20010504012499I

Incident

FAA incident report · Swrngn SA227-AC · Rapid City, SD · May 4, 2001

Date
May 4, 2001 · 06:14 local
Place
Rapid City, SD
Airport
Rapid City Regional
Phase of flight
Normal Cruise
Operating rules
Air taxi and commuter (Part 135)
Operator
DUFA
Aircraft
N3108B
Reported as
Swrngn SA227AC
Reported engine
Garrett TPE33111U
People aboard
1
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 may 4, 2001 a fairchild m/n SA-227-AC, N3108B, operated by business avaiation courier (dufa), was en route from sioux falls, SD (fsd) to Rapid City, SD (rap). 30 miles east of Rapid City at approximately 0614 am MDT, the pilot delcared an emergency due to a hydraulic failure. The aircraft landed at the Rapid City Regional Airport on runway 32 at 0620 am MDT without incident. This was a cargo flight under CFR part 135 when the incident occurred. Visual meteorological conditions prevailed at the time and an IFR flight plan was filed. After inspection it was determined that the hydraulic failure was due to a cracked line in the right hand wing root area. Mechanical reliability report forthcoming.

As the FAA filed it

(-23)ON MAY 4, 2001 A FAIRCHILD M/N SA-227-AC, N3108B, OPERATED BY BUSINESS AVAIATION COURIER (DUFA), WAS EN ROUTE FROM SIOUX FALLS, SD (FSD) TO RAPID CITY, SD (RAP). 30 MILES EAST OF RAPID CITY AT APPROXIMATELY 0614 AM MDT, THE PILOT DELCARED AN EMERGENCY DUE TO A HYDRAULIC FAILURE. THE AIRCRAFT LANDED AT THE RAPID CITY REGIONAL AIRPORT ON RUNWAY 32 AT 0620 AM MDT WITHOUT INCIDENT. THIS WAS A CARGO FLIGHT UNDER CFR PART 135 WHEN THE INCIDENT OCCURRED. VISUAL METEOROLOGICAL CONDITIONS PREVAILED AT THE TIME AND AN IFR FLIGHT PLAN WAS FILED. AFTER INSPECTION IT WAS DETERMINED THAT THE HYDRAULIC FAILURE WAS DUE TO A CRACKED LINE IN THE RIGHT HAND WING ROOT AREA. MECHANICAL RELIABILITY REPORT FORTHCOMING.

Other reports on N3108B · 3

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