Ops
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N160WC
Reported as
Braero BAE125800A
People aboard
4
Fatal injuries
0
Pilot’s flight hours
13,000 total100 in this make and model12 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) As the left engine rotated during the start cycle, and before it had fired, with hydraulic pressure rising, the nose gear collapsed while the aircraft was waiting on the apron to taxi out. The aircraft was on the chalks with electrical power provided by the auxiliary power unit. When the engine driven hydraulic pump begun to cause hydraulic pressure to rise, the main landing gear doors closed. Thereafter hydraulic pressure increased sufficient to actuate the nose gear over center and cause the aircraft to settle onto the nose gear doors as the nose gear itself slowly retracted. The aircraft sustained damage central to the nose gear door attaches points, which was determined by the NTSB to not be substantial. Investigation indicates no mechanical malfunction and pilot statements suggest no pilot error.

As the FAA filed it

(-23) AS THE LEFT ENGINE ROTATED DURING THE START CYCLE, AND BEFORE IT HAD FIRED, WITH HYDRAULIC PRESSURE RISING, THE NOSE GEAR COLLAPSED WHILE THE AIRCRAFT WAS WAITING ON THE APRON TO TAXI OUT. THE AIRCRAFT WAS ON THE CHALKS WITH ELECTRICAL POWER PROVIDED BY THE AUXILIARY POWER UNIT. WHEN THE ENGINE DRIVEN HYDRAULIC PUMP BEGUN TO CAUSE HYDRAULIC PRESSURE TO RISE, THE MAIN LANDING GEAR DOORS CLOSED. THEREAFTER HYDRAULIC PRESSURE INCREASED SUFFICIENT TO ACTUATE THE NOSE GEAR OVER CENTER AND CAUSE THE AIRCRAFT TO SETTLE ONTO THE NOSE GEAR DOORS AS THE NOSE GEAR ITSELF SLOWLY RETRACTED. THE AIRCRAFT SUSTAINED DAMAGE CENTRAL TO THE NOSE GEAR DOOR ATTACHES POINTS, WHICH WAS DETERMINED BY THE NTSB TO NOT BE SUBSTANTIAL. INVESTIGATION INDICATES NO MECHANICAL MALFUNCTION AND PILOT STATEMENTS SUGGEST NO PILOT ERROR.