20000328001919I

Incident

FAA incident report · Dhav DHC-8-102 · Pittsburgh, PA · March 28, 2000

Date
March 28, 2000 · 09:59 local
Place
Pittsburgh, PA
Airport
Greater Pittsburgh International
Phase of flight
Normal Cruise
Operating rules
Air carrier (Part 121)
Operator
PCAA
Aircraft
N822EX
Reported as
Dhav DHC8102
People aboard
18
Fatal injuries
0
Pilot’s flight hours
15,766 total2,413 in this make and model262 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 March 28, 2000, at 0959E, DHC-8, s/n 187, registered as N822EX, landed at pit after the crew reported the elevator manual trim had jammed in cruise flight. The electric trim system continued to operate and the autopilot was disengaged. The checklist was followed and the aircraft landed at pit and taxied to the gate without incident. Maintenance checked the system and found that the manual trim actuator had water in the jack screw and that the manual and electric trim both operated properly. The manual trim jack screw was lubed per the mm and the aircraft was returned to service. Investigation by desk audit and closed.

As the FAA filed it

(-23) ON MARCH 28, 2000, AT 0959E, DHC-8, S/N 187, REGISTERED AS N822EX, LANDED AT PIT AFTER THE CREW REPORTED THE ELEVATOR MANUAL TRIM HAD JAMMED IN CRUISE FLIGHT. THE ELECTRIC TRIM SYSTEM CONTINUED TO OPERATE AND THE AUTOPILOT WAS DISENGAGED. THE CHECKLIST WAS FOLLOWED AND THE AIRCRAFT LANDED AT PIT AND TAXIED TO THE GATE WITHOUT INCIDENT. MAINTENANCE CHECKED THE SYSTEM AND FOUND THAT THE MANUAL TRIM ACTUATOR HAD WATER IN THE JACK SCREW AND THAT THE MANUAL AND ELECTRIC TRIM BOTH OPERATED PROPERLY. THE MANUAL TRIM JACK SCREW WAS LUBED PER THE MM AND THE AIRCRAFT WAS RETURNED TO SERVICE. INVESTIGATION BY DESK AUDIT AND CLOSED.