20030201007879I

Incident

FAA incident report · Dhav DHC-8-102 · Binghamton, NY · February 1, 2003

Date
February 1, 2003 · 06:59 local
Place
Binghamton, NY
Airport
Edwin A Link Field
Phase of flight
To Init Climb(1st Pwr Reduct)
Operating rules
Air carrier (Part 121)
Operator
PCAA
Aircraft
N825EX
Reported as
Dhav DHC8102
People aboard
35
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 February 1, 2003, flt. 3577, N825EX, DHC-8, on climb-out, gear was selected "up", and hydraulic quantity on #2 system went to "0". Aircraft landed without incident. Maintenance replaced o rings on pressure warning switch, pressure transmitter, and low pressure warning switch. An o ring was also replaced on fitting for inlet pressure on right pressure manifold. Right engine driven hydraulic pump also replaced. Standby hydraulic pump ran in hangar for about 15 minutes. No leaks were noted. Aircraft ground run and hydraulic system cycled. No leaks were noted. Aircraft returned to service. The aircraft departed bgm for a test flight, and the crew reported hydraulic quantity on #2 side was lost in flight when gear was selected down. Crew returned to bgm, and maintenance found a cracked a.n. fitting on #2 engine driven pump manifold inlet. The fitting was replaced, and leak checked good on morning run up. The aircraft was returned to service. This incident is considered closed.

As the FAA filed it

(-23) ON FEBRUARY 1, 2003, FLT. 3577, N825EX, DHC-8, ON CLIMB-OUT, GEAR WAS SELECTED "UP", AND HYDRAULIC QUANTITY ON #2 SYSTEM WENT TO "0". AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED O RINGS ON PRESSURE WARNING SWITCH, PRESSURE TRANSMITTER, AND LOW PRESSURE WARNING SWITCH. AN O RING WAS ALSO REPLACED ON FITTING FOR INLET PRESSURE ON RIGHT PRESSURE MANIFOLD. RIGHT ENGINE DRIVEN HYDRAULIC PUMP ALSO REPLACED. STANDBY HYDRAULIC PUMP RAN IN HANGAR FOR ABOUT 15 MINUTES. NO LEAKS WERE NOTED. AIRCRAFT GROUND RUN AND HYDRAULIC SYSTEM CYCLED. NO LEAKS WERE NOTED. AIRCRAFT RETURNED TO SERVICE. THE AIRCRAFT DEPARTED BGM FOR A TEST FLIGHT, AND THE CREW REPORTED HYDRAULIC QUANTITY ON #2 SIDE WAS LOST IN FLIGHT WHEN GEAR WAS SELECTED DOWN. CREW RETURNED TO BGM, AND MAINTENANCE FOUND A CRACKED A.N. FITTING ON #2 ENGINE DRIVEN PUMP MANIFOLD INLET. THE FITTING WAS REPLACED, AND LEAK CHECKED GOOD ON MORNING RUN UP. THE AIRCRAFT WAS RETURNED TO SERVICE. THIS INCIDENT IS CONSIDERED CLOSED.

Other reports on N825EX · 2

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