20000101001159I

Incident

FAA incident report · Dhav DHC-8-102 · Binghamton, NY · January 1, 2000

Date
January 1, 2000 · 12:06 local
Place
Binghamton, NY
Airport
Edwin A Link Field
Phase of flight
Climb
Operating rules
Air carrier (Part 121)
Operator
PCAA
Aircraft
N841EX
Reported as
Dhav DHC8102
People aboard
8
Fatal injuries
0

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 Saturday, January 1, 2000, at 1206 local, allegheny airlines d/b/a us air express, DHC-8-102, N841EX, diverted into bgm due to a possible vibration in the propeller. The aircraft landed on runway 28 and taxied to the ramp without incident. Maintenance inspected the engine, propeller and engine mounts with no defectws found. During the engine run after inspection, the vibration was still present. After inspecting the rest of the aircraft, the left outboard hoprizontal stab deice boot was found to be peeling off the top of the stab surface. The boot would flap in the prop wash during engine runs. Maintenance replaced the leading edge and boot assembly and returned the aircraft to service. This incident is considered closed.

As the FAA filed it

(-23) ON SATURDAY, JANUARY 1, 2000, AT 1206 LOCAL, ALLEGHENY AIRLINES D/B/A US AIR EXPRESS, DHC-8-102, N841EX, DIVERTED INTO BGM DUE TO A POSSIBLE VIBRATION IN THE PROPELLER. THE AIRCRAFT LANDED ON RUNWAY 28 AND TAXIED TO THE RAMP WITHOUT INCIDENT. MAINTENANCE INSPECTED THE ENGINE, PROPELLER AND ENGINE MOUNTS WITH NO DEFECTWS FOUND. DURING THE ENGINE RUN AFTER INSPECTION, THE VIBRATION WAS STILL PRESENT. AFTER INSPECTING THE REST OF THE AIRCRAFT, THE LEFT OUTBOARD HOPRIZONTAL STAB DEICE BOOT WAS FOUND TO BE PEELING OFF THE TOP OF THE STAB SURFACE. THE BOOT WOULD FLAP IN THE PROP WASH DURING ENGINE RUNS. MAINTENANCE REPLACED THE LEADING EDGE AND BOOT ASSEMBLY AND RETURNED THE AIRCRAFT TO SERVICE. THIS INCIDENT IS CONSIDERED CLOSED.

Other reports on N841EX · 1

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