Zone

Crash of a Swearingen SA26T Merlin IIB in Saint George: 2 killed

Date & Time: Jul 7, 1998 at 1547 LT
Type of aircraft:
Operator:
Registration:
N501FS
Flight Type:
Survivors:
No
Site:
Schedule:
Anchorage - Saint George
MSN:
T26-146
YOM:
1969
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
13000
Captain / Total hours on type:
250.00
Aircraft flight hours:
7799
Circumstances:
The flight departed Anchorage, Alaska, and was en route to Saint George, Alaska, to pick up passengers for a return flight to Anchorage. The pilot-in-command (PIC) was seated in the right seat, and the copilot was seated in the left seat. This was the copilot's third flight in this make and model airplane, and he was not qualified as a crewman in it under 14 CFR Part 135. There was no record of when the copilot last performed a non directional beacon (NDB) approach. The NDB indicator in the cockpit was on the left side of the left control column, partially blocked from the view of the PIC. The minimum altitude for the segment of the approach prior to the final approach fix (FAF) was 1,700 feet. The Minimum Descent Altitude (MDA) for the final segment of the approach was 880 feet. The reported ceiling was 100 feet overcast. The Air Route Traffic Control Center radar altitude readout for the airplane revealed that the airplane descended below 600 feet prior to reaching the FAF. The radar ground track revealed the airplane on course prior to the course reversal procedure turn on the published approach. The radar ground track showed that after the course reversal, the airplane continued through the published final approach course, and turned to parallel the inbound track three miles north of course. The radar plot terminates about the location of the 550 feet high cliffs where the airplane was located. Weather at the time of the accident was reported as 100 foot overcast. This location was 5.5 miles (DME) from the airport. A review of radar tapes from the day prior to the accident, show the same airplane and PIC tracking the published course outbound and inbound, and descending below the published approach minima to below 500 feet. This flight successfully landed at the airport. An interview with the copilot from the successful flight revealed that the PIC intentionally descended to 300 feet on the approach until he acquired visual contact with the ocean, then flew to the airport to land. An aircraft flying on the published inbound final approach course at 5.5 DME is over water, approximately three miles from the nearest terrain.
Probable cause:
The pilot-in-command's failure to adequately monitor the instrument approach and the copilot's failure to intercept and maintain the proper NDB bearing on the approach. Contributing factors were the pilot-in-command's obstructed view of the NDB indicator and his overconfidence in his personal ability, the terrain (cliffs), low ceiling, and the flight crew's disregard of the minimum descent altitude.
Final Report:

Crash of a Swearingen SA227AC Metro III in Saint George

Date & Time: May 3, 1996 at 1630 LT
Type of aircraft:
Operator:
Registration:
N670PA
Survivors:
Yes
Schedule:
Saint Paul - Saint George
MSN:
AC-613
YOM:
1985
Flight number:
KS661
Crew on board:
2
Crew fatalities:
Pax on board:
11
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
19100
Captain / Total hours on type:
5500.00
Aircraft flight hours:
17167
Circumstances:
According to passenger's accounts, the airplane was flying low and approached the runway at an angle. The airplane made a right turn and dragged the right wing on the runway's surface. The airplane landed hard and sheared off the right main landing gear and the nose gear. The weather reported by AWOS was 300 foot overcast with a visibility of 2.5 miles with fog. The Captain stated the airplane drifted to the left side of the runway due to the crosswind, and he executed a right turn to realign with the runway. The cockpit voice recorder indicated that the stall warning horn sounded as the First Officer called for the application of power.
Probable cause:
Failure of the captain to maintain proper altitude and wingtip clearance, while aligning the airplane with the runway before landing. His delay in aligning the aircraft with the runway was a related factor.
Final Report: