20001214036559I

Incident · Substantial damage

FAA incident report · Beech 1900C · Omaha, NE · December 14, 2000

Date
December 14, 2000 · 09:30 local
Place
Omaha, NE
Airport
Eppley Airfield
Phase of flight
Ground Taxi, Other Airplane
Operating rules
Air taxi and commuter (Part 135)
Operator
JDWA
Damage
Substantial damage
Aircraft
N719GL
Reported as
Beech 1900C
People aboard
1
Fatal injuries
0
Pilot’s flight hours
14,400 total2,500 in this make and model

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 December 14, 2000, approx. 0930 CST, Beech 1900 c, N719GL, struck a light pole during a taxi operations at Omaha Eppley Airfield. The aircraft, owned and operated by suburban air freight, inc. encountered glare ice on a sloped ramp following cargo unloading at the us post office ramp. Gusty wind conditions, coupled with ineffective braking contributed to an unrecoverable skid resulting in damage to the RH wing leading edge at ws 249.75 when the aircraft made contact with a pole. The application of LH engine reverse thrust and feathering the RH propeller prevented damage to the engine and fuselage assemblies. No injury was reported by the PIC.

As the FAA filed it

(-23) ON DECEMBER 14, 2000, APPROX. 0930 CST, BEECH 1900 C, N719GL, STRUCK A LIGHT POLE DURING A TAXI OPERATIONS AT OMAHA EPPLEY AIRFIELD. THE AIRCRAFT, OWNED AND OPERATED BY SUBURBAN AIR FREIGHT, INC. ENCOUNTERED GLARE ICE ON A SLOPED RAMP FOLLOWING CARGO UNLOADING AT THE US POST OFFICE RAMP. GUSTY WIND CONDITIONS, COUPLED WITH INEFFECTIVE BRAKING CONTRIBUTED TO AN UNRECOVERABLE SKID RESULTING IN DAMAGE TO THE RH WING LEADING EDGE AT WS 249.75 WHEN THE AIRCRAFT MADE CONTACT WITH A POLE. THE APPLICATION OF LH ENGINE REVERSE THRUST AND FEATHERING THE RH PROPELLER PREVENTED DAMAGE TO THE ENGINE AND FUSELAGE ASSEMBLIES. NO INJURY WAS REPORTED BY THE PIC.

Other reports on N719GL · 3

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